Part 66

Easy Access Rules for Continuing Airworthiness Annex III (Part-66)
(Regulation (EU) No 1321/2014)

GENERAL
ANNEX III (PART-66)

GENERAL
66.1 Competent authority

Regulation (EU) No 1321/2014
(a) For the purpose of this Annex (Part-66), the competent authority shall be:
1. the authority designated by the Member State to whom a person first applies for the
issuance of an aircraft maintenance licence; or
2. the authority designated by another Member State, in case it would be different, subject
to agreement with the authority referred to in point 1. In that case, the licence referred
to in point 1 shall be revoked, all the records mentioned in point 66.B.20 shall be
transferred and a new licence shall be issued on the basis of these records.
(b) The Agency shall be responsible for defining:
1. the list of aircraft types; and
2. what airframe/engine combinations are included in each particular aircraft type rating.
AMC 66.1(a) Competent Authority

ED Decision 2015/029/R
A competent authority may be a ministry, a national aviation authority, or any aviation body
designated by the Member State and located within that Member State. A Member State may
designate more than one competent authority to cover different areas of responsibility, as long as the
designation decision contains a list of the competencies of each authority and there is only one
competent authority responsible for each given area of responsibility.
The purpose of 66.1(a)2 is to allow the possibility for a person who already holds a Part-66 licence
issued by one Member State (i.e. Member State X) to replace it by a Part-66 licence issued by another
Member State (i.e. Member State Y). This may be useful, for example, in cases where a person holding
a licence from ‘Member State X’ is developing his/her career in a maintenance organisation located in
‘Member State Y’. In this case, this person may need to endorse new type ratings based on courses
directly approved by the competent authority of ‘Member State Y’ or may need to endorse new
licence (sub)categories based on basic examinations performed by the competent authority of
‘Member State Y’.
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SECTION A — TECHNICAL
REQUIREMENTS
SECTION A — TECHNICAL REQUIREMENTS
SUBPART A — AIRCRAFT MAINTENANCE LICENCE
66.A.1 Scope
This section defines the aircraft maintenance licence and establishes the requirements for application,
issue and continuation of its validity.
66.A.3 Licence categories and subcategories

Regulation (EU) 2018/1142
Aircraft maintenance licences include the following categories and, where applicable, subcategories
and system ratings:
(a) Category A, divided into the following subcategories:
− A1 Aeroplanes Turbine;
− A2 Aeroplanes Piston;
− A3 Helicopters Turbine;
− A4 Helicopters Piston.
(b) Category B1, divided into the following subcategories:
− B1.1 Aeroplanes Turbine;
− B1.2 Aeroplanes Piston;
− B1.3 Helicopters Turbine;
− B1.4 Helicopters Piston.
(c) Category B2
The B2 licence is applicable to all aircraft.
(d) Category B2L
The B2L licence is applicable to all aircraft other than those in Group 1 as set out in Point
66.A.5(1) and is divided into the following ‘system ratings’:
− communication/navigation (com/nav),
− instruments,
− autoflight,
− surveillance,
− airframe systems.
A B2L licence shall contain, as a minimum, one system rating.

REQUIREMENTS
(e) Category B3
The B3 licence is applicable to piston-engine non-pressurised aeroplanes of 2 000 kg Maximum
Take-off Mass (MTOM) and below.
(f) Category L, divided into the following subcategories:
− L1C: composite sailplanes,
− L1: sailplanes,
− L2C: composite powered sailplanes and composite ELA1 aeroplanes,
− L2: powered sailplanes and ELA1 aeroplanes,
− L3H: hot-air balloons,
− L3G: gas balloons,
− L4H: hot-air airships,
− L4G: ELA2 gas airships,
− L5: gas airships other than ELA2.
(g) Category C
The C licence is applicable to aeroplanes and helicopters.
GM 66.A.3 Licence categories

‘ELA1 aeroplanes’ refers to those aeroplanes which meet the definition of ‘ELA1 aircraft’ that is
contained in Article 2(k) of Regulation (EU) No 1321/2014.
‘ELA2 gas airships’ refers to those gas airships which meet the definition of ‘ELA2 aircraft’ that is
contained in Article 2(ka) of Regulation (EU) No 1321/2014.
‘Gas airships other than ELA2’ refers to those gas airships which do not meet at least one condition of
the definition of ‘ELA2 aircraft’ that is contained in Article 2(ka) of Regulation (EU) No 1321/2014.
NOTE: The ‘ELA2 aircraft’ category includes all ‘ELA1 aircraft’.
The term ‘powered sailplane’ includes:
− those powered sailplanes which may take off solely by means of their own power (self-launching
sailplanes); and
− self-sustaining powered sailplanes; and
− touring motor gliders (TMGs).
While the L1C subcategory only includes composite sailplanes, the L1 subcategory includes all
sailplanes (composite, metal and wood).
While the L2C subcategory only includes composite powered sailplanes and composite ELA1
aeroplanes, the L2 subcategory includes all powered sailplanes and ELA1 aeroplanes (composite,
metal and wood).
In the case of maintenance of mixed balloons (combination of gas and hot air), it is required to hold
both L3G and L3H subcategories.

REQUIREMENTS
For the B2L licence, a ‘system rating’ is a rating which gives privileges to release maintenance on the
aircraft systems covered by the ‘system rating’ and electrical systems.
The sentence ‘shall contain, as a minimum, one system rating’ refers to the fact that the application
for a B2L licence should be made for any of the system ratings or any combination of the system
ratings specified in 66.A.3.
There is no specific order in which the system ratings should be applied for. Any combination of system
ratings is possible.
The description of systems covered by the different system ratings is provided in Appendix I ‘Basic
Knowledge Requirements’ under paragraph ‘2. Modularisation’, subparagraph related to ‘Categories
B2 and B2L’.
66.A.5 Aircraft groups

For the purpose of ratings on aircraft maintenance licences, aircraft shall be classified into the
following groups:
(1) Group 1: complex motor-powered aircraft, helicopters with multiple engines, aeroplanes with
maximum certified operating altitude exceeding FL290, aircraft equipped with fly-by-wire
systems, gas airships other than ELA2 and other aircraft requiring an aircraft type rating when
defined as such by the Agency.
The Agency may decide to classify into Group 2, Group 3 or Group 4, as appropriate, an aircraft
which meets the conditions set out in the first subparagraph, if it considers that the lower
complexity of the particular aircraft justifies so.
(2) Group 2: aircraft other than those in Group 1 belonging to the following subgroups:
(i) subgroup 2a:
− single turboprop engine aeroplanes,
− those turbojet and multiple-turboprop aeroplanes classified by the Agency in this
subgroup because of their lower complexity.
(ii) subgroup 2b:
− single turbine engine helicopters,
− those multiple turbine engine helicopters classified by the Agency in this subgroup
because of their lower complexity.
(iii) subgroup 2c:
− single piston engine helicopters,
− those multiple piston engine helicopters classified by the Agency in this subgroup
because of their lower complexity.
(3) Group 3: piston engine aeroplanes other than those in Group 1.
(4) Group 4: sailplanes, powered sailplanes, balloons and airships, other than those in Group 1.

REQUIREMENTS
GM 66.A.5 Aircraft groups

The following table summarises the applicability of categories/subcategories of Part-66 licences versus
the groups/subgroups of aircraft:
Category/subcategory L
A, B1 L1C L2C L3H L4H
B2 B2L B3
and C and and and and L5
Groups L1 L2 L3G L4G
1
— Complex motor-powered
aircraft
— Multi-engine helicopters
X X
— Aeroplanes above FL290
— Aircraft with fly-by-wire systems
— Any other aircraft when defined
by the Agency
1
X X
— Gas airships other than ELA2
2
2a: Single turboprop aeroplanes
X X X
2b: Single turbine helicopters
2c: Single piston helicopters
3
X X X
— Piston engine aeroplanes
3
— Piston engine aeroplanes (non-
X X X X
pressurised of 2 000 kg MTOM
and below)
3
X X X X X
— ELA1 piston engine aeroplanes
4
— Sailplanes X X X X
— Powered sailplanes X X X
— Balloons X X X
— Airships not in Group 1 X X X X
66.A.10 Application
(a) An application for an aircraft maintenance licence or change to such licence shall be made on
an EASA Form 19 (see Appendix V) in a manner established by the competent authority and
submitted thereto.
(b) An application for the change to an aircraft maintenance licence shall be made to the competent
authority of the Member State that issued the aircraft maintenance licence.
(c) In addition to the documents required in points 66.A.10(a), 66.A.10(b) and 66.B.105, as
appropriate, the applicant for additional basic categories or subcategories to an aircraft
maintenance licence shall submit his/her current original aircraft maintenance licence to the
competent authority together with the EASA Form 19.

REQUIREMENTS
(d) Where the applicant for change of the basic categories qualifies for such change via the
procedure referred to in point 66.B.100 in a Member State other than the Member State which
issued the license, the application shall be sent to the competent authority referred to in point
66.1.
(e) Where the applicant for change of the basic categories qualifies for such change via the
procedure referred to in point 66.B.105 in a Member State other than the Member State which
issued the license, the maintenance organisation approved in accordance with Annex II (Part-
145) shall send the aircraft maintenance licence together with the EASA Form 19 to the
competent authority referred to in point 66.1 for stamp and signature of the change or reissue
of the licence, as appropriate.
(f) Each application shall be supported by documentation to demonstrate compliance with the
applicable theoretical knowledge, practical training and experience requirements at the time of
application.
AMC 66.A.10 Application

1. Maintenance experience should be written up in a manner that the reader has a reasonable
understanding of where, when and what maintenance constitutes the experience. A task by
task account is not necessary but at the same time a bland statement ‘X years maintenance
experience completed’ is not acceptable. A log book of maintenance experience is desirable and
some competent authorities may require such log book to be kept. It is acceptable to cross refer
in the EASA Form 19 to other documents containing information on maintenance.
2. Applicants claiming the maximum reduction in 66.A.30(a) total experience based upon having
successfully completed 147.A.200 approved basic training should include the Part-147
certificate of recognition for approved basic training.
3. Applicants claiming reduction in 66.A.30(a) total experience based upon having successfully
completed technical training in an organisation or institute recognised by the competent
authority as a competent organisation or institute, should include the relevant certificate of
successful completion of training.
GM 66.A.10(a) Application
When an application is made for a licence in the B2L category, the applicant should specify on the
EASA Form 19:
− the system rating or the combination of system ratings the applicant applies for; and
− the aircraft rating,
considering that according to 66.A.45(e), a B2L licence endorsed with full subgroup 2b can be
endorsed also with full subgroup 2c.
When applying for the addition of a system rating on a B2L licence, the applicant should provide
together with the application, the demonstration of compliance with the experience requirements
related to the system the applicant applies for.
When a B2L licence holder applies for the extension of a B2L licence to add a new system rating,
he/she needs to demonstrate the practical experience required by 66.A.30(a)(2a) for the system rating
but also the practical experience required by 66.A.45(e) and (f) in case the aircraft group is different.

REQUIREMENTS
When a B2L licence holder applies for the change of his/her B2L licence to the B2 category, he/she
needs only to:
− demonstrate by examination the differences between the basic knowledge corresponding to
the B2L licence held and the basic knowledge of the B2 licence, as described in Appendix I; and
− demonstrate the additional experience described in Appendix IV.
These requirements can be found also for the competent authority in 66.B.110.
When an applicant applies for the extension of his/her B2L licence to a B2 licence and he/she meets
the relevant requirements, the B2L licence is replaced by the B2 licence.
66.A.15 Eligibility
An applicant for an aircraft maintenance licence shall be at least 18 years of age.
66.A.20 Privileges
(a) The following privileges shall apply:

1. A category A aircraft maintenance licence permits the holder to issue certificates of
release to service following minor scheduled line maintenance and simple defect
rectification within the limits of tasks specifically endorsed on the certification
authorisation referred to in point 145.A.35 of Annex II (Part-145). The certification
privileges shall be restricted to work that the licence holder has personally performed in
the maintenance organisation that issued the certification authorisation.
2. A category B1 aircraft maintenance licence shall permit the holder to issue certificates of
release to service and to act as B1 support staff following:
− maintenance performed on aircraft structure, powerplant and mechanical and
electrical systems,
− work on avionic systems requiring only simple tests to prove their serviceability
and not requiring troubleshooting.
Category B1 includes the corresponding A subcategory.
3. A category B2 aircraft maintenance licence shall permit the holder:
(i) to issue certificates of release to service and to act as B2 support staff for following:
− maintenance performed on avionic and electrical systems, and
− electrical and avionics tasks within powerplant and mechanical systems,
requiring only simple tests to prove their serviceability; and
(ii) to issue certificates of release to service following minor scheduled line
maintenance and simple defect rectification within the limits of tasks specifically
endorsed on the certification authorisation referred to in point 145.A.35 of Annex
II (Part-145). This certification privilege shall be restricted to work that the licence
holder has personally performed in the maintenance organisation which issued the
certification authorisation and limited to the ratings already endorsed in the B2
licence.

REQUIREMENTS
The category B2 licence does not include any A subcategory.

4. A category B2L aircraft maintenance licence shall permit the holder to issue certificates
of release to service and to act as B2L support staff for the following:
− maintenance performed on electrical systems;
− maintenance performed on avionics systems within the limits of the system ratings
specifically endorsed on the licence, and
− when holding the ‘airframe system’ rating, performance of electrical and avionics
tasks within power plant and mechanical systems, requiring only simple tests to
prove their serviceability.
5. A category B3 aircraft maintenance licence shall permit the holder to issue certificates of
release to service and to act as B3 support staff for the following:
− maintenance performed on aeroplane structure, power plant and mechanical and
electrical systems; and
− work on avionics systems requiring only simple tests to prove their serviceability
and not requiring troubleshooting.
6. A category L aircraft maintenance licence shall permit the holder to issue certificates of
release to service and to act as L support staff for the following:
− maintenance performed on aircraft structure, power plant and mechanical and
electrical systems;
− work on radio, Emergency Locator Transmitters (ELT) and transponder systems;
and
− work on other avionics systems requiring simple tests to prove their serviceability.
Subcategory L2 includes subcategory L1. Any limitation to subcategory L2 in accordance
with point 66.A.45(h) becomes also applicable to subcategory L1.
Subcategory L2C includes subcategory L1C.
7. A category C aircraft maintenance licence shall permit the holder to issue certificates of
release to service following base maintenance of the aircraft. The privileges apply to the
aircraft in its entirety.
(b) The holder of an aircraft maintenance licence may not exercise its privileges unless:
1. in compliance with the applicable requirements of Annex I (Part-M), Annex II (Part-145),
Annex Vb (Part-ML) and Annex Vd (Part-CAO); and
2. in the preceding 2-year period he/she has, either had 6 months of maintenance
experience in accordance with the privileges granted by the aircraft maintenance licence
or, met the provision for the issue of the appropriate privileges; and
3. he/she has the adequate competence to certify maintenance on the corresponding
aircraft; and
4. he/she is able to read, write and communicate to an understandable level in the
language(s) in which the technical documentation and procedures necessary to support
the issue of the certificate of release to service are written.

REQUIREMENTS
GM 66.A.20(a) Privileges
1. The following definitions apply:

Electrical system means the aircraft electrical power supply source, plus the distribution system
to the different components contained in the aircraft and relevant connectors. Lighting systems
are also included in this definition. When working on cables and connectors which are part of
these electrical systems, the following typical practices are included in the privileges:
− Continuity, insulation and bonding techniques and testing;
− Crimping and testing of crimped joints;
− Connector pin removal and insertion;
− Wiring protection techniques.
Avionics system means an aircraft system that transfers, processes, displays or stores analogue
or digital data using data lines, data buses, coaxial cables, wireless or other data transmission
medium, and includes the system’s components and connectors. Examples of avionics systems
include the following:
− Autoflight;
− Communication, Radar and Navigation;
− Instruments (see NOTE below);
− In Flight Entertainment Systems;
− Integrated Modular Avionics (IMA);
− On-Board Maintenance Systems;
− Information Systems;
− Fly by Wire Systems (related to ATA27 ‘Flight Controls’);
− Fibre Optic Control Systems.
NOTE: Instruments are formally included within the privileges of the B2 and B2L with system
rating ‘instruments’. However, maintenance on electromechanical and pitot-static components
may also be released by a B1, B3 or L licence holder.
Simple test means a test described in approved maintenance data and meeting all the following
criteria:
− The serviceability of the system can be verified using aircraft controls, switches, Built-in
Test Equipment (BITE), Central Maintenance Computer (CMC) or external test equipment
not involving special training.
− The outcome of the test is a unique go – no go indication or parameter, which can be a
single value or a value within an interval tolerance. No interpretation of the test result or
interdependence of different values is allowed.
− The test does not involve more than 10 actions as described in the approved maintenance
data (not including those required to configure the aircraft prior to the test, i.e. jacking,
flaps down, etc, or to return the aircraft to its initial configuration). Pushing a control,
switch or button, and reading the corresponding outcome may be considered as a single
step even if the maintenance data shows them separated.

REQUIREMENTS
Troubleshooting means the procedures and actions necessary, using approved maintenance
data, in order to identify the root cause of a defect or malfunction. It may include the use of
BITE or external test equipment.
Line maintenance: refer to AMC1 145.A.10
Base maintenance: refer to AMC1 145.A.10
2. The category B3 licence does not include any A subcategory. Nevertheless, this does not prevent
the B3 licence holder from releasing maintenance tasks typical of the A1.2 subcategory for
piston-engine non-pressurized aeroplanes of 2 000 kg MTOM and below, within the limitations
contained in the B3 licence.
3. The B1.2 and B3 licences do not include any L subcategory. Nevertheless, the holder of a B1.2
or B3 licence with the appropriate ratings is entitled to receive, upon application, licences in the
L1 and L2 subcategories under the conditions described in point 66.B.110(d).
4. The privileges of the B2 licence with given aircraft ratings include the privileges of the B2L
licence for all the system ratings for the same aircraft ratings. Nevertheless, the holder of a B2
licence with given aircraft ratings may apply for a B2L licence in order to include a different
aircraft rating if the applicant only wants to demonstrate compliance with the experience
requirements for certain system ratings.
5. The category C licence permits certification of scheduled base maintenance by the issue of a
single certificate of release to service for the complete aircraft after the completion of all such
maintenance. The basis for this certification is that the maintenance has been carried out by
competent mechanics, and category B1, B2, B2L, B3 and L support staff, as appropriate, have
signed for the maintenance tasks under their respective specialisation. The principal function of
the category C certifying staff is to ensure that all required maintenance has been called up and
signed off by the category B1, B2, B2L, B3 and L support staff, as appropriate, before issue of
the certificate of release to service. Only category C personnel who also hold category B1, B2,
B2L, B3 or L qualifications may perform both roles in base maintenance.
AMC 66.A.20(a)(4) Privileges

‘Within the limits of the system ratings specifically endorsed on the licence’ refers to the fact that the
privileges of the licence holder are limited:
− to the group/subgroup of aircraft endorsed on the licence, but also
− to the system rating(s) endorsed.
When an applicant wishes to get the privilege to issue certificates of release to service and to act as
support staff for electrical and avionics tasks within powerplant and mechanical systems, he/she
should apply for the rating ‘airframe system’ on the B2L licence. The reason is that the ‘airframe
systems’ rating is the only rating which covers completely the electrical and avionics tasks of the
powerplant and mechanical systems of the aircraft.

REQUIREMENTS
− Operation performed e.g. 100 FH check, MLG wheel change, engine oil check and
complement, SB embodiment, trouble shooting, structural repair, STC embodiment, etc.;
− In the particular case of Part-145 organisations, the type of maintenance i.e. base, line;
− Type of activity i.e. perform, supervise, release;
− Subcategory used (A1, A2, A3, A4, B1.1, B1.2, B1.3, B1.4, B2, B2L, B3, C or L1, L1C, L2, L2C,
L3G, L3H, L4G, L4H, L5);
− Duration in days or partial-days.
GM 66.A.20(b)2 Privileges
The sentence ‘met the provision for the issue of the appropriate privileges’ included in 66.A.20(b)2
means that during the previous 2 years the person has met all the requirements for the endorsement
of the corresponding aircraft rating (for example, in the case of aircraft in Group 1, theoretical plus
practical element plus, if applicable, on-the-job training). This supersedes the need for 6 months of
experience for the first 2 years. However, the requirement of 6 months of experience in the preceding
2 years will need to be met after the second year.
AMC 66.A.20(b)3 Privileges

The wording ‘has the adequate competence to certify maintenance on the corresponding aircraft’
means that the licence holder and, if applicable, the organisation where he/she is
contracted/employed, should ensure that he/she has acquired the appropriate knowledge, skills,
attitude and experience to release the aircraft being maintained. This is essential because some
systems and technology present in the particular aircraft being maintained may not have been
covered by the training/examination/experience required to obtain the licence and ratings.
This is typically the case, among others, in the following situations:
− Type ratings which have been endorsed on a licence in accordance with Appendix I to AMC to
Part-66 ‘List of Type Ratings’ after attending type training/on-the-job training which did not
cover all the models/variants included in such rating. For example, a licence endorsed with the
rating Airbus A318/A319/A320/A321 (CFM56) after attending type training/on-the-job training
covering only the Airbus 320 (CFM56).
− Type ratings which have been endorsed on a licence in accordance with Appendix I to AMC to
Part-66 ‘List of Type Ratings’ after a new variant has been added to the rating in Appendix I,
without performing difference training. For example, a licence endorsed with the rating Boeing
737-600/700/800/900 for a person who already had the rating Boeing 737-600/700/800,
without performing any difference training for the 737-900.
− Work being carried out on a model/variant for which the technical design and maintenance
techniques have significantly evolved from the original model used in the type training/on-the-
job training.
− Specific technology and options selected by each customer which may not have been covered
by the type training/on-the-job training.
− Changes in the basic knowledge requirements of Appendix I to Part-66 not requiring re-
examination of existing licence holders (grandfathered privileges).

REQUIREMENTS
− The endorsement of group/subgroup ratings based on experience on a representative number

of tasks/aircraft or based on type training/examination on a representative number of aircraft.
− Persons meeting the requirements of 6 months of experience every 2 years only on certain
similar aircraft types as allowed by AMC 66.A.20(b)2.
− Persons holding a Part-66 licence with limitations, obtained through conversion of national
qualifications (66.A.70), where such limitations are going to be lifted after performing the
corresponding basic knowledge examinations. In this case, the type ratings endorsed in the
licence may have been obtained in the national system without covering all the aircraft systems
(because of the previous limitations) and there will be a need to assess and, if applicable, to
train this person on the missing systems.
Additional information is provided in AMC 145.A.35(a).
GM 66.A.20(b)4 Privileges
1. Holders of a Part-66 aircraft maintenance licence may not exercise certification privileges unless
they have a general knowledge of the language used within the maintenance environment
including knowledge of common aeronautical terms in the language. The level of knowledge
should be such that the licence holder is able to:
− read and understand the instructions and technical manuals used for the performance of
maintenance;
− make written technical entries and any maintenance documentation entries, which can
be understood by those with whom they are normally required to communicate;
− read and understand the maintenance organisation procedures;
− communicate at such a level as to prevent any misunderstanding when exercising
certification privileges.
2. In all cases, the level of understanding should be compatible with the level of certification
privileges exercised.
66.A.25 Basic knowledge requirements

(a) For licences other than category L, an applicant for an aircraft maintenance licence, or for the
addition of a category or subcategory to such a licence, shall demonstrate by examination a
level of knowledge of the appropriate subject modules in accordance with Appendix I to Annex
III (Part-66). The examination shall comply with the standard set out in Appendix II to Annex III
(Part-66) and shall be conducted either by a training organisation appropriately approved in
accordance with Annex IV (Part-147), or by the competent authority.
(b) An applicant for an aircraft maintenance licence in category L within a given subcategory, or for
the addition of a different subcategory, shall demonstrate by examination a level of knowledge
of the appropriate subject modules in accordance with Appendix VII to Annex III (Part-66). The
examination shall comply with the standard set out in Appendix VIII to Annex III (Part-66) and
shall be conducted by a training organisation appropriately approved in accordance with
Annex IV (Part-147), by the competent authority or as agreed by the competent authority.

REQUIREMENTS
The holder of an aircraft maintenance licence in subcategory B1.2 or category B3 is deemed to

meet the basic knowledge requirements for a licence in subcategories L1C, L1, L2C and L2.
The basic knowledge requirements for subcategory L4H include the basic knowledge
requirements for subcategory L3H.
The basic knowledge requirements for subcategory L4G include the basic knowledge
requirements for subcategory L3G.
(c) An applicant for an aircraft maintenance licence in category B2L for a particular ‘system rating’,
or for the addition of another ‘system rating’, shall demonstrate by examination a level of
knowledge of the appropriate subject modules in accordance with Appendix I to Annex III (Part-
66). The examination shall comply with the standard set out in Appendix II to Annex III (Part-66)
and shall be conducted either by a training organisation appropriately approved in accordance
with Annex IV (Part-147), or by the competent authority.
(d) The training courses and examinations shall have been passed within 10 years prior to the
application for an aircraft maintenance licence or the addition of a category or subcategory to
such a licence. Should this not be the case, examination credits may be obtained in accordance
with point (e).
(e) The applicant may apply to the competent authority for full or partial examination credits for
the basic knowledge requirements for:
(i) basic knowledge examinations that do not meet the requirement laid down in point (d);
(ii) any other technical qualification considered by the competent authority to be equivalent
to the knowledge standard of Annex III (Part-66).
Credits shall be granted in accordance with Subpart E of Section B of this Annex (Part-66).
(f) Credits expire 10 years after they were granted to the applicant by the competent authority.
The applicant may apply for new credits after expiration.
AMC 66.A.25 Basic knowledge requirements

1. For an applicant being a person qualified by holding an academic degree in an aeronautical,

mechanical or electronic discipline from a recognised university or other higher educational
institute the need for any examination will depend upon the course taken in relation to
Appendix I to Part-66.
2. Knowledge gained and examinations passed during previous experiences, for example, in
military aviation and civilian apprenticeships will be credited where the competent authority is
satisfied that such knowledge and examinations are equivalent to that required by Appendix I
to Part-66.
GM 66.A.25(a) Basic knowledge requirements

The levels of knowledge for each licence (sub)category are directly related to the complexity of the
certifications related to the corresponding licence (sub)category, which means that category A should
demonstrate a limited but adequate level of knowledge, whereas category B1, B2, B2L and B3 should
demonstrate a complete level of knowledge in the appropriate subject modules.

REQUIREMENTS
GM 66.A.25(b) Basic knowledge requirements

‘Or as agreed by the competent authority’ refers to the examination that is conducted by an
organisation under a formal agreement (and oversight) of the competent authority.
66.A.30 Basic experience requirements

(a) An applicant for an aircraft maintenance licence shall have acquired:

1. for category A, subcategories B1.2 and B1.4 and category B3:
(i) 3 years of practical maintenance experience on operating aircraft, if the applicant
has no previous relevant technical training; or
(ii) 2 years of practical maintenance experience on operating aircraft and completion
of training considered relevant by the competent authority as a skilled worker, in
a technical trade; or
(iii) 1 year of practical maintenance experience on operating aircraft and completion
of a basic training course approved in accordance with Annex IV (Part-147);
2. for category B2 and subcategories B1.1 and B1.3:
(i) 5 years of practical maintenance experience on operating aircraft if the applicant
has no previous relevant technical training; or
(ii) 3 years of practical maintenance experience on operating aircraft and completion
of training considered relevant by the competent authority as a skilled worker, in
a technical trade; or
(iii) 2 years of practical maintenance experience on operating aircraft and completion
of a basic training course approved in accordance with Annex IV (Part-147);
2a. for category B2L:
(i) 3 years of practical maintenance experience in operating aircraft, covering the
corresponding system rating(s), if the applicant has no previous relevant technical
training; or
(ii) 2 years of practical maintenance experience in operating aircraft, covering the
corresponding system rating(s), and completion of training, considered relevant by
the competent authority, as a skilled worker in a technical trade; or
(iii) 1 year of practical maintenance experience in operating aircraft, covering the
corresponding system rating(s), and completion of a Part-147 approved basic
training course. For the addition of (a) new system rating(s) to an existing B2L
licence, 3 months of practical maintenance experience relevant to the new system
rating(s) shall be required for each system rating added.
2b. for category L:
(i) 2 years of practical maintenance experience in operating aircraft covering a
representative cross section of maintenance activities in the corresponding
subcategory;

REQUIREMENTS
(ii) as a derogation from point (i), 1 year of practical maintenance experience in

operating aircraft covering a representative cross section of maintenance activities
in the corresponding subcategory, subject to the introduction of the limitation
provided for in point 66.A.45(h)(ii)(3).
For the inclusion of an additional subcategory in an existing L licence, the experience
required by points (i) and (ii) shall be 12 and 6 months respectively.
The holder of an aircraft maintenance licence in category/subcategory B1.2 or B3 is
deemed to meet the basic experience requirements for a licence in subcategories L1C,
L1, L2C and L2.
3. for category C with respect to complex motor-powered aircraft:
(i) 3 years of experience exercising category B1.1, B1.3 or B2 privileges on complex
motor-powered aircraft or as support staff according to point 145.A.35, or, a
combination of both; or
(ii) 5 years of experience exercising category B1.2 or B1.4 privileges on complex motor-
powered aircraft or as support staff according to point 145.A.35, or a combination
of both;
4. for category C with respect to other than complex motor-powered aircraft: 3 years of
experience exercising category B1 or B2 privileges on other than complex motor-powered
aircraft or as support staff according to point 145.A.35, or a combination of both;
5. for category C obtained through the academic route: an applicant holding an academic
degree in a technical discipline, from a university or other higher educational institution
recognised by the competent authority, 3 years of experience working in a civil aircraft
maintenance environment on a representative selection of tasks directly associated with
aircraft maintenance including 6 months of observation of base maintenance tasks.
(b) An applicant for an extension to an aircraft maintenance licence shall have a minimum civil
aircraft maintenance experience requirement appropriate to the additional category or
subcategory of licence applied for as defined in Appendix IV to this Annex (Part-66).
(c) The experience shall be practical and involve a representative cross section of maintenance
tasks on aircraft.
(d) At least 1 year of the required experience shall be recent maintenance experience on aircraft of
the category/subcategory for which the initial aircraft maintenance licence is sought. For
subsequent category/subcategory additions to an existing aircraft maintenance licence, the
additional recent maintenance experience required may be less than 1 year, but shall be at least
3 months. The required experience shall be dependent upon the difference between the licence
category/subcategory held and applied for. Such additional experience shall be typical of the
new licence category/subcategory sought.
(e) Notwithstanding point (a), aircraft maintenance experience gained outside a civil aircraft
maintenance environment shall be accepted when such maintenance is equivalent to that
required by this Annex (Part-66) as established by the competent authority. Additional
experience of civil aircraft maintenance shall, however, be required to ensure adequate
understanding of the civil aircraft maintenance environment.
(f) Experience shall have been acquired within the 10 years preceding the application for an aircraft
maintenance licence or the addition of a category or subcategory to such a licence.

REQUIREMENTS
AMC 66.A.30(a) Basic experience requirements

1. For a category C applicant holding an academic degree the representative selection of tasks
should include the observation of hangar maintenance, maintenance planning, quality
assurance, record-keeping, approved spare parts control and engineering development.
2. While an applicant to a category C licence may be qualified by having 3 years experience as
category B1 or B2 certifying staff only in line maintenance, it is however recommended that any
applicant to a category C holding a B1 or B2 licence demonstrate at least 12 months experience
as a B1 or B2 support staff.
3. A skilled worker is a person who has successfully completed a training, acceptable to the
competent authority, involving the manufacture, repair, overhaul or inspection of mechanical,
electrical or electronic equipment. The training would include the use of tools and measuring
devices.
4. Maintenance experience on operating aircraft:
− means the experience of being involved in maintenance tasks on aircraft which are being
operated by airlines, air taxi organisations, aero clubs, owners, etc., as relevant to the
licence category/subcategory;
− should cover a wide range of tasks in terms of length, complexity and variety;
− aims at gaining sufficient experience in the real environment of maintenance as opposed
to only the training school environment;
− may be gained within different types of maintenance organisations (Part-145, M.A.
Subpart F, Part-CAO, FAR-145, etc.) or under the supervision of independent certifying
staff;
− May be combined with Part-147 approved training (or other training approved by the
competent authority) so that periods of training can be intermixed with periods of
experience, similar to an apprenticeship;
− may be full-time or part-time, either as professional or on a voluntary basis;
− in the case of the L licence, it is acceptable that the 1 or 2 years of experience required
by 66.A.30(a)(2b) covers maintenance performed only during the weekends (or
equivalent periods) as long as the applicant has achieved a sufficient level of competency
related to the applicable licence subcategory as attested by the corresponding
statement(s) issued by the maintenance organisation(s) or independent certifying staff
that supervised the applicant.
5. In the case of an applicant for a licence including several categories/subcategories, it is
acceptable to combine the periods of experience as long as there is a sufficient experience for
each category/subcategory during the required period. Examples:
− Application for a B1.1 (turbine aeroplanes) + B1.3 (turbine helicopters): The Regulation
requires 5 years of experience for B1.1 and 5 years of experience for B1.3 for an applicant
with no relevant previous technical training:
− It is not acceptable to combine the experience in a single 5-year period where the
applicant has been working for 3 years on turbine aeroplanes and 2 years on
turbine helicopters.

REQUIREMENTS
− However, it is acceptable to combine the experience in a single 5-year period if the

applicant has been working for 5 years on turbine aeroplanes and turbine
helicopters (for example, aeroplanes in the morning, helicopters in the afternoon,
or a few days every week on aeroplanes and a few days every week on helicopters).
− Application for a B1.1 (turbine aeroplanes) + B2 (avionics): The Regulation requires 5
years of experience for B1.1 and 5 years of experience for B2 for an applicant with no
relevant previous technical training.
− It is not acceptable to combine the experience in a single 5-year period where the
applicant has been working for 3 years on turbine aeroplanes (with no avionics
work) and 2 years on avionics systems.
− However, it is acceptable to combine the experience in a single 5-year period if the
applicant has been working for 5 years on structures, powerplant, mechanical and
electrical systems and avionics (for B1.1 tasks in the morning, B2 tasks in the
afternoon, or a few days every week for B1.1 tasks and a few days every week for
B2 tasks).
− Application for a B1.1, B1.2, B1.3, B1.4 and B2: The Regulation requires 5 years of
experience for B1.1, B1.3 and B2 and 3 years of experience for B1.2 and B1.4 for an
applicant with no relevant previous technical training.
− In this case, it is very unlikely that the experience for each category/subcategory
would be sufficient.
AMC 66.A.30(c) Basic experience requirements

In the case of the category B2L licence, the sentence ‘a representative cross section of maintenance
tasks on aircraft’ refers to the person that has carried out some maintenance tasks that are
representative of the systems corresponding to the system ratings for which he/she applies (see
66.A.3). These tasks may include troubleshooting, modifications or repairs.
AMC 66.A.30(d) Basic experience requirements

To be considered as recent experience; at least 50% of the required 12-month recent experience
should be gained within the 12 month period prior to the date of application for the aircraft
maintenance licence. The remainder of the recent experience should have been gained within the 7-
year period prior to application. It must be noted that the rest of the basic experience required by
66.A.30 must be obtained within the 10 years prior to the application as required by 66.A.30(f).
AMC 66.A.30(e) Basic experience requirements

1. For categories A and L, the additional experience should be a minimum of 6 months in a civil
aircraft maintenance environment. For categories B1, B2, B2L or B3, the additional experience
should be a minimum of 12 months in a civil aircraft maintenance environment.
2. Aircraft maintenance experience gained outside a civil aircraft maintenance environment may
include aircraft maintenance experience gained in armed forces, coast guards, police etc. or in
aircraft manufacturing.

REQUIREMENTS
66.A.40 Continued validity of the aircraft maintenance licence

(a) The aircraft maintenance licence becomes invalid 5 years after its last issue or change, unless
the holder submits his/her aircraft maintenance licence to the competent authority that issued
it, in order to verify that the information contained in the licence is the same as that contained
in the competent authority records, pursuant to point 66.B.120.
(b) The holder of an aircraft maintenance licence shall complete the relevant parts of EASA Form
19 (see Appendix V) and submit it with the holder's copy of the licence to the competent
authority that issued the original aircraft maintenance licence, unless the holder works in a
maintenance organisation approved in accordance with Annex II (Part-145) that has a
procedure in its exposition whereby such organisation may submit the necessary
documentation on behalf of the aircraft maintenance licence holder.
(c) Any certification privilege based upon a aircraft maintenance licence becomes invalid as soon
as the aircraft maintenance licence is invalid.
(d) The aircraft maintenance licence is only valid (i) when issued and/or changed by the competent
authority and (ii) when the holder has signed the document.
GM 66.A.40 Continued validity of the aircraft maintenance licence

The validity of the aircraft maintenance licence is not affected by recency of maintenance experience
whereas the validity of the 66.A.20 privileges is affected by maintenance experience as specified in
66.A.20(a).
66.A.45 Endorsement with aircraft ratings

(a) In order to be entitled to exercise certification privileges on a specific aircraft type, the holder
of an aircraft maintenance licence needs to have their licence endorsed with the relevant
aircraft ratings:
− For category B1, B2 or C, the relevant aircraft ratings are the following:
(i) for Group 1 aircraft, the appropriate aircraft type rating;
(ii) for Group 2 aircraft, the appropriate aircraft type rating, manufacturer subgroup
rating or full subgroup rating;
(iii) for Group 3 aircraft, the appropriate aircraft type rating or full group rating;
(iv) for Group 4 aircraft, for the category B2 licence, the full group rating.
− For category B2L, the relevant aircraft ratings are the following:
(i) for Group 2 aircraft, the appropriate manufacturer subgroup rating or full
subgroup rating;
(ii) for Group 3 aircraft, the full group rating;
(iii) for Group 4 aircraft, the full group rating.
− For category B3, the relevant rating is ‘piston-engine non-pressurised aeroplanes of
2 000 kg MTOM and below’.

REQUIREMENTS
− For category L, the relevant aircraft ratings are the following:

(i) for subcategory L1C, the rating ‘composite sailplanes’;
(ii) for subcategory L1, the rating ‘sailplanes’;
(iii) for subcategory L2C, the rating ‘composite powered sailplanes and composite ELA1
aeroplanes’;
(iv) for subcategory L2, the rating ‘powered sailplanes and ELA1 aeroplanes’;
(v) for subcategory L3H, the rating ‘hot-air balloons’;
(vi) for subcategory L3G, the rating ‘gas balloons’
(vii) for subcategory L4H, the rating ‘hot-air airships’;
(viii) for subcategory L4G, the rating ‘ELA2 gas airships’;
(ix) for subcategory L5, the appropriate airship type rating.
− For category A, no rating is required, subject to compliance with the requirements of
point 145.A.35 of Annex II (Part-145).
(b) The endorsement of aircraft type ratings requires the satisfactory completion of one of the
following:
− the relevant category B1, B2 or C aircraft type training in accordance with Appendix III to
Annex III (Part-66);
− in the case of gas airship type ratings on a B2 or L5 licence, a type training approved by
the competent authority in accordance with point 66.B.130.
(c) For other than category C licences, in addition to the requirements of point (b), the
endorsement of the first aircraft type rating within a given category/subcategory requires
satisfactory completion of the corresponding on-the-job training. This on-the-job training shall
comply with Appendix III to Annex III (Part-66), except in the case of gas airships, where it shall
be directly approved by the competent authority.
(d) By derogation from points (b) and (c), for Group 2 and 3 aircraft, aircraft type ratings may also
be endorsed on a licence after completing the following steps:
− satisfactory completion of the relevant category B1, B2 or C aircraft type examination in
accordance with Appendix III to this Annex (Part-66);
− in the case of B1 and B2 category, demonstration of practical experience in the aircraft
type. In that case, the practical experience shall include a representative cross section of
maintenance activities relevant to the licence category.
In the case of a category C rating, for a person qualified through the academic route as referred
to in point (a)(5) of point 66.A.30, the first relevant aircraft type examination shall be at the
category B1 or B2 level.
(e) For Group 2 aircraft:
(i) the endorsement of manufacturer subgroup ratings for category B1 and C licence holders
requires complying with the aircraft type rating requirements for at least two aircraft
types from the same manufacturer, which combined are representative of the applicable
manufacturer subgroup;

REQUIREMENTS
(ii) the endorsement of full subgroup ratings for category B1 and C licence holders requires
complying with the aircraft type rating requirements for at least three aircraft types from
different manufacturers, which combined are representative of the applicable subgroup;
(iii) the endorsement of manufacturer subgroup and full subgroup ratings for category B2
and B2L licence holders requires demonstration of practical experience which shall
include a representative cross section of maintenance activities relevant to the licence
category and to the applicable aircraft subgroup and, in the case of the B2L licence,
relevant to the applicable system rating(s);
(iv) by derogation from point (e)(iii), the holder of a B2 or B2L licence, endorsed with a full
subgroup 2b, is entitled to be endorsed with a full subgroup 2c.
(f) For Group 3 and 4 aircraft:
(i) the endorsement of the full Group 3 rating for category B1, B2, B2L and C licence holders
and the endorsement of the full Group 4 rating for B2 and B2L licence holders require
demonstration of practical experience, which shall include a representative cross section
of maintenance activities relevant to the licence category and to Group 3 or 4, as
applicable;
(ii) for category B1, unless the applicant provides evidence of appropriate experience, Group
3 rating shall be subject to the following limitations, which shall be endorsed on the
licence:
− pressurised aeroplanes,
− metal-structure aeroplanes,
− composite-structure aeroplanes,
− wooden-structure aeroplanes,
− aeroplanes with metal-tubing structure covered with fabric;
(iii) by derogation from point (f)(i), the holder of a B2L licence, endorsed with a full subgroup
2a or 2b, is entitled to be endorsed with Groups 3 and 4.
(g) For the B3 licence:
(i) the endorsement of the rating ‘piston engine non-pressurised aeroplanes of 2 000 kg
MTOM and below’ requires demonstration of practical experience, which shall include a
representative cross section of maintenance activities relevant to the licence category;
(ii) unless the applicant provides evidence of appropriate experience, the rating referred to
in point (i) shall be subject to the following limitations, which shall be endorsed on the
licence:
− wooden-structure aeroplanes,
− aeroplanes with metal-tubing structure covered with fabric,
− metal-structure aeroplanes,
− composite-structure aeroplanes.
(h) For all L licence subcategories, other than L5:
(i) the endorsement of ratings requires demonstration of practical experience which shall
include a representative cross section of maintenance activities relevant to the licence
subcategory;

REQUIREMENTS
(ii) unless the applicant provides evidence of appropriate experience, the ratings shall be
subject to the following limitations, which shall be endorsed on the licence:
(1) for ratings ‘sailplanes’ and ‘powered sailplanes and ELA1 aeroplanes’:
− wooden-structure aircraft covered with fabric,
− aircraft with metal-tubing structure covered with fabric,
− metal-structure aircraft,
− composite-structure aircraft,
(2) for the rating ‘gas balloons’:
− other than ELA1 gas balloons; and
(3) if the applicant has only provided evidence of one-year experience in accordance
with the derogation contained in point 66.A.30(a)(2b)(ii), the following limitation
shall be endorsed on the licence:
‘complex maintenance tasks provided for in Appendix VII to Annex I (Part-M),
standard changes provided for in point 21.A.90B of Annex I (Part-21) to Regulation
(EU) No 748/2012 and standard repairs provided for in point 21.A.431B of Annex I
(Part-21) to Regulation (EU) No 748/2012.’
The holder of an aircraft maintenance licence in subcategory B1.2 endorsed with
the Group 3 rating, or in category B3 endorsed with the rating ‘piston engine non-
pressurised aeroplanes of 2 000 kg MTOM and below’, is deemed to meet the
requirements for the issuance of a licence in subcategories L1 and L2 with the
corresponding full ratings and with the same limitations as the B1.2/B3 licence
held.
GM 66.A.45 Endorsement with aircraft ratings

The following table shows a summary of the aircraft rating requirements contained in 66.A.45, 66.A.50
and Appendix III to Part-66.
The table contains the following:
− The different aircraft groups.
− For each licence (sub)category, which ratings are possible (at the choice of the applicant):
− Individual type ratings.
− Full and/or Manufacturer (sub)group ratings
− For each rating option, which are the qualification options.
− For the B1.2 licence (Group 3 aircraft), the B3 licence (piston-engine non-pressurised aeroplanes
of 2 000 kg MTOM and below) and the L licences, which are the possible limitations and ratings
to be included in the licence if not sufficient experience can be demonstrated in those areas.
Note: OJT means ‘On-the-Job Training’ (Appendix III to Part-66, Section 6) and is only required for the
first aircraft rating in the licence (sub)category.

REQUIREMENTS
Aircraft rating requirements

Aircraft B1/B3/L licence B2/B2L licence C licence
Group 1 aircraft, except (For B1) (For B2)
airships
Individual TYPE RATING Individual TYPE RATING Individual TYPE RATING
- Complex motor-
powered aircraft. Type training: Type training: Type training:
- Multiple engine - Theory + examination - Theory + examination - Theory + examination
helicopters. - Practical + assessment - Practical + assessment
- Aeroplanes certified PLUS PLUS
above FL290. OJT (for first aircraft in OJT (for first aircraft in
- Aircraft equipped with licence subcategory) licence subcategory)
fly-by-wire.
- Other aircraft when
defined by the Agency.
Group 1 airships (For L5 licence) (For B2)
Individual TYPE RATING Individual TYPE RATING
Type training: Type training:

- Theory + examination - Theory + examination Not applicable
- Practical + assessment - Practical + assessment
PLUS PLUS
OJT (for first aircraft in OJT (for first aircraft in
licence subcategory) licence category)
Group 2 aircraft (For B1.1, B1.3, B1.4) (For B2)
Subgroups: Individual TYPE RATING Individual TYPE RATING Individual TYPE RATING
(type training + OJT) or (type training + OJT) or type training or type
2a: single turboprop (type examination + (type examination + examination
aeroplanes (*) practical experience) practical experience)
2b: single turbine Full SUBGROUP RATING (For B2 and B2L) Full SUBGROUP RATING
engine helicopters (*) (type training + OJT) or type training or type
(type examination + Full SUBGROUP RATING examination on at least
2c: single piston practical experience) on based on demonstration 3 aircraft representative
engine helicopters (*) at least 3 aircraft of practical experience of that subgroup
representative of that
(*) Except those subgroup
classified in Group 1.
Manufacturer Manufacturer Manufacturer
SUBGROUP RATING SUBGROUP RATING SUBGROUP RATING
(type training + OJT) based on demonstration type training or type
or (type examination + of practical experience examination on at least
practical experience) on 2 aircraft representative
at least 2 aircraft of that manufacturer
representative subgroup
of that manufacturer
subgroup

REQUIREMENTS
GM 66.A.45(b) Endorsement with aircraft ratings

An aircraft type rating includes all the aircraft models/variants listed in column 2 of Appendix I to AMC
to Part-66.
When a person already holds a type rating on the licence and such type rating is amended in the
Appendix I to AMC to Part-66 in order to include additional models/variants, there is no need for
additional type training for the purpose of amending the type rating in the licence. The rating should
be amended to include the new variants, upon request by the applicant, without additional
requirements. However, it is the responsibility of the licence holder and, if applicable, the
maintenance organisation where he/she is employed to comply with 66.A.20(b)3, 145.A.35(a),
M.A.607(a), and CAO.A.040 as applicable, before he/she exercises certification privileges.
Similarly, type training courses covering certain, but not all the models/variants included in a type
rating, are valid for the purpose of endorsing the full type rating.
AMC 66.A.45(d);(e)3;(f)1;(g)1;(h) Endorsement with aircraft ratings

1. The ‘practical experience’ should cover a representative cross section including at least:
− for categories B1, B2, B2L and B3: 50 % of the tasks contained in Appendix II to the AMC
relevant to the licence category and to the applicable aircraft type ratings or aircraft
(sub)group ratings being endorsed;
− for category L:
− in the subcategories L1, L1C, L2 or L2C: 50 % as in the paragraph related to B1, B2,
B2L or B3;
− in the subcategories L3H and L3G for ‘Balloons’ or L4H, L4G and L5 for ‘Airships’,
80 % of the tasks should be demonstrated, and should include the tasks identified
with an asterisk (*) in the Appendix;
This experience should cover tasks from each paragraph of the Appendix II list. Other tasks than
those in the Appendix II may be considered as a replacement when they are relevant. In the
case of (sub)group ratings, this experience may be shown by covering one or several aircraft
types of the applicable (sub)group and may include experience on aircraft classified in group 1,
2 and/or 3 as long as the experience is relevant. The practical experience should be obtained
under the supervision of authorised certifying staff.
2. In the case of endorsement of individual type ratings for Group 2 and Group 3 aircraft, for the
second aircraft type of each manufacturer (sub)group the practical experience should be
reduced to 30% of the tasks contained in Appendix II to AMC relevant to the licence category
and to the applicable aircraft type. For subsequent aircraft types of each manufacturer (sub)
group this should be reduced to 20%.
3. Practical experience should be demonstrated by the submission of records or a log book
showing the Appendix II tasks performed by the applicant. Typical data to be recorded are
similar to those described in AMC 66.A.20(b)2.

REQUIREMENTS
GM 66.A.45(h)2 Endorsement with aircraft ratings

For subcategories L1 and L2, it is possible to endorse the corresponding ratings with limitations
depending on the type of structures covered by the experience gained.
For subcategory L3G, it is possible to endorse the rating ‘gas balloons’ with a limitation to ‘other than
ELA1 gas balloons’ if the experience gained only covers ELA1 gas balloons.
However, no limitations are possible for the subcategories L1C, L2C, L3H, L4H and L4G. The ratings on
these licences can only be obtained after demonstration of the appropriate experience representative
of the full scope of the licence subcategory.
66.A.50 Limitations
(a) Limitations introduced on an aircraft maintenance licence are exclusions from the certification
privileges and, in the case of limitations referred to in point 66.A.45, they affect the aircraft in
its entirety.
(b) For limitations referred to in point 66.A.45, limitations shall be removed upon:
1. demonstration of appropriate experience; or
2. after a satisfactory practical assessment performed by the competent authority.
(c) For limitations referred to in point 66.A.70, limitations shall be removed upon satisfactory
completion of examination on those modules/subjects defined in the applicable conversion
report referred to in point 66.B.300.
AMC 66.A.50(b) Limitations

1. The appropriate experience required to remove the limitations referred to in 66.A.45(f),(g) and
(h) should consist of the performance of a variety of tasks appropriate to the limitations under
the supervision of authorised certifying staff. This should include the tasks required by a
scheduled annual inspection. Alternatively, this experience may also be gained, if agreed by the
competent authority, by theoretical and practical training provided by the manufacturer, as
long as an assessment is further carried out and recorded by this manufacturer.
2. It is acceptable to have this experience in just one aircraft type, provided this type is
representative of the (sub)group in relation to the limitation being removed.
3. It is acceptable that this experience is gained in aircraft not covered by the Basic Regulation,
provided that this experience is relevant and representative of the corresponding (sub)group.
An example could be the experience required to remove a limitation such as ‘aircraft with metal
tubing structure covered with fabric’, which may be gained in ultralight aircraft (Annex I
aircraft).
4. The application for the limitation removal should be supported by a record of experience signed
by the authorised certifying staff or by an assessment signed by the manufacturer after
completion of the applicable theoretical and practical training.

REQUIREMENTS
66.A.55 Evidence of qualification

Personnel exercising certification privileges as well as support staff shall produce their licence, as
evidence of qualification, within 24 hours upon request by an authorised person.
66.A.70 Conversion provisions

(a) The holder of a certifying staff qualification valid in a Member State, prior to the date of entry
into force of Annex III (Part-66) shall be issued an aircraft maintenance licence by the competent
authority of this Member State without further examination subject to the conditions specified
in Section B Subpart D.
(b) A person undergoing a certifying staff qualification process valid in a Member State, prior to the
date of entry into force of Annex III (Part-66) may continue to be qualified. The holder of a
certifying staff qualification gained following such process shall be issued an aircraft
maintenance licence by the competent authority of this Member State without further
examination subject to the conditions specified in Section B Subpart D.
(c) Where necessary, the aircraft maintenance licence shall contain limitations in accordance with
point 66.A.50 to reflect the differences between:
(i) the scope of the certifying staff qualification valid in the Member State before the entry
into force of the applicable licence category or subcategory provided for in this Annex
(Part-66);
(ii) the basic knowledge requirements and the basic examination standards laid down in
Appendices I and II to this Annex (Part-66).
(d) By derogation from point (c), for aircraft not used by licenced air carriers in accordance with
Regulation (EC) No 1008/2008, other than complex motor-powered aircraft, and for balloons,
sailplanes, motor-powered sailplanes and airships, the aircraft maintenance licence shall
contain limitations in accordance with point 66.A.50 to ensure that the certifying staff privileges
valid in the Member State before the entry into force of the applicable Part-66 licence
category/subcategory and those of the converted Part-66 aircraft maintenance licence remain
the same.
GM 66.A.70 Conversion provisions

1. As described in point 66.A.70, the conversion provisions apply to the holder of a certifying staff
qualification valid in a Member State prior to the date of entry into force of Annex III (Part-66).
The sentence ‘the holder of a certifying staff qualification valid in a Member State’ means any
person who had a qualification valid in that Member State allowing that person the
performance of activities identical to the privileges of ‘certifying staff’ contained in Regulation
(EU) 1321/2014. This means that the signature of that person was sufficient to declare that the
maintenance had been properly performed and the aircraft was ready for service and fit for
flight in respect to such maintenance.
This should not been mistaken with the responsibilities linked to the airworthiness review,
which was performed at different periods (typically varying from 6 months to 3 years) in the
national systems. This is an activity which is performed at very specific points of time and not
after every maintenance activity. Since an airworthiness review (or equivalent term used in the

REQUIREMENTS
submitted prior to those dates. The applicant is entitled to have the conversion performed
irrespective of when he/she applies for conversion.
5. A certifying staff qualification can be subject to more than one conversion process and can also
be converted to more than one licence (sub)category (with any applicable limitations). This
could be the case, for example, of a person who already had the certifying staff qualification
converted in the past to a B1.2 licence with limitations linked to some missing elements of the
Part-66 Appendix I and II standard (following 66.A.70(c)). This person would be entitled to apply
and have his/her certifying staff qualification converted to a B1.2 or a B3 or L licence on the
basis of 66.A.70(d), which would mean no need to compare with the Part-66 Appendix I, II or
VII standard, introducing only those limitations required in order to maintain the existing
privileges.
GM 66.A.70(c) Conversion provisions

For example, a limitation could be where a person holds a pre-existing certifying staff qualification
which covered, to the standard of Part-66 Appendix I and II, all the modules/subjects corresponding
to the B1 licence except for electrical power systems. This person would be issued a Part-66 aircraft
maintenance licence in the B1 category with a limitation (exclusion) on electrical power systems.
For removal of limitations, refer to 66.A.50(c).
GM 66.A.70(d) Conversion provisions

For aircraft not used by air carriers licensed in accordance with Regulation (EC) No 1008/2008 other
than complex motor-powered aircraft, an example of limitations could be where a person holds a pre-
Part-66 qualification which covered privileges to release work performed on aircraft structures,
powerplant, mechanical and electrical systems but excluded privileges on aircraft equipped with
turbine engine, aircraft above 2 000 kg MTOM, pressurised aircraft and aircraft equipped with
retractable landing gear. This person would be issued with a Part-66 aircraft maintenance licence in
the B1.2 or B3 (sub)category with the following limitations (exclusions):
− aircraft used by air carriers licensed in accordance with Regulation (EC) No 1008/2008 (this
limitation always exists);
− aircraft above 2 000 kg MTOM;
− pressurised aircraft;
− aircraft equipped with retractable landing gear.
Another example of limitations could be where a pilot-owner holds a pre-Part-66 qualification which
covered privileges to release work performed on aircraft structures, powerplant, mechanical and
electrical systems but limited to their own aircraft and limited to a particular aircraft type (for example,
a Cessna 172). This pilot-owner would receive a Part-66 aircraft maintenance licence in the B1.2 or B3
(sub)category with the following limitations (exclusions):
− aircraft used by air carriers licensed in accordance with Regulation (EC) No 1008/2008 (this
limitation always exists);
− aircraft other than a Cessna 172;
− aircraft not owned by the licence holder.

REQUIREMENTS
One more example would be the case where a person holds a pre-Part-66 qualification that covers
privileges to release work on composite and metal sailplanes and powered sailplanes, covering aircraft
structures, powerplant, mechanical and electrical systems. This person would be issued a Part-66
aircraft maintenance licence in the L2 subcategory, with the following limitations (exclusions):
− ELA1 aeroplanes;
− wooden-structure aircraft covered with fabric;
− aeroplanes with metal-tubing structure covered with fabric.
And one more example would be the case where a person holds a pre-Part-66 qualification that covers
privileges to release work on composite sailplanes up to the annual inspection but not including
complex maintenance tasks, repairs and changes. This person would be issued a Part-66 aircraft
maintenance licence in the L1C subcategory, with the following limitations:
− complex maintenance tasks described in Appendix VII to Annex I (Part-M), standard changes
described in Part 21 point 21.A.90B, and standard repairs described in Part 21 point 21.A.431B.
The essential aspect is that the limitations are established in order to maintain the privileges of the
pre-Part-66 qualification without comparing the previous qualification with the standard of Part-66
Appendix I and II.
For removal of limitations, refer to 66.A.50(c).

SECTION B — PROCEDURES FOR
COMPETENT AUTHORITIES
SECTION B — PROCEDURES FOR COMPETENT AUTHORITIES
SUBPART A — GENERAL
66.B.1 Scope
This section establishes the procedures including the administrative requirements to be followed by
the competent authorities in charge of the implementation and the enforcement of Section A of this
Annex (Part-66).
66.B.10 Competent authority

(a) General
The Member State shall designate a competent authority with allocated responsibilities for the
issuance, continuation, change, suspension or revocation of aircraft maintenance licences.
This competent authority shall establish an adequate organisational structure to ensure
compliance with this Annex (Part-66).
(b) Resources
The competent authority shall be appropriately staffed to ensure the implementation of the
requirements of this Annex (Part-66).
(c) Procedures
The competent authority shall establish documented procedures detailing how compliance with
this Annex (Part-66) is accomplished. These procedures shall be reviewed and amended to
ensure continued compliance.
66.B.20 Record-keeping
(a) The competent authority shall establish a system of record-keeping that allows adequate
traceability of the process to issue, revalidate, change, suspend or revoke each aircraft
maintenance licence.
(b) These records shall include for each licence:
1. the application for an aircraft maintenance licence or change to that licence, including all
supporting documentation;
2. a copy of the aircraft maintenance licence including any changes;
3. copies of all relevant correspondence;
4. details of any exemption and enforcement actions;
5. any report from other competent authorities relating to the aircraft maintenance licence
holder;
6. the records of examinations conducted by the competent authority;
7. the applicable conversion report used for conversion;

8. the applicable credit report used for crediting.

(c) Records referred to in points 1 to 5 of point (b) shall be kept at least 5 years after the end of the
licence validity.
(d) Records referred to in points 6, 7 and 8 of point (b) shall be kept for an unlimited period.
AMC 66.B.20 Record-keeping

1. The record-keeping system should ensure that all records are accessible whenever needed
within a reasonable time. These records should be organized in a consistent way throughout
the competent authority (chronological, alphabetical order, etc.).
2. All records containing sensitive data regarding applicants or organisations should be stored in a
secure manner with controlled access to ensure confidentiality of this kind of data.
3. All computer hardware used to ensure data backup should be stored in a different location from
that containing the working data in an environment that ensures they remain in good condition.
When hardware or software changes take place special care should be taken that all necessary
data continues to be accessible at least through the full period specified in 66.B.20.
66.B.25 Mutual exchange of information

(a) The competent authorities shall participate in a mutual exchange of information in accordance
with Article 72(1) of Regulation (EU) 2018/1139.
(b) Without prejudice to the competencies of the Member States, in the case of a potential safety
threat involving several Member States, the concerned competent authorities shall assist each
other in carrying out the necessary oversight action.
66.B.30 Exemptions
All exemptions granted in accordance with Article 71(1) of Regulation (EU) 2018/1139 shall be
recorded and retained by the competent authority.

SUBPART B — ISSUE OF AN AIRCRAFT MAINTENANCE LICENCE

This Subpart provides the procedures to be followed by the competent authority to issue, change or
continue an aircraft maintenance licence.
66.B.100 Procedure for the issue of an aircraft maintenance licence

by the competent authority
(a) On receipt of EASA Form 19 and any supporting documentation, the competent authority shall
verify EASA Form 19 for completeness and ensure that the experience claimed meets the
requirement of this Annex (Part-66).
(b) The competent authority shall verify an applicant's examination status and/or confirm the
validity of any credits to ensure that all module requirements of Appendix I or Appendix VII, as
applicable, have been met as required by this Annex (Part-66).
(c) When having verified the identity and date of birth of the applicant and being satisfied that the
applicant meets the standards of knowledge and experience required by this Annex (Part-66),
the competent authority shall issue the relevant aircraft maintenance licence to the applicant.
The same information shall be kept on competent authority records.
(d) In the case where aircraft types or groups are endorsed at the time of the issuance of the first
aircraft maintenance licence, the competent authority shall verify compliance with point
66.B.115.
AMC 66.B.100 Procedure for the issue of an aircraft maintenance

licence by the competent authority
1. Applicants claiming the maximum reduction in 66.A.30(a) total experience based upon
successful completion of a 147.A.200 approved basic training course should include the Part-
147 certificate of recognition for approved basic training.
2. Applicants claiming reduction in 66.A.30(a) total experience based upon successful completion
of training considered relevant by the competent authority as a skilled worker in a technical
trade, should include the relevant certificate of successful completion of training.
3. Applicants claiming credit against the 66.A.30(a) total experience requirement by virtue of
66.A.30(a) non-civil aircraft maintenance experience may only be granted such credit where the
Member State has recognised such non-civil aircraft maintenance experience. The competent
authority in recognising non-civil aircraft maintenance experience should have specified who
within the non-civil environment may make a statement that the applicant has met relevant
maintenance experience. The applicant should include a detailed statement of such
maintenance experience signed by the non-civil maintenance authority in accordance with the
conditions specified by the competent authority.
4. The competent authority should check that the experience record satisfies above paragraphs in
terms of content and the countersigning signature.

AMC 66.B.100 to 115

Aircraft type endorsement should use the standard codes contained in Appendix I to the AMCs.
GM 66.B.100 Procedure for the issue of an aircraft maintenance

licence by the competent authority
At the issue or renewal of a B2L licence:

− one or several system ratings; and
− one or several group/subgroup ratings,
should be endorsed on the licence (EASA Form 26).
A licences should be issued with a subcategory without type ratings.
B1, B2 and C licences may be issued without an aircraft type or group rating.
B2L licences may be issued without an aircraft type or group rating. The B2L licence should always be
issued with at least one system rating. This is based on the demonstrated initial experience that at
least should be sufficient to endorse one system rating.
B3 licences should be issued with the rating ‘piston engine non-pressurised aeroplanes of 2 000 kg
MTOM and below’ endorsed as the experience requirement for the rating is at least covered by the 1,
2 or 3 years of experience for that category.
L licences should be issued with at least one subcategory and the relevant aircraft rating.
66.B.105 Procedure for the issue of an aircraft maintenance licence

via a maintenance organisation approved in accordance with
Annex II (Part-145)
(a) A maintenance organisation approved in accordance with Annex II (Part-145), when authorised
to carry out this activity by the competent authority, may (i) prepare the aircraft maintenance
licence on behalf of the competent authority or (ii) make recommendations to the competent
authority regarding the application from an individual for a aircraft maintenance licence so that
the competent authority may prepare and issue such licence.
(b) Maintenance organisations referred to in point (a) shall ensure compliance with points
66.B.100(a) and (b).
(c) In all cases, the aircraft maintenance licence can only be issued to the applicant by the
competent authority.

AMC 66.B.105 Procedure for the issue of an aircraft maintenance

licence via the Part-145 approved maintenance organisation
1. The maintenance organisation approved under Part-145 should include the procedure in the
organisation’s exposition (Chapter 3.21), and this procedure should be audited by the
competent authority at least once in each 12-month period. This procedure should include a
limitation stating that it is only applicable to the case where the competent authority for the
Part-145 approval and for the Part-66 licence is the same.
2. The Part-145 organisation should check that the experience records have been properly
countersigned.
3. The maintenance organisation approved under Part-145 may keep the experience record of
applicants in a different form from that of application EASA Form 19 but such different form or
manner should be acceptable to the competent authority.
66.B.110 Procedure for the change of an aircraft maintenance

licence to include an additional basic category or subcategory
(a) At the completion of the procedures specified in points 66.B.100 or 66.B.105, the competent
authority shall endorse the additional basic category, subcategory or, for category B2L, system
rating(s) on the aircraft maintenance licence by stamp and signature or shall reissue the licence.
(b) The record system of the competent authority shall be changed accordingly.
(c) Upon request by the applicant, the competent authority shall replace a licence in category B2L
with a licence in category B2 endorsed with the same aircraft rating(s) when the holder has
demonstrated both of the following:
(i) by examination the differences between the basic knowledge corresponding to the B2L
licence held and the basic knowledge of the B2 licence, as set out in Appendix I;
(ii) the practical experience required in Appendix IV.
(d) In the case of a holder of an aircraft maintenance licence in subcategory B1.2 endorsed with the
Group 3 rating or in category B3 endorsed with the rating ‘piston engine non-pressurised
aeroplanes of 2 000 kg MTOM and below’, the competent authority shall issue, upon
application, a fully rated licence in subcategories L1 and L2, with the same limitations as the
B1.2/B3 licence held.
AMC 66.B.110 Procedure for the change of an aircraft maintenance

licence to include an additional basic category or subcategory
In the case of computer-generated licences, the licence should be reissued.

When the conditions set in the rule for extending a B2L licence to include the B2 category are met,
the B2L licence should be replaced by a B2 licence.
The B2L licence replaced by a B2 licence should be retained by the competent authority.

66.B.115 Procedure for the change of an aircraft maintenance

licence to include an aircraft rating or to remove limitations
(a) On receipt of a satisfactory EASA Form 19 and any supporting documentation demonstrating
compliance with the requirements of the applicable rating together with the accompanying
aircraft maintenance licence, the competent authority shall either:
1. endorse the applicant's aircraft maintenance licence with the applicable aircraft rating;
or
2. reissue the said licence to include the applicable aircraft rating; or
3. remove the applicable limitations in accordance with point 66.A.50.
The competent authority record system shall be changed accordingly.
(b) In the case where the complete type training is not conducted by maintenance training
organisation appropriately approved in accordance with Annex IV (Part-147), the competent
authority shall be satisfied that all type training requirements are complied with before the type
rating is issued.
(c) In the case where the On the Job Training is not required, the aircraft type rating shall be
endorsed based on a Certificate of Recognition issued by a maintenance training organisation
approved in accordance with Annex IV (part-147).
(d) In the case where the aircraft type training is not covered by a single course, the competent
authority shall be satisfied prior to the type rating endorsement that the content and length of
the courses fully satisfy the scope of the licence category and that the interface areas have been
appropriately addressed.
(e) In the case of differences training, the competent authority shall be satisfied that (i) the
applicant's previous qualification, supplemented by (ii) either a course approved in accordance
with Annex IV (Part-147) or a course directly approved by the competent authority, are
acceptable for type rating endorsement.
(f) The competent authority shall ensure that compliance with the practical elements of the type
training is demonstrated by one of the following:
(i) by the provision of detailed practical training records or a logbook provided by the
organisation which delivered the course directly approved by the competent authority in
accordance with point 66.B.130;
(ii) where available, by a training certificate, covering the practical training element, issued
by a maintenance training organisation appropriately approved in accordance with Annex
IV (Part-147).
(g) Aircraft type endorsement shall use the aircraft type ratings specified by the Agency.

AMC 66.B.115 Procedure for the change of an aircraft maintenance

licence to include an aircraft rating or to remove limitations
(a) Where the type training has not been conducted by a Part-147 organisation, there should be
supporting documents confirming to the competent authority that:
− The type training has been approved by the competent authority in accordance with
66.B.130,
− the applicant has completed the elements of the approved type training; and
− the trainee has been successfully examined/assessed.
(b) Aircraft type training may be subdivided in airframe and/or powerplant and/or
avionics/electrical systems type training courses.
1. Airframe type training course means a type training course including all relevant aircraft
structure and electrical and mechanical systems excluding the powerplant.
2. Powerplant type training course means a type training course on the bare engine,
including the build-up to a quick engine change unit.
3. The interface of the engine/airframe systems should be addressed by either airframe or
powerplant type training course. In some cases, such as for general aviation, it may be
more appropriate to cover the interface during the airframe course due to the large
variety of aircraft that can have the same engine type installed.
4. Avionics/electrical systems type training course means type training on avionics and
electrical systems covered by but not necessarily limited to ATA Chapters 22, 23, 24, 25,
27, 31, 33, 34, 42, 44, 45, 46, 73 and 77 or equivalent.
(c) For the acceptance of the OJT programme described in Section 6 of Appendix III to Part-66, the
licensing competent authority should develop adequate procedures which may be similar to the
procedure described in AMC 66.B.130 for the ‘direct approval of aircraft type training’.
In the case where the licensing competent authority is different from the competent authority
of the maintenance organisation which provides the OJT, the licensing authority may take into
consideration the fact that the maintenance organisation may already have the OJT programme
accepted by their own competent authority (directly approved or through Chapter 3.20 of the
MOE, as described in AMC1 145.A.70(a)).
66.B.120 Procedure for the renewal of an aircraft maintenance

licence validity
(a) The competent authority shall compare the holder's aircraft maintenance licence with the
competent authority records and verify any pending revocation, suspension or change action
pursuant to point 66.B.500. If the documents are identical and no action is pending pursuant to
point 66.B.500, the holder's copy shall be renewed for 5 years and the file endorsed accordingly.
(b) If the competent authority records are different from the aircraft maintenance licence held by
the licence holder:
1. the competent authority shall investigate the reasons for such differences and may
choose not to renew the aircraft maintenance licence.

2. the competent authority shall inform the licence holder and any known maintenance
organisation approved in accordance with Annex I (Part-M) Subpart F, Annex II (Part-145)
or Annex Vd (Part-CAO) that may be directly affected by such fact.
3. the competent authority shall, if necessary, take action in accordance with point 66.B.500
to revoke, suspend or change the licence in question.
AMC 66.B.120 Procedure for the renewal of an aircraft

maintenance licence validity
The competent authority should not carry out any investigation to ensure that the licence holder is in
current maintenance practice as this is not a condition for the renewal of a licence. Ensuring the
continued validity of the certification privileges is a matter for the approved Part-145 / M.A. Subpart F
/ Part-CAO maintenance organisation or the certifying staff in accordance with M.A.801(b)1.
For the purpose of ensuring the continued validity of the certification privileges, the competent
authority may, when periodically reviewing the organisations in accordance with 145.B.305, M.B.604
or CAO.B.055, or during on-the-spot checks, request the licence holder to provide documentary
evidence of compliance with 66.A.20(b) when exercising certification privileges.
66.B.125 Procedure for the conversion of licences including group

ratings
(a) Individual aircraft type ratings already endorsed on the aircraft maintenance licence referred to
in point 4 of Article 5 shall remain on the licence and shall not be converted to new ratings
unless the licence holder fully meets the requirements for endorsement defined in point
66.A.45 of this Annex (Part-66) for the corresponding group/sub-group ratings.
(b) The conversion shall be performed in accordance with the following conversion table:
1. for category B1 or C:
− helicopter piston engine, full group: converted to ‘full subgroup 2c’ plus the aircraft
type ratings for those single piston engine helicopters which are in Group 1;
− helicopter piston engine, manufacturer group: converted to the corresponding
‘manufacturer subgroup 2c’ plus the aircraft type ratings for those single piston
engine helicopters of that manufacturer which are in Group 1;
− helicopter turbine engine, full group: converted to ‘full subgroup 2b’ plus the
aircraft type ratings for those single turbine engine helicopters which are in
Group 1;
− helicopter turbine engine, manufacturer group: converted to the corresponding
‘manufacturer subgroup 2b’ plus the aircraft type ratings for those single turbine
engine helicopters of that manufacturer which are in Group 1;
− aeroplane single piston engine — metal structure, either full group or
manufacturer group: converted to ‘full group 3’. For the B1 licence, the following
limitations shall be included: composite-structure aeroplanes, wooden-structure
aeroplanes, and metal-tubing and fabric aeroplanes;

− aeroplane multiple piston engines — metal structure, either full group or

manufacturer group: converted to ‘full group 3’ plus the aircraft type ratings for
those aeroplanes with multiple piston engines of the corresponding
full/manufacturer group which are in Group 1. For the B1 licence, the following
limitations shall be included: composite-structure aeroplanes, wooden-structure
aeroplanes and metal-tubing and fabric aeroplanes;
− aeroplane single piston engine — wooden structure, either full group or
limitations shall be included: pressurised aeroplanes, metal-structure aeroplanes,
composite-structure aeroplanes and metal-tubing and fabric aeroplanes;
− aeroplane multiple piston engines — wooden structure, either full group or
composite-structure aeroplanes and metal-tubing and fabric aeroplanes;
− aeroplane single piston engine — composite structure, either full group or
wooden-structure aeroplanes and metal-tubing and fabric aeroplanes;
− aeroplane multiple piston engines — composite structure, either full group or
wooden-structure aeroplanes and metal-tubing and fabric aeroplanes;
− aeroplane turbine — single engine, full group: converted to ‘full sub-group 2a’ plus
the aircraft type ratings for those single turboprop aeroplanes which did not
require an aircraft type rating in the previous system and are in Group 1;
− aeroplane turbine — single engine, manufacturer group: converted to the
corresponding ‘manufacturer subgroup 2a’ plus the aircraft type ratings for those
single turboprop aeroplanes of that manufacturer which did not require an aircraft
type rating in the previous system and are in Group 1;
− aeroplane turbine — multiple engines, full group: converted to the aircraft type
ratings for those aeroplanes with multiple turboprop engines which did not require
an aircraft type rating in the previous system.
2. for category B2:
− aeroplane: converted to ‘full sub-group 2a’ and ‘full group 3’, plus the aircraft type
ratings for those aeroplanes which did not require an aircraft type rating in the
previous system and are in group 1,
− helicopter: converted to ‘full sub-groups 2b and 2c’, plus the aircraft type ratings
for those helicopters which did not require an aircraft type rating in the previous
system and are in group 1;
3. for category C:
− aeroplane: converted to ‘full sub-group 2a’ and ‘full group 3’, plus the aircraft type
ratings for those aeroplanes which did not require an aircraft type rating in the
previous system and are in group 1,

− helicopter: converted to ‘full sub-groups 2b and 2c’, plus the aircraft type ratings
for those helicopters which did not require an aircraft type rating in the previous
system and are in group 1.
(c) If the licence was subject to limitations following the conversion process referred to in point
66.A.70, these limitations shall remain on the licence, unless they are removed under the
conditions defined in the relevant conversion report referred to in point 66.B.300.
66.B.130 Procedure for the direct approval of aircraft type training

(a) In the case of type training for aircraft other than airships, the competent authority may
approve aircraft type training not conducted by a maintenance training organisation approved
in accordance with Annex IV (Part-147), pursuant to point 1 of Appendix III to this Annex (part-
66). In such case, the competent authority shall have a procedure to ensure that the aircraft
type training complies with Appendix III to this Annex (Part-66).
(b) In the case of type training for airships in Group 1, the courses shall be directly approved by the
competent authority in all cases. The competent authority shall have a procedure to ensure that
the syllabus of the airship-type training covers all the elements contained in the maintenance
data from the Design Approval Holder (DAH).
AMC 66.B.130 Procedure for the direct approval of aircraft type

training
In the case of type training for aircraft other than airships:

1. The procedure for the direct approval of type training courses by the competent authority
should require that the following aspects are described by the organisation providing the
training:
− The content and the duration of the theoretical and/or practical elements, as applicable,
in accordance with Appendix III to Part-66, including the Training Need Analysis (TNA);
− The teaching methods and instructional equipment;
− The material and documentation provided to the student;
− The qualification of instructors, examiners and/or assessors, as applicable;
− The examination and/or assessment procedure, as applicable. Further guidance about
the assessment and the designated assessors is given in Appendix III to AMC to Part-66.
− The documentation and records to be provided to the student to justify the satisfactory
completion of the training course and related examination/assessment. This should
include not only a certificate of completion but enough documentation and records to
justify that the content and duration approved has been met and that the
examination/assessment has been successfully passed.
2. The above criteria apply to a full course as well as to a partial course such as the practical
element of a type training course and its assessment.
3. The procedure should also indicate how the competent authority is going to audit the proper
performance of the approved course.

4. The direct approval of aircraft type training should be done on a case by case basis and should
not be granted for long term periods, since it is not a privilege of the organisation providing the
training.

SUBPART C — EXAMINATIONS
Regulation (EU) No 1321/2014;
This Subpart provides the procedures to be followed for the examinations conducted by the
competent authority.
66.B.200 Examination by the competent authority

(a) All examination questions shall be kept in a secure manner prior to an examination, to ensure
that candidates will not know which particular questions will form the basis of the examination.
(b) The competent authority shall nominate:
1. persons who control the questions to be used for each examination;
2. examiners who shall be present during all examinations to ensure the integrity of the
examination.
(c) Basic examinations shall follow the standard specified in Appendices I and II or in Appendices
VII and VIII to this Annex (Part-66), as applicable.
(d) Type training examinations and type examinations shall follow the standard specified in
Appendix III to this Annex (Part-66).
(e) New essay questions shall be raised at least every 6 months and questions already used
withdrawn or rested from use. A record of the questions used shall be retained in the records
for reference.
(f) All examination papers shall be handed out at the start of the examination to the candidate and
handed back to the examiner at the end of the allotted examination time period. No
examination paper may be removed from the examination room during the allotted
examination time period.
(g) Apart from specific documentation needed for type examinations, only the examination paper
may be available to the candidate during the examination.
(h) Examination candidates shall be separated from each other so that they cannot read each
other's examination papers. They may not speak to any person other than the examiner.
(i) Candidates who are proven to be cheating shall be banned from taking any further examination
within 12 months of the date of the examination in which they were found cheating.
GM 66.B.200 Examination by the competent authority

1. Questions may be prepared in the national language but the use of aviation English is
recommended wherever possible.
2. The primary purpose of essay questions is to determine that the candidate can express
themselves in a clear and concise manner and can prepare a concise technical report for the
maintenance record, which is why only a few essay questions are required.
3. Oral type questions may not be used as the primary means of examination because of the
difficulty in establishing consistency of standards between examiners or day-to-day.

6. Essay question generation

(a) The purpose of the essay is to allow the competent authority to determine if candidates
can express themselves in a clear and concise manner in the form of a written response,
in a technical report format using the technical language of the aviation industry. The
essay examination also allows to assess, in part, the technical knowledge retained by the
individual and with a practical application relevant to a maintenance scenario.
(b) Questions should be written so as to be broad enough to be answered by candidates for
any A or B licence category or subcategories and comply with the following general
guidelines:
− the question topic selected should be generic, applicable to mechanical as well as
avionic licence categories and have a common technical difficulty level as indicated
in Part-66 Appendix I or Appendix VII;
− cover technology applicable to most areas of aircraft maintenance;
− reflects common working practices;
− it is not type- or manufacturer-specific and avoids subjects which are rarely found
in practice;
− when drafting a question, there is need to ensure consideration is given to the
limited practical experience that most candidates will have.
(c) To make the questions and the marking procedures are as consistent as possible, each
question and model answer, with the required key areas required (see below), should be
reviewed independently by at least 2 technical staff members.
(d) When raising questions the following should be considered:
− Each essay question will have a time allowance of 20 minutes.
− A complete A4 side is provided for each question and answer, if required the
answer can be extended onto the reverse side of the page.
− The question should be such that the answer expected will be at the level shown
for that subject in the module syllabus.
− The question should not be ambiguous but should seek a broad reply rather than
be limited in scope for answer.
− The question should lend itself to be written in a technical report style, in a logical
sequence (beginning, middle and end), containing the applicable and relevant
technical words needed in the answer.
− Do not ask for drawings/sketches to support the essay.
− The question should be relevant to the category and level of difficulty listed in the
syllabus, e.g. a description of a typical general aviation system may not be
acceptable for a typical commercial aeroplane.
− Subject to obvious constraints in relation to the topic being addressed the question
should have a strong bias towards the practical maintenance of a
system/component and the answer should show an understanding of normal and
deteriorated conditions of an aircraft and its systems.

Variations on alternative possible answers which have not been thought of, may
have to be taken into account to aid the examiner when marking. If considered
relevant, the model answer should be amended to include these new points.
(e) Because of the difficulty in marking an essay answer using key points only, there is a need
for the way in which the report was written to be assessed and taken into consideration.
(f) The total points for each question will add up to 100 and will need to reflect both the
combination of the technical (key point) element and the report style element.
(g) Each key point will be graded upon its importance and have point weighting allocated to
it. The total weight will represent 60% of the mark.
(h) Key points are the ‘important elements’ that may be knowledge or experience-based and
will include other maintenance orientated factors such as relevant safety precautions or
legislative practices if applicable. Excessive reference to the need for MM referral or
safety checks may be considered wasteful.
(i) The question answer will be analysed for the clarity and manner in which the essay report
is presented and have a weighting allocated to it which will represent 40% of the mark.
(j) The answer should show the candidate's ability to express himself in technical language.
This includes readability of the language, basic grammar and use of terminology.
(k) The report starts in the beginning and has logical process to reach a conclusion.
(l) Supporting diagrams should not be encouraged but if used should supplement the
answer and not replace the need for a broad text answer.
(m) The report should not be indexed, itemised or listed.
(n) Within reason the candidate should not be penalised for incorrect spelling.
(o) A zero mark should only be given in exceptional circumstances. Even if the student
misunderstands the question and gives an answer to a different question, a sympathetic
mark even if only for the report style should be given, this could up to the maximum
percentage allowed.
(p) The two allocated marks should be added together and written into the answer paper.
(q) If a question answer resulting in a borderline failure is principally due to ‘written report
errors,’ the paper should be discussed and the mark agreed if possible with another
examiner.

SUBPART D — CONVERSION OF CERTIFYING STAFF QUALIFICATIONS

This Subpart provides the procedures for the conversion of certifying staff qualifications referred to in
point 66.A.70 to aircraft maintenance licences.
66.B.300 General
(a) The competent authority may only convert qualifications

(i) obtained in the Member State for which it is competent, without prejudice to bilateral
agreements and
(ii) valid prior to the entry into force of the applicable requirements of this Annex (Part-66).
(b) The competent authority may only perform the conversion in accordance with a conversion
report established pursuant to points 66.B.305 or 66.B.310, as applicable.
(c) Conversion reports shall be either
(i) developed by the competent authority or
(ii) approved by the competent authority to ensure compliance with this Annex (Part-66).
(d) Conversion reports together with any change of these shall be kept on record by the competent
authority in accordance with point 66.B.20.
GM 66.B.300 General
As described in point 66.B.300, certifying staff qualifications eligible for conversion are those valid
‘prior to the entry into force of the applicable requirements of this Annex (Part-66)’, which means
those qualifications valid before the following dates:
− 28 September 2005 for aircraft above 5 700 kg MTOM (ref. (EC) No 2042/2003, Article 7, point
3(e));
− 28 September 2006 for aircraft of 5 700 kg MTOM and below (ref. (EC) No 2042/2003, Article 7,
point 3(f)).
Nevertheless, since the B3 licence did not exist at those dates, certifying staff qualifications eligible
for conversion to a B3 licence are those valid before 28 September 2012, which is the date where the
authority has been obliged to start issuing such licences in accordance with (EC) No 2042/2003, Article
7, point 3(h), item (i).
66.B.305 Conversion report for national qualifications

(a) The conversion report for national certifying staff qualifications shall describe the scope of each
type of qualification, including the associated national licence, if any, the associated privileges
and include a copy of the relevant national regulations defining these.

3. the conditions to remove the limitations, specifying the module/subjects on which

examination is needed to remove the limitations and obtain a full aircraft maintenance
licence, or to include an additional (sub-) category. This shall include the modules defined
in Appendix III to this Annex (Part-66) not covered by the national qualification.
AMC 66.B.310(a) Conversion report for approved maintenance

organisations' authorisations
1. Conversion reports prepared on the basis of point 66.A.70(c) should include a comparison
between the qualification required for each type of organisation authorisation and the scope of
the Part-66 licence qualification, which should be performed on the basis of a detailed analysis
of the organisation and Part-66 basic qualification standards. The report should identify where
a difference between the two standards exists and where such a difference would lead to a
limitation on the Part-66 licence.
2. Conversion reports prepared on the basis of point 66.A.70(d), which are limited to other-than-
complex motor-powered aircraft that are not used by air carriers licensed in accordance with
Regulation (EC) No 1008/2008 should include the privileges associated to the organisation
authorisation. The reports should identify which limitations are needed to the Part-66 licence
in order to maintain these privileges.
GM 66.B.310(b)3 Conversion report for approved maintenance

organisations authorisations
As conversions performed on the basis of 66.A.70(d) are aimed to maintain the privileges of the pre-
existing organisation authorisations, the limitations introduced on the Part-66 licence are not linked
to possible differences between the qualification required for the organisation authorisation and the
Part-66 licence qualification. This conversion does not include such comparison.
This means that, in order to remove such limitations, full compliance with the conditions of Part-66
needs to be demonstrated.

SUBPART E — EXAMINATION CREDITS

This Subpart provides the procedures for granting examination credits referred to in point 66.A.25(e).
66.B.400 General
(a) The competent authority may only grant credit on the basis of a credit report prepared in
accordance with point 66.B.405.
(b) The credit report shall be either
(i) developed by the competent authority or
(ii) approved by the competent authority to ensure compliance with this Annex (Part-66).
(c) Credit reports together with any change of these shall be dated and kept on record by the
competent authority in accordance with point 66.B.20.
66.B.405 Examination credit report

(a) The credit report shall include a comparison between the following:
(i) the modules, submodules, subjects and knowledge levels contained in Appendices I or
VII to this Annex (Part-66), as applicable;
(ii) the syllabus of the technical qualification concerned, relevant to the particular category
being sought.
This comparison shall state whether compliance has been demonstrated and contain the
justifications for each statement.
(b) Credits for examinations, other than basic knowledge examinations carried out in maintenance
training organisations approved in accordance with Annex IV (Part-147), can only be granted by
the competent authority of the Member State in which the qualification has been obtained,
unless a formal agreement exists with such competent authority advising otherwise.
(c) No credit can be granted unless there is a statement of compliance for each module and
submodule, indicating where the equivalent standard can be found in the technical
qualification.
(d) The competent authority shall check on a regular basis whether the following have changed:
(i) the national qualification standard;
(ii) Appendices I or VII to this Annex (Part-66), as applicable.
The competent authority shall also assess if changes to the credit report are consequently
required. Such changes shall be documented, dated and recorded.

66.B.410 Examination credit validity

(a) The competent authority shall notify to the applicant in writing any credits granted together
with the reference to the credit report used.
(b) Credits shall expire 10 years after they are granted.
(c) Upon expiration of the credits, the applicant may apply for new credits. The competent
authority shall extend the validity of the credits for an additional period of 10 years without
further consideration if the basic knowledge requirements defined in Appendices I or VII to this
Annex (Part-66), as applicable, have not been changed.
GM 66.B.410 Examination credit validity

In the case of credits expired in accordance with 66.A.25(d) and 66.B.410(b), the new application for
credits will lead to a reassessment in accordance with 66.B.405 and 66.B.410 only in those cases where
the requirements contained in Appendix I to Part-66 have changed. This may lead to a requirement
for further examinations on particular modules/sub-modules/subjects.

SUBPART F — CONTINUING OVERSIGHT

This Subpart describes the procedures for the continuing oversight of the aircraft maintenance licence
and in particular for the revocation, suspension or limitation of the aircraft maintenance licence.
66.B.500 Revocation, suspension or limitation of the aircraft

maintenance licence
The competent authority shall suspend, limit or revoke the aircraft maintenance licence where it has
identified a safety issue or if it has clear evidence that the person has carried out or been involved in
one or more of the following activities:
1. obtaining the aircraft maintenance licence and/or the certification privileges by falsification of
documentary evidence;
2. failing to carry out requested maintenance combined with failure to report such fact to the
organisation or person who requested the maintenance;
3. failing to carry out required maintenance resulting from own inspection combined with failure
to report such fact to the organisation or person for whom the maintenance was intended to
be carried out;
4. negligent maintenance;
5. falsification of the maintenance record;
6. issuing a certificate of release to service knowing that the maintenance specified on the
certificate of release to service has not been carried out or without verifying that such
maintenance has been carried out;
7. carrying out maintenance or issuing a certificate of release to service when adversely affected
by alcohol or drugs;
8. issuing certificate of release to service while not in compliance with this Regulation.

APPENDICES TO ANNEX III (Part-66)
APPENDICES TO ANNEX III (PART-66)
Appendix I — Basic Knowledge Requirements (except for category L

licence)
1. Knowledge levels for Category A, B1, B2, B2L, B3 and C aircraft maintenance licences
Basic knowledge for categories A, B1, B2, B2L and B3 is indicated by knowledge levels (1, 2 or 3) of
each applicable subject. Category C applicants shall meet either the category B1 or the category B2
basic knowledge levels.
The knowledge level indicators are defined on 3 levels as follows:
− LEVEL 1: A familiarisation with the principal elements of the subject.
Objectives:
(a) The applicant should be familiar with the basic elements of the subject.
(b) The applicant should be able to give a simple description of the whole subject, using
common words and examples.
(c) The applicant should be able to use typical terms.
− LEVEL 2: A general knowledge of the theoretical and practical aspects of the subject and an
ability to apply that knowledge.
Objectives:
(a) The applicant should be able to understand the theoretical fundamentals of the subject.
(b) The applicant should be able to give a general description of the subject using, as
appropriate, typical examples.
(c) The applicant should be able to use mathematical formulae in conjunction with physical
laws describing the subject.
(d) The applicant should be able to read and understand sketches, drawings and schematics
describing the subject.
(e) The applicant should be able to apply his knowledge in a practical manner using detailed
procedures.
− LEVEL 3: A detailed knowledge of the theoretical and practical aspects of the subject and a
capacity to combine and apply the separate elements of knowledge in a logical and
comprehensive manner.
Objectives:
(a) The applicant should know the theory of the subject and interrelationships with other
subjects.
(b) The applicant should be able to give a detailed description of the subject using theoretical
fundamentals and specific examples.
(c) The applicant should understand and be able to use mathematical formulae related to
the subject.

(d) The applicant should be able to read, understand and prepare sketches, simple drawings
and schematics describing the subject.
(e) The applicant should be able to apply his knowledge in a practical manner using
manufacturer's instructions.
(f) The applicant should be able to interpret results from various sources and measurements
and apply corrective action where appropriate.
2. Modularisation
Qualification on basic subjects for each aircraft maintenance licence category or subcategory shall be
in accordance with the following matrix, where applicable subjects are indicated by an ‘X’:
For categories A, B1 and B3:
A or B1 aeroplane with: A or B1 helicopter with: B3
Piston engine
Subject non-pressurised
module Turbine Turbine
Piston engine(s) Piston engine(s) aeroplanes
engine(s) engine(s)
2 000 kg MTOM
and below
1 X X X X X
2 X X X X X
3 X X X X X
4 X X X X X
5 X X X X X
6 X X X X X
7A X X X X
7B X
8 X X X X X
9A X X X X
9B X
10 X X X X X
11A X
11B X
11C X
12 X X
13
14
15 X X
16 X X X
17A X X
17B X

For categories B2 and B2L:

Subject module/submodules B2 B2L
1 X X
2 X X
3 X X
4 X X
5 X X
6 X X
7A X X
7B
8 X X
9A X X
9B
10 X X
11A
11B
11C
12
13.1 and 13.2 X X
13.3(a) X X (for system rating 'Autoflight')
13.3(b) X
13.4(a) X X (for system rating 'Com/Nav')
13.4(b) X X (for system rating 'Surveillance')
13.4(c) X
13.5 X X
13.6 X
13.7 X X (for system rating 'Autoflight')
13.8 X X (for system rating 'Instruments')
13.9 X X
13.10 X
13.11 to 13.18 X X (for system rating 'Airframe systems')
13.19 to 13.22 X
14 X X (for system rating 'instruments' and
'Airframe systems')
15
16
17A
17B

MODULE 1. MATHEMATICS
LEVEL
MODULE 1. MATHEMATICS A B1 B2 B3
B2L
1.1 Arithmetic 1 2 2 2
Arithmetical terms and signs, methods of multiplication and division,
fractions and decimals, factors and multiples, weights, measures and
conversion factors, ratio and proportion, averages and percentages,
areas and volumes, squares, cubes, square and cube roots.
1.2 Algebra
(a) Evaluating simple algebraic expressions, addition, subtraction, 1 2 2 2
multiplication and division, use of brackets, simple algebraic
fractions;
(b) Linear equations and their solutions; — 1 1 1
Indices and powers, negative and fractional indices;
Binary and other applicable numbering systems;
Simultaneous equations and second degree equations with
one unknown;
Logarithms.
1.3 Geometry
(a) Simple geometrical constructions; — 1 1 1
(b) Graphical representation; nature and uses of graphs, graphs of 2 2 2 2
equations/functions;
(c) Simple trigonometry; trigonometrical relationships, use of — 2 2 2
tables and rectangular and polar coordinates.
MODULE 2. PHYSICS
LEVEL
MODULE 2. PHYSICS A B1 B2 B3
B2L
2.1 Matter 1 1 1 1
Nature of matter: the chemical elements, structure of atoms,
molecules;
Chemical compounds;
States: solid, liquid and gaseous;
Changes between states.
2.2 Mechanics
2.2.1 Statics 1 2 1 1
Forces, moments and couples, representation as vectors;
Centre of gravity;
Elements of theory of stress, strain and elasticity: tension,
compression, shear and torsion;
Nature and properties of solid, fluid and gas;
Pressure and buoyancy in liquids (barometers).

LEVEL
MODULE 2. PHYSICS A B1 B2 B3
B2L
2.2.2 Kinetics 1 2 1 1
Linear movement: uniform motion in a straight line, motion
under constant acceleration (motion under gravity);
Rotational movement: uniform circular motion
(centrifugal/centripetal forces);
Periodic motion: pendular movement;
Simple theory of vibration, harmonics and resonance;
Velocity ratio, mechanical advantage and efficiency.
2.2.3 Dynamics
(a) Mass; 1 2 1 1
Force, inertia, work, power, energy (potential, kinetic and
total energy), heat, efficiency;
(b) Momentum, conservation of momentum; 1 2 2 1
Impulse;
Gyroscopic principles;
Friction: nature and effects, coefficient of friction (rolling
resistance).
2.2.4 Fluid dynamics
(a) Specific gravity and density; 2 2 2 2
(b) Viscosity, fluid resistance, effects of streamlining; 1 2 1 1
Effects of compressibility on fluids;
Static, dynamic and total pressure: Bernoulli's Theorem,
venturi.
2.3 Thermodynamics
(a) Temperature: thermometers and temperature scales: Celsius, 2 2 2 2
Fahrenheit and Kelvin; Heat definition;
(b) Heat capacity, specific heat; — 2 2 1
Heat transfer: convection, radiation and conduction;
Volumetric expansion;
First and second law of thermodynamics;
Gases: ideal gases laws; specific heat at constant volume and
constant pressure, work done by expanding gas;
Isothermal, adiabatic expansion and compression, engine
cycles, constant volume and constant pressure, refrigerators
and heat pumps;
Latent heats of fusion and evaporation, thermal energy, heat
of combustion.
2.4 Optics (Light) — 2 2 —
Nature of light; speed of light;
Laws of reflection and refraction: reflection at plane surfaces,
reflection by spherical mirrors, refraction, lenses;
Fibre optics.
2.5 Wave Motion and Sound — 2 2 —
Wave motion: mechanical waves, sinusoidal wave motion,
interference phenomena, standing waves;
Sound: speed of sound, production of sound, intensity, pitch and
quality, Doppler effect.

MODULE 3. ELECTRICAL FUNDAMENTALS

LEVEL
MODULE 3. ELECTRICAL FUNDAMENTALS A B1 B2 B3
B2L
3.1 Electron Theory 1 1 1 1
Structure and distribution of electrical charges within: atoms,
molecules, ions, compounds;
Molecular structure of conductors, semiconductors and insulators.
3.2 Static Electricity and Conduction 1 2 2 1
Static electricity and distribution of electrostatic charges;
Electrostatic laws of attraction and repulsion;
Units of charge, Coulomb's Law;
Conduction of electricity in solids, liquids, gases and a vacuum.
3.3 Electrical Terminology 1 2 2 1
The following terms, their units and factors affecting them: potential
difference, electromotive force, voltage, current, resistance,
conductance, charge, conventional current flow, electron flow.
3.4 Generation of Electricity 1 1 1 1
Production of electricity by the following methods: light, heat,
friction, pressure, chemical action, magnetism and motion.
3.5 DC Sources of Electricity 1 2 2 2
Construction and basic chemical action of: primary cells, secondary
cells, lead acid cells, nickel cadmium cells, other alkaline cells;
Cells connected in series and parallel;
Internal resistance and its effect on a battery;
Construction, materials and operation of thermocouples;
Operation of photo-cells.
3.6 DC Circuits — 2 2 1
Ohms Law, Kirchoff's Voltage and Current Laws;
Calculations using the above laws to find resistance, voltage and
current;
Significance of the internal resistance of a supply.
3.7 Resistance/Resistor
(a) Resistance and affecting factors; — 2 2 1
Specific resistance;
Resistor colour code, values and tolerances, preferred values,
wattage ratings;
Resistors in series and parallel;
Calculation of total resistance using series, parallel and series
parallel combinations;
Operation and use of potentiometers and rheostats;
Operation of Wheatstone Bridge;
(b) Positive and negative temperature coefficient conductance; — 1 1 —
Fixed resistors, stability, tolerance and limitations, methods of
construction;
Variable resistors, thermistors, voltage dependent resistors;
Construction of potentiometers and rheostats;
Construction of Wheatstone Bridge.

LEVEL
B2L
3.8 Power — 2 2 1
Power, work and energy (kinetic and potential);
Dissipation of power by a resistor;
Power formula;
Calculations involving power, work and energy.
3.9 Capacitance/Capacitor — 2 2 1
Operation and function of a capacitor;
Factors affecting capacitance area of plates, distance between
plates, number of plates, dielectric and dielectric constant, working
voltage, voltage rating;
Capacitor types, construction and function;
Capacitor colour coding;
Calculations of capacitance and voltage in series and parallel circuits;
Exponential charge and discharge of a capacitor, time constants;
Testing of capacitors.
3.10 Magnetism
(a) Theory of magnetism; — 2 2 1
Properties of a magnet;
Action of a magnet suspended in the Earth's magnetic field;
Magnetisation and demagnetisation;
Magnetic shielding;
Various types of magnetic material;
Electromagnets construction and principles of operation;
Hand clasp rules to determine: magnetic field around current
carrying conductor;
(b) Magnetomotive force, field strength, magnetic flux density, — 2 2 1
permeability, hysteresis loop, retentivity, coercive force
reluctance, saturation point, eddy currents;
Precautions for care and storage of magnets.
3.11 Inductance/Inductor — 2 2 1
Faraday's Law;
Action of inducing a voltage in a conductor moving in a magnetic
field;
Induction principles;
Effects of the following on the magnitude of an induced voltage:
magnetic field strength, rate of change of flux, number of conductor
turns;
Mutual induction;
The effect the rate of change of primary current and mutual
inductance has on induced voltage;
Factors affecting mutual inductance: number of turns in coil,
physical size of coil, permeability of coil, position of coils with
respect to each other;
Lenz's Law and polarity determining rules;
Back emf, self induction;
Saturation point;
Principle uses of inductors.

LEVEL
B2L
3.12 DC Motor/Generator Theory — 2 2 1
Basic motor and generator theory;
Construction and purpose of components in DC generator;
Operation of, and factors affecting output and direction of current
flow in DC generators;
Operation of, and factors affecting output power, torque, speed and
direction of rotation of DC motors;
Series wound, shunt wound and compound motors;
Starter Generator construction.
3.13 AC Theory 1 2 2 1
Sinusoidal waveform: phase, period, frequency, cycle;
Instantaneous, average, root mean square, peak, peak to peak
current values and calculations of these values, in relation to
voltage, current and power;
Triangular/Square waves;
Single/3 phase principles.
3.14 Resistive (R), Capacitive (C) and Inductive (L) Circuits — 2 2 1
Phase relationship of voltage and current in L, C and R circuits,
parallel, series and series parallel;
Power dissipation in L, C and R circuits;
Impedance, phase angle, power factor and current calculations;
True power, apparent power and reactive power calculations.
3.15 Transformers — 2 2 1
Transformer construction principles and operation;
Transformer losses and methods for overcoming them;
Transformer action under load and no-load conditions;
Power transfer, efficiency, polarity markings;
Calculation of line and phase voltages and currents;
Calculation of power in a three phase system;
Primary and Secondary current, voltage, turns ratio, power,
efficiency;
Auto transformers.
3.16 Filters — 1 1 —
Operation, application and uses of the following filters: low pass,
high pass, band pass, band stop.
3.17 AC Generators — 2 2 1
Rotation of loop in a magnetic field and waveform produced;
Operation and construction of revolving armature and revolving
field type AC generators;
Single phase, two phase and three phase alternators;
Three phase star and delta connections advantages and uses;
Permanent Magnet Generators.
3.18 AC Motors — 2 2 1
Construction, principles of operation and characteristics of: AC
synchronous and induction motors both single and polyphase;
Methods of speed control and direction of rotation;
Methods of producing a rotating field: capacitor, inductor, shaded or
split pole.

MODULE 4. ELECTRONIC FUNDAMENTALS

LEVEL
MODULE 4. ELECTRONIC FUNDAMENTALS A B1 B2 B3
B2L
4.1 Semiconductors
4.1.1 Diodes
(a) Diode symbols; — 2 2 1
Diode characteristics and properties;
Diodes in series and parallel;
Main characteristics and use of silicon controlled rectifiers
(thyristors), light emitting diode, photo conductive diode,
varistor, rectifier diodes;
Functional testing of diodes.
(b) Materials, electron configuration, electrical properties; — — 2 —
P and N type materials: effects of impurities on conduction,
majority and minority characters;
PN junction in a semiconductor, development of a potential
across a PN junction in unbiased, forward biased and reverse
biased conditions;
Diode parameters: peak inverse voltage, maximum forward
current, temperature, frequency, leakage current, power
dissipation;
Operation and function of diodes in the following circuits:
clippers, clampers, full and half wave rectifiers, bridge
rectifiers, voltage doublers and triplers;
Detailed operation and characteristics of the following
devices: silicon controlled rectifier (thyristor), light emitting
diode, Schottky diode, photo conductive diode, varactor
diode, varistor, rectifier diodes, Zener diode.
4.1.2 Transistors
(a) Transistor symbols; — 1 2 1
Component description and orientation;
Transistor characteristics and properties.
(b) Construction and operation of PNP and NPN transistors; — — 2 —
Base, collector and emitter configurations;
Testing of transistors;
Basic appreciation of other transistor types and their uses;
Application of transistors: classes of amplifier (A, B, C);
Simple circuits including: bias, decoupling, feedback and
stabilisation;
Multistage circuit principles: cascades, push-pull, oscillators,
multivibrators, flip-flop circuits.
4.1.3 Integrated Circuits
(a) Description and operation of logic circuits and linear — 1 — 1
circuits/operational amplifiers;
(b) Description and operation of logic circuits and linear circuits; — — 2 —
Introduction to operation and function of an operational
amplifier used as: integrator, differentiator, voltage follower,
comparator;
Operation and amplifier stages connecting methods: resistive
capacitive, inductive (transformer), inductive resistive (IR),
direct;

LEVEL
MODULE 4. ELECTRONIC FUNDAMENTALS A B1 B2 B3
B2L
Advantages and disadvantages of positive and negative
feedback.
4.2 Printed Circuit Boards — 1 2 —
Description and use of printed circuit boards.
4.3 Servomechanisms
(a) Understanding of the following terms: Open and closed loop — 1 — —
systems, feedback, follow up, analogue transducers;
Principles of operation and use of the following synchro
system components/features: resolvers, differential, control
and torque, transformers, inductance and capacitance
transmitters;
(b) Understanding of the following terms: Open and closed loop, — — 2 —
follow up, servomechanism, analogue, transducer, null,
damping, feedback, deadband;
Construction operation and use of the following synchro
system components: resolvers, differential, control and
torque, E and I transformers, inductance transmitters,
capacitance transmitters, synchronous transmitters;
Servomechanism defects, reversal of synchro leads, hunting.
MODULE 5. DIGITAL TECHNIQUES/ELECTRONIC INSTRUMENT SYSTEMS

LEVEL
MODULE 5. DIGITAL TECHNIQUES/ELECTRONIC INSTRUMENT
SYSTEMS B1.1 B1.2 B2
A B3
B1.3 B1.4 B2L
5.1 Electronic Instrument Systems 1 2 2 3 1
Typical systems arrangements and cockpit layout of
electronic instrument systems.
5.2 Numbering Systems — 1 — 2 —
Numbering systems: binary, octal and hexadecimal;
Demonstration of conversions between the decimal and
binary, octal and hexadecimal systems and vice versa.
5.3 Data Conversion — 1 — 2 —
Analogue Data, Digital Data;
Operation and application of analogue to digital, and digital
to analogue converters, inputs and outputs, limitations of
various types.
5.4 Data Buses — 2 — 2 —
Operation of data buses in aircraft systems, including
knowledge of ARINC and other specifications.
Aircraft Network/Ethernet.
5.5 Logic Circuits
(a) Identification of common logic gate symbols, tables — 2 — 2 —
and equivalent circuits;
Applications used for aircraft systems, schematic
diagrams.
(b) Interpretation of logic diagrams. — — — 2 —

LEVEL
A B3
B1.3 B1.4 B2L
5.6 Basic Computer Structure
(a) Computer terminology (including bit, byte, software, 1 2 — — —
hardware, CPU, IC, and various memory devices such
as RAM, ROM, PROM);
Computer technology (as applied in aircraft systems).
(b) Computer related terminology; — — — 2 —
Operation, layout and interface of the major
components in a micro computer including their
associated bus systems;
Information contained in single and multiaddress
instruction words;
Memory associated terms;
Operation of typical memory devices;
Operation, advantages and disadvantages of the
various data storage systems.
5.7 Microprocessors — — — 2 —
Functions performed and overall operation of a
microprocessor;
Basic operation of each of the following microprocessor
elements: control and processing unit, clock, register,
arithmetic logic unit.
5.8 Integrated Circuits — — — 2 —
Operation and use of encoders and decoders;
Function of encoder types;
Uses of medium, large and very large scale integration.
5.9 Multiplexing — — — 2 —
Operation, application and identification in logic diagrams
of multiplexers and demultiplexers.
5.10 Fibre Optics — 1 1 2 —
Advantages and disadvantages of fibre optic data
transmission over electrical wire propagation;
Fibre optic data bus;
Fibre optic related terms;
Terminations;
Couplers, control terminals, remote terminals;
Application of fibre optics in aircraft systems.
5.11 Electronic Displays — 2 1 2 1
Principles of operation of common types of displays used in
modern aircraft, including Cathode Ray Tubes, Light
Emitting Diodes and Liquid Crystal Display.
5.12 Electrostatic Sensitive Devices 1 2 2 2 1
Special handling of components sensitive to electrostatic
discharges;
Awareness of risks and possible damage, component and
personnel anti-static protection devices.

LEVEL
A B3
B1.3 B1.4 B2L
5.13 Software Management Control — 2 1 2 1
Awareness of restrictions, airworthiness requirements and
possible catastrophic effects of unapproved changes to
software programmes.
5.14 Electromagnetic Environment — 2 2 2 1
Influence of the following phenomena on maintenance
practices for electronic system:
EMC-Electromagnetic Compatibility
EMI-Electromagnetic Interference
HIRF-High Intensity Radiated Field
Lightning/lightning protection.
5.15 Typical Electronic/Digital Aircraft Systems — 2 2 2 1
General arrangement of typical electronic/digital aircraft
systems and associated BITE (Built In Test Equipment) such
as:
(a) For B1 and B2 only:
ACARS-ARINC Communication and Addressing and
Reporting System
EICAS-Engine Indication and Crew Alerting System
FBW-Fly-by-Wire
FMS-Flight Management System
IRS-Inertial Reference System;
(b) For B1, B2 and B3:
ECAM-Electronic Centralised Aircraft Monitoring
EFIS-Electronic Flight Instrument System
GPS-Global Positioning System
TCAS-Traffic Alert Collision Avoidance System
Integrated Modular Avionics
Cabin Systems
Information Systems.
MODULE 6. MATERIALS AND HARDWARE

LEVEL
MODULE 6. MATERIALS AND HARDWARE A B1 B2 B3
B2L
6.1 Aircraft Materials — Ferrous
(a) Characteristics, properties and identification of common alloy 1 2 1 2
steels used in aircraft;
Heat treatment and application of alloy steels.
(b) Testing of ferrous materials for hardness, tensile strength, — 1 1 1
fatigue strength and impact resistance.
6.2 Aircraft Materials — Non-Ferrous
(a) Characteristics, properties and identification of common non- 1 2 1 2
ferrous materials used in aircraft;
Heat treatment and application of non-ferrous materials;
(b) Testing of non-ferrous material for hardness, tensile strength, — 1 1 1
fatigue strength and impact resistance.

LEVEL
B2L
6.3 Aircraft Materials — Composite and Non-Metallic
6.3.1 Composite and non-metallic other than wood and fabric
(a) Characteristics, properties and identification of common 1 2 2 2
composite and non-metallic materials, other than wood,
used in aircraft;
Sealant and bonding agents;
(b) The detection of defects/deterioration in composite and 1 2 — 2
non-metallic material;
Repair of composite and non-metallic material.
6.3.2 Wooden structures 1 2 — 2
Construction methods of wooden airframe structures;
Characteristics, properties and types of wood and glue used in
aeroplanes;
Preservation and maintenance of wooden structure;
Types of defects in wood material and wooden structures;
The detection of defects in wooden structure;
Repair of wooden structure.
6.3.3 Fabric covering 1 2 — 2
Characteristics, properties and types of fabrics used in
aeroplanes;
Inspections methods for fabric;
Types of defects in fabric;
Repair of fabric covering.
6.4 Corrosion
(a) Chemical fundamentals; 1 1 1 1
Formation by, galvanic action process, microbiological, stress;
(b) Types of corrosion and their identification; 2 3 2 2
Causes of corrosion;
Material types, susceptibility to corrosion.
6.5 Fasteners
6.5.1 Screw threads 2 2 2 2
Screw nomenclature;
Thread forms, dimensions and tolerances for standard threads
used in aircraft;
Measuring screw threads.
6.5.2 Bolts, studs and screws 2 2 2 2
Bolt types: specification, identification and marking of aircraft
bolts, international standards;
Nuts: self locking, anchor, standard types;
Machine screws: aircraft specifications;
Studs: types and uses, insertion and removal;
Self tapping screws, dowels.
6.5.3 Locking devices 2 2 2 2
Tab and spring washers, locking plates, split pins, pal-nuts, wire
locking, quick release fasteners, keys, circlips, cotter pins.
6.5.4 Aircraft rivets 1 2 1 2
Types of solid and blind rivets: specifications and identification,
heat treatment.
6.6 Pipes and Unions

LEVEL
B2L
(a) Identification of, and types of rigid and flexible pipes and their 2 2 2 2
connectors used in aircraft;
(b) Standard unions for aircraft hydraulic, fuel, oil, pneumatic and 2 2 1 2
air system pipes.
6.7 Springs — 2 1 1
Types of springs, materials, characteristics and applications.
6.8 Bearings 1 2 2 1
Purpose of bearings, loads, material, construction;
Types of bearings and their application.
6.9 Transmissions 1 2 2 1
Gear types and their application;
Gear ratios, reduction and multiplication gear systems, driven and
driving gears, idler gears, mesh patterns;
Belts and pulleys, chains and sprockets.
6.10 Control Cables 1 2 1 2
Types of cables;
End fittings, turnbuckles and compensation devices;
Pulleys and cable system components;
Bowden cables;
Aircraft flexible control systems.
6.11 Electrical Cables and Connectors 1 2 2 2
Cable types, construction and characteristics;
High tension and co-axial cables;
Crimping;
Connector types, pins, plugs, sockets, insulators, current and voltage
rating, coupling, identification codes.
MODULE 7A. MAINTENANCE PRACTICES

Note: This module does not apply to category B3. Relevant subject matters for category B3 are defined
in module 7B.
LEVEL
MODULE 7A. MAINTENANCE PRACTICES A B1 B2
B2L
7.1 Safety Precautions-Aircraft and Workshop 3 3 3
Aspects of safe working practices including precautions to take when
working with electricity, gases especially oxygen, oils and chemicals.
Also, instruction in the remedial action to be taken in the event of a fire
or another accident with one or more of these hazards including
knowledge on extinguishing agents.
7.2 Workshop Practices 3 3 3
Care of tools, control of tools, use of workshop materials;
Dimensions, allowances and tolerances, standards of workmanship;
Calibration of tools and equipment, calibration standards.

LEVEL
B2L
7.3 Tools 3 3 3
Common hand tool types;
Common power tool types;
Operation and use of precision measuring tools;
Lubrication equipment and methods.
Operation, function and use of electrical general test equipment.
7.4 Avionic General Test Equipment — 2 3
Operation, function and use of avionic general test equipment.
7.5 Engineering Drawings, Diagrams and Standards 1 2 2
Drawing types and diagrams, their symbols, dimensions, tolerances and
projections;
Identifying title block information;
Microfilm, microfiche and computerised presentations;
Specification 100 of the Air Transport Association (ATA) of America;
Aeronautical and other applicable standards including ISO, AN, MS, NAS
and MIL;
Wiring diagrams and schematic diagrams.
7.6 Fits and Clearances 1 2 1
Drill sizes for bolt holes, classes of fits;
Common system of fits and clearances;
Schedule of fits and clearances for aircraft and engines;
Limits for bow, twist and wear;
Standard methods for checking shafts, bearings and other parts.
7.7 Electrical Wiring Interconnection System (EWIS) 1 3 3
Continuity, insulation and bonding techniques and testing;
Use of crimp tools: hand and hydraulic operated;
Testing of crimp joints;
Connector pin removal and insertion;
Co-axial cables: testing and installation precautions;
Identification of wire types, their inspection criteria and damage
tolerance.
Wiring protection techniques: Cable looming and loom support, cable
clamps, protective sleeving techniques including heat shrink wrapping,
shielding;
EWIS installations, inspection, repair, maintenance and cleanliness
standards.
7.8 Riveting 1 2 —
Riveted joints, rivet spacing and pitch;
Tools used for riveting and dimpling;
Inspection of riveted joints.
7.9 Pipes and Hoses 1 2 —
Bending and belling/flaring aircraft pipes;
Inspection and testing of aircraft pipes and hoses;
Installation and clamping of pipes.
7.10 Springs 1 2 —
Inspection and testing of springs.

LEVEL
B2L
7.11 Bearings 1 2 —
Testing, cleaning and inspection of bearings;
Lubrication requirements of bearings;
Defects in bearings and their causes.
7.12 Transmissions 1 2 —
Inspection of gears, backlash;
Inspection of belts and pulleys, chains and sprockets;
Inspection of screw jacks, lever devices, push-pull rod systems.
7.13 Control Cables 1 2 —
Swaging of end fittings;
Inspection and testing of control cables;
Bowden cables; aircraft flexible control systems.
7.14 Material handling
7.14.1 Sheet Metal — 2 —
Marking out and calculation of bend allowance;
Sheet metal working, including bending and forming;
Inspection of sheet metal work.
7.14.2 Composite and non-metallic — 2 —
Bonding practices;
Environmental conditions;
Inspection methods.
7.15 Welding, Brazing, Soldering and Bonding
(a) Soldering methods; inspection of soldered joints. — 2 2
(b) Welding and brazing methods; — 2 —
Inspection of welded and brazed joints;
Bonding methods and inspection of bonded joints.
7.16 Aircraft Weight and Balance
(a) Centre of Gravity/Balance limits calculation: use of relevant — 2 2
documents;
(b) Preparation of aircraft for weighing; — 2 —
Aircraft weighing.
7.17 Aircraft Handling and Storage 2 2 2
Aircraft taxiing/towing and associated safety precautions;
Aircraft jacking, chocking, securing and associated safety precautions;
Aircraft storage methods;
Refuelling/defuelling procedures;
De-icing/anti-icing procedures;
Electrical, hydraulic and pneumatic ground supplies.
Effects of environmental conditions on aircraft handling and operation.
7.18 Disassembly, Inspection, Repair and Assembly Techniques
(a) Types of defects and visual inspection techniques; 2 3 3
Corrosion removal, assessment and reprotection;
(b) General repair methods, Structural Repair Manual; — 2 —
Ageing, fatigue and corrosion control programmes;
(c) Non-destructive inspection techniques including, penetrant, — 2 1
radiographic, eddy current, ultrasonic and boroscope methods;
(d) Disassembly and re-assembly techniques; 2 2 2
(e) Trouble shooting techniques. — 2 2

LEVEL
B2L
7.19 Abnormal Events
(a) Inspections following lightning strikes and HIRF penetration; 2 2 2
(b) Inspections following abnormal events such as heavy landings and 2 2 —
flight through turbulence.
7.20 Maintenance Procedures 1 2 2
Maintenance planning;
Modification procedures;
Stores procedures;
Certification/release procedures;
Interface with aircraft operation;
Maintenance Inspection/Quality Control/Quality Assurance;
Additional maintenance procedures;
Control of life limited components.
MODULE 7B. MAINTENANCE PRACTICES

Note: The scope of this module shall reflect the technology of aeroplanes relevant to the B3 category.
LEVEL
B3
7.1 Safety Precautions-Aircraft and Workshop 3
Aspects of safe working practices including precautions to take when working with
electricity, gases especially oxygen, oils and chemicals.
Also, instruction in the remedial action to be taken in the event of a fire or another
accident with one or more of these hazards including knowledge on extinguishing
agents.
7.2 Workshop Practices 3
Care of tools, control of tools, use of workshop materials;
Dimensions, allowances and tolerances, standards of workmanship;
Calibration of tools and equipment, calibration standards.
7.3 Tools 3
Common hand tool types;
Common power tool types;
Operation and use of precision measuring tools;
Lubrication equipment and methods;
Operation, function and use of electrical general test equipment.
7.4 Avionic General Test Equipment 1
Operation, function and use of avionic general test equipment.
7.5 Engineering Drawings, Diagrams and Standards 2
Drawing types and diagrams, their symbols, dimensions, tolerances and projections;
Identifying title block information;
Microfilm, microfiche and computerised presentations;
Specification 100 of the Air Transport Association (ATA) of America;
Aeronautical and other applicable standards including ISO, AN, MS, NAS and MIL;
Wiring diagrams and schematic diagrams.

LEVEL
B3
7.6 Fits and Clearances 2
Drill sizes for bolt holes, classes of fits;
Common system of fits and clearances;
Schedule of fits and clearances for aircraft and engines;
Limits for bow, twist and wear;
Standard methods for checking shafts, bearings and other parts.
7.7 Electrical Cables and Connectors 2
Continuity, insulation and bonding techniques and testing;
Use of crimp tools: hand and hydraulic operated;
Testing of crimp joints;
Connector pin removal and insertion;
Co-axial cables: testing and installation precautions;
Wiring protection techniques: Cable looming and loom support, cable clamps,
protective sleeving techniques including heat shrink wrapping, shielding.
7.8 Riveting 2
Riveted joints, rivet spacing and pitch;
Tools used for riveting and dimpling;
Inspection of riveted joints.
7.9 Pipes and Hoses 2
Bending and belling/flaring aircraft pipes;
Inspection and testing of aircraft pipes and hoses;
Installation and clamping of pipes.
7.10 Springs 2
Inspection and testing of springs.
7.11 Bearings 2
Testing, cleaning and inspection of bearings;
Lubrication requirements of bearings;
Defects in bearings and their causes.
7.12 Transmissions 2
Inspection of gears, backlash;
Inspection of belts and pulleys, chains and sprockets;
Inspection of screw jacks, lever devices, push-pull rod systems.
7.13 Control Cables 2
Swaging of end fittings;
Inspection and testing of control cables;
Bowden cables; aircraft flexible control systems.
7.14 Material handling
7.14.1 Sheet Metal 2
Marking out and calculation of bend allowance;
Sheet metal working, including bending and forming;
Inspection of sheet metal work.
7.14.2 Composite and non-metallic 2
Bonding practices;
Environmental conditions;
Inspection methods.
7.15 Welding, Brazing, Soldering and Bonding
(a) Soldering methods; inspection of soldered joints; 2
(b) Welding and brazing methods; 2
Inspection of welded and brazed joints;

LEVEL
B3
Bonding methods and inspection of bonded joints.
7.16 Aircraft Weight and Balance
(a) Centre of Gravity/Balance limits calculation: use of relevant documents; 2
(b) Preparation of aircraft for weighing; 2
Aircraft weighing.
7.17 Aircraft Handling and Storage 2
Aircraft taxiing/towing and associated safety precautions;
Aircraft jacking, chocking, securing and associated safety precautions;
Aircraft storage methods;
Refuelling/defuelling procedures;
De-icing/anti-icing procedures;
Electrical, hydraulic and pneumatic ground supplies;
Effects of environmental conditions on aircraft handling and operation.
7.18 Disassembly, Inspection, Repair and Assembly Techniques
(a) Types of defects and visual inspection techniques; 3
Corrosion removal, assessment and reprotection;
(b) General repair methods, Structural Repair Manual; 2
Ageing, fatigue and corrosion control programmes;
(c) Non-destructive inspection techniques including, penetrant, radiographic, eddy 2
current, ultrasonic and boroscope methods;
(d) Disassembly and re-assembly techniques; 2
(e) Trouble shooting techniques. 2
7.19 Abnormal Events
(a) Inspections following lightning strikes and HIRF penetration. 2
(b) Inspections following abnormal events such as heavy landings and flight through 2
turbulence.
7.20 Maintenance Procedures 2
Maintenance planning;
Modification procedures;
Stores procedures;
Certification/release procedures;
Interface with aircraft operation;
Maintenance Inspection/Quality Control/Quality Assurance;
Additional maintenance procedures;
Control of life limited components.

MODULE 8. BASIC AERODYNAMICS

LEVEL
MODULE 8. BASIC AERODYNAMICS A B1 B2 B3
B2L
8.1 Physics of the Atmosphere 1 2 2 1
International Standard Atmosphere (ISA), application to
aerodynamics.
8.2 Aerodynamics 1 2 2 1
Airflow around a body;
Boundary layer, laminar and turbulent flow, free stream flow,
relative airflow, upwash and downwash, vortices, stagnation;
The terms: camber, chord, mean aerodynamic chord, profile
(parasite) drag, induced drag, centre of pressure, angle of attack,
wash in and wash out, fineness ratio, wing shape and aspect
ratio;
Thrust, Weight, Aerodynamic Resultant;
Generation of Lift and Drag: Angle of Attack, Lift coefficient, Drag
coefficient, polar curve, stall;
Aerofoil contamination including ice, snow, frost.
8.3 Theory of Flight 1 2 2 1
Relationship between lift, weight, thrust and drag;
Glide ratio;
Steady state flights, performance;
Theory of the turn;
Influence of load factor: stall, flight envelope and structural
limitations;
Lift augmentation.
8.4 Flight Stability and Dynamics 1 2 2 1
Longitudinal, lateral and directional stability (active and passive).
MODULE 9A. HUMAN FACTORS

in module 9B.
LEVEL
MODULE 9A. HUMAN FACTORS A B1 B2
B2L
9.1 General 1 2 2
The need to take human factors into account;
Incidents attributable to human factors/human error;
‘Murphy's’ law.
9.2 Human Performance and Limitations 1 2 2
Vision;
Hearing;
Information processing;
Attention and perception;
Memory;
Claustrophobia and physical access.

LEVEL
MODULE 9A. HUMAN FACTORS A B1 B2
B2L
9.3 Social Psychology 1 1 1
Responsibility: individual and group;
Motivation and de-motivation;
Peer pressure;
‘Culture’ issues;
Team working;
Management, supervision and leadership.
9.4 Factors Affecting Performance 2 2 2
Fitness/health;
Stress: domestic and work related;
Time pressure and deadlines;
Workload: overload and underload;
Sleep and fatigue, shiftwork;
Alcohol, medication, drug abuse.
9.5 Physical Environment 1 1 1
Noise and fumes;
Illumination;
Climate and temperature;
Motion and vibration;
Working environment.
9.6 Tasks 1 1 1
Physical work;
Repetitive tasks;
Visual inspection;
Complex systems.
9.7 Communication 2 2 2
Within and between teams;
Work logging and recording;
Keeping up to date, currency;
Dissemination of information.
9.8 Human Error 1 2 2
Error models and theories;
Types of error in maintenance tasks;
Implications of errors (i.e. accidents);
Avoiding and managing errors.
9.9 Hazards in the Workplace 1 2 2
Recognising and avoiding hazards;
Dealing with emergencies.

MODULE 9B. HUMAN FACTORS

Note: The scope of this module shall reflect the less demanding environment of maintenance for B3
licence holders.
LEVEL
B3
9.1 General 2
The need to take human factors into account;
Incidents attributable to human factors/human error;
‘Murphy's’ law.
9.2 Human Performance and Limitations 2
Vision;
Hearing;
Information processing;
Attention and perception;
Memory;
Claustrophobia and physical access.
9.3 Social Psychology 1
Responsibility: individual and group;
Motivation and de-motivation;
Peer pressure;
‘Culture’ issues;
Team working;
Management, supervision and leadership.
9.4 Factors Affecting Performance 2
Fitness/health;
Stress: domestic and work related;
Time pressure and deadlines;
Workload: overload and underload;
Sleep and fatigue, shiftwork;
Alcohol, medication, drug abuse.
9.5 Physical Environment 1
Noise and fumes;
Illumination;
Climate and temperature;
Motion and vibration;
Working environment.
9.6 Tasks 1
Physical work;
Repetitive tasks;
Visual inspection;
Complex systems.
9.7 Communication 2
Within and between teams;
Work logging and recording;
Keeping up to date, currency;
Dissemination of information.

LEVEL
B3
9.8 Human Error 2
Error models and theories;
Types of error in maintenance tasks;
Implications of errors (i.e. accidents);
Avoiding and managing errors.
9.9 Hazards in the Workplace 2
Recognising and avoiding hazards;
Dealing with emergencies.
MODULE 10. AVIATION LEGISLATION

LEVEL
MODULE 10. AVIATION LEGISLATION A B1 B2 B3
B2L
10.1 Regulatory Framework 1 1 1 1
Role of the International Civil Aviation Organisation;
Role of the European Commission;
Role of EASA;
Role of the Member States and National Aviation Authorities;
Regulations (EU) 2018/1139, Regulation (EU) No 748/2012,
Regulation (EU) No 1321/2014 and Regulation (EU) No 376/2014;
Relation between the various Annexes (Parts) of Regulation (EU)
No 748/2012, Regulation (EU) No 1321/2014 and Regulation (EU)
No 965/2012
10.2 Certifying Staff — Maintenance 2 2 2 2
Detailed understanding of Part-66.
10.3 Approved Maintenance Organisations 2 2 2 2
Detailed understanding of Part-145 and Part-M Subpart F.
10.4 Air operations 1 1 1 1
General understanding of Regulation (EU) No 965/2012.
Air Operators Certificates;
Operator's responsibilities, in particular regarding continuing
airworthiness and maintenance;
Aircraft Maintenance Programme;
MEL//CDL;
Documents to be carried on board;
Aircraft placarding (markings).
10.5 Certification of aircraft, parts and appliances
(a) General — 1 1 1
General understanding of Part 21 and EASA certification
specifications CS-23, 25, 27, 29.
(b) Documents — 2 2 2
Certificate of Airworthiness; restricted certificates of
airworthiness and permit to fly;
Certificate of Registration;
Noise Certificate;
Weight Schedule;
Radio Station Licence and Approval.

LEVEL
MODULE 10. AVIATION LEGISLATION A B1 B2 B3
B2L
10.6 Continuing airworthiness 2 2 2 2
Detailed understanding of Part 21 provisions related to continuing
airworthiness.
Detailed understanding of Part-M.
10.7 Applicable National and International Requirements for (if not
superseded by EU requirements).
(a) Maintenance Programmes, Maintenance checks and 1 2 2 2
inspections;
Airworthiness Directives;
Service Bulletins, manufacturers service information;
Modifications and repairs;
Maintenance documentation: maintenance manuals,
structural repair manual, illustrated parts catalogue, etc.;
Only for A to B2 licences:
Master Minimum Equipment Lists, Minimum Equipment List,
Dispatch Deviation Lists;
(b) Continuing airworthiness; — 1 1 1
Minimum equipment requirements — Test flights;
Only for B1 and B2 licences:
ETOPS, maintenance and dispatch requirements;
All Weather Operations, Category 2/3 operations.
MODULE 11A. TURBINE AEROPLANE AERODYNAMICS, STRUCTURES AND SYSTEMS

LEVEL
A1 B1.1
11.1 Theory of Flight
11.1.1. Aeroplane Aerodynamics and Flight Controls 1 2
Operation and effect of:
— roll control: ailerons and spoilers,
— pitch control: elevators, stabilators, variable incidence stabilisers and canards,
— yaw control, rudder limiters;
Control using elevons, ruddervators;
High lift devices, slots, slats, flaps, flaperons;
Drag inducing devices, spoilers, lift dumpers, speed brakes;
Effects of wing fences, saw tooth leading edges;
Boundary layer control using, vortex generators, stall wedges or leading edge
devices;
Operation and effect of trim tabs, balance and antibalance (leading) tabs, servo
tabs, spring tabs, mass balance, control surface bias, aerodynamic balance
panels.
11.1.2. High Speed Flight 1 2
Speed of sound, subsonic flight, transonic flight, supersonic flight;
Mach number, critical Mach number, compressibility buffet, shock wave,
aerodynamic heating, area rule;
Factors affecting airflow in engine intakes of high speed aircraft;
Effects of sweepback on critical Mach number.

LEVEL
A1 B1.1
11.2 Airframe Structures — General Concepts
(a) Airworthiness requirements for structural strength; 2 2
Structural classification, primary, secondary and tertiary;
Fail safe, safe life, damage tolerance concepts;
Zonal and station identification systems;
Stress, strain, bending, compression, shear, torsion, tension, hoop stress,
fatigue;
Drains and ventilation provisions;
System installation provisions;
Lightning strike protection provision;
Aircraft bonding.
(b) Construction methods of: stressed skin fuselage, formers, stringers, longerons, 1 2
bulkheads, frames, doublers, struts, ties, beams, floor structures,
reinforcement, methods of skinning, anti-corrosive protection, wing,
empennage and engine attachments;
Structure assembly techniques: riveting, bolting, bonding;
Methods of surface protection, such as chromating, anodising, painting;
Surface cleaning;
Airframe symmetry: methods of alignment and symmetry checks.
11.3 Airframe Structures — Aeroplanes
11.3.1 Fuselage (ATA 52/53/56) 1 2
Construction and pressurisation sealing;
Wing, stabiliser, pylon and undercarriage attachments;
Seat installation and cargo loading system;
Doors and emergency exits: construction, mechanisms, operation and safety
devices;
Windows and windscreen construction and mechanisms.
11.3.2 Wings (ATA 57) 1 2
Construction;
Fuel storage;
Landing gear, pylon, control surface and high lift/drag attachments.
11.3.3 Stabilisers (ATA 55) 1 2
Construction;
Control surface attachment.
11.3.4 Flight Control Surfaces (ATA 55/57) 1 2
Construction and attachment;
Balancing — mass and aerodynamic.
11.3.5 Nacelles/Pylons (ATA 54) 1 2
Nacelles/Pylons:
— Construction,
— Firewalls,
— Engine mounts.
11.4 Air Conditioning and Cabin Pressurisation (ATA 21)
11.4.1 Air supply 1 2
Sources of air supply including engine bleed, APU and ground cart.
11.4.2 Air Conditioning 1 3
Air conditioning systems;
Air cycle and vapour cycle machines;
Distribution systems;
Flow, temperature and humidity control system.

LEVEL
A1 B1.1
11.4.3 Pressurisation 1 3
Pressurisation systems;
Control and indication including control and safety valves;
Cabin pressure controllers.
11.4.4 Safety and warning devices 1 3
Protection and warning devices.
11.5 Instruments/Avionic Systems
11.5.1 Instrument Systems (ATA 31) 1 2
Pitot static: altimeter, air speed indicator, vertical speed indicator;
Gyroscopic: artificial horizon, attitude director, direction indicator, horizontal
situation indicator, turn and slip indicator, turn coordinator;
Compasses: direct reading, remote reading;
Angle of attack indication, stall warning systems;
Glass cockpit;
Other aircraft system indication.
11.5.2 Avionic Systems 1 1
Fundamentals of system lay-outs and operation of:
— Auto Flight (ATA 22),
— Communications (ATA 23),
— Navigation Systems (ATA 34).
11.6 Electrical Power (ATA 24) 1 3
Batteries Installation and Operation;
DC power generation;
AC power generation;
Emergency power generation;
Voltage regulation;
Power distribution;
Inverters, transformers, rectifiers;
Circuit protection;
External/Ground power.
11.7 Equipment and Furnishings (ATA 25)
(a) Emergency equipment requirements; 2 2
Seats, harnesses and belts.
(b) Cabin lay-out; 1 1
Equipment lay-out;
Cabin Furnishing installation;
Cabin entertainment equipment;
Galley installation;
Cargo handling and retention equipment;
Airstairs.
11.8 Fire Protection (ATA 26)
(a) Fire and smoke detection and warning systems; 1 3
Fire extinguishing systems;
System tests;
(b) Portable fire extinguisher. 1 2

LEVEL
A1 B1.1
11.9 Flight Controls (ATA 27) 1 3
Primary controls: aileron, elevator, rudder, spoiler;
Trim control;
Active load control;
High lift devices;
Lift dump, speed brakes;
System operation: manual, hydraulic, pneumatic, electrical, fly-by-wire;
Artificial feel, Yaw damper, Mach trim, rudder limiter, gust lock systems;
Balancing and rigging;
Stall protection/warning system.
11.10 Fuel Systems (ATA 28) 1 3
System lay-out;
Fuel tanks;
Supply systems;
Dumping, venting and draining;
Cross-feed and transfer;
Indications and warnings;
Refuelling and defuelling;
Longitudinal balance fuel systems.
11.11 Hydraulic Power (ATA 29) 1 3
System lay-out;
Hydraulic fluids;
Hydraulic reservoirs and accumulators;
Pressure generation: electric, mechanical, pneumatic;
Emergency pressure generation;
Filters;
Pressure Control;
Power distribution;
Indication and warning systems;
Interface with other systems.
11.12 Ice and Rain Protection (ATA 30) 1 3
Ice formation, classification and detection;
Anti-icing systems: electrical, hot air and chemical;
De-icing systems: electrical, hot air, pneumatic and chemical;
Rain repellent;
Probe and drain heating;
Wiper systems.
11.13 Landing Gear (ATA 32) 2 3
Construction, shock absorbing;
Extension and retraction systems: normal and emergency;
Indications and warning;
Wheels, brakes, antiskid and autobraking;
Tyres;
Steering;
Air-ground sensing.
11.14 Lights (ATA 33) 2 3
External: navigation, anti collision, landing, taxiing, ice;
Internal: cabin, cockpit, cargo;
Emergency.

LEVEL
A1 B1.1
11.15 Oxygen (ATA 35) 1 3
System lay-out: cockpit, cabin;
Sources, storage, charging and distribution;
Supply regulation;
Indications and warnings.
11.16 Pneumatic/Vacuum (ATA 36) 1 3
System lay-out;
Sources: engine/APU (Auxiliary Power Unit), compressors, reservoirs, ground
supply;
Pressure and vacuum pumps;
Pressure control;
Distribution;
Interfaces with other systems.
11.17 Water/Waste (ATA 38) 2 3
Water system lay-out, supply, distribution, servicing and draining;
Toilet system lay-out, flushing and servicing;
Corrosion aspects.
11.18 On Board Maintenance Systems (ATA 45) 1 2
Central maintenance computers;
Data loading system;
Electronic library system;
Printing;
Structure monitoring (damage tolerance monitoring).
11.19 Integrated Modular Avionics (ATA42) 1 2
Functions that may be typically integrated in the Integrated Modular Avionic (IMA)
modules are, among others:
Bleed Management, Air Pressure Control, Air Ventilation and Control, Avionics and
Cockpit Ventilation Control, Temperature Control, Air Traffic Communication,
Avionics Communication Router, Electrical Load Management, Circuit Breaker
Monitoring, Electrical System BITE, Fuel Management, Braking Control, Steering
Control, Landing Gear Extension and Retraction, Tyre Pressure Indication, Oleo
Pressure Indication, Brake Temperature Monitoring, etc.
Core System; Network Components.
11.20 Cabin Systems (ATA44) 1 2
The units and components which furnish a means of entertaining the passengers
and providing communication within the aircraft (Cabin Intercommunication Data
System (CIDS)) and between the aircraft cabin and ground stations (Cabin Network
Service (CNS)). They include voice, data, music and video transmissions.
CIDS provides an interface between cockpit/cabin crew and cabin systems. These
systems support data exchange between the different related Line Replaceable
Units (LRUs) and they are typically operated via Flight Attendant Panels (FAPs).
CNS typically consists of a server, interfacing with, among others, the following
systems:
— Data/Radio Communication;
— Cabin Core System (CCS);
— In-flight Entertainment System (IFES);
— External Communication System (ECS);
— Cabin Mass Memory System (CMMS);

LEVEL
A1 B1.1
— Cabin Monitoring System (CMS);
— Miscellaneous Cabin Systems (MCSs).
CNS may host functions such as:
— access to pre-departure/departure reports;
— e-mail/intranet/internet access; passenger database.
11.21 Information Systems (ATA46) 1 2
The units and components which furnish a means of storing, updating and retrieving
digital information traditionally provided on paper, microfilm or microfiche. Includes
units that are dedicated to the information storage and retrieval function such as
the electronic library mass storage and controller. Does not include units or
components installed for other uses and shared with other systems, such as flight
deck printer or general use display.
Typical examples include Air Traffic and Information Management Systems and
Network Server Systems
Aircraft General Information System;
Flight Deck Information System;
Maintenance Information System;
Passenger Cabin Information System;
Miscellaneous Information System.
MODULE 11B. PISTON AEROPLANE AERODYNAMICS, STRUCTURES AND SYSTEMS

Note 1: This module does not apply to category B3. Relevant subject matters for category B3 are
defined in module 11C.
Note 2: The scope of this Module shall reflect the technology of aeroplanes pertinent to the A2 and
B1.2 subcategory.
LEVEL
A2 B1.2
11.1.1. Aeroplane Aerodynamics and Flight Controls 1 2
— roll control: ailerons and spoilers,
Drag inducing devices, spoilers, lift dumpers, speed brakes;
Boundary layer control using, vortex generators, stall wedges or leading edge
devices;
Operation and effect of trim tabs, balance and antibalance (leading) tabs, servo
tabs, spring tabs, mass balance, control surface bias, aerodynamic balance
panels.
11.1.2. High Speed Flight — N/A — —

LEVEL
A2 B1.2
fatigue;
Aircraft bonding.
(b) Construction methods of: stressed skin fuselage, formers, stringers, 1 2
longerons, bulkheads, frames, doublers, struts, ties, beams, floor
structures, reinforcement, methods of skinning, anti-corrosive protection,
wing, empennage and engine attachments;
Surface cleaning;
11.3.1 Fuselage (ATA 52/53/56) 1 2
Construction and pressurisation sealing;
Wing, tail-plane, pylon and undercarriage attachments;
Seat installation;
Doors and emergency exits: construction and operation;
Windows and windscreen attachment.
11.3.2 Wings (ATA 57) 1 2
Construction;
Fuel storage;
11.3.3 Stabilisers (ATA 55) 1 2
Construction;
11.3.4 Flight Control Surfaces (ATA 55/57) 1 2
11.3.5 Nacelles/Pylons (ATA 54) 1 2
Nacelles/Pylons:
— Construction,
— Firewalls,
— Engine mounts.
11.4 Air Conditioning and Cabin Pressurisation (ATA 21) 1 3
Pressurisation and air conditioning systems;
Cabin pressure controllers, protection and warning devices;
Heating systems.

LEVEL
A2 B1.2
Glass cockpit;
Voltage regulation;
Power distribution;
Circuit protection;
Inverters, transformers.
Seats, harnesses and belts;
(b) Cabin lay-out; 1 1
Equipment lay-out;
Cabin Furnishing installation;
Cabin entertainment equipment;
Galley installation;
Cargo handling and retention equipment;
Airstairs.
(a) Fire and smoke detection and warning systems; 1 3
System tests;
(b) Portable fire extinguisher. 1 2
11.9 Flight Controls (ATA 27) 1 3
Primary controls: aileron, elevator, rudder;
Trim tabs;
High lift devices;
System operation: manual;
Gust locks;
Stall warning system.

MODULE 11C. PISTON AEROPLANE AERODYNAMICS, STRUCTURES AND SYSTEMS

Note: The scope of this module shall reflect the technology of aeroplanes pertinent to the B3 category.
LEVEL
B3
Aeroplane Aerodynamics and Flight Controls 1
— roll control: ailerons,
Drag inducing devices, lift dumpers, speed brakes;
Boundary layer control using, vortex generators, stall wedges or leading edge devices;
Operation and effect of trim tabs, balance and anti-balance (leading) tabs, servo tabs,
spring tabs, mass balance, control surface bias, aerodynamic balance panels.
(a) Airworthiness requirements for structural strength; 2
Stress, strain, bending, compression, shear, torsion, tension, hoop stress, fatigue;
Aircraft bonding;
(b) Construction methods of: stressed skin fuselage, formers, stringers, longerons, 2
bulkheads, frames, doublers, struts, ties, beams, floor structures, reinforcement,
methods of skinning, anti-corrosive protection, wing, empennage and engine
attachments;
Surface cleaning;
11.3.1 Fuselage (ATA 52/53/56) 1
Construction;
Wing, tail-plane, pylon and undercarriage attachments;
Seat installation;
Doors and emergency exits: construction and operation;
Window and windscreen attachment.
11.3.2 Wings (ATA 57) 1
Construction;
Fuel storage;
11.3.3 Stabilisers (ATA 55) 1
Construction;
11.3.4 Flight Control Surfaces (ATA 55/57) 1

LEVEL
B3
11.3.5 Nacelles/Pylons (ATA 54) 1
Nacelles/Pylons:
— Construction,
— Firewalls,
— Engine mounts.
11.4 Air Conditioning (ATA 21)
Heating and ventilation systems. 1
11.5.1 Instrument Systems (ATA 31) 1
Glass cockpit;
11.5.2 Avionic Systems 1
11.6 Electrical Power (ATA 24) 2
Voltage regulation;
Power distribution;
Circuit protection;
Inverters, transformers.
11.7 Equipment and Furnishings (ATA 25) 2
Emergency equipment requirements;
Seats, harnesses and belts.
11.8 Fire Protection (ATA 26) 2
Portable fire extinguisher.
11.9 Flight Controls (ATA 27) 3
Primary controls: aileron, elevator, rudder;
Trim tabs;
High lift devices;
System operation: manual;
Gust locks;
Stall warning system.
11.10 Fuel Systems (ATA 28) 2
System lay-out;
Fuel tanks;
Supply systems;
Refuelling and defuelling.

LEVEL
B3
11.11 Hydraulic Power (ATA 29) 2
System lay-out;
Hydraulic fluids;
Pressure generation: electric, mechanical;
Filters;
Pressure Control;
Power distribution;
Indication and warning systems.
11.12 Ice and Rain Protection (ATA 30) 1
De-icing systems: electrical, hot air, pneumatic and chemical;
Wiper systems.
11.13 Landing Gear (ATA 32) 2
Wheels, brakes, antiskid and autobraking;
Tyres;
Steering.
11.14 Lights (ATA 33) 2
External: navigation, anti collision, landing, taxiing, ice;
Emergency.
11.15 Oxygen (ATA 35) 2
System lay-out: cockpit, cabin;
Sources, storage, charging and distribution;
Supply regulation;
Indications and warnings.
11.16 Pneumatic/Vacuum (ATA 36) 2
System lay-out;
Sources: engine/APU, compressors, reservoirs, ground supply;
Pressure and vacuum pumps
Pressure control;
Distribution;

MODULE 12. HELICOPTER AERODYNAMICS, STRUCTURES AND SYSTEMS

LEVEL
MODULE 12. HELICOPTER AERODYNAMICS, STRUCTURES AND SYSTEMS A3 B1.3
A4 B1.4
12.1 Theory of Flight — Rotary Wing Aerodynamics 1 2
Terminology;
Effects of gyroscopic precession;
Torque reaction and directional control;
Dissymmetry of lift, Blade tip stall;
Translating tendency and its correction;
Coriolis effect and compensation;
Vortex ring state, power settling, overpitching;
Auto-rotation;
Ground effect.
12.2 Flight Control Systems 2 3
Cyclic control;
Collective control;
Swashplate;
Yaw control: Anti-Torque Control, Tail rotor, bleed air;
Main Rotor Head: Design and Operation features;
Blade Dampers: Function and construction;
Rotor Blades: Main and tail rotor blade construction and attachment;
Trim control, fixed and adjustable stabilisers;
System operation: manual, hydraulic, electrical and fly-by-wire;
Artificial feel;
Balancing and rigging.
12.3 Blade Tracking and Vibration Analysis 1 3
Rotor alignment;
Main and tail rotor tracking;
Static and dynamic balancing;
Vibration types, vibration reduction methods;
Ground resonance.
12.4 Transmission 1 3
Gear boxes, main and tail rotors;
Clutches, free wheel units and rotor brake;
Tail rotor drive shafts, flexible couplings, bearings, vibration dampers and
bearing hangers.
12.5 Airframe Structures
fatigue;
(b) Construction methods of: stressed skin fuselage, formers, stringers, 1 2
longerons, bulkheads, frames, doublers, struts, ties, beams, floor
structures, reinforcement, methods of skinning and anti-corrosive
protection.

LEVEL
A4 B1.4
Pylon, stabiliser and undercarriage attachments;
Seat installation;
Doors: construction, mechanisms, operation and safety devices;
Windows and windscreen construction;
Fuel storage;
Firewalls;
Engine mounts;
Surface cleaning.
12.6 Air Conditioning (ATA 21)
12.6.1 Air supply 1 2
Sources of air supply including engine bleed and ground cart.
12.6.2 Air conditioning 1 3
Air conditioning systems;
Distribution systems;
Flow and temperature control systems;
Gyroscopic: artificial horizon, attitude director, direction indicator,
horizontal situation indicator, turn and slip indicator, turn coordinator;
Vibration indicating systems — HUMS;
Glass cockpit;
Fundamentals of system layouts and operation of:
Auto Flight (ATA 22);
Communications (ATA 23);
Navigation Systems (ATA 34).
DC power generation, AC power generation;
Voltage regulation, Circuit protection.
Power distribution;
Seats, harnesses and belts;
Lifting systems;
(b) Emergency flotation systems; 1 1
Cabin lay-out, cargo retention;
Equipment lay-out;
Cabin Furnishing Installation.

LEVEL
A4 B1.4
12.10 Fire Protection (ATA 26) 1 3
Fire and smoke detection and warning systems;
System tests.
12.11 Fuel Systems (ATA 28) 1 3
System lay-out;
Fuel tanks;
Supply systems;
Dumping, venting and draining;
Refuelling and defuelling.
12.12 Hydraulic Power (ATA 29) 1 3
System lay-out;
Hydraulic fluids;
Pressure generation: electric, mechanical, pneumatic;
Emergency pressure generation;
Filters;
Pressure Control;
Power distribution;
Indication and warning systems;
Interface with other systems.
12.13 Ice and Rain Protection (ATA 30) 1 3
Anti-icing and De-icing systems: electrical, hot air and chemical;
Rain repellent and removal;
Wiper system.
12.14 Landing Gear (ATA 32) 2 3
Wheels, Tyres, brakes;
Steering;
Air-ground sensing;
Skids, floats.
12.15 Lights (ATA 33) 2 3
External: navigation, landing, taxiing, ice;
Emergency.
12.16 Pneumatic/Vacuum (ATA 36) 1 3
System lay-out;
Sources: engine/APU, compressors, reservoirs, ground supply;
Pressure and vacuum pumps;
Pressure control;
Distribution;

LEVEL
A4 B1.4
12.17 Integrated Modular Avionics (ATA42) 1 2
Functions that may be typically integrated in the Integrated Modular Avionic
(IMA) modules are, among others:
Bleed Management, Air Pressure Control, Air Ventilation and Control, Avionics
and Cockpit Ventilation Control, Temperature Control, Air Traffic
Communication, Avionics Communication Router, Electrical Load
Management, Circuit Breaker Monitoring, Electrical System BITE, Fuel
Management, Braking Control, Steering Control, Landing Gear Extension and
Retraction, Tyre Pressure Indication, Oleo Pressure Indication, Brake
Temperature Monitoring, etc.
Core System;
Network Components.
12.18 On Board Maintenance Systems (ATA45) 1 2
Data loading system;
Electronic library system;
Printing;
Structure monitoring (damage tolerance monitoring).
12.19 Information Systems (ATA46) 1 2
The units and components which furnish a means of storing, updating and
retrieving digital information traditionally provided on paper, microfilm or
microfiche. Includes units that are dedicated to the information storage and
retrieval function such as the electronic library mass storage and controller.
Does not include units or components installed for other uses and shared with
other systems, such as flight deck printer or general use display.
Typical examples include Air Traffic and Information Management Systems and
Network Server Systems.
Aircraft General Information System;
Flight Deck Information System;
Maintenance Information System;
Passenger Cabin Information System;
Miscellaneous Information System.
MODULE 13. AIRCRAFT AERODYNAMICS, STRUCTURES AND SYSTEMS

LEVEL
MODULE 13. AIRCRAFT AERODYNAMICS, STRUCTURES AND SYSTEMS B2
B2L
(a) Aeroplane Aerodynamics and Flight Controls 1
— roll control: ailerons and spoilers;
— pitch control: elevators, stabilators, variable incidence stabilisers and canards;
and
— yaw control: rudder limiters;
High lift devices: slots, slats, flaps;

LEVEL
B2L
Drag inducing devices: spoilers, lift dumpers, speed brakes; and
Operation and effect of trim tabs, servo tabs and control surface bias.
(b) High Speed Flight 1
Speed of sound, subsonic flight, transonic flight, supersonic flight;
Mach number, critical Mach number.
(c) Rotary Wing Aerodynamics 1
Terminology;
Operation and effect of cyclic, collective and anti-torque controls.
13.2 Structures — General Concepts
Fundamentals of Structural Systems 1
Zonal and Station Identification Systems 2
Electrical bonding 2
Lightning strike protection provision. 2
13.3 Autoflight (ATA 22)
(a) 3
Fundamentals of automatic flight control including working principles and current
terminology;
Command signal processing;
Modes of operation: roll, pitch and yaw channels;
Yaw dampers;
Stability Augmentation System in helicopters;
Automatic trim control;
Autopilot navigation aids interface;
(b) 3
Autothrottle systems;
Automatic landing systems: principles and categories, modes of operation, approach,
glideslope, land, go-around, system monitors and failure conditions.
13.4 Communication/Navigation (ATA 23/34)
(a) 3
Fundamentals of radio wave propagation, antennas, transmission lines, communication,
receiver and transmitter;
Working principles of following systems:
— Very High Frequency (VHF) communication;
— High Frequency (HF) communication;
— Audio;
— Emergency Locator Transmitters (ELTs);
— Cockpit Voice Recorder (CVR);
— Very High Frequency Omnidirectional Range (VOR);
— Automatic Direction Finding (ADF);
— Instrument Landing System (ILS);
— Flight Director Systems (FDSs), Distance Measuring Equipment (DME);
— Area navigation, RNAV systems;
— Flight Management Systems (FMSs);
— Global Positioning System (GPS), Global Navigation Satellite Systems (GNSSs);
— Data Link.

LEVEL
B2L
(b) 3
— Air Traffic Control transponder, secondary surveillance radar;
— Traffic Alert and Collision Avoidance System (TCAS);
— Weather avoidance radar;
— Radio altimeter;
— Automatic Dependent Surveillance — Broadcast (ADS-B).
(c) 3
— Microwave Landing System (MLS);
— Very Low Frequency and hyperbolic navigation (VLF/Omega);
— Doppler navigation;
— Inertial Navigation System (INS);
— ARINC (Aircraft Radio Incorporated) communication and reporting.
13.5 Electrical Power (ATA 24) 3
Batteries installation and operation;
Direct Current (DC) power generation;
Alternating Current (AC) power generation;
Voltage regulation;
Power distribution;
Circuit protection;
13.6 Equipment and Furnishings (ATA 25) 3
Electronic emergency equipment requirements;
Cabin entertainment equipment.
13.7 Flight Controls (ATA 27)
(a) 2
Primary controls: aileron, elevator, rudder, spoiler;
Trim control;
Active load control;
High lift devices;
Lift dump, speed brakes;
System operation: manual, hydraulic, pneumatic;
Artificial feel, Yaw damper, Mach trim, rudder limiter, gust locks;
Stall protection systems.
(b) 3
System operation: electrical, fly-by-wire.

LEVEL
B2L
13.8 Instruments (ATA 31) 3
Classification;
Atmosphere;
Terminology;
Pressure-measuring devices and systems;
Pitot-static systems;
Altimeters;
Vertical-speed indicators;
Airspeed indicators;
Machmeters;
Altitude-reporting/alerting systems;
Air data computers;
Instrument pneumatic systems;
Direct-reading pressure and temperature gauges;
Temperature-indicating systems;
Fuel-quantity-indicating systems;
Gyroscopic principles;
Artificial horizons;
Slip indicators;
Directional gyros;
Ground Proximity Warning Systems (GPWSs);
Compass systems;
Flight Data Recording Systems (FDRSs);
Electronic Flight Instrument Systems (EFISs);
Instrument warning systems including master warning systems and centralised warning
panels;
Stall warning systems and angle of attack-indicating systems;
Vibration measurement and indication;
Glass cockpit.
13.9 Lights (ATA 33) 3
External: navigation, landing, taxiing, ice;
Emergency.
13.10 On Board Maintenance Systems (ATA 45) 3
Data-loading system;
Electronic-library system;
Printing system;
Structure-monitoring (damage tolerance monitoring).
13.11 Air Conditioning and Cabin Pressurisation (ATA 21)
13.11.1. Air supply 2
Sources of air supply including engine bleed, APU and ground cart;
13.11.2. Air Conditioning
Air-conditioning systems; 2
Air cycle and vapour cycle machines; 3
Distribution systems; 1
Flow, temperature and humidity control system. 3
13.11.3. Pressurisation 3

LEVEL
B2L
Pressurisation systems;
Control and indication including control and safety valves;
Cabin pressure controllers.
13.11.4. Safety and warning devices 3
(a) 3
Fire and smoke detection and warning systems;
Fire-extinguishing systems;
System tests;
(b) 1
Portable fire extinguisher.
13.13 Fuel Systems (ATA 28)
System layout; 1
Fuel tanks; 1
Supply systems; 1
Dumping, venting and draining; 1
Cross feed and transfer; 2
Indications and warnings; 3
Refuelling and defuelling; 2
Longitudinal-balance fuel systems. 3
13.14 Hydraulic Power (ATA 29)
System layout; 1
Hydraulic fluids; 1
Hydraulic reservoirs and accumulators; 1
Pressure generation: electrical, mechanical, pneumatic; 3
Emergency pressure generation; 3
Filters; 1
Pressure control; 3
Power distribution; 1
Indication and warning systems; 3
Interface with other systems. 3
13.15 Ice and Rain Protection (ATA 30)
Ice formation, classification and detection; 2
Anti-icing systems: electrical, hot-air and chemical; 2
De-icing systems: electrical, hot-air, pneumatic, chemical; 3
Rain-repellent; 1
Probe and drain-heating; 3
Wiper systems. 1
13.16 Landing Gear (ATA 32)
Construction, shock absorbing; 1
Extension and retraction systems: normal and emergency; 3
Wheels, brakes, antiskid and automatic braking systems; 3
Tyres; 1

LEVEL
B2L
Steering; 3
Air-ground sensing. 3
13.17 Oxygen (ATA 35)
System layout: cockpit, cabin; 3
Sources, storage, charging and distribution; 3
Supply regulation; 3
Indications and warnings. 3
13.18 Pneumatic/Vacuum (ATA 36)
System layout; 2
Sources: engine/APU, compressors, reservoirs, ground supply; 2
Pressure control; 3
Distribution; 1
Interfaces with other systems. 3
13.19 Water/Waste (ATA 38) 2
Water system layout, supply, distribution, servicing and draining;
Toilet system layout, flushing and servicing.
13.20 Integrated Modular Avionics (ATA 42) 3
Core system;
Network components.
Note: Functions that may be typically integrated into the IMA modules are among others:
— bleed management;
— air pressure control;
— air ventilation and control;
— avionics and cockpit ventilation control, temperature control;
— air traffic communication;
— avionics communication router;
— electrical load management;
— circuit breaker monitoring;
— electrical system Built-In Test Equipment (BITE);
— fuel management;
— braking control;
— steering control;
— landing gear extension and retraction;
— tyre pressure indication;
— oleo pressure indication;
— brake temperature monitoring.
13.21 Cabin Systems (ATA 44) 3
The units and components which furnish a means of entertaining the passengers and
providing communication within the aircraft (Cabin Intercommunication Data System
(CIDS)) and between the aircraft cabin and ground stations (Cabin Network Service
(CNS)). They include voice, data, music and video transmissions.
CIDS provides an interface between cockpit/cabin crew and cabin systems. These systems
support data exchange between the different related Line Replaceable Units (LRUs) and
they are typically operated via Flight Attendant Panels (FAPs).
CNS typically consists of a server, interfacing with, among others, the following systems:

LEVEL
B2L
— Data/Radio Communication;
— Cabin Core System (CCS);
— In-flight Entertainment System (IFES);
— External Communication System (ECS);
— Cabin Mass Memory System (CMMS);
— Cabin Monitoring System (CMS);
— Miscellaneous Cabin Systems (MCSs).
CNS may host functions such as:
— access to pre-departure/departure reports;
— e-mail/intranet/internet access;
— passenger database.
13.22 Information Systems (ATA 46) 3
The units and components which furnish a means of storing, updating and retrieving
digital information traditionally provided on paper, microfilm or microfiche. They include
units that are dedicated to the information storage and retrieval function such as the
electronic library mass storage and controller, but they do not include units or
components installed for other uses and shared with other systems, such as flight deck
printer or general-use display.
Typical examples include:

— Air Traffic and Information Management systems and Network Server systems.
— Aircraft general information system;
— Flight deck information system;
— Maintenance information system;
— Passenger cabin information system;
— Miscellaneous information systems.
MODULE 14. PROPULSION

LEVEL
MODULE 14. PROPULSION B2
B2L
14.1 Turbine Engines
(a) Constructional arrangement and operation of turbojet, turbofan, turboshaft and 1
turbopropeller engines;
(b) Electronic Engine control and fuel metering systems (FADEC). 2
14.2 Engine Indicating Systems 2
Exhaust gas temperature/Interstage turbine temperature systems;
Engine speed;
Engine Thrust Indication: Engine Pressure Ratio, engine turbine discharge pressure or jet
pipe pressure systems;
Oil pressure and temperature;
Fuel pressure, temperature and flow;
Manifold pressure;
Engine torque;
Propeller speed.

LEVEL
MODULE 14. PROPULSION B2
B2L
14.3 Starting and Ignition Systems 2
Operation of engine start systems and components;
Ignition systems and components;
Maintenance safety requirements.
MODULE 15. GAS TURBINE ENGINE

LEVEL
A B1
15.1 Fundamentals 1 2
Potential energy, kinetic energy, Newton's laws of motion, Brayton cycle;
The relationship between force, work, power, energy, velocity, acceleration;
Constructional arrangement and operation of turbojet, turbofan, turboshaft,
turboprop.
15.2 Engine Performance — 2
Gross thrust, net thrust, choked nozzle thrust, thrust distribution, resultant thrust,
thrust horsepower, equivalent shaft horsepower, specific fuel consumption;
Engine efficiencies;
By-pass ratio and engine pressure ratio;
Pressure, temperature and velocity of the gas flow;
Engine ratings, static thrust, influence of speed, altitude and hot climate, flat rating,
limitations.
15.3 Inlet 2 2
Compressor inlet ducts
Effects of various inlet configurations;
Ice protection.
15.4 Compressors 1 2
Axial and centrifugal types;
Constructional features and operating principles and applications;
Fan balancing;
Operation:
Causes and effects of compressor stall and surge;
Methods of air flow control: bleed valves, variable inlet guide vanes, variable stator
vanes, rotating stator blades;
Compressor ratio.
15.5 Combustion Section 1 2
Constructional features and principles of operation.
15.6 Turbine Section 2 2
Operation and characteristics of different turbine blade types;
Blade to disk attachment;
Nozzle guide vanes;
Causes and effects of turbine blade stress and creep.
15.7 Exhaust 1 2
Constructional features and principles of operation;
Convergent, divergent and variable area nozzles;
Engine noise reduction;
Thrust reversers.

LEVEL
A B1
15.8 Bearings and Seals — 2
Constructional features and principles of operation.
15.9 Lubricants and Fuels 1 2
Properties and specifications;
Fuel additives;
Safety precautions.
15.10 Lubrication Systems 1 2
System operation/lay-out and components.
15.11 Fuel Systems 1 2
Operation of engine control and fuel metering systems including electronic engine
control (FADEC);
Systems lay-out and components.
15.12 Air Systems 1 2
Operation of engine air distribution and anti-ice control systems, including internal
cooling, sealing and external air services.
15.13 Starting and Ignition Systems 1 2
Operation of engine start systems and components;
Ignition systems and components;
Maintenance safety requirements.
15.14 Engine Indication Systems 1 2
Exhaust Gas Temperature/Interstage Turbine Temperature;
Engine Thrust Indication: Engine Pressure Ratio, engine turbine discharge pressure
or jet pipe pressure systems;
Fuel pressure and flow;
Engine speed;
Vibration measurement and indication;
Torque;
Power.
15.15 Power Augmentation Systems — 1
Operation and applications;
Water injection, water methanol;
Afterburner systems.
15.16 Turbo-prop Engines 1 2
Gas coupled/free turbine and gear coupled turbines;
Reduction gears;
Integrated engine and propeller controls;
Overspeed safety devices.
15.17 Turbo-shaft Engines 1 2
Arrangements, drive systems, reduction gearing, couplings, control systems.
15.18 Auxiliary Power Units (APUs) 1 2
Purpose, operation, protective systems.
15.19 Powerplant Installation 1 2
Configuration of firewalls, cowlings, acoustic panels, engine mounts, anti-vibration
mounts, hoses, pipes, feeders, connectors, wiring looms, control cables and rods,
lifting points and drains.
15.20 Fire Protection Systems 1 2

LEVEL
A B1
Operation of detection and extinguishing systems.
15.21 Engine Monitoring and Ground Operation 1 3
Procedures for starting and ground run-up;
Interpretation of engine power output and parameters;
Trend (including oil analysis, vibration and boroscope) monitoring;
Inspection of engine and components to criteria, tolerances and data specified by
engine manufacturer;
Compressor washing/cleaning;
Foreign Object Damage.
15.22 Engine Storage and Preservation — 2
Preservation and depreservation for the engine and accessories/systems.
MODULE 16. PISTON ENGINE

LEVEL
A B1 B3
16.1 Fundamentals 1 2 2
Mechanical, thermal and volumetric efficiencies;
Operating principles — 2 stroke, 4 stroke, Otto and Diesel;
Piston displacement and compression ratio;
Engine configuration and firing order.
16.2 Engine Performance 1 2 2
Power calculation and measurement;
Factors affecting engine power;
Mixtures/leaning, pre-ignition.
16.3 Engine Construction 1 2 2
Crank case, crank shaft, cam shafts, sumps;
Accessory gearbox;
Cylinder and piston assemblies;
Connecting rods, inlet and exhaust manifolds;
Valve mechanisms;
Propeller reduction gearboxes.
16.4 Engine Fuel Systems
16.4.1 Carburettors 1 2 2
Types, construction and principles of operation;
Icing and heating.
16.4.2 Fuel injection systems 1 2 2
Types, construction and principles of operation.
16.4.3 Electronic engine control 1 2 2
Operation of engine control and fuel metering systems including
electronic engine control (FADEC);
Systems lay-out and components.
16.5 Starting and Ignition Systems 1 2 2
Starting systems, pre-heat systems;
Magneto types, construction and principles of operation;
Ignition harnesses, spark plugs;
Low and high tension systems.

LEVEL
A B1 B3
16.6 Induction, Exhaust and Cooling Systems 1 2 2
Construction and operation of: induction systems including alternate air
systems;
Exhaust systems, engine cooling systems — air and liquid.
16.7 Supercharging/Turbocharging 1 2 2
Principles and purpose of supercharging and its effects on engine
parameters;
Construction and operation of supercharging/turbocharging systems;
System terminology;
Control systems;
System protection.
16.8 Lubricants and Fuels 1 2 2
Properties and specifications;
Fuel additives;
Safety precautions.
16.9 Lubrication Systems 1 2 2
System operation/lay-out and components.
16.10 Engine Indication Systems 1 2 2
Engine speed;
Cylinder head temperature;
Coolant temperature;
Exhaust Gas Temperature;
Fuel pressure and flow;
Manifold pressure.
16.11 Powerplant Installation 1 2 2
Configuration of firewalls, cowlings, acoustic panels, engine mounts, anti-
vibration mounts, hoses, pipes, feeders, connectors, wiring looms, control
cables and rods, lifting points and drains.
16.12 Engine Monitoring and Ground Operation 1 3 2
Procedures for starting and ground run-up;
Interpretation of engine power output and parameters;
Inspection of engine and components: criteria, tolerances, and data
specified by engine manufacturer.
16.13 Engine Storage and Preservation — 2 1
Preservation and depreservation for the engine and accessories/systems.

MODULE 17A. PROPELLER

in module 17B.
LEVEL
MODULE 17A. PROPELLER
A B1
17.1 Fundamentals 1 2
Blade element theory;
High/low blade angle, reverse angle, angle of attack, rotational speed;
Propeller slip;
Aerodynamic, centrifugal, and thrust forces;
Torque;
Relative airflow on blade angle of attack;
Vibration and resonance.
17.2 Propeller Construction 1 2
Construction methods and materials used in wooden, composite and metal
propellers;
Blade station, blade face, blade shank, blade back and hub assembly;
Fixed pitch, controllable pitch, constant speeding propeller;
Propeller/spinner installation.
17.3 Propeller Pitch Control 1 2
Speed control and pitch change methods, mechanical and electrical/electronic;
Feathering and reverse pitch;
Overspeed protection.
17.4 Propeller Synchronising — 2
Synchronising and synchrophasing equipment.
17.5 Propeller Ice Protection 1 2
Fluid and electrical de-icing equipment.
17.6 Propeller Maintenance 1 3
Blade tracking;
Assessment of blade damage, erosion, corrosion, impact damage, delamination;
Propeller treatment/repair schemes;
Propeller engine running.
17.7 Propeller Storage and Preservation 1 2
Propeller preservation and depreservation.

MODULE 17B. PROPELLER

Note: The scope of this Module shall reflect the propeller technology of aeroplanes pertinent to the
B3 category.
LEVEL
MODULE 17B. PROPELLER
B3
17.1 Fundamentals 2
Blade element theory;
High/low blade angle, reverse angle, angle of attack, rotational speed;
Propeller slip;
Aerodynamic, centrifugal, and thrust forces;
Torque;
Relative airflow on blade angle of attack;
Vibration and resonance.
17.2 Propeller Construction 2
Construction methods and material used in wooden, composite and metal propellers;
Blade station, blade face, blade shank, blade back and hub assembly;
Fixed pitch, controllable pitch, constant speeding propeller;
Propeller/spinner installation.
17.3 Propeller Pitch Control 2
Speed control and pitch change methods, mechanical and electrical/electronic;
Feathering and reverse pitch;
Overspeed protection.
17.4 Propeller Synchronising 2
Synchronising and synchrophasing equipment.
17.5 Propeller Ice Protection 2
Fluid and electrical de-icing equipment.
17.6 Propeller Maintenance 2
Blade tracking;
Assessment of blade damage, erosion, corrosion, impact damage, delamination;
Propeller treatment/repair schemes;
Propeller engine running.
17.7 Propeller Storage and Preservation 2
Propeller preservation and depreservation.

Appendix II — Basic examination standard (except for category L

licence)
1. General
1.1. All basic examinations shall be carried out using the multi-choice question format and essay
questions as specified below. The incorrect alternatives shall seem equally plausible to anyone
ignorant of the subject. All of the alternatives shall be clearly related to the question and of
similar vocabulary, grammatical construction and length. In numerical questions, the incorrect
answers shall correspond to procedural errors such as corrections applied in the wrong sense
or incorrect unit conversions: they shall not be mere random numbers.
1.2. Each multi-choice question shall have three alternative answers of which only one shall be the
correct answer and the candidate shall be allowed a time per module which is based upon a
nominal average of 75 seconds per question.
1.3. Each essay question requires the preparation of a written answer and the candidate shall be
allowed 20 minutes to answer each such question.
1.4. Suitable essay questions shall be drafted and evaluated using the knowledge syllabus in
Appendix I Modules 7A, 7B, 9A, 9B and 10.
1.5. Each question will have a model answer drafted for it, which will also include any known
alternative answers that may be relevant for other subdivisions.
1.6. The model answer will also be broken down into a list of the important points known as Key
Points.
1.7. The pass mark for each module and sub-module multi-choice part of the examination is 75 %.
1.8. The pass mark for each essay question is 75 % in that the candidates answer shall contain 75 %
of the required key points addressed by the question and no significant error related to any
required key point.
1.9. If either the multi-choice part only or the essay part only is failed, then it is only necessary to
retake the multi-choice or essay part, as appropriate.
1.10. Penalty marking systems shall not be used to determine whether a candidate has passed.
1.11. A failed module may not be retaken for at least 90 days following the date of the failed module
examination, except in the case of a maintenance training organisation approved in accordance
with Annex IV (Part-147) which conducts a course of retraining tailored to the failed subjects in
the particular module when the failed module may be retaken after 30 days.
1.12. The time periods required by point 66.A.25 apply to each individual module examination, with
the exception of those module examinations which were passed as part of another category
licence, where the licence has already been issued.
1.13. The maximum number of consecutive attempts for each module is three. Further sets of three
attempts are allowed with a 1 year waiting period between sets.
The applicant shall confirm in writing to the approved maintenance training organisation or the
competent authority to which they apply for an examination, the number and dates of attempts
during the last year and the organisation or the competent authority where these attempts took
place. The maintenance training organisation or the competent authority is responsible for
checking the number of attempts within the applicable timeframes.

2. Number of questions per module

2.1. MODULE 1 — MATHEMATICS

Category A: 16 multi-choice and 0 essay questions. Time allowed 20 minutes.
Category B1: 32 multi-choice and 0 essay questions. Time allowed 40 minutes.
Category B2 and B2L: 32 multi-choice and 0 essay questions. Time allowed 40 minutes.
2.2. MODULE 2 — PHYSICS
2.3. MODULE 3 — ELECTRICAL FUNDAMENTALS
2.4. MODULE 4 — ELECTRONIC FUNDAMENTALS
2.5. MODULE 5 — DIGITAL TECHNIQUES/ELECTRONIC INSTRUMENT SYSTEMS
Category B1.1 and B1.3: 40 multi-choice and 0 essay questions. Time allowed 50 minutes.
Category B1.2 and B1.4: 20 multi-choice and 0 essay questions. Time allowed 25 minutes.
2.6. MODULE 6 — MATERIALS AND HARDWARE
2.7. MODULE 7A — MAINTENANCE PRACTICES
Category A: 72 multi-choice and 2 essay questions. Time allowed 90 minutes plus 40 minutes.
Category B1: 80 multi-choice and 2 essay questions. Time allowed 100 minutes plus 40 minutes.

Category B2 and B2L: 60 multi-choice and 2 essay questions. Time allowed 75 minutes plus 40
minutes.
MODULE 7B — MAINTENANCE PRACTICES
2.8. MODULE 8 — BASIC AERODYNAMICS
2.9. MODULE 9A — HUMAN FACTORS
Category A: 20 multi-choice and 1 essay question. Time allowed 25 minutes plus 20 minutes.
Category B1: 20 multi-choice and 1 essay question. Time allowed 25 minutes plus 20 minutes.
Category B2 and B2L: 20 multi-choice and 1 essay question. Time allowed 25 minutes plus 20
minutes.
MODULE 9B — HUMAN FACTORS
2.10. MODULE 10 — AVIATION LEGISLATION
Category A: 32 multi-choice and 1 essay question. Time allowed 40 minutes plus 20 minutes.
Category B1: 40 multi-choice and 1 essay question. Time allowed 50 minutes plus 20 minutes.
Category B2 and B2L: 40 multi-choice and 1 essay question. Time allowed 50 minutes plus 20
minutes.
2.11. MODULE 11A — TURBINE AEROPLANE AERODYNAMICS, STRUCTURES AND SYSTEMS
MODULE 11B — PISTON AEROPLANE AERODYNAMICS, STRUCTURES AND SYSTEMS
MODULE 11C — PISTON AEROPLANE AERODYNAMICS, STRUCTURES AND SYSTEMS
2.12. MODULE 12 — HELICOPTER AERODYNAMICS, STRUCTURES AND SYSTEMS:
2.13. MODULE 13 — AIRCRAFT AERODYNAMICS, STRUCTURES AND SYSTEMS
Category B2: 180 multiple-choice and 0 essay questions. Time allowed: 225 minutes. Questions
and time allowed may be split into two examinations, as appropriate.

Category B2L:
System rating Number of multiple- Time allowed (minutes)
choice questions
Basic requirements 28 35
(Submodules 13.1, 13.2, 13.5 and 13.9)
COM/NAV 24 30
(Submodule 13.4(a))
INSTRUMENTS 20 25
(Submodule 13.8)
AUTOFLIGHT 28 35
(Submodules 13.3(a) and 13.7)
SURVEILLANCE 8 10
(Submodule 13.4(b))
AIRFRAME SYSTEMS 32 40
(Submodules 13.11 to 13.18)
2.14. MODULE 14 — PROPULSION

Category B2 and B2L: 24 multiple-choice and 0 essay questions. Time allowed 30 minutes.
NOTE: The B2L examination for module 14 is only applicable to the ‘Instruments’ and ‘Airframe
Systems’ ratings.
2.15. MODULE 15 — GAS TURBINE ENGINE
2.16. MODULE 16 — PISTON ENGINE
2.17. MODULE 17A — PROPELLER
MODULE 17B — PROPELLER

Appendix III — Aircraft type training and examination standard —

On the job training
1. General
Aircraft type training shall consist of theoretical training and examination, and, except for the category
C ratings, practical training and assessment.
(a) Theoretical training and examination shall comply with the following requirements:
(i) Shall be conducted by a maintenance training organisation appropriately approved in
accordance with Annex IV (Part-147) or, when conducted by other organisations, as
directly approved by the competent authority.
(ii) Shall comply, except as permitted by the differences training provided for in point (c),
with the standard set out in point 3.1 of this Appendix and, if available, the relevant
elements defined in the mandatory part of the operational suitability data established in
accordance with Regulation (EU) No 748/2012.
(iii) In the case of a category C person qualified by holding an academic degree as specified
in point 66.A.30(a)(5), the first relevant aircraft type theoretical training shall be at the
category B1 or B2 level.
(iv) Shall have been started and completed within the 3 years preceding the application for a
type rating endorsement.
(b) Practical training and assessment shall comply with the following requirements:
(i) Shall be conducted by a maintenance training organisation appropriately approved in
accordance with Annex IV (Part-147) or, when conducted by other organisations, as
directly approved by the competent authority.
(ii) Shall comply, except as permitted by the differences training described in point (c), with
the standard set out in point 3.2 of this Appendix and, if available, the relevant elements
defined in the mandatory part of the operational suitability data established in
accordance with Regulation (EU) No 748/2012.
(iii) Shall include a representative cross section of maintenance activities relevant to the
aircraft type.
(iv) Shall include demonstrations using equipment, components, simulators, other training
devices or aircraft.
(v) Shall have been started and completed within the 3 years preceding the application for a
type rating endorsement.
(c) Differences training
(i) Differences training is the training required in order to cover the differences between
two different aircraft type ratings of the same manufacturer as determined by the
Agency.
(ii) Differences training has to be defined on a case-to-case basis taking into account the
requirements contained in this Appendix III in respect of both theoretical and practical
elements of type rating training.
(iii) A type rating shall only be endorsed on a licence after differences training when the
applicant also complies with one of the following conditions:

− having already endorsed on the licence the aircraft type rating from which the
differences are being identified, or
− having completed the type training requirements for the aircraft from which the
differences are being identified.
2. Aircraft type training levels

The three levels listed below define the objectives, the depth of training and the level of knowledge
that the training is intended to achieve.
− Level 1: A brief overview of the airframe, systems and powerplant as outlined in the Systems
Description Section of the Aircraft Maintenance Manual/Instructions for Continued
Airworthiness.
Course objectives: Upon completion of Level 1 training, the student will be able to:
(a) provide a simple description of the whole subject, using common words and examples,
using typical terms and identify safety precautions related to the airframe, its systems
and powerplant;
(b) identify aircraft manuals, maintenance practices important to the airframe, its systems
and powerplant;
(c) define the general layout of the aircraft's major systems;
(d) define the general layout and characteristics of the powerplant;
(e) identify special tooling and test equipment used with the aircraft.
− Level 2: Basic system overview of controls, indicators, principal components, including their
location and purpose, servicing and minor troubleshooting. General knowledge of the
theoretical and practical aspects of the subject.
Course objectives: In addition to the information contained in the Level 1 training, at the
completion of Level 2 training, the student will be able to:
(a) understand the theoretical fundamentals; apply knowledge in a practical manner using
detailed procedures;
(b) recall the safety precautions to be observed when working on or near the aircraft,
powerplant and systems;
(c) describe systems and aircraft handling particularly access, power availability and sources;
(d) identify the locations of the principal components;
(e) explain the normal functioning of each major system, including terminology and
nomenclature;
(f) perform the procedures for servicing associated with the aircraft for the following
systems: Fuel, Power Plants, Hydraulics, Landing Gear, Water/Waste, and Oxygen;
(g) demonstrate proficiency in use of crew reports and on-board reporting systems (minor
troubleshooting) and determine aircraft airworthiness per the MEL/CDL;
(h) demonstrate the use, interpretation and application of appropriate documentation
including instructions for continued airworthiness, maintenance manual, illustrated parts
catalogue, etc.

− Level 3: Detailed description, operation, component location, removal/installation and bite and
troubleshooting procedures to maintenance manual level.
Course objectives: In addition to the information contained in Level 1 and Level 2 training, at
the completion of Level 3 training, the student will be able to:
(a) demonstrate a theoretical knowledge of aircraft systems and structures and
interrelationships with other systems, provide a detailed description of the subject using
theoretical fundamentals and specific examples and to interpret results from various
sources and measurements and apply corrective action where appropriate;
(b) perform system, powerplant, component and functional checks as specified in the
aircraft maintenance manual;
(c) demonstrate the use, interpret and apply appropriate documentation including
structural repair manual, troubleshooting manual, etc.;
(d) correlate information for the purpose of making decisions in respect of fault diagnosis
and rectification to maintenance manual level;
(e) describe procedures for replacement of components unique to aircraft type.
3. Aircraft type training standard

Although aircraft type training includes both theoretical and practical elements, courses can be
approved for the theoretical element, the practical element or for a combination of both.
3.1. Theoretical element

(a) Objective:
On completion of a theoretical training course the student shall be able to demonstrate, to the
levels identified in the Appendix III syllabus, the detailed theoretical knowledge of the aircraft's
applicable systems, structure, operations, maintenance, repair, and troubleshooting according
to approved maintenance data. The student shall be able to demonstrate the use of manuals
and approved procedures, including the knowledge of relevant inspections and limitations.
(b) Level of training:
Training levels are those levels defined in point 2 above.
After the first type course for category C certifying staff all subsequent courses need only be to
level 1.
During a level 3 theoretical training, level 1 and 2 training material may be used to teach the full
scope of the chapter if required. However, during the training the majority of the course
material and training time shall be at the higher level.

(c) Duration:
The theoretical training minimum tuition hours are contained in the following table:
Category Hours
Aeroplanes with a maximum take-off mass above 30000 kg:
B1.1 150
B1.2 120
B2 100
C 30
Aeroplanes with a maximum take-off mass equal or less than 30000 kg and above 5700 kg:
B1.1 120
B1.2 100
B2 100
C 25
1
Aeroplanes with a maximum take-off mass of 5700 kg and below
B1.1 80
B1.2 60
B2 60
C 15
2
Helicopters
B1.3 120
B1.4 100
B2 100
C 25
For the purpose of the table above, a tuition hour means 60 minutes of teaching and exclude
any breaks, examination, revision, preparation and aircraft visit.
These hours apply only to theoretical courses for complete aircraft/engine combinations
according to the type rating as defined by the Agency.
(d) Justification of course duration:
Training courses carried out in a maintenance training organisation approved in accordance
with Annex IV (Part-147) and courses directly approved by the competent authority shall justify
their hour duration and the coverage of the full syllabus by a training needs analysis based on:
− the design of the aircraft type, its maintenance needs and the types of operation,
− detailed analysis of applicable chapters — see contents table in point 3.1(e) below,
− detailed competency analysis showing that the objectives as stated in point 3.1(a) above
are fully met.
Where the training needs analysis shows that more hours are needed, course lengths shall be
longer than the minimum specified in the table.
Similarly, tuition hours of differences courses or other training course combinations (such as
combined B1/B2 courses), and in cases of theoretical type training courses below the figures
1 For non-pressurised piston engine aeroplanes below 2 000 kg MTOM, the minimum duration can be reduced by 50 %.
2
For helicopters in Group 2 (as defined in point 66.A.5), the minimum duration can be reduced by 30 %.

given in point 3.1(c) above, these shall be justified to the competent authority by the training
needs analysis as described above.
In addition, the course must describe and justify the following:
− The minimum attendance required to the trainee, in order to meet the objectives of the
course.
− The maximum number of hours of training per day, taking into account pedagogical and
human factors principles.
If the minimum attendance required is not met, the certificate of recognition shall not be issued.
Additional training may be provided by the training organisation in order to meet the minimum
attendance time.
(e) Content:
As a minimum, the elements in the Syllabus below that are specific to the aircraft type shall be
covered. Additional elements introduced due to type variations, technological changes, etc.
shall also be included.
The training syllabus shall be focused on mechanical and electrical aspects for B1 personnel,
and electrical and avionic aspects for B2.
Level Aeroplanes Aeroplanes Helicopters Helicopters Avionics
Chapters turbine piston turbine piston
Licence category B1 C B1 C B1 C B1 C B2
Introduction module:
05 Time limits/maintenance 1 1 1 1 1 1 1 1 1
checks
06 Dimensions/Areas (MTOM, 1 1 1 1 1 1 1 1 1
etc.)
07 Lifting and Shoring 1 1 1 1 1 1 1 1 1
08 Levelling and weighing 1 1 1 1 1 1 1 1 1
09 Towing and taxiing 1 1 1 1 1 1 1 1 1
10 Parking/mooring, Storing 1 1 1 1 1 1 1 1 1
and Return to Service
11 Placards and Markings 1 1 1 1 1 1 1 1 1
12 Servicing 1 1 1 1 1 1 1 1 1
20 Standard practices — only 1 1 1 1 1 1 1 1 1
type particular
Helicopters
18 Vibration and Noise — — — — 3 1 3 1 —

Analysis (Blade tracking)
60 Standard Practices Rotor — — — — 3 1 3 1 —
62 Rotors — — — — 3 1 3 1 1
62A Rotors — Monitoring and — — — — 3 1 3 1 3
indicating
63 Rotor Drives — — — — 3 1 3 1 1
63A Rotor Drives — — — — — 3 1 3 1 3
Monitoring and indicating
64 Tail Rotor — — — — 3 1 3 1 1


64A Tail rotor — Monitoring — — — — 3 1 3 1 3
and indicating
65 Tail Rotor Drive — — — — 3 1 3 1 1
65A Tail Rotor Drive — — — — — 3 1 3 1 3
66 Folding Blades/Pylon — — — — 3 1 3 1 —
67 Rotors Flight Control — — — — 3 1 3 1 —
53 Airframe Structure — — — — 3 1 3 1 —
(Helicopter)
25 Emergency Flotation — — — — 3 1 3 1 1
Equipment
Airframe structures
51 Standard practices and 3 1 3 1 — — — — 1

structures (damage
classification, assessment and
repair)
53 Fuselage 3 1 3 1 — — — — 1
54 Nacelles/Pylons 3 1 3 1 — — — — 1
55 Stabilisers 3 1 3 1 — — — — 1
56 Windows 3 1 3 1 — — — — 1
57 Wings 3 1 3 1 — — — — 1
27A Flight Control Surfaces 3 1 3 1 — — — — 1
(All)
52 Doors 3 1 3 1 — — — — 1
Zonal and Station 1 1 1 1 1 1 1 1 1
Identification Systems.
Airframe systems:
21 Air Conditioning 3 1 3 1 3 1 3 1 3
21A Air Supply 3 1 3 1 3 1 3 1 2
21B Pressurisation 3 1 3 1 3 1 3 1 3
21C Safety and Warning 3 1 3 1 3 1 3 1 3
Devices
22 Autoflight 2 1 2 1 2 1 2 1 3
23 Communications 2 1 2 1 2 1 2 1 3
24 Electrical Power 3 1 3 1 3 1 3 1 3
25 Equipment and Furnishings 3 1 3 1 3 1 3 1 1
25A Electronic Equipment 1 1 1 1 1 1 1 1 3
including emergency
equipment
26 Fire Protection 3 1 3 1 3 1 3 1 3
27 Flight Controls 3 1 3 1 3 1 3 1 2
27A Sys. Operation: 3 1 — — — — — — 3
Electrical/Fly-by-Wire
28 Fuel Systems 3 1 3 1 3 1 3 1 2


28A Fuel Systems — 3 1 3 1 3 1 3 1 3
29 Hydraulic Power 3 1 3 1 3 1 3 1 2
29A Hydraulic Power — 3 1 3 1 3 1 3 1 3
30 Ice and Rain Protection 3 1 3 1 3 1 3 1 3
31 Indicating/Recording 3 1 3 1 3 1 3 1 3
Systems
31A Instrument Systems 3 1 3 1 3 1 3 1 3
32 Landing Gear 3 1 3 1 3 1 3 1 2
32A Landing Gear — 3 1 3 1 3 1 3 1 3
33 Lights 3 1 3 1 3 1 3 1 3
34 Navigation 2 1 2 1 2 1 2 1 3
35 Oxygen 3 1 3 1 — — — — 2
36 Pneumatic 3 1 3 1 3 1 3 1 2
36A Pneumatic — Monitoring 3 1 3 1 3 1 3 1 3
and indicating
37 Vacuum 3 1 3 1 3 1 3 1 2
38 Water/Waste 3 1 3 1 — — — — 2
41 Water Ballast 3 1 3 1 — — — — 1
42 Integrated modular 2 1 2 1 2 1 2 1 3
avionics
44 Cabin Systems 2 1 2 1 2 1 2 1 3
45 On-Board Maintenance 3 1 3 1 3 1 — — 3
System (or covered in 31)
46 Information Systems 2 1 2 1 2 1 2 1 3
50 Cargo and Accessory 3 1 3 1 3 1 3 1 1
Compartments
Turbine Engine
70 Standard Practices — 3 1 — — 3 1 — — 1
Engines,
70A constructional 3 1 — — 3 1 — — 1
arrangement and operation
(Installation Inlet,
Compressors, Combustion
Section, Turbine Section,
Bearings and Seals,
Lubrication Systems).
70B Engine Performance 3 1 — — 3 1 — — 1
71 Powerplant 3 1 — — 3 1 — — 1
72 Engine Turbine/Turbo 3 1 — — 3 1 — — 1
Prop/Ducted Fan/Unducted
fan
73 Engine Fuel and Control 3 1 — — 3 1 — — 1


75 Air 3 1 — — 3 1 — — 1
76 Engine controls 3 1 — — 3 1 — — 1
78 Exhaust 3 1 — — 3 1 — — 1
79 Oil 3 1 — — 3 1 — — 1
80 Starting 3 1 — — 3 1 — — 1
82 Water Injections 3 1 — — 3 1 — — 1
83 Accessory Gear Boxes 3 1 — — 3 1 — — 1
84 Propulsion Augmentation 3 1 — — 3 1 — — 1
73A FADEC 3 1 — — 3 1 — — 3
74 Ignition 3 1 — — 3 1 — — 3
77 Engine Indicating Systems 3 1 — — 3 1 — — 3
49 Auxiliary Power Units 3 1 — — — — — — 2
(APUs)
Piston Engine
70 Standard Practices — — — 3 1 — — 3 1 1
Engines
70A Constructional — — 3 1 — — 3 1 1
arrangement and operation
(Installation, Carburettors,
Fuel injection systems,
Induction, Exhaust and
Cooling Systems,
Supercharging/Turbochargin,
Lubrication Systems).
70B Engine Performance — — 3 1 — — 3 1 1
71 Powerplant — — 3 1 — — 3 1 1
73 Engine Fuel and Control — — 3 1 — — 3 1 1
76 Engine Control — — 3 1 — — 3 1 1
79 Oil — — 3 1 — — 3 1 1
80 Starting — — 3 1 — — 3 1 1
81 Turbines — — 3 1 — — 3 1 1
82 Water Injections — — 3 1 — — 3 1 1
83 Accessory Gear Boxes — — 3 1 — — 3 1 1
84 Propulsion Augmentation — — 3 1 — — 3 1 1
73A FADEC — — 3 1 — — 3 1 3
74 Ignition — — 3 1 — — 3 1 3
77 Engine Indication Systems — — 3 1 — — 3 1 3
Propellers
60A Standard Practices — 3 1 3 1 — — — — 1

Propeller
61 Propellers/Propulsion 3 1 3 1 — — — — 1
61A Propeller Construction 3 1 3 1 — — — — —
61B Propeller Pitch Control 3 1 3 1 — — — — —


61C Propeller Synchronising 3 1 3 1 — — — — 1
61D Propeller Electronic 2 1 2 1 — — — — 3
control
61E Propeller Ice Protection 3 1 3 1 — — — — —
61F Propeller Maintenance 3 1 3 1 — — — — 1
(f) Multimedia Based Training (MBT) methods may be used to satisfy the theoretical training
element either in the classroom or in a virtual controlled environment subject to the acceptance
of the competent authority approving the training course.
3.2. Practical element

(a) Objective:
The objective of practical training is to gain the required competence in performing safe
maintenance, inspections and routine work according to the maintenance manual and other
relevant instructions and tasks as appropriate for the type of aircraft, for example
troubleshooting, repairs, adjustments, replacements, rigging and functional checks. It includes
the awareness of the use of all technical literature and documentation for the aircraft, the use
of specialist/special tooling and test equipment for performing removal and replacement of
components and modules unique to type, including any on-wing maintenance activity.
(b) Content:
At least 50 % of the crossed items in the table below, which are relevant to the particular aircraft
type, shall be completed as part of the practical training.
Tasks crossed represent subjects that are important for practical training purposes to ensure
that the operation, function, installation and safety significance of key maintenance tasks is
adequately addressed; particularly where these cannot be fully explained by theoretical training
alone. Although the list details the minimum practical training subjects, other items may be
added where applicable to the particular aircraft type.
Tasks to be completed shall be representative of the aircraft and systems both in complexity
and in the technical input required to complete that task. While relatively simple tasks may be
included, other more complex tasks shall also be incorporated and undertaken as appropriate
to the aircraft type.
Glossary of the table: LOC: Location; FOT: Functional/Operational Test; SGH: Service and
Ground Handling; R/I: Removal/Installation; MEL: Minimum Equipment List; TS:
TroubleShooting.
Chapters B1/B2 B1 B2
LOC FOT SGH R/I MEL TS FOT SGH R/I MEL TS
Introduction module:
5 Time X/X — — — — — — — — — —
limits/maintenance
checks

6 Dimensions/Areas X/X — — — — — — — — — —
(MTOM, etc.)
7 Lifting and Shoring X/X — — — — — — — — — —
8 Levelling and X/X — X — — — — X — — —
weighing
9 Towing and taxiing X/X — X — — — — X — — —
10 Parking/mooring, X/X — X — — — — X — — —
Storing and Return to
Service
11 Placards and X/X — — — — — — — — — —
Markings
12 Servicing X/X — X — — — — X — — —
20 Standard practices X/X — X — — — — X — — —
— only type
particular
Helicopters:
18 Vibration and X/— — — — — X — — — — —

Noise Analysis (Blade
tracking)
60 Standard Practices X/X — X — — — — X — — —
Rotor — only type
specific
62 Rotors X/— — X X — X — — — — —
62A Rotors — X/X X X X X X — — X — X
Monitoring and
indicating
63 Rotor Drives X/— X — — — X — — — — —
63A Rotor Drives — X/X X — X X X — — X — X
Monitoring and
indicating
64 Tail Rotor X/— — X — — X — — — — —
64A Tail rotor - X/X X — X X X — — X — X
Monitoring and
indicating
65 Tail Rotor Drive X/— X — — — X — — — — —
65A Tail Rotor Drive X/X X — X X X — — X — X
— Monitoring and
indicating
66 Folding X/— X X — — X — — — — —
Blades/Pylon
67 Rotors Flight X/— X X — X X — — — — —
Control
53 Airframe
Structure
(Helicopter)
Note: covered under
Airframe structures

25 Emergency X/X X X X X X X X — — —
Flotation Equipment
Airframe structures:
51 Standard Practices
and Structures
(damage
classification,
assessment and
repair)
53 Fuselage X/— — — — — X — — — — —
54 Nacelles/Pylons X/— — — — — — — — — — —
55 Stabilisers X/— — — — — — — — — — —
56 Windows X/— — — — — X — — — — —
57 Wings X/— — — — — — — — — — —
27A Flight Control X/— — — — — X — — — — —
Surfaces
52 Doors X/X X X — — — — X — — —
Airframe systems:
21 Air Conditioning X/X X X — X X X X — X X

21A Air Supply X/X X — — — — X — — — —
21B Pressurisation X/X X — — X X X — — X X
21C Safety and X/X — X — — — — X — — —
warning Devices
22 Autoflight X/X — — — X — X X X X X
23 Communications X/X — X — X — X X X X X
24 Electrical Power X/X X X X X X X X X X X
25 Equipment and X/X X X X — — X X X — —
Furnishings
25A Electronic X/X X X X — — X X X — —
Equipment including
emergency
equipment
26 Fire Protection X/X X X X X X X X X X X
27 Flight Controls X/X X X X X X X — — — —
27A Sys. Operation: X/X X X X X — X — X — X
Electrical/Fly-by-Wire
28 Fuel Systems X/X X X X X X X X — X —
28A Fuel Systems — X/X X — — — — X — X — X
Monitoring and
indicating
29 Hydraulic Power X/X X X X X X X X — X —
29A Hydraulic Power X/X X — X X X X — X X X
— Monitoring and
indicating

30 Ice and Rain X/X X X — X X X X — X X
Protection
31 X/X X X X X X X X X X X
Indicating/Recording
Systems
31A Instrument X/X X X X X X X X X X X
Systems
32 Landing Gear X/X X X X X X X X X X —
32A Landing Gear — X/X X — X X X X — X X X
Monitoring and
indicating
33 Lights X/X X X — X — X X X X —
34 Navigation X/X — X — X — X X X X X
35 Oxygen X/— X X X — — X X — — —
36 Pneumatic X/— X — X X X X — X X X
36A Pneumatic — X/X X X X X X X X X X X
Monitoring and
indicating
37 Vacuum X/— X — X X X — — — — —
38 Water/Waste X/— X X — — — X X — — —
41 Water Ballast X/— — — — — — — — — — —
42 Integrated X/X — — — — — X X X X X
modular avionics
44 Cabin Systems X/X — — — — — X X X X X
45 On-Board X/X X X X X X X X X X X
Maintenance System
(or covered in 31)
46 Information X/X — — — — — X — X X X
Systems
50 Cargo and X/X — X — — — — — — — —
Accessory
Compartments
Turbine/Piston
Engine Module:
70 Standard Practices — — X — — — — X — — —
— Engines — only
type particular
70A Constructional X/X — — — — — — — — — —
arrangement and
operation
(Installation Inlet,
Compressors,
Combustion Section,
Turbine Section,
Bearings and Seals,
Lubrication Systems)

73A FADEC Systems X/X X — X X X X X X X X
74 Ignition X/X X — — — — X — — — —
76 Engine Controls X/— X — — — X — — — — —
77 Engine Indicating X/X X — — X X X — — X X
78 Exhaust X/— X — — X X — — — — —
79 Oil X/— — X X — — — — — — —
80 Starting X/— X — — X X — — — — —
81 Turbines X/— X X X — X — — — — —
82 Water Injection X/— X — — — — — — — — —
83 Accessory X/— — X X — — — — — — —
Gearboxes
84 Propulsion X/— X — — — — — — — — —
Augmentation
Propellers:
60A Standard — — — X — — — — — — —
Practices — Propeller
61 Propellers/ X/X X X — X X — — — — —
Propulsion
61A Propeller X/X — X — — — — — — — —
Construction
61B Propeller Pitch X/— X — X X X — — — — —
Control
61C Propeller X/— X — — — X — — — X —
Synchronising
61D Propeller X/X X X X X X X X X X X
Electronic control
61E Propeller Ice X/— X — X X X — — — — —
Protection
61F Propeller X/X X X X X X X X X X X
Maintenance
4. Type training examination and assessment standard
4.1. Theoretical element examination standard

After the theoretical portion of the aircraft type training has been completed, a written examination
shall be performed, which shall comply with the following:
(a) Format of the examination is of the multi-choice type. Each multi-choice question shall have 3
alternative answers of which only one shall be the correct answer. The total time is based on
the total number of questions and the time for answering is based upon a nominal average of
90 seconds per question.
(b) The incorrect alternatives shall seem equally plausible to anyone ignorant of the subject. All the
alternatives shall be clearly related to the question and of similar vocabulary, grammatical
construction and length.

(c) In numerical questions, the incorrect answers shall correspond to procedural errors such as the
use of incorrect sense (+ versus -) or incorrect measurement units. They shall not be mere
random numbers.
(d) The level of examination for each chapter1 shall be the one defined in point 2 ‘Aircraft type
training levels’. However, the use of a limited number of questions at a lower level is acceptable.
(e) The examination shall be of the closed book type. No reference material is permitted. An
exception will be made for the case of examining a B1 or B2 candidate's ability to interpret
technical documents.
(f) The number of questions shall be at least 1 question per hour of instruction. The number of
questions for each chapter and level shall be proportionate to:
− the effective training hours spent teaching at that chapter and level,
− the learning objectives as given by the training needs analysis.
The competent authority of the Member State will assess the number and the level of the
questions when approving the course.
(g) The minimum examination pass mark is 75 %. When the type training examination is split in
several examinations, each examination shall be passed with at least a 75 % mark. In order to
be possible to achieve exactly a 75 % pass mark, the number of questions in the examination
shall be a multiple of 4.
(h) Penalty marking (negative points for failed questions) is not to be used.
(i) End of module phase examinations cannot be used as part of the final examination unless they
contain the correct number and level of questions required.
4.2. Practical element assessment standard

After the practical element of the aircraft type training has been completed, an assessment must be
performed, which must comply with the following:
(a) The assessment shall be performed by designated assessors appropriately qualified.
(b) The assessment shall evaluate the knowledge and skills of the trainee.
5. Type examination standard

Type examination shall be conducted by training organisations appropriately approved under Part-
147 or by the competent authority.
The examination shall be oral, written or practical assessment based, or a combination thereof and it
shall comply with the following requirements:
(a) Oral examination questions shall be open.
(b) Written examination questions shall be essay type or multi-choice questions.
(c) Practical assessment shall determine a person's competence to perform a task.
1
For the purpose of this point 4, a ‘chapter’ means each one of the rows preceded by a number in the table contained in point 3.1(e).

(d) Examinations shall be on a sample of chapters1 drawn from point 3 type training/examination
syllabus, at the indicated level.
(e) The incorrect alternatives shall seem equally plausible to anyone ignorant of the subject. All of
the alternatives shall be clearly related to the question and of similar vocabulary, grammatical
construction and length.
(f) In numerical questions, the incorrect answers shall correspond to procedural errors such as
corrections applied in the wrong sense or incorrect unit conversions: they shall not be mere
random numbers.
(g) The examination shall ensure that the following objectives are met:
1. Properly discuss with confidence the aircraft and its systems.
2. Ensure safe performance of maintenance, inspections and routine work according to the
maintenance manual and other relevant instructions and tasks as appropriate for the
type of aircraft, for example troubleshooting, repairs, adjustments, replacements, rigging
and functional checks such as engine run, etc., if required.
3. Correctly use all technical literature and documentation for the aircraft.
4. Correctly use specialist/special tooling and test equipment, perform removal and
replacement of components and modules unique to type, including any on-wing
maintenance activity
(h) The following conditions apply to the examination:
1. The maximum number of consecutive attempts is three. Further sets of three attempts
are allowed with a 1 year waiting period between sets. A waiting period of 30 days is
required after the first failed attempt within one set, and a waiting period of 60 days is
required after the second failed attempt.
The applicant shall confirm in writing to the maintenance training organisation or the
competent authority to which they apply for an examination, the number and dates of
attempts during the last year and the maintenance training organisation or the
competent authority where these attempts took place. The maintenance training
organisation or the competent authority is responsible for checking the number of
attempts within the applicable timeframes.
2. The type examination shall be passed and the required practical experience shall be
completed within the 3 years preceding the application for the rating endorsement on
the aircraft maintenance licence.
3. Type examination shall be performed with at least one examiner present. The
examiner(s) shall not have been involved in the applicant's training.
(i) A written and signed report shall be made by the examiner(s) to explain why the candidate has
passed or failed.
1
For the purpose of this point 5, a ‘chapter’ means each one of the rows preceded by a number in the tables contained in points 3.1(e)
and 3.2(b).

6. On the Job Training

On the Job Training (OJT) shall be approved by the competent authority who has issued the licence.
It shall be conducted at and under the control of a maintenance organisation appropriately approved
for the maintenance of the particular aircraft type and shall be assessed by designated assessors
appropriately qualified.
It shall have been started and completed within the 3 years preceding the application for a type rating
endorsement.
(a) Objective:
The objective of OJT is to gain the required competence and experience in performing safe
maintenance.
(b) Content:
OJT shall cover a cross section of tasks acceptable to the competent authority. The OJT tasks to
be completed shall be representative of the aircraft and systems both in complexity and in the
technical input required to complete that task. While relatively simple tasks may be included,
other more complex maintenance tasks shall also be incorporated and undertaken as
appropriate to the aircraft type.
Each task shall be signed off by the student and countersigned by a designated supervisor. The
tasks listed shall refer to an actual job card/work sheet, etc.
The final assessment of the completed OJT is mandatory and shall be performed by a designated
assessor appropriately qualified.
The following data shall be addressed on the OJT worksheets/logbook:
1. Name of Trainee;
2. Date of Birth;
3. Approved Maintenance Organisation;
4. Location;
5. Name of supervisor(s) and assessor, (including licence number if applicable);
6. Date of task completion;
7. Description of task and job card/work order/tech log, etc.;
8. Aircraft type and aircraft registration;
9. Aircraft rating applied for.
In order to facilitate the verification by the competent authority, demonstration of the OJT shall
consist of (i) detailed worksheets/logbook and (ii) a compliance report demonstrating how the
OJT meets the requirement of this Part.

AMC to Appendix III to Part-66 ‘Aircraft Type Training and

Examination Standard. On-the-Job Training’
Aircraft Type Training and On-the-Job Training

The theoretical and practical training providers, as well as the OJT provider, may contract the services
of a language translator in the case where training is imparted to students not conversant in the
language of the training material. Nevertheless, it remains essential that the students understand all
the relevant maintenance documentation.
During the performance of examinations and assessments, the assistance of the translator should be
limited to the translation of the questions, but should not provide clarifications or help in relation to
those questions.
AMC to Section 1 of Appendix III to Part-66 ‘Aircraft Type Training

and Examination Standard. On-the-Job Training’
Aircraft Type Training

1. Aircraft type training may be sub-divided in airframe and/or powerplant and/or
avionics/electrical systems type training courses.
− Airframe type training course means a type training course including all relevant aircraft
structure and electrical and mechanical systems excluding the powerplant.
− Powerplant type training course means a type training course on the bare engine,
including the build-up to a quick engine change unit.
− The interface of the engine/airframe systems should be addressed by either airframe or
powerplant type training course. In some cases, such as for general aviation, it may be
more appropriate to cover the interface during the airframe course due to the large
variety of aircraft that can have the same engine type installed.
− Avionics/electrical systems type training course means type training on avionics and
electrical systems covered by but not necessarily limited to ATA (Air Transport
Association) Chapters 22, 23, 24, 25, 27, 31, 33, 34, 42, 44, 45, 46, 73 and 77 or equivalent.
2. Practical training may be performed either following or integrated with the theoretical
elements. However, it should not be performed before theoretical training.
3. The content of the theoretical and practical training should:
− address the different parts of the aircraft which are representative of the structure, the
systems/components installed and the cabin; and
− include training on the use of technical manuals, maintenance procedures and the
interface with the operation of the aircraft.
Therefore it should be based on the following elements:
− Type design including relevant type design variants, new technology and techniques;
− Feedback from in-service difficulties, occurrence reporting, etc;
− Significant applicable airworthiness directives and service bulletins;

− Known human factor issues associated with the particular aircraft type;
− Use of common and specific documentation, (when applicable, such as MMEL, AMM,
MPD, TSM, SRM, WD, AFM, tool handbook), philosophy of the troubleshooting, etc.;
− Knowledge of the maintenance on-board reporting systems and ETOPS maintenance
conditions where applicable;
− Use of special tooling and test equipment and specific maintenance practises including
critical safety items and safety precautions;
− Significant and critical tasks/aspects from the MMEL, CDL, Fuel Tank Safety (FTS),
airworthiness limitation items (ALI) including Critical Design Configuration Control
Limitations (CDCCL), CMR and all ICA documentation such as MRB, MPD, SRM, AMM, etc.,
when applicable.
− Maintenance actions and procedures to be followed as a consequence of specific
certification requirements, such as, but not limited to, RVSM (Reduced Vertical
Separation Minimum) and NVIS (Night Vision Imaging Systems);
− Knowledge of relevant inspections and limitations as applicable to the effects of
environmental factors or operational procedures such as cold and hot climates, wind,
moisture, sand, de-icing / anti-icing, etc.
The type training does not necessarily need to include all possible customer options
corresponding to the type rating described in the Appendix I to AMC to Part-66.
4. Limited avionic system training should be included in the category B1 type training as the B1
privileges include work on avionics systems requiring simple tests to prove their serviceability.
5. Electrical systems should be included in both categories of B1 and B2 type training.
6. The theoretical and practical training should be complementary and may be:
− Integrated or split
− Supported by the use of training aids, such as trainers, virtual aircraft, aircraft
components, synthetic training devices (STD), computer based training devices (CBT), etc.
AMC to Paragraphs 1(b), 3.2 and 4.2 of Appendix III to Part-66

‘Aircraft Type Training and Examination Standard. On-the-Job
Training’
Practical Element of the Aircraft Type Training

1. The practical training may include instruction in a classroom or in simulators but part of the
practical training should be conducted in a real maintenance or manufacturer environment.
2. The tasks should be selected because of their frequency, complexity, variety, safety, criticality,
novelty, etc. The selected tasks should cover all the chapters described in the table contained
in paragraph 3.2 of Appendix III to Part-66.
3. The duration of the practical training should ensure that the content of training required by
paragraph 3.2 of Appendix III to Part-66 is completed.
Nevertheless, for aeroplanes with a MTOM equal or above 30000kg, the duration for the
practical element of a type rating training course should not be less than two weeks unless a

shorter duration meeting the objectives of the training and taking into account pedagogical
aspects (maximum duration per day) is justified to the competent authority.
4. The organisation providing the practical element of the type training should provide trainees a
schedule or plan indicating the list of tasks to be performed under instruction or supervision. A
record of the tasks completed should be entered into a logbook which should be designed such
that each task or group of tasks may be countersigned by the designated assessor. The logbook
format and its use should be clearly defined.
5. In paragraph 4.2 of Appendix III to Part-66, the term ‘designated assessors appropriately
qualified’ means that the assessors should demonstrate training and experience on the
assessment process being undertaken and be authorised to do so by the organisation.
Further guidance about the assessment and the designated assessors is provided in Appendix
III to AMC to Part-66.
6. The practical element (for powerplant and avionic systems) of the Type Rating Training may be
subcontracted by the approved Part-147 organisation under its quality system according to the
provisions of 147.A.145(d)3 and the corresponding Guidance Material.
AMC to Paragraph 1(c) of Appendix III to Part-66 ‘Aircraft Type

Training and Examination Standard. On-the-Job Training’
Differences Training
Approved difference training is not required for different variants within the same aircraft type rating
(as specified in Appendix I to AMC to Part-66) for the purpose of type rating endorsement on the
aircraft maintenance licence.
However, this does not necessarily mean that no training is required before a certifying staff
authorisation can be issued by the maintenance organisation (refer to AMC 66.A.20(b)3).
AMC to point 3.1(d) of Appendix III to Part-66 ‘Aircraft Type

Training and Examination Standard. On-the-Job Training’
Training Needs Analysis for the Theoretical Element of the Aircraft Type Training
1. The minimum duration for the theoretical element of the type rating training course, as
described in Appendix III to Part-66, has been determined based on:
− generic categories of aircraft and minimum standard equipment fit
− the estimated average duration of standard courses imparted in Europe
2. The purpose of the Training Needs Analysis (TNA) is to adapt and justify the duration of the
course for a specific aircraft type. This means that the TNA is the main driver for determining
the duration of the course, regardless of whether it is above or below the minimum duration
described in Appendix III to Part-66.
In the particular case of type training courses approved on the basis of the requirements valid
before Regulation (EU) No 1149/2011 was applicable (1 August 2012) and having a duration for
the theoretical element equal to or above the minimum duration contained in paragraph 3.1(c)
of Appendix III to Part-66, it is acceptable that the TNA only covers the differences introduced

by Regulation (EU) No 1149/2011 in paragraph 3.1(e) ‘Content’ and the criteria introduced in
paragraph 3.1(d) ‘Justification of course duration’ related to the minimum attendance and the
maximum number of training hours per day. This TNA may result in a change in the duration of
the theoretical element.
3. The content and the duration deriving from this TNA may be supported by an analysis from the
Type Certificate holder.
4. In order to approve a reduction of such minimum duration, the evaluation done by the
competent authority should be performed on a case-by-case basis appropriate to the aircraft
type. For example, while it would be exceptional for a theoretical course for a transport
category complex motor-powered aircraft such as an A330 or B757 to be below the minimum
duration shown, it would not necessarily be exceptional in the case of a General Aviation (GA)
business aircraft such as a Learjet 45 or similar. Typically the TNA for a GA aircraft course would
demonstrate that a course of a shorter duration satisfies the requirements.
5. When developing the TNA the following should be considered:
(a) The TNA should include an analysis identifying all the areas and elements where there is
a need for training as well as the associated learning objectives, considering the design
philosophy of the aircraft type, the operational environment, the type of operations and
the operational experience. This analysis should be written in a manner which provides a
reasonable understanding of which areas and elements constitute the course in order to
meet the learning objectives.
(b) As a minimum, the Training Need Analysis (TNA) should take into account all the
applicable elements contained in paragraph 3.1 of Part-66 Appendix III and associated
AMCs.
(c) The TNA should set-up the course content considering the Appendix III objectives for each
level of training and the prescribed topics in the theoretical element table contained in
paragraph 3.1 of Part-66 Appendix III.
(d) For each chapter described in the theoretical element table contained in paragraph 3.1
of Part-66 Appendix III, the corresponding training time should be recorded.
(e) Typical documents to be used in order to identify the areas and elements where there is
a need for training typically include, among others, the Aircraft Maintenance Manual,
MRB report, CMRs, airworthiness limitations, Troubleshooting Manual, Structural Repair
Manual, Illustrated Parts Catalogue, Airworthiness Directives and Service Bulletins.
(f) During the analysis of these documents:
− Consideration should be given to the following typical activities:
− Activation/reactivation;
− Removal/Installation;
− Testing;
− Servicing;
− Inspection, check and repairs;
− Troubleshooting / diagnosis.

− For the purpose of identifying the specific elements constituting the training
course, it is acceptable to use a filtering method based on criteria such as:
− Frequency of the task;
− Human factor issues associated to the task;
− Difficulty of the task;
− Criticality and safety impact of the task;
− In-service experience;
− Novel or unusual design features (not covered by Part-66 Appendix I);
− Similarities with other aircraft types;
− Special tests and tools/equipment.
− It is acceptable to follow an approach based on:
− Tasks or groups of tasks, or
− Systems or subsystems or components
(g) The TNA should:
− Identify the learning objectives for each task, group of tasks, system, subsystem or
component;
− Associate the identified tasks to be trained to the regulatory requirements (table
in Paragraph 3.1 of Appendix III to Part-66);
− Organise the training into modules in a logical sequence (adequate combination of
chapters as defined in Appendix III of Part-66);
− Determine the sequence of learning (within a lesson and for the whole syllabus);
− Identify the scope of information and level of detail with regard the minimum
standard to which the topics of the TNA should be taught according to the set-up
objectives.
− Address the following:
− Description of each system/component including the structure (where
applicable);
− System/component operation taking into account:
(a) Complexity of the system (e.g. the need of further break down into
subsystems, etc.);
(b) Design specifics which may require more detailed presentation or may
contribute to maintenance errors;
(c) Normal and emergency functioning;
(d) Troubleshooting;
(e) Interpretation of indications and malfunctions;
(f) Use of maintenance publications;

(g) Identification of special tools and equipment required for servicing

and maintaining the aircraft;
(h) Maintenance Practices;
(i) Routine inspections, functional or operational tests,
rigging/adjustment, etc.
− Describe the following:
− The instructional methods and equipment, teaching methods and blending
of the teaching methods in order to ensure the effectiveness of the training;
− The maintenance training documentation/material to be delivered to the
student;
− Facilitated discussions, questioning session, additional practiced-oriented
training, etc.;
− The homework, if developed;
− The training provider’s resources available to the learner.
(h) It is acceptable to differentiate between issues which have to be led by an instructor and
issues which may be delivered through interactive simulation training devices and/or
covered by web based elements. Overall time of the course will be allocated accordingly.
(i) The maximum number of training hours per day for the theoretical element of type
training should not be more than 6 hours. A training hour means 60 minutes of tuition
excluding any breaks, examination, revision, preparation and aircraft visit. In exceptional
cases, the competent authority may allow deviation from this standard when it is
properly justified that the proposed number of hours follows pedagogical and human
factors principles. These principles are especially important in those cases where:
− Theoretical and practical training are performed at the same time;
− Training and normal maintenance duty/apprenticeship are performed at the same
time.
(j) The minimum participation time for the trainee in order to meet the objectives of the
course should not be less than 90 % of the tuition hours of the theoretical training course.
Additional training may be provided by the training organisation in order to meet the
minimum participation time. If the minimum participation defined for the course is not
met, a certificate of recognition should not be issued.
(k) The TNA is a living process and should be reviewed/updated based on operation
feedback, maintenance occurrences, airworthiness directives, major service bulletins
impacting maintenance activities or requiring new competencies for mechanics, alert
service bulletins, feedback from trainees or customer satisfaction, evolution of the
maintenance documentation such as MRBs, MPDs, MMs, etc. The frequency at which the
TNA should be reviewed/updated is left to the discretion of the organisation conducting
the course.
NOTE: The examination is not part of the TNA. However, it should be prepared in accordance with the
learning objectives described in the TNA.


Type Examination Standard

This Section 5 ‘Type Examination Standard’ does not apply to the examination performed as part of
type training. This Section only applies to those cases where type examination is performed as a
substitute for type training.

On-the-Job Training (OJT)

1. ‘A maintenance organisation appropriately approved for the maintenance of the particular
aircraft type’ means a Part-145, M.A. Subpart F or Part-CAO approved maintenance
organisation holding an A rating for such aircraft.
2. The OJT should include one to one supervision and should involve actual work task performance
on aircraft/components, covering line and/or base maintenance tasks.
3. The use of simulators for OJT should not be allowed.
4. The OJT should cover at least 50% of the tasks contained in Appendix II to AMC to Part-66. Some
tasks should be selected from each paragraph of the Appendix II list. Tasks should be selected
among those applicable to the type of aircraft and licence (sub)category applied for. Other tasks
than those in the Appendix II may be considered as a replacement when they are relevant.
Typically, in addition to the variety and the complexity, the OJT tasks should be selected because
of their frequency, safety, novelty, etc.
5. Up to 50% of the required OJT may be undertaken before the aircraft theoretical type training
starts.
6. The organisation providing the on-the-job training should provide trainees a schedule or plan
indicating the list of tasks to be performed under supervision. A record of the tasks completed
should be entered into a logbook which should be designed such that each task or group of
tasks is countersigned by the corresponding supervisor. The logbook format and its use should
be clearly defined.
7. Regarding the day-to-day supervision of the OJT programme in the approved maintenance
organisation and the role of the supervisor(s), the following should be considered:
− It is sufficient that the completion of individual OJT tasks is confirmed by the direct
supervisor(s), without being necessary the direct evaluation of the assessor.
− During the day-to-day OJT performance, the supervision aims at overseeing the complete
process, including task completion, use of manuals and procedures, observance of safety
measures, warnings and recommendations and adequate behaviour in the maintenance
environment.
− The supervisor(s) should personally observe the work being performed to ensure the safe
completeness and should be readily available for consultation, if needed during the OJT
performance.

− The supervisor(s) should countersign the tasks and release the maintenance tasks as the
trainee is still not qualified to do so.
− The supervisor(s) should therefore:
− have certifying staff or support staff privileges relevant to the OJT tasks;
− be competent for the selected tasks;
− be safety-orientated;
− be capable to coach (setting objectives, giving training, performing supervision,
evaluating, handling trainee’s reactions and cultural issues, managing objectively
and positively debriefing sessions, determining the need for extra training or
reorientate the training, reporting, etc.);
− be designated by the approved maintenance organisation to carry out the
supervision.
8. Regarding the assessor, the following should be considered:
− The function of the assessor, as described in Section 6 of Appendix III to Part-66, is to
conduct the final assessment of the completed OJT. This assessment should include
confirmation of the completion of the required diversity and quantity of OJT and should
be based on the supervisor(s) reports and feedback.
− In Section 6 of Appendix III to Part-66, the term ‘designated assessor appropriately
qualified’ means that the assessor should demonstrate training and experience on the
assessment process being undertaken and should be authorised to do so by the
organisation. Further guidance about the assessment and the designated assessors is
provided in Appendix III to AMC to Part-66.
9. The procedures for OJT of a Part-145 organisation should be included into the approved
maintenance organisation exposition (Chapter 3.20, as indicated in AMC1 145.A.70(a)).
However, since these procedures are approved by the competent authority of the maintenance
organisation, and providing training is not one of the privileges of a maintenance organisation,
they can only be used when the licensing authority is the same as the competent authority of
the maintenance organisation. In other cases, it is up to the licensing authority to decide
whether it accepts such procedures for the purpose of approving the OJT (refer to
AMC 66.B.115).

Appendix IV — Experience requirements for extending a Part-66

aircraft maintenance licence
The table below shows the experience requirements for adding a new category or subcategory to an
existing Part-66 licence.
The experience shall be practical maintenance experience in operating aircraft in the subcategory
relevant to the application.
The experience requirement will be reduced by 50 % if the applicant has completed an approved
Part-147 course relevant to the subcategory.
To
A1 A2 A3 A4 B1.1 B1.2 B1.3 B1.4 B2 B2L B3
From
A1 — 6 6 6 2 years 6 2 years 1 year 2 years 1 year 6
months months months months months
A2 6 — 6 6 2 years 6 2 years 1 year 2 years 1 year 6
A3 6 6 — 6 2 years 1 year 2 years 6 2 years 1 year 1 year
months months months months
A4 6 6 6 — 2 years 1 year 2 years 6 2 years 1 year 1 year
B1.1 None 6 6 6 — 6 6 6 1 year 1 year 6
months months months months months months months
B1.2 6 None 6 6 2 years — 2 years 6 2 years 1 year None
B1.3 6 6 None 6 6 6 — 6 1 year 1 year 6
months months months months months months months
B1.4 6 6 6 None 2 years 6 2 years — 2 years 1 year 6
B2 6 6 6 6 1 year 1 year 1 year 1 year — — 1 year
B2L 6 6 6 6 1 year 1 year 1 year 1 year 1 year — 1 year
B3 6 None 6 6 2 years 6 2 years 1 year 2 years 1 year —

Appendix V — Application Form — EASA Form 19

1. This Appendix contains an example of the form used for applying for the aircraft maintenance
licence referred to in Annex III (Part-66).
2. The competent authority of the Member State may modify the EASA Form 19 only to include
additional information necessary to support the case where the national requirements permit
or require the aircraft maintenance licence issued in accordance with Annex III (Part-66) to be
used outside the requirements of this Regulation.
APPLICATION FOR INITIAL/AMENDMENT/RENEWAL OF PART-66 AIRCRAFT EASA FORM 19
MAINTENANCE LICENCE (AML)
APPLICANT’S DETAILS:
Name: ………………………………………………………………………………………………………………………………………………………
Address: ……………………………………………………………………………………………………………………………………………………
Tel: ……………………………………………………………………….. E-mail: …………………………………………………………………….
Nationality: …………………………………………………………... Date and Place of Birth: ………………………………………….
PART-66 AML DETAILS (if applicable):
Licence No: …………………………………………………………………. Date of Issue: …………………………………………………….
EMPLOYER’S DETAILS:
Name: ………………………………………………………………………………………………………………………………………………………
Address: ……………………………………………………………………………………………………………………………………………………
………………………………………………………………………………………………………………………………………………………………….
Maintenance Organisation Approval Reference: ………………………………………………………………………………………
Tel: …………………………………………………………………………….. Fax: ……………………………………………………………………
APPLICATION FOR: (Tick relevant boxes)
Initial AML Amendment of AML Renewal of AML
(Sub)categories A B1 B2 B2L B3 C L (see below)
Aeroplane Turbine
Aeroplane Piston
Helicopter Turbine
Helicopter Piston
Avionics See system ratings below
Piston engine non-pressurised aeroplanes of MTOM of 2t and below
Complex motor-powered aircraft
Aircraft other than complex motor-powered aircraft
System ratings for B2L licence:
1. autoflight
2. instruments
3. com/nav
4. surveillance
5. airframe systems
L-licence subcategories:
L1C: Composite sailplanes
L1: Sailplanes
L2C: Composite powered sailplanes and composite ELA1 aeroplanes
L2: Powered sailplanes and ELA1 aeroplanes

L3H: Hot-air balloons

L3G: Gas balloons
L4H: Gas balloons
L4H: Hot-air airships
L4G: ELA2 gas airships
L5: Gas airship other than ELA2
Type endorsements/Rating endorsement/Limitation removal (if applicable):
…………………………………………………………………………………………………………………………………………………………………….
I wish to apply for initial/amendment of/renewal of Part-66 AML, as indicated, and confirm that the
information contained in this form was correct at the time of application.
I herewith confirm that:
1. I am not holding any Part-66 AML issued in another Member State;
2. I have not applied for any Part-66 AML in another Member State; and
3. I never had a Part-66 AML issued in another Member State which was revoked or suspended in any
other Member State.
I also understand that any incorrect information could disqualify me from holding a Part-66 AML.
Signed: …………………………………………………………………. Name: ……………………………………………………………………….
Date: ………………………………………………………………………………………………………………………………………………………….
I wish to claim the following credits (if applicable):
…………………………………………………………………………………………………………………………………………………………………….
…………………………………………………………………………………………………………………………………………………………………….
…………………………………………………………………………………………………………………………………………………………………….
Experience credits for Part-147 training
…………………………………………………………………………………………………………………………………………………………………….
…………………………………………………………………………………………………………………………………………………………………….
…………………………………………………………………………………………………………………………………………………………………….
Examination credits for equivalent exam certificates
…………………………………………………………………………………………………………………………………………………………………….
…………………………………………………………………………………………………………………………………………………………………….
…………………………………………………………………………………………………………………………………………………………………….
Please enclose all relevant certificates
Recommendation (if applicable): It is hereby certified that the applicant has met the relevant Part-66
maintenance knowledge and experience requirements and it is recommended that the competent authority
grants or endorses the Part-66 AML.
Signed: .............................................................. Name: ..................................................................................

Position: ........................................................... Date: ....................................................................................
EASA Form 19 Issue 5

Appendix VI — Aircraft Maintenance Licence referred to in Annex III

(Part-66) — EASA Form 26
1. An example of the aircraft maintenance licence referred to in Annex III (Part-66) can be found
on the following pages.
2. The document shall be printed in the standardised form shown but may be reduced in size to
allow it being generated by computer. When the size is reduced, care shall be taken to ensure
that sufficient space is available in those places where official seals or stamps are required.
Computer-generated documents need not have all the boxes incorporated when any such box
remains blank, so long as the document can clearly be recognised as an aircraft maintenance
licence issued in accordance with Annex III (Part-66).
3. The document may be filled in either in English or the official language of the Member State of
the competent authority. In the latter case, a second copy in English shall be attached to the
document for any licence holder who needs to use the licence outside that Member State to
ensure understanding for the purpose of mutual recognition.
4. Each licence holder shall have a unique licence holder number, established on the basis of a
national identifier and an alpha-numeric designator.
5. The document may have the pages in a different order to the one of this example and needs
not have some or any divider lines as long as the information contained is positioned in such a
manner that each page lay-out can clearly be identified with the format of the example of the
aircraft maintenance licence contained herein.
6. The document shall be prepared by the competent authority. However, it may also be prepared
by any maintenance organisation approved in accordance with Annex II (Part-145), where the
competent authority agrees to this and the preparation takes place in accordance with a
procedure laid down in the maintenance organisation exposition referred to in point 145.A.70
of Annex II (Part-145). In all cases, the competent authority shall issue the document.
7. The preparation of any change to an existing aircraft maintenance licence shall be carried out
by the competent authority. However, it may also be prepared by any maintenance organisation
approved in accordance with Annex II (Part-145), where the competent authority agrees to this
and the preparation takes place in accordance with a procedure laid down in the maintenance
organisation exposition referred to in point 145.A.70 of Annex II (Part-145). In all cases, the
competent authority shall change the document.
8. The holder of the aircraft maintenance licence shall keep it in good condition and shall ensure
that no unauthorised entries are made. Failure to comply with this rule may invalidate the
license or lead to the holder not being permitted to hold any certification privilege. It may also
result in prosecution under national law.
9. The aircraft maintenance licence issued in accordance with Annex III (Part-66) shall be
recognised in all Member States and it is not required to exchange the document when working
in another Member State.
10. The Annex to EASA Form 26 is optional and may only be used to include national privileges,
where such privileges are covered by national law outside the scope of Annex III (Part-66).
11. With regard to the aircraft type rating page of the aircraft maintenance licence, the competent
authority may decide not to issue this page until the first aircraft type rating needs to be
endorsed and may need to issue more than one aircraft type rating page depending on the
number of type ratings to be listed.

12. Notwithstanding point 11, each page issued shall be in the format of this example and contain
the specified information for that page.
13. The aircraft maintenance licence shall clearly indicate that the limitations are exclusions from
the certification privileges. If there are no limitations applicable, the LIMITATIONS page shall
state ‘No limitations’.
14. Where a pre-printer format is used for issuing the aircraft maintenance licence, any category,
subcategory or type rating box which does not contain a rating entry shall be marked to show
that the rating is not held.

IVa. Full name of holder:
I.
EUROPEAN UNION (*) IVb. Date and place of birth:
[STATE]
[AUTHORITY NAME & LOGO] V. Address of holder:
II.
VI. Nationality of holder:
Part-66
AIRCRAFT MAINTENANCE
LICENCE VII. Signature of holder:
III.
Licence No. [MEMBER STATE
CODE].66.[XXXX]
EASA FORM 26 Issue 5 III. Licence No:
IX. Part-66 CATEGORIES

VIII. CONDITIONS:
VALIDITY A B1 B2 B2L B3 L C
Aeroplanes Turbine n/a n/a n/a n/a

This licence shall be signed by the holder and be accompanied by
an identity document containing a photograph of the licence Aeroplanes Piston n/a n/a n/a n/a
holder.
Endorsement of any categories on the page(s) entitled 'Part-66 Helicopters Turbine n/a n/a n/a n/a
CATEGORIES' only, does not permit the holder to issue a
certificate of release to service for an aircraft. Helicopters Piston n/a n/a n/a n/a
This licence, when endorsed with an aircraft rating, meets the
intent of ICAO Annex 1. Avionics n/a n/a n/a n/a n/a
The privileges of this licence holder are prescribed by Regulation

Complex motor-powered n/a n/a n/a n/a n/a
(EU) No 1321/2014 and, in particular, Annex III (Part-66) thereto.
aircraft
This licence remains valid until the date specified on the
Aircraft other than complex n/a n/a n/a n/a n/a
limitation page unless previously suspended or revoked.
motor-powered aircraft
The privileges of this licence may not be exercised unless in the
Sailplanes, powered n/a n/a n/a n/a n/a
preceding two-year period, the holder had either six months of
sailplanes, ELA1 aeroplanes,
maintenance experience in accordance with the privileges
balloons and airships
granted by the licence, or met the provisions for the issue of the
appropriate privileges. Piston engine non n/a n/a n/a n/a n/a
pressurised aeroplanes of 2
000 kg MTOM and below
X. Signature of issuing officer & date:
XI. Seal or stamp of issuing authority:

III. Licence No: III. Licence No:

XII. PART-66 RATINGS XIII. PART-66 LIMITATIONS
Aircraft Rating/ Category/Subcategory Stamp & Date

System ratings
Valid until:
III. Licence No: III. Licence No:
Annex to EASA FORM 26

XIV. NATIONAL PRIVILEGES outside the scope of Part-66, in
accordance with [National Legislation] (Valid only in [Member
State])
INTENTIONALLY LEFT BLANK
Official Stamp & Date
III. Licence No:
EASA Form 26 Issue 5

Appendix VII — Basic knowledge requirements for category L

aircraft maintenance licence
The definitions of the different levels of knowledge required in this Appendix are the same as those
contained in point 1 of Appendix I to Annex III (Part-66).
Subcategories Modules required for each subcategory (refer to
the syllabus table below)
L1C: composite sailplanes 1L, 2L, 3L, 5L, 7L and 12L
L1: sailplanes 1L, 2L, 3L, 4L, 5L, 6L, 7L and 12L
L2C: composite powered sailplanes and composite 1L, 2L, 3L, 5L, 7L, 8L and 12L
ELA1 aeroplanes
L2: powered sailplanes and ELA1 aeroplanes 1L, 2L, 3L, 4L, 5L, 6L, 7L, 8L and 12L
L3H: hot-air balloons 1L, 2L, 3L, 9L and 12L
L3G: gas balloons 1L, 2L, 3L, 10L and 12L
L4H: hot-air airships 1L, 2L, 3L, 8L, 9L, 11L and 12L
L4G: ELA2 gas airships 1L, 2L, 3L, 8L, 10L, 11L and 12L
L5: gas airships above ELA2 Basic knowledge requirements for any B1
subcategory plus
8L (for B1.1 and B1.3), 10L, 11L and 12L
TABLE OF CONTENTS:
Module Designation
1L ‘Basic knowledge’
2L ‘Human factors’
3L ‘Aviation legislation’
4L ‘Airframe wooden/metal tube and fabric’
5L ‘Airframe composite’
6L ‘Airframe metal’
7L ‘Airframe general’
8L ‘Power plant’
9L ‘Balloon/Airship hot air’
10L ‘Balloon/Airship gas (free/tethered)’
11L ‘Airships hot air/gas’
12L ‘Radio Com/ELT/Transponder/Instruments’

MODULE 1L — BASIC KNOWLEDGE

MODULE 1L — BASIC KNOWLEDGE Level
1L.1 Mathematics 1
Arithmetic
— Arithmetical terms and signs;
— Methods of multiplication and division;
— Fractions and decimals;
— Factors and multiples;
— Weights, measures and conversion factors;
— Ratio and proportion;
— Averages and percentages;
— Areas and volumes, squares, cubes.
Algebra
— Evaluating simple algebraic expressions: addition, subtraction, multiplication and division;
— Use of brackets;
— Simple algebraic fractions.
Geometry
— Simple geometrical constructions;
— Graphical representation: nature and uses of graphs.
1L.2 Physics Matter 1
— Nature of matter: the chemical elements;
— Chemical compounds;
— States: solid, liquid and gaseous;
— Changes between states.
Mechanics
— Forces, moments and couples, representation as vectors;
— Centre of gravity;
— Tension, compression, shear and torsion;
— Nature and properties of solids, fluids and gases.
Temperature
— Thermometers and temperature scales: Celsius, Fahrenheit and Kelvin;
— Heat definition.
1L.3 Electrics 1
DC Circuits
— Ohm's law, Kirchoff's voltage and current laws;
— Significance of the internal resistance of a supply;
— Resistance/resistor;
— Resistor colour code, values and tolerances, preferred values, wattage ratings;
— Resistors in series and parallel.
1L.4 Aerodynamics/aerostatics 1
International Standard Atmosphere (ISA), application to aerodynamics and aerostatics.
Aerodynamics
— Airflow around a body;
— Boundary layer, laminar and turbulent flow;
— Thrust, weight, aerodynamic resultant;
— Generation of lift and drag: angle of attack, polar curve, stall.
Aerostatics
Effect on envelopes, wind effect, altitude and temperature effects.
1L.5 Workplace safety and environmental protection 2
— Safe working practices and precautions when working with electricity, gases (especially
oxygen), oils and chemicals;
— Labelling, storage and disposal of hazardous (to safety and environment) materials;
— Remedial action in the event of a fire or another accident with one or more hazards,
including knowledge of extinguishing agents.

MODULE 2L — HUMAN FACTORS

MODULE 2L — HUMAN FACTORS Level
2L.1 General 1
— The need to take human factors into account;
— Incidents attributable to human factors/human error;
— Murphy's Law.
2L.2 Human performance and limitations 1
Vision, hearing, information processing, attention and perception, memory.
2L.3 Social psychology 1
Responsibility, motivation, peer pressure, teamwork.
2L.4 Factors affecting performance 1
Fitness/health, stress, sleep, fatigue, alcohol, medication, drug abuse.
2L.5 Physical environment 1
Working environment (climate, noise, illumination).
MODULE 3L — AVIATION LEGISLATION

MODULE 3L — AVIATION LEGISLATION Level
3L.1 Regulatory framework 1
— Role of the European Commission, EASA and National Aviation Authorities (NAAs);
— Applicable parts of Part-M and Part-66.
3L.2 Repairs and modifications 2
— Approval of changes (repairs and modifications);
— Standard changes and standard repairs.
3L.3 Maintenance data 2
— Airworthiness Directives (ADs), Instructions for Continuing Airworthiness (ICA) (AMM, IPC,
etc.);
— Flight Manual;
— Maintenance records.
MODULE 4L — AIRFRAME WOODEN/METAL TUBE AND FABRIC

MODULE 4L — AIRFRAME WOODEN/METAL TUBE AND FABRIC Level
4L.1 Airframe wooden/combination of metal tube and fabric 2
— Timber, plywood, adhesives, preservation, power line, properties, machining;
— Covering (covering materials, adhesives and finishes, natural and synthetic covering materials
and adhesives);
— Paint, assembly and repair processes;
— Recognition of damages from overstressing of wooden/metal-tube and fabric structures;
— Deterioration of wood components and coverings;
— Crack test (optical procedure, e.g., magnifying glass) of metal components. Corrosion and
preventive methods. Health and fire safety protections.
4L.2 Material 2
— Types of wood, stability, and machining properties;
— Steel and light alloy tubes and fittings, fracture inspections of welded seams;
— Plastics (overview, understanding of the properties);
— Paints and paint removal;
— Glues, adhesives;
— Covering materials and technologies (natural and synthetic polymers).
4L.3 Identifying damage 3
— Overstress of wood / metal-tubing and fabric structures;
— Load transfers;
— Fatigue strength and crack testing.

MODULE 4L — AIRFRAME WOODEN/METAL TUBE AND FABRIC Level

4L.4 Performance of practical activities 2
— Locking of pins, screws, castellated nuts, turnbuckles;
— Thimble splice;
— Nicopress and Talurit repairs;
— Repair of coverings;
— Repair of transparencies;
— Repair exercises (plywood, stringer, handrails, skins);
— Aircraft Rigging. Calculation of control surface mass balance and range of movement of the
control surfaces, measurement of operating forces;
— Performance of 100-hours/annual inspections on a wood or combination of metal-tube and
fabric airframe.
MODULE 5L — AIRFRAME COMPOSITE

MODULE 5L — AIRFRAME COMPOSITE Level
5L.1 Airframe fibre-reinforced plastic (FRP) 2
— Basic principles of FRP construction;
— Resins (Epoxy, polyester, phenolic resins, vinyl ester resins);
— Reinforcement materials glass, aramide and carbon fibres, features;
— Fillers;
— Supporting cores (balsa, honeycombs, foamed plastics);
— Constructions, load transfers (solid FRP shell, sandwiches);
— Identification of damage during overstressing of components;
— Procedure for FRP projects (according to Maintenance Organisation Manual) including
storage conditions for material.
5L.2 Material 2
— Thermosetting plastics, thermoplastic polymers, catalysts;
— Understanding properties, machining technologies, detaching, bonding, welding;
— Resins for FRP: epoxy resins, polyester resins, vinyl ester resins, phenolic resins;
— Reinforcement materials;
— From elementary fibre to filaments (release agent, finish), weaving patterns;
— Properties of individual reinforcement materials (E-glass fibre, aramide fibre, carbon fibre);
— Problem with multiple-material systems, matrix;
— Adhesion/cohesion, various behaviours of fibre materials;
— Filling materials and pigments;
— Technical requirements for filling materials;
— Property change of the resin composition through the use of E-glass, micro balloon, aerosols,
cotton, minerals, metal powder, organic substances;
— Paint assembly and repair technologies;
— Support materials;
— Honeycombs (paper, FRP, metal), balsa wood, Divinycell (Contizell), development trends.
5L.3 Assembly of Fibre-Reinforced Composite-Structure Airframes 2
— Solid shell;
— Sandwiches;
— Assembly of aerofoils, fuselages, control surfaces.
5L.4 Identifying Damage 3
— Behaviour of FRP components in the event of overstressing;
— Identifying delaminations, loose bonds;
— Bending vibration frequency in aerofoils;
— Load transfer;
— Frictional connection and positive locking;
— Fatigue strength and corrosion of metal parts;

MODULE 5L — AIRFRAME COMPOSITE Level

— Metal bonding, surface finishing of steel and aluminium components during bonding with
FRP.
5L.5 Mold making 2
— Plaster molds, mold ceramics;
— GFK molds, Gel-coat, reinforcement materials, rigidity problems;
— Metal molds;
— Male and female molds.
— Locking of pin, screws, castellated nuts, turnbuckles;
— Thimble splice;
— Repair of coverings;
— Repair of solid FRP shells;
— Mold fabrication/molding of a component (e.g. fuselage nose, landing gear fairing, wing tip
and winglet);
— Repair of sandwich shell where interior and exterior layer are damaged;
— Repair of sandwich shell by pressing with a vacuum bag;
— Transparency repair (PMMA) with one- and two-component adhesive;
— Bonding of transparency with the canopy frame;
— Tempering of transparencies and other components;
— Performance of a repair on a sandwich shell (minor repair less than 20 cm);
— Performance of 100-hour/annual inspections on an FRP airframe.
MODULE 6L — AIRFRAME METAL

MODULE 6L — AIRFRAME METAL Level
6L.1 Airframe metal 2
— Metallic materials and semi-finished products, machining methods;
— Fatigue strength and crack test;
— Assembly of metal-construction components, riveted joints, adhesive joints;
— Identification of damage to overstressed components, effects of corrosion;
— Health and fire protection.
6L.2 Material 2
— Steel and its alloys;
— Light metals and their light alloys;
— Rivet materials;
— Plastics;
— Colours and paints;
— Metal adhesives;
— Types of corrosion;
— Covering materials and technologies (natural and synthetic).
6L.3 Identifying damage 3
— Overstressed metal airframes, levelling, measurement of symmetry;
— Load transfers;
— Fatigue strength and crack test;
— Identifying loose riveted joints.
6L.4 Assembly of metal- and composite-construction airframes 2
— Skins;
— Frames;
— Stringers and longerons;
— Frame construction;

MODULE 6L — AIRFRAME METAL Level

— Problems in multiple-material systems.
6L.5 Fasteners 2
— Classifications of fits and clearances;
— Metric and imperial measuring systems;
— Oversize bolt.
— Locking of pins, screws, castellated nuts, turnbuckles;
— Thimble splice;
— Repair of coverings, surface damage, stop drilling techniques;
— Repair of transparencies;
— Cutting out sheet metals (aluminiums and light alloys, steel and alloys);
— Folding bending, edging, beating, smoothening, beading;
— Repair riveting of metal airframes according to repair instruction or drawings;
— Evaluation of rivet errors;
— Performance of 100-hour/annual inspections on a metal airframe.
MODULE 7L — AIRFRAME GENERAL

MODULE 7L — AIRFRAME GENERAL Level
7L.1 Flight control system 3
— Cockpit controls: controls in cockpit, colour markings, knob shapes;
— Flight controls surfaces, flaps, air brakes surfaces, controls, hinges, bearings, brackets, push-
pull rods, bell cranks, horns, pulleys, cables, chains, tubes, rollers, tracks, jack screws, surfaces,
movements, lubrication, stabilisers, balancing of controls;
— Combination of controls: flap ailerons, flap air brakes;
— Trim systems.
7L.2 Airframe 2
— Landing gear: characteristics of landing gears and shock absorber strut, extension, brakes,
drum, disks, wheel, tyre, retraction mechanism, electrical retraction, emergency;
— Wing to fuselage mounting points, empennage (fin and tail plane) to fuselage mounting
points, control surface mounting points;
— Permissible maintenance measures;
— Towing: towing/lifting equipment/mechanism;
— Cabin: seats and safety harness, cabin arrangement, windshields, windows, placards, baggage
compartment, cockpit controls, cabin air system, blower;
— Water ballast: water reservoirs, lines, valves, drains, vents, tests;
— Fuel system: tanks, lines, filters, vents, drains, filling, selector valve, pumps, indication, tests,
bonding;
— Hydraulics: system layout, accumulators, pressure and power distribution, indication;
— Liquid and gas: hydraulic, other fluids, levels, reservoir, lines, valves, filter;
— Protections: firewalls, fire protection, lightning strike bonding, turnbuckles, locking devices,
dischargers.
7L.3 Fasteners 2
— Reliability of pins, rivets, screws;
— Control cables, turnbuckles;
— Quick-release couplings (L'Hotellier, SZD, Poland).
7L.4 Locking equipment 2
— Admissibility of locking methods, locking pins, spring steel pins, locking wire, stop nuts, paint;
— Quick-release couplings.
7L.5 Weight and balance levelling 2

MODULE 7L — AIRFRAME GENERAL Level

7L.6 Rescue systems 2
7L.7 On-board modules 2
— Pitot-static system, vacuum/dynamic system, hydrostatic test;
— Flight instruments: airspeed indicator, altimeter, vertical-speed indicator, connection and
functioning, markings;
— Arrangement and display, panel, electrical wires;
— Gyroscopes, filters, indicating instruments; testing of function;
— Magnetic compass: installation and compass swing;
— Sailplanes: acoustic vertical-speed indicator, flight recorders, anticollision aid;
— Oxygen system.
7L.8 On-board modules installation and connections 2
— Flight instruments, mounting requirements (emergency landing conditions as per CS-22);
— Electric wiring, power sources, types of storage batteries, electrical parameters, electric
generator, circuit breaker, energy balance, earth/ground, connectors, terminals, warnings,
fuses, lamps, lightings, switches, voltmeters, ampere meters, electrical gauges.
7L.9 Piston engine propulsion 2
Interface between power plant and airframe.
7L.10 Propeller 2
— Inspection;
— Replacement;
— Balancing.
7L.11 Retraction system 2
— Propeller position control;
— Engine and/or propeller retraction system.
7L.12 Physical inspection procedures 2
— Cleaning, use of lighting and mirrors;
— Measuring tools;
— Measure of controls deflection;
— Torque of screws and bolts;
— Wear of bearings;
— Inspection equipment;
— Calibration of measuring tools.
MODULE 8L — POWER PLANT

MODULE 8L — POWER PLANT Level
8L.1 Noise limits 1
— Explanation of the concept of ‘noise level’;
— Noise certificate;
— Enhanced sound proofing;
— Possible reduction of sound emissions.
8L.2 Piston engines 2
— Four-stroke spark ignition engine, air-cooled engine, fluid-cooled engine;
— Two-stroke engine;
— Rotary-piston engine;
— Efficiency and influencing factors (pressure–volume diagram, power curve);
— Noise control devices.
8L.3 Propeller 2
— Blade, spinner, backplate, accumulator pressure, hub;
— Operation of propellers;
— Variable-pitch propellers, ground and in-flight adjustable propellers, mechanically, electrically
and hydraulically;


— Balancing (static, dynamic);
— Noise problems.
8L.4 Engine control devices 2
— Mechanical control devices;
— Electrical control devices;
— Tank displays;
— Functions, characteristics, typical errors and error indications.
8L.5 Hosepipes 2
— Material and machining of fuel and oil hoses;
— Control of life limit.
8L.6 Accessories 2
— Operation of magneto ignition;
— Control of maintenance limits;
— Operation of carburettors;
— Maintenance instructions on characteristic features;
— Electric fuel pumps;
— Operation of propeller controls;
— Electrically operated propeller control;
— Hydraulically operated propeller control.
8L.7 Ignition system 2
— Constructions: coil ignition, magneto ignition, and thyristor ignition;
— Efficiency of the ignition and preheat system;
— Modules of the ignition and preheat system;
— Inspection and testing of a spark plug.
8L.8 Induction and exhaust systems 2
— Operation and assembly;
— Silencers and heater installations;
— Nacelles and cowlings;
— Inspection and test;
— CO emission test.
8L.9 Fuels and lubricants 2
— Fuel characteristics;
— Labelling, environmentally friendly storage;
— Mineral and synthetic lubricating oils and their parameters: labelling and characteristics,
application;
— Environmentally friendly storage and proper disposal of used oil.
8L.10 Documentation 2
— Manufacturer documents for the engine and propeller;
— Instructions for Continuing Airworthiness (ICA);
— Aircraft Flight Manuals (AFMs) and Aircraft Maintenance Manuals (AMMs);
— Time Between Overhaul (TBO);
— Airworthiness Directives (ADs), technical notes and service bulletins.
8L.11 Illustrative material 2
— Cylinder unit with valve;
— Carburettor;
— High-tension magneto;
— Differential-compression tester for cylinders;
— Overheated/damaged pistons;
— Spark plugs of engines that were operated differently.
8L.12 Practical experience 2
— Work safety/accident prevention (handling of fuels and lubricants, start-up of engines);
— Rigging-engine control rods and Bowden cables;


— Setting of no-load speed;
— Checking and setting the ignition point;
— Operational test of magnetos;
— Checking the ignition system;
— Testing and cleaning of spark plugs;
— Performance of the engine tasks contained in an aeroplane 100-hour/annual inspection;
— Cylinder compression test;
— Static test and evaluation of the engine run;
— Documentation of maintenance work including replacement of components.
8L.13 Gas exchange in internal-combustion engines 2
— Four-stroke reciprocating engine and control units;
— Energy losses;
— Ignition timing;
— Direct flow behaviour of control units;
— Wankel engine and control units;
— Two-stroke engine and control units;
— Scavenging;
— Scavenging blower;
— Idle range and power range.
8L.14 Ignition, combustion and carburation 2
— Ignition;
— Spark plugs;
— Ignition system;
— Combustion process;
— Normal combustion;
— Efficiency and medium pressure;
— Engine knock and octane rating;
— Combustion chamber shapes;
— Fuel/air mix in the carburettor;
— Carburettor principle, carburettor equation;
— Simple carburettor;
— Problems of the simple carburettor and their solutions;
— Carburettor models;
— Fuel/air mix during injection;
— Mechanically controlled injection;
— Electronically controlled injection;
— Continuous injection;
— Carburettor-injection comparison.
8L.15 Flight instruments in aircraft with injection engines 2
— Special flight instruments (injection engine);
— Interpretation of indications in a static test;
— Interpretation of indications in flight at various flight levels.
8L.16 Maintenance of aircraft with injection engines 2
— Documentation, manufacturer documents, etc.;
— General maintenance instructions (hourly inspections);
— Functional tests;
— Ground test run;
— Test flight;
— Troubleshooting in the event of faults in the injection system and their correction.
8L.17 Workplace safety and safety provisions Work safety and safety provisions for work on 2
injection systems.
8L.18 Visual aids: 2
— Carburettor;


— Components of injection system;
— Aircraft with injection engine;
— Tool for work on injection systems.
8L.19 Electrical propulsion 2
— Energy system, accumulators, installation;
— Electrical motor;
— Heat, noise and vibration checks;
— Testing windings;
— Electrical wiring and control systems;
— Pylon, extension and retraction systems;
— Motor/propeller brake systems;
— Motor ventilation systems;
— Practical experience of 100-hour/annual inspections.
8L.20 Jet propulsion 2
— Engine installation;
— Pylon, extension and retraction systems;
— Fire protection;
— Fuel systems including lubrication;
— Engine starting systems, gas assist;
— Engine damage assessment;
— Engine servicing;
— Engine removal / refit and test;
— Practical experience of conditional / run time / annual inspections;
— Conditional inspections.
8L.21 Full authority digital engine control (FADEC) 2
MODULE 9L — BALLOON/AIRSHIP HOT AIR

MODULE 9L — BALLOON/AIRSHIP HOT AIR Level
9L.1 Basic principles and assembly of hot-air balloons/airships 3
— Assembly and individual parts;
— Envelopes;
— Envelope Materials;
— Envelope Systems;
— Conventional and special shapes;
— Fuel System;
— Burner, burner frame and burner support rods;
— Compressed-gas cylinders and compressed-gas hoses;
— Basket and alternative devices (seats);
— Rigging accessories;
— Maintenance and servicing tasks;
— Annual/100-hour inspection;
— Log Books;
— Rigging and launch preparation (launch restraint);
— Launch.
9L.2 Practical training 3
Operating controls, maintenance and servicing jobs (according to flight manual).
9L.3 Envelope 3
— Fabrics;
— Seams;
— Load tapes, rip stoppers;
— Crown rings;

MODULE 9L — BALLOON/AIRSHIP HOT AIR Level

— Parachute valve and fast-deflation systems;
— Ripping panel;
— Turning vent;
— Diaphragms/catenaries (special shapes and airships);
— Rollers, pulleys;
— Control and shroud lines;
— Knots;
— Temperature indication label, temperature flag, envelope thermometer;
— Flying wires;
— Fittings, karabiners.
9L.4 Burner and fuel system 3
— Burner coils;
— Blast, liquid and pilot valves;
— Burners/jets;
— Pilot lights/vaporisers/jets;
— Burner frame;
— Fuel lines/hoses;
— Fuel cylinders, valves and fittings.
9L.5 Basket and basket suspension (incl. alternative devices) 3
— Types of baskets (incl. alternative devices);
— Basket materials: cane and willow, hide, wood, trim materials, suspension cables;
— Seats, roller bearings;
— Karabiner, shackle and pins;
— Burner support rods;
— Fuel cylinder straps;
— Accessories.
9L.6 Equipment 3
— Fire extinguisher, fire blanket;
— Instruments (single or combined).
9L.7 Minor repairs 3
— Stitching;
— Bonding;
— Basket hide/trim repairs.
9L.8 Procedures for physical inspection 2
— Measure of controls deflection (only airships);
— Wear of bearings (only airships);
— Calibration of measuring tools;
— Fabric Grab Test.
MODULES 10L — BALLOON/AIRSHIP GAS (FREE/TETHERED)

MODULES 10L — BALLOON/AIRSHIP GAS (FREE/TETHERED) Level
10L.1 Basic principles and assembly of gas balloons/airships 3
— Assembly of individual parts;
— Envelope and netting material;
— Envelope, ripping panel, emergency opening, cords and belts;
— Rigid gas valve;
— Flexible gas valve (parachute);
— Netting;


— Load ring;
— Basket and accessories (including alternative devices);
— Electrostatic discharge paths;
— Mooring line and drag rope;
— Maintenance and servicing;
— Annual inspection;
— Flight papers;
— Rigging and launch preparation;
— Launch.
— Operating controls;
— Maintenance and servicing jobs (according to AMM and AFM);
— Safety rules when using hydrogen as lifting gas.
10L.3 Envelope 3
— Fabrics;
— Poles and reinforcement of pole;
— Ripping panel and cord;
— Parachute and shroud lines;
— Valves and cords;
— Filler neck, Poeschel-ring and cords;
— Electrostatic discharge paths.
10L.4 Valve 3
— Springs;
— Gaskets;
— Screwed joints;
— Control lines;
10L.5 Netting or rigging (without net) 3
— Kinds of net and other lines;
— Mesh sizes and angles;
— Net ring;
— Knotting methods;
10L.6 Load ring 3
10L.7 Basket (incl. alternative devices) 3
— Kinds of baskets (incl. alternative devices);
— Strops and toggles;
— Ballast system (bags and supports);
10L.8 Ripping cord and valve cords 3
10L.9 Mooring line and drag rope 3
10L.10 Minor repairs 3
— Bonding;
— Splicing hemp ropes.
10L.11 Equipment 3
Instruments (single or combined).
10L.12 Tether cable (tethered gas balloons (TGB) only) 3
— Kinds of cables;
— Acceptable damage of cable;
— Cable swivel;
— Cable clamps.


10L.13 Winch (tethered gas balloons only) 3
— Kinds of winches;
— Mechanical system;
— Electrical system;
— Emergency system;
— Grounding/ballasting of winch.
10L.14 Procedures for physical inspection 2
— Measure of controls deflection (only airships);
— Wear of bearings (only airships);
— Calibration of measuring tools;
— Fabric grab test.
MODULES 11L — AIRSHIPS HOT AIR/GAS

MODULES 11L — AIRSHIPS HOT AIR/GAS Level
11L.1 Basic principles and assembly of small airships 3
— Envelope, ballonnets;
— Valves, openings;
— Gondola;
— Propulsion;
— Rigging and launch preparation.
— Operating controls;
— Maintenance and servicing jobs (according to AMM and AFM).
11L.3 Envelope 3
— Fabrics;
— Ripping panel and cords;
— Valves;
— Catenary system.
11L.4 Gondola (incl. alternative devices) 3
— Kinds of gondolas (incl. alternative devices);
— Airframe types and materials;
— Identification of damage.
11L.5 Electrical system 3
— Basics about on-board electrical circuits;
— Electrical sources (accumulators, fixation, ventilation, corrosion);
— Lead, nickel-cadmium (NiCd) or other accumulators, dry batteries;
— Generators;
— Wiring, electrical connections;
— Fuses;
— External power source;
— Energy balance.
11L.6 Propulsion 3
— Fuel system: tanks, lines, filters, vents, drains, filling, selector valve, pumps, indication, tests,
bonding;
— Propulsion instruments;
— Basics about measuring and instruments;
— Revolution measuring;

— Pressure measuring;
— Temperature measuring;
— Available fuel/power measuring.
11L.7 Equipment 3
— Fire extinguisher, fire blanket;
— Instruments (single or combined).
MODULE 12L — RADIO COM/ELT/TRANSPONDER/INSTRUMENTS

MODULE 12L — RADIO COM/ELT/TRANSPONDER/INSTRUMENTS Level
12L.1 Radio Com/ELT 2
— Channel spacing;
— Basic functional test;
— Batteries;
— Testing and maintenance requirements.
12L.2 Transponder 2
— Basic operation;
— Typical portable configuration including antenna;
— Explanation of Modes A, C, S;
— Testing and maintenance requirements.
12L.3 Instruments 2
— Handheld altimeter/variometers;
— Batteries;
— Basic functional test.

Appendix VIII — Basic examination standard for category L aircraft

maintenance licence
(a) The standardisation basis for examinations related to the Appendix VII basic knowledge
requirements shall be as follows:
(i) all examinations must be carried out using the multiple-choice question format as
specified in point (ii). The incorrect alternatives must seem equally plausible to anyone
ignorant of the subject. All of the alternatives should be clearly related to the question
and of similar vocabulary, grammatical construction and length. In numerical questions,
the incorrect answers should correspond to procedural errors such as corrections applied
in the wrong sense or incorrect unit conversions: they must not be mere random
numbers;
(ii) each multiple-choice question must have three alternative answers of which only one
must be the correct answer and the candidate must be allowed a time per module which
is based upon a nominal average of 75 seconds per question;
(iii) the pass mark for each module is 75 %;
(iv) penalty marking (negative points for failed questions) is not to be used;
(v) the level of knowledge required in the questions must be proportionate to the level of
technology of the aircraft category.
(b) The number of questions per module shall be as follows:
(i) module 1L ‘Basic knowledge’: 12 questions. Time allowed: 15 minutes;
(ii) module 2L ‘Human factors’: 8 questions. Time allowed: 10 minutes;
(iii) module 3L ‘Aviation legislation’: 24 questions. Time allowed: 30 minutes;
(iv) module 4L ‘Airframe wooden/metal tube and fabric’: 32 questions. Time allowed: 40
minutes;
(v) module 5L ‘Airframe composite’: 32 questions. Time allowed: 40 minutes;
(vi) module 6L ‘Airframe metal’: 32 questions. Time allowed: 40 minutes;
(vii) module 7L ‘Airframe general’: 64 questions. Time allowed: 80 minutes;
(viii) module 8L ‘Power plant’: 48 questions. Time allowed: 60 minutes;
(ix) module 9L ‘Balloon/Airship hot air’: 36 questions. Time allowed: 45 minutes;
(x) module 10L ‘Balloon/Airship gas (free/tethered)’: 40 questions. Time allowed: 50
minutes;
(xi) module 11L ‘Airships hot air/gas’: 36 questions. Time allowed: 45 minutes;
(xii) Module 12L ‘Radio Com/ELT/transponder/instruments’: 16 questions. Time allowed 20
minutes.

APPENDICES TO AMC TO ANNEX III
(Part-66)
APPENDICES TO AMC TO ANNEX III (PART-66)
Appendix I — Aircraft Type Ratings for Part-66 Aircraft

Maintenance Licences
The following aircraft type ratings should be used to ensure a common standard throughout the
Member States.
In order to keep this list up-to-date, if a Member State needs to issue a type rating that is not included
in this list, the information should be passed on to EASA using the EASA ‘Contact us’ webpage
(https://www.easa.europa.eu/contact-us).
The tables may erroneously contain aircraft models that fall within the definition of Annex I aircraft of
Regulation (EU) 2018/1139. The requirements of Part-66 do not apply to these aircraft.
Notes on type rating (TR) endorsement covering several models/variants:
The endorsement of a type rating (TR) on the aircraft maintenance licence (AML), covering several
models/variants, does not automatically imply that the AML holder has acquired the appropriate
knowledge on each model/variant. In fact, the AML holder may only have received TR training and/or
gained experience that was limited to one or several models or variants.
To demonstrate adequate competence on the relevant model(s)/variant(s), the AML holder and/or
the maintenance organisation where the AML holder is contracted/employed is (are) responsible to
verify that the model/variant has been adequately covered by the TR course or gained experience and
is up to date.
Further explanation can be found in AMC 66.A.20(b)3 and AMC 145.A.35(a).
Notes on when and how the licences should be modified:
The licensing authorities should implement the new type rating list within 6 months after publication
of this Decision. During this implementation period, the old type ratings may still be endorsed. New
applications for type ratings that are no longer certified by EASA should not be accepted. Licences with
the old type ratings shall be endorsed with the amended type ratings, whenever the licensing
authority deems necessary or the holder requests it; however, no later than the next renewal of the
licence.
The instructions on how to endorse a modified type rating (for example, in the case of combined or
split TRs) are included in the chapter ‘Details of the changes’ of explanatory note of the decision.
Notes on aircraft modified by a Supplemental Type Certificate (STC):
− This Appendix intends to include the type ratings of aircraft resulting from STCs for installation
of a different engine. These STCs are those approved by EASA and those approved by the
Member States before 2003 and grandfathered by EASA. STCs other than those for engines are
not considered.
Example: The STC from JET AVIATION AG, approved by the LBA for replacement of GE CF 700 by
Honeywell TFE731 on Fan Jet Falcon Series E, results in a new rating called ‘Falcon 20E
(Honeywell TFE731)’.
− However, the ratings from STCs for installation of an engine:
− on part of the original airframe models, or

(Part-66)
− from the same manufacturer, but of a type very similar to the original one, have not been
added because they would have resulted in an already existing rating.
Examples:
− The STC from SILVERHAWK CONVERSIONS approved by EASA for installation of PT6A-
135A on Beech C90, C90A and E90 would result in the Beech C90/C90A/E90 (PWC PT6)
rating, but this is not listed because it is already included in the original Beech 90 Series
(PWC PT6) rating.
− The STC from Air-Service Wildgruber GmbH approved by LBA for replacement of PWC
PT6A-20 by PWC PT6A-27 would result in the De Havilland DHC-6-100 (PWC PT6) rating,
but this is not listed because it is already included in the De Havilland DHC-6 (PWC PT6)
rating in the table.
− EASA has not received all the information concerning STCs that have been previously approved
by the Member States. As a result, not all STCs are considered by this publication.
− When the STC concerns the installation of an engine that falls under a different subcategory,
e.g. replacement of a piston engine by a turboprop (a turbine engine), then the new type rating
endoresment requires compliance with all the relevant criteria for basic knowledge, experience,
type training, and on-the-job training (OJT).
− In case a type rating resulting from an STC has not been yet defined by EASA, the latter shall be
contacted by the competent authority to agree on a new type rating to be used.
In the following tables:
− The table is alphabetically sorted first by TC/STC Holder, then by TR endorsement, and finally
by Model.
− The column ‘TC Holder’ includes the TC holder as defined in the type certificate data sheets
(TCDS) (EASA, FAA or other) or the specific airworthiness specifications (SAS).
− The column ‘STC Holder’ includes the STC holder as defined in the supplemental type certificate
data sheets (STCDS) (EASA, FAA or other).
− Some TC holders’ designations have been corrected to add the information: ‘Aircraft with an
SAS’, this means that the aircraft listed under this TC holder designation is considered to be an
‘orphan aircraft’or General Aviation aircraft form CIS (former Sovjet Union) countries.
− In Group 3, the column ‘Type of structure’ intends to assist the competent authorities in
identifying the experience required for this type with a view to removing existing limitations on
the licence.
− In Group 4, the column ‘Type of structure’ intends to assist the competent authorities in
identifying the required ‘L’ subcategories.
− Wooden structure covered with fabric is considered to fall under wooden structure. For
aeroplanes with a combination of structures, e.g. metal tubing fuselage and wooden wings,
both experiences ‘metal tube covered with fabric’ and ‘wooden structure’ are required.
− In Group 3, the column ‘MTOM’ intends to assist the competent authorities in identifying the
aeroplane types where the maximum take-off mass (MTOM) is:
− above 2t requires a B1.2 and B2 or B2L licence, or
− 2t and below requires a B1.2 or B3 and B2 or B2L licence.

(Part-66)
− The column ‘NOTE’ in every table includes some useful information, when relevant, e.g.:
− ELA1 or ELA2 aircraft.
− ‘OSD Approved’ or ‘Pending OSD Approval’ means that an OSD-MCS (operational
suitability data for maintenance certifying staff) exists or is still under the approval
process at the date of publication of this ED Decision. OSD data is owned by the TCH
(see TCHs contact list: https://www.easa.europa.eu/document-library/operational-
suitability-data/osd-contact-list).
Type training courses approved before the approval of the OSD-MCS shall include the
OSD elements within 2 years after the OSD-MCS approval.
− STC reference number.
− ‘TC (or STC) not yet released’ means that the type certificate (or STC) has not yet been
released by EASA at the date of publication of this ED Decision, but the final model
configuration is sufficiently mature that the type rating endorsement can be already
defined. In this case, the initial training and licensing may start and be used for approval
of type training courses and Part-66 licence endorsement. On the contrary, the associated
rating for the maintenance organisation can be granted only after the type certification
of the aircraft (or after the approval of the STC).
GROUP 1 AEROPLANES
GROUP 1 AEROPLANES
TC Holder Model Com. des. Part-66 type rating endorsement Note
328 Support Dornier 328- Dornier 328-100 (PWC PW119)
Services 100
328 Support Dornier 328- Dornier 328-300 (PWC PW306)
Services 300
AIR TRACTOR, AT-802 Air Tractor AT-800 Series (PWC PT6)
INC.
AIR TRACTOR, AT-802A Air Tractor AT-800 Series (PWC PT6)
INC.
AIRBUS A300 B1 Airbus A300 basic model (GE CF6)
AIRBUS A300 B2-1A Airbus A300 basic model (GE CF6)
AIRBUS A300 B2-1C Airbus A300 basic model (GE CF6)
AIRBUS A300 B2-202 Airbus A300 basic model (GE CF6)
AIRBUS A300 B2K-3C Airbus A300 basic model (GE CF6)
AIRBUS A300 B4-2C Airbus A300 basic model (GE CF6)
AIRBUS A300 C4-203 Airbus A300 basic model (GE CF6)
AIRBUS A300 F4-203 Airbus A300 basic model (GE CF6)
AIRBUS A300 B2-320 Airbus A300 basic model (PW JT9D)
AIRBUS A300 B4-601 Airbus A300-600 (GE CF6)

(Part-66)
GROUP 1 AEROPLANES
AIRBUS A300 B4-603 Airbus A300-600 (GE CF6)
AIRBUS A300 B4-605 R Airbus A300-600 (GE CF6)
AIRBUS A300 C4-605 R Airbus A300-600 (GE CF6)
Variant F
AIRBUS A300 F4-605 R Airbus A300-600 (GE CF6)
AIRBUS A300 B4-622 Airbus A300-600 (PW 4000)
AIRBUS A300 B4-622 R Airbus A300-600 (PW 4000)
AIRBUS A300 F4-622 R Airbus A300-600 (PW 4000)
AIRBUS A300 B4-620 Airbus A300-600 (PW JT9D)
AIRBUS A300 C4-620 Airbus A300-600 (PW JT9D)
AIRBUS A300F4-608ST Beluga Airbus A300-600ST (GE CF6)
AIRBUS A310-203 Airbus A310 (GE CF6)
AIRBUS A310-203 C Airbus A310 (GE CF6)
AIRBUS A310-324 Airbus A310 (PW 4000)
AIRBUS A310-221 Airbus A310 (PW JT9D)
AIRBUS A318-111 Airbus A318/A319/A320/A321
(CFM56)
(CFM56)
(CFM56)
(CFM56)
(CFM56)
(CFM56)
(CFM56)
(CFM56)
(CFM56)
(CFM56)
(CFM56)

(Part-66)
GROUP 1 AEROPLANES
(CFM56)
(CFM56)
(CFM56)
(CFM56)
(CFM56)
(CFM56)
AIRBUS A319-151N A319 NEO Airbus A319/A320/A321 (CFM LEAP-
1A)
AIRBUS A319-152N A319 NEO Airbus A319/A320/A321 (CFM LEAP- TC not yet
1A) released
1A)
1A)
1A)
1A)
1A)
AIRBUS A321-251NX A321 NEO Airbus A319/A320/A321 (CFM LEAP-
1A)
1A)
1A)
1A)
1A)
AIRBUS A319-171N A319 NEO Airbus A319/A320/A321 (IAE TC not yet
PW1100G) released
PW1100G) released
PW1100G) released
AIRBUS A320-271N A320 NEO Airbus A319/A320/A321 (IAE
PW1100G)
PW1100G)
PW1100G)

(Part-66)
GROUP 1 AEROPLANES
PW1100G)
AIRBUS A321-271NX A321 NEO Airbus A319/A320/A321 (IAE
PW1100G)
PW1100G)
AIRBUS A321-272NX A321 NEO Airbus A319/A320/A321 (IAE
PW1100G)
AIRBUS A319-131 Airbus A319/A320/A321 (IAE V2500)
AIRBUS A330-223F Airbus A330 (PW 4000)
AIRBUS A330-743L Beluga XL Airbus A330 (RR Trent 700) TC not yet
released
AIRBUS A330-243 Airbus A330 (RR Trent 700)
AIRBUS A330-243F Airbus A330 (RR Trent 700)
AIRBUS A330-841 A330 NEO Airbus A330 (RR Trent 7000) TC not yet
released
AIRBUS A330-941 A330 NEO Airbus A330 (RR Trent 7000)
AIRBUS A340-211 Airbus A340 (CFM56)

(Part-66)
GROUP 1 AEROPLANES
AIRBUS A350-1041 Airbus A350 (RR Trent XWB)
AIRBUS A350-941 Airbus A350 (RR Trent XWB)
AIRBUS A380-861 Airbus A380 (EA GP7200)
Airbus Canada BD-500-1A10 A220-100 Bombardier BD-500 Series
Limited (PW PW1500G)
Partnership
Airbus Canada BD-500-1A11 A220-300 Bombardier BD-500 Series
Limited (PW PW1500G)
Partnership
Airbus Military A400M-180 Airbus A400M (EPI TP400)
Sociedad
Limitada (AMSL)
Aircraft L410 NG Turbolet Let L-410 (GE H80)
Industries, a.s.
Aircraft L410 UVP-E20 Turbolet Let L-410 (GE H80)
Industries, a.s.
Aircraft L410 UVP-E20 Turbolet Let L-410 (GE H80)
Industries, a.s. CARGO
Aircraft L410 M Turbolet Let L-410 (Walter M601)
Industries, a.s. Turbolet
Aircraft L410 UVP - Turbolet Let L-410 (Walter M601)
Industries, a.s. Turbolet
Aircraft L410 UVP-E Turbolet Let L-410 (Walter M601)
Industries, a.s.
Aircraft L410 UVP-E20 Turbolet Let L-410 (Walter M601)
Industries, a.s.
Industries, a.s. CARGO
Industries, a.s.
Aircraft L410 UVP-E- Turbolet Let L-410 (Walter M601)
Industries, a.s. LW
Aircraft L410 UVP-LW Turbolet Let L-410 (Walter M601)
Industries, a.s.
Aircraft L420 Let L-420 (Walter M601)
Industries, a.s.
ALENIA C-27J Alenia C-27 (Allison/RR AE2100)
AERMACCHI
ANTONOV AN-26 Antonov AN26 (Ivchenko AI-24)
ANTONOV AN-26B Antonov AN26 (Ivchenko AI-24)

(Part-66)
GROUP 1 AEROPLANES
Antonov Antonov An-28 Antonov An-28 (ТВД) Refer to
Aeronautical EASA.SAS.A.
Scientific and 091 for s/n
Technical applicability.
Complex
(Aircraft with
SAS)
ASI AVIATION F 406 Reims-Cessna F 406 (PWC PT6)
ATR-GIE Avions ATR 42-200 ATR 42-200/300 series (PWC PW120)
de Transport
Régional
de Transport
Régional
de Transport
Régional
ATR-GIE Avions ATR 42-400 ATR 42-400/500/72-212A (PWC
de Transport PW120)
Régional
ATR-GIE Avions ATR 42-500 42-500 ATR 42-400/500/72-212A (PWC
de Transport 42-600 PW120)
Régional
ATR-GIE Avions ATR 72-212 A 72-500 ATR 42-400/500/72-212A (PWC
de Transport 72-600 PW120)
Régional
de Transport
Régional
de Transport
Régional
de Transport
Régional
de Transport
Régional
de Transport
Régional
de Transport
Régional
BAE SYSTEMS ATP ATP (PWC PW120)
(OPERATIONS)
Ltd

(Part-66)
GROUP 1 AEROPLANES
BAE SYSTEMS AVRO 146- BAe 146/ AVRO 146-RJ (Honeywell
(OPERATIONS) RJ100 ALF500 Series)
Ltd
Ltd
Ltd
Ltd
BAE SYSTEMS BAe 146 Series BAe 146/ AVRO 146-RJ (Honeywell
(OPERATIONS) 100 ALF500 Series)
Ltd
Ltd
Ltd
BAE SYSTEMS HS 748 Series HS748 (RRD Dart)
(OPERATIONS) 1
Ltd
(OPERATIONS) 2
Ltd
(OPERATIONS) 2A
Ltd
(OPERATIONS) 2B
Ltd
BAE SYSTEMS Jetstream Jetstream 31 Jetstream 31/32 (Honeywell TPE331)
(OPERATIONS) 3100 Series
Ltd
BAE SYSTEMS Jetstream Jetstream Jetstream 31/32 (Honeywell TPE331)
(OPERATIONS) 3200 Series 32/32EP
Ltd
BAE SYSTEMS Jetstream Jetstream 41 (Honeywell TPE331)
(OPERATIONS) 4100 Series
Ltd
BEECHCRAFT 200 Beech 200 Series (PWC PT6)
Corporation
BEECHCRAFT 300LW Super King Air Beech 300 Series (PWC PT6)
Corporation
BEECHCRAFT F90 King Air Beech 90 Series (PWC PT6)
Corporation

(Part-66)
GROUP 1 AEROPLANES
BEECHCRAFT A99 Airliner Beech 99/100 Series (PWC PT6)
Corporation
BEECHCRAFT A99A Airliner Beech 99/100 Series (PWC PT6)
Corporation
BEECHCRAFT B99 Airliner Beech 99/100 Series (PWC PT6)
Corporation
BEECHCRAFT C99 Airliner Beech 99/100 Series (PWC PT6)
Corporation
BEECHCRAFT 100 King Air Beech 99/100 Series (PWC PT6)
Corporation
BEECHCRAFT A100 King Air Beech 99/100 Series (PWC PT6)
Corporation
BEECHCRAFT A100A King Air Beech 99/100 Series (PWC PT6)
Corporation
BEECHCRAFT 99 Beech 99/100 Series (PWC PT6)
Corporation
BEECHCRAFT 99A Beech 99/100 Series (PWC PT6)
Corporation
BEECHCRAFT B100 Beech B100 (Honeywell TPE331)
Corporation
BERIEV Aircraft Be-200ES-E Beriev 200 (Ivchenko D-436TP)
Company
B-N GROUP Ltd. BN2T Turbine Britten-Norman BN2T Series
(Britten- Islander (RR Corp 250)
Norman)
B-N GROUP Ltd. BN2T-2 Turbine Britten-Norman BN2T Series
Norman)
B-N GROUP Ltd. BN2T-2R Turbine Britten-Norman BN2T Series
Norman)
B-N GROUP Ltd. BN2T-4R Turbine Britten-Norman BN2T Series
Norman)
B-N GROUP Ltd. BN2T-4S Turbine Britten-Norman BN2T Series
Norman)
BOEING 707-200 B707 Boeing 707 (PW JT4)
COMPANY (THE)
BOEING 707-300 Series B707 Boeing 707 (PW JT4)
COMPANY (THE)
BOEING 707-400 B707 Boeing 707 (RR Conway)
COMPANY (THE)
BOEING 720 B707 Boeing 707/720 (PW JT3D)
COMPANY (THE)
BOEING 707-100 Long B707 Boeing 707/720 (PW JT3D)
COMPANY (THE) Body

(Part-66)
GROUP 1 AEROPLANES
BOEING 707-100B Long B707 Boeing 707/720 (PW JT3D)
COMPANY (THE) Body
BOEING 707-100B B707 Boeing 707/720 (PW JT3D)
COMPANY (THE) Short Body
BOEING 707-300 B707 Boeing 707/720 (PW JT3D)
COMPANY (THE)
BOEING 707-300C B707 Boeing 707/720 (PW JT3D)
COMPANY (THE)
BOEING 720B B707 Boeing 707/720 (PW JT3D)
COMPANY (THE)
BOEING 727 B727 Boeing 727 (PW JT8D)
COMPANY (THE)
BOEING 727-100 B727 Boeing 727 (PW JT8D)
COMPANY (THE)
BOEING 727-100C B727 Boeing 727 (PW JT8D)
COMPANY (THE)
BOEING 727-200 B727 Boeing 727 (PW JT8D)
COMPANY (THE)
BOEING 727-200F B727 Boeing 727 (PW JT8D)
COMPANY (THE)
BOEING 727C B727 Boeing 727 (PW JT8D)
COMPANY (THE)
BOEING 737-100 B737 Classic Boeing 737-100/200 (PW JT8D)
COMPANY (THE)
BOEING 737-200 B737 Classic Boeing 737-100/200 (PW JT8D)
COMPANY (THE)
BOEING 737-200C B737 Classic Boeing 737-100/200 (PW JT8D)
COMPANY (THE)
BOEING 737-300 B737 Classic Boeing 737-300/400/500 (CFM56)
COMPANY (THE)
COMPANY (THE)
COMPANY (THE)
BOEING 737-600 B737 Next Boeing 737-600/700/800/900
COMPANY (THE) Generation (CFM56)
BOEING 737-900ER B737 Next Boeing 737-600/700/800/900
BOEING 737-7 B737 MAX Boeing 737-7/8/9 (CFM LEAP-1B) TC not yet
COMPANY (THE) released
BOEING 737-8 B737 MAX Boeing 737-7/8/9 (CFM LEAP-1B)
COMPANY (THE)

(Part-66)
GROUP 1 AEROPLANES
BOEING 737-8200 B737 MAX Boeing 737-7/8/9 (CFM LEAP-1B) TC not yet
COMPANY (THE) released
BOEING 737-9 B737 MAX Boeing 737-7/8/9 (CFM LEAP-1B)
COMPANY (THE)
BOEING 747-100 B747 Boeing 747-100 (PW JT9D)
COMPANY (THE)
BOEING 747-200 B747 Boeing 747-200/300 (GE CF6)
COMPANY (THE)
BOEING 747-200C B747 Boeing 747-200/300 (GE CF6)
COMPANY (THE)
BOEING 747-200F B747 Boeing 747-200/300 (GE CF6)
COMPANY (THE)
BOEING 747-300 B747 Boeing 747-200/300 (GE CF6)
COMPANY (THE)
BOEING 747-200 B747 Boeing 747-200/300 (PW JT9D)
COMPANY (THE)
BOEING 747-200C B747 Boeing 747-200/300 (PW JT9D)
COMPANY (THE)
BOEING 747-200F B747 Boeing 747-200/300 (PW JT9D)
COMPANY (THE)
COMPANY (THE)
BOEING 747-200 B747 Boeing 747-200/300 (RR RB211)
COMPANY (THE)
BOEING 747-200C B747 Boeing 747-200/300 (RR RB211)
COMPANY (THE)
BOEING 747-200F B747 Boeing 747-200/300 (RR RB211)
COMPANY (THE)
COMPANY (THE)
BOEING 747-400 B747 Boeing 747-400 (GE CF6)
COMPANY (THE)
BOEING 747-400F B747 Boeing 747-400 (GE CF6)
COMPANY (THE)
BOEING 747-400BCF B747F/SF Boeing 747-400 (GE CF6)
COMPANY (THE)
BOEING 747-400 B747 Boeing 747-400 (PW 4000)
COMPANY (THE)
BOEING 747-400F B747 Boeing 747-400 (PW 4000)
COMPANY (THE)
BOEING 747-400CF B747F/SF Boeing 747-400 (PW 4000)
COMPANY (THE)
BOEING 747-400 B747 Boeing 747-400 (RR RB211)
COMPANY (THE)
BOEING 747-400F B747 Boeing 747-400 (RR RB211)
COMPANY (THE)
BOEING 747-400CF B747F/SF Boeing 747-400 (RR RB211)
COMPANY (THE)

(Part-66)
GROUP 1 AEROPLANES
BOEING 747-8 B747 Boeing 747-8 (GE GEnx)
COMPANY (THE)
BOEING 747-8F Freighter Boeing 747-8 (GE GEnx)
COMPANY (THE)
BOEING 747SP Boeing 747SP (PW JT9D)
COMPANY (THE)
BOEING 757-200 B757 Boeing 757-200/300 (PW 2000)
COMPANY (THE)
BOEING 757-200PF B757 Boeing 757-200/300 (PW 2000)
COMPANY (THE)
COMPANY (THE)

COMPANY (THE)
BOEING 757-200PF B757 Boeing 757-200/300 (RR RB211)
COMPANY (THE)
COMPANY (THE)
COMPANY (THE)
COMPANY (THE)
BOEING 767-300CF B767 Boeing 767-200/300 (PW 4000)
COMPANY (THE)
COMPANY (THE)
COMPANY (THE)
BOEING 767-300CF B767 Boeing 767-200/300 (PW JT9D)
COMPANY (THE)
BOEING 767-200 B767 Boeing 767-200/300/400 (GE CF6)
COMPANY (THE)
BOEING 767-300 B767 Boeing 767-200/300/400 (GE CF6)
COMPANY (THE)
BOEING 767-300CF B767 Boeing 767-200/300/400 (GE CF6)
COMPANY (THE)
BOEING 767-300F B767 Boeing 767-200/300/400 (GE CF6)
COMPANY (THE)
BOEING 767-400ER B767 Boeing 767-200/300/400 (GE CF6)
COMPANY (THE)
BOEING 767-300 B767 Boeing 767-300 (RR RB211)
COMPANY (THE)
BOEING 777-200 B777 Boeing 777-200/300 (GE 90)
COMPANY (THE)
BOEING 777-200LR B777 Boeing 777-200/300 (GE 90)
COMPANY (THE)

(Part-66)
GROUP 1 AEROPLANES
BOEING 777-300ER B777 Boeing 777-200/300 (GE 90)
COMPANY (THE)
BOEING 777F Freighter Boeing 777-200/300 (GE 90)
COMPANY (THE)
COMPANY (THE)
COMPANY (THE)
BOEING 777-200 B777 Boeing 777-200/300 (RR Trent 800)
COMPANY (THE)
BOEING 777-300 B777 Boeing 777-200/300 (RR Trent 800)
COMPANY (THE)
BOEING 787-10 Dreamliner Boeing 787-8/9/10 (GEnx)
COMPANY (THE)
COMPANY (THE)
COMPANY (THE)
BOEING 787-10 Dreamliner Boeing 787-8/9/10 (RR Trent 1000)
COMPANY (THE)
COMPANY (THE)
COMPANY (THE)
BOMBARDIER BD-100-1A10 Challenger 300 Bombardier BD-100-1A10 (Honeywell
Challenger 350 AS907)
BOMBARDIER BD-700-1A11 Global 5000 Bombardier BD-700 Series
Global 5000 (RRD BR700-710)
GVFD
Global 5500
BOMBARDIER BD-700-1A10 Global Express Bombardier BD-700 Series
Global 6000 (RRD BR700-710)
Global 6500
BOMBARDIER BD-700-2A12 Global 7500 Bombardier BD-700 2A12
(GE Passport 20)
BOMBARDIER CL-600-1A11 Challenger 600 Bombardier CL-600-1A11
(600) (Honeywell ALF502)
BOMBARDIER CL-600-2A12 Challenger 601 Bombardier CL-600-2A12/2B16
(601 Variant) (601/601-3A/3R Variant) (GE CF34)
BOMBARDIER CL-600-2B16 Challenger Bombardier CL-600-2A12/2B16
(601-3A 601-3A (601/601-3A/3R Variant) (GE CF34)
Variant)
BOMBARDIER CL-600-2B16 Challenger Bombardier CL-600-2A12/2B16
(601-3R 601-3R (601/601-3A/3R Variant) (GE CF34)
Variant)
BOMBARDIER CL-600-2B16 Challenger 604 Bombardier CL-600-2B16
(604 Variant) (MSN < 5701) (604 Variant) (GE CF34)
Challenger 605

(Part-66)
GROUP 1 AEROPLANES
(5701<=MSN
<= 5990)
Challenger 650
(MSN ≥ 6050)
BOMBARDIER CL-600-2B19 Regional Jet Bombardier CL-600-2B19 (GE CF34)
(RJ Series 100) Series
100/200/440/
Challenger
850/ CRJ SE
BOMBARDIER CL-600-2E25 Regional Jet Bombardier CL-600-
(RJ Series Series 1000 2C10/2D15/2D24/2E25 (GE CF34)
1000)
BOMBARDIER CL-600-2C10 Regional Jet Bombardier CL-600-
(RJ 700/701/ Series 2C10/2D15/2D24/2E25 (GE CF34)
702) 700/701/702
BOMBARDIER CL-600-2D15 Regional Jet Bombardier CL-600-
(RJ Series 705) Series 705 2C10/2D15/2D24/2E25 (GE CF34)
BOMBARDIER CL-600-2D24 Regional Jet Bombardier CL-600-
(RJ Series 900) Series 900 2C10/2D15/2D24/2E25 (GE CF34)
BOMBARDIER DHC-8-102 DHC-8 Series Bombardier DHC-8-100/200/300
100 (PWC PW 120)
100 (PWC PW 120)
100 (PWC PW 120)
200 (PWC PW 120)
200 (PWC PW 120)
300 (PWC PW 120)
300 (PWC PW 120)
300 (PWC PW 120)
300 (PWC PW 120)
BOMBARDIER DHC-8-401 DHC-8 Series Bombardier DHC-8-400
400 (PWC PW150)
BOMBARDIER DHC-8-402 DHC-8 Series Bombardier DHC-8-400
400 (PWC PW150)
BOMBARDIER CL-215-1A10 Canadair CL-215 (PW R2800)
BOMBARDIER CL-215-6B11 Canadair CL-215 (PWC PW120)
(CL-215T
Variant)
BOMBARDIER CL-215-6B11 Canadair CL-415 (PWC PW123)
(CL-415
Variant)

(Part-66)
GROUP 1 AEROPLANES
CIRRUS Design SF50 CIRRUS SF50 (Williams FJ33)
Corporation
DAHER TBM700 A Socata TBM700 (PWC PT6)
AEROSPACE
DAHER TBM700 B Socata TBM700 (PWC PT6)
AEROSPACE
DAHER TBM700 C1 Socata TBM700 (PWC PT6)
AEROSPACE
DAHER TBM700 C2 Socata TBM700 (PWC PT6)
AEROSPACE
DAHER TBM700 N Socata TBM700 (PWC PT6)
AEROSPACE
DASSAULT Falcon 10 Falcon 10 (Honeywell TFE731)
AVIATION
DASSAULT Fan Jet Falcon (Basic) Fan Jet Falcon 20 (GE CF700)
AVIATION Falcon
DASSAULT Fan Jet Falcon Falcon 20 (GE CF700)
AVIATION C
AVIATION D
AVIATION E
AVIATION F
DASSAULT Fan Jet Falcon Falcon 200 (Honeywell ATF 3-6)
AVIATION G
DASSAULT Mystère Falcon 200 (Honeywell ATF 3-6)
AVIATION Falcon 200
DASSAULT Mystère Falcon 200 (Honeywell ATF 3-6)
AVIATION Falcon 20GF
DASSAULT Falcon 2000 Falcon 2000 (CFE 738)
AVIATION
DASSAULT Falcon 2000EX Falcon 2000EX (PWC PW308) OSD
AVIATION approved
on
30.10.2015.
DASSAULT Falcon 2000EX F2000EX EASy Falcon 2000EX EASy (PWC PW308C) OSD
AVIATION F2000DX approved
F2000LX on
F2000LXS 30.10.2015.
F2000S
DASSAULT Mystère Falcon 20-5 (Honeywell TFE731)
AVIATION Falcon 20-C5
AVIATION Falcon 20-D5
AVIATION Falcon 20-E5

(Part-66)
GROUP 1 AEROPLANES
AVIATION Falcon 20-F5
DASSAULT Mystère Falcon 50 (Honeywell TFE731)
AVIATION Falcon 50
DASSAULT Mystère F50EX Falcon 50EX (Honeywell TFE731)
AVIATION Falcon 50
DASSAULT Falcon 7X Falcon 7X Falcon 7X (PW307) OSD
AVIATION Falcon 8X approved
on
30.6.2016.
DASSAULT Mystère Falcon 900 Falcon 900 (Honeywell TFE731)
AVIATION Falcon 900 Falcon 900B
DASSAULT Mystère F900C Falcon 900C/EX (Honeywell TFE 731)
AVIATION Falcon 900
DASSAULT Falcon 900EX Falcon 900C/EX (Honeywell TFE 731)
AVIATION
DASSAULT Falcon 900EX F900EX EASy Falcon 900EX EASy
AVIATION F900DX (Honeywell TFE731)
F900LX
DORNIER Seastar CD2 Dornier Seastar CD2 (PWC PT6)
SEAWINGS
GmbH
EADS CASA C-212-CB Aviocar CASA C-212 (Honeywell TPE331)
EADS CASA C-212-CC Aviocar CASA C-212 (Honeywell TPE331)
EADS CASA C-212-CD Aviocar CASA C-212 (Honeywell TPE331)
EADS CASA C-212-CE Aviocar CASA C-212 (Honeywell TPE331)
EADS CASA C-212-CF Aviocar CASA C-212 (Honeywell TPE331)
EADS CASA C-212-DD Aviocar CASA C-212 (Honeywell TPE331)
EADS CASA C-212-DF Aviocar CASA C-212 (Honeywell TPE331)
EADS CASA C-212-EE Aviocar CASA C-212 (Honeywell TPE331)
EADS CASA C-212-VA Aviocar CASA C-212 (Honeywell TPE331)
EADS CASA C-212-DE Aviocar CASA C-212 (PWC PT6)
EADS CASA C-295 CASA C-295 (PWC PW127)
EADS CASA CN-235 CASA CN-235 (GE CT7)
EADS CASA CN-235-100 CASA CN-235 (GE CT7)

ECLIPSE EA500 Eclipse EA500 (PWC PW610)
AEROSPACE Inc.
EMBRAER S.A. EMB-110K1 Bandeirante Embraer EMB-110 (PWC PT6)
EMBRAER S.A. EMB-110P1 Bandeirante Embraer EMB-110 (PWC PT6)
EMBRAER S.A. EMB-110P2 Bandeirante Embraer EMB-110 (PWC PT6)
EMBRAER S.A. EMB-120 Brasilia Embraer EMB-120
(PWC PW110 Series)

(Part-66)
GROUP 1 AEROPLANES
EMBRAER S.A. EMB-120ER Brasilia Embraer EMB-120
(PWC PW110 Series)
EMBRAER S.A. EMB-120RT Brasilia Embraer EMB-120
(PWC PW110 Series)
EMBRAER S.A. EMB-121A Xingu I Embraer EMB-121 (PWC PT6)
EMBRAER S.A. EMB-121A1 Xingu II Embraer EMB-121 (PWC PT6)
EMBRAER S.A. EMB-135BJ Legacy 600 Embraer EMB-135/145
Legacy 650 (RR Corp AE3007A)
EMBRAER S.A. EMB-135ER Embraer EMB-135/145
(RR Corp AE3007A)
EMBRAER S.A. EMB-135LR Embraer EMB-135/145
(RR Corp AE3007A)
EMBRAER S.A. EMB-145 Embraer EMB-135/145
(RR Corp AE3007A)
EMBRAER S.A. EMB-145EP Embraer EMB-135/145
(RR Corp AE3007A)
EMBRAER S.A. EMB-145ER Embraer EMB-135/145
(RR Corp AE3007A)
EMBRAER S.A. EMB-145EU Embraer EMB-135/145
(RR Corp AE3007A)
EMBRAER S.A. EMB-145LR Embraer EMB-135/145
(RR Corp AE3007A)
EMBRAER S.A. EMB-145LU Embraer EMB-135/145
(RR Corp AE3007A)
EMBRAER S.A. EMB-145MK Embraer EMB-135/145
(RR Corp AE3007A)
EMBRAER S.A. EMB-145MP Embraer EMB-135/145
(RR Corp AE3007A)
EMBRAER S.A. EMB-500 Phenom 100 Embraer EMB-500 (PWC PW617)
EMBRAER S.A. EMB-505 Phenom 300 Embraer EMB-505 (PWC PW535)
EMBRAER S.A. EMB-545 Legacy 450 Embraer EMB-545/550
(Honeywell AS907)
EMBRAER S.A. EMB-550 Legacy 500 Embraer EMB-545/550
(Honeywell AS907)
EMBRAER S.A. ERJ 170-100 LR ERJ-170 Embraer ERJ-170 Series (GE CF34)
EMBRAER S.A. ERJ 170-100 ERJ-170 Embraer ERJ-170 Series (GE CF34)
STD
STD
SR
STD
EMBRAER S.A. ERJ 190-100 ERJ-190 AR Embraer ERJ-190 Series (GE CF34)
IGW

(Part-66)
GROUP 1 AEROPLANES
STD
EMBRAER S.A. ERJ 190-200 ERJ-195 AR Embraer ERJ-190 Series (GE CF34)
IGW
EMBRAER S.A. ERJ 190-100 Lineage 1000 Embraer ERJ-190 Series (GE CF34)
ECJ
EMBRAER S.A. ERJ 190-300 EMBRAER Embraer ERJ-190 Series (PW 1900G)
190E2
EMBRAER S.A. ERJ 190-400 EMBRAER Embraer ERJ-190 Series (PW 1900G)
195-E2
FOKKER F27 Mark 050 Fokker 50 Fokker 50/60 Series
SERVICES (PWC PW 125/127)
FOKKER F28 Mark 0100 Fokker 100 Fokker 70/100 (RRD Tay)
SERVICES
FOKKER F28 Mark 0070 Fokker 70 Fokker 70/100 (RRD Tay)
SERVICES
FOKKER F27 Mark 100 Friendship Fokker F27 / Fairchild F-27/FH-227
SERVICES Series (RRD Dart)
FOKKER F28 Mark 1000 Fellowship Fokker F28 Series (RRD Spey)
SERVICES
FOKKER F28 Mark Fellowship Fokker F28 Series (RRD Spey)
SERVICES 1000C
SERVICES
SERVICES
SERVICES 3000C
SERVICES 3000R

(Part-66)
GROUP 1 AEROPLANES
SERVICES 3000RC
SERVICES
GROB Aircraft G520 EGRETT Grob G 520 Series
AG (Honeywell TPE331)
GROB Aircraft G520T Grob G 520 Series
AG (Honeywell TPE331)
GULFSTREAM G-1159 Gulfstream II Gulfstream G-1159 Series (RRD Spey)
AEROSPACE
Corporation
GULFSTREAM G-1159A Gulfstream IIB Gulfstream G-1159 Series (RRD Spey)
AEROSPACE
Corporation
GULFSTREAM G-1159B Gulfstream III Gulfstream G-1159 Series (RRD Spey)
AEROSPACE
Corporation
GULFSTREAM G-159 Gulfstream I Gulfstream G-159 (RRD Dart)
AEROSPACE
Corporation
GULFSTREAM G-IV Gulfstream Gulfstream GIV/GIV-SP Series
AEROSPACE G-IV/GIV-SP (RRD Tay)
Corporation
GULFSTREAM GIV-X Gulfstream Gulfstream GIV-X Series
AEROSPACE G350 (RRD Tay)
Corporation Gulfstream
G450
GULFSTREAM GV Gulfstream GV Gulfstream GV basic model
AEROSPACE (RRD BR710)
Corporation
GULFSTREAM GVI (G650) G650 Gulfstream GVI (RRD BR725)
AEROSPACE G650ER
Corporation
GULFSTREAM GVII-G500 Gulfstream GVII (PWC PW800GA) OSD
AEROSPACE mandatory.
Corporation
GULFSTREAM GVII-G600 Gulfstream GVII (PWC PW800GA) Not yet
AEROSPACE certified.
Corporation OSD
mandatory.
GULFSTREAM GV-SP Gulfstream Gulfstream GV-SP Series
AEROSPACE G500 (RRD BR710)
Corporation Gulfstream
G550
GULFSTREAM 1125 Astra Gulfstream (IAI) 100/1125/Astra SPX
AEROSPACE LP Westwind (Honeywell TFE731)
(GALP) Astra

(Part-66)
GROUP 1 AEROPLANES
GULFSTREAM Gulfstream G100/Astra Gulfstream (IAI) 100/1125/Astra SPX
AEROSPACE LP 100/Astra SPX SPX (Honeywell TFE731)
(GALP)
GULFSTREAM 1125 Astra SP Gulfstream (IAI) 100/1125/Astra SPX
AEROSPACE LP (Honeywell TFE731)
(GALP)
GULFSTREAM Gulfstream G200/Galaxy Gulfstream (IAI) 200/Galaxy
AEROSPACE LP 200/Galaxy (PWC PW306)
(GALP)
GULFSTREAM Gulfstream G150 Gulfstream (IAI) G150
AEROSPACE LP G150 (Honeywell TFE731)
(GALP)
GULFSTREAM Gulfstream G280 Gulfstream (IAI) G280
AEROSPACE LP G280 (Honeywell AS907)
(GALP)
HAWKER BAe.125 Series BAe.125 BAe 125 Series (Honeywell TFE731)
BEECHCRAFT 800A
HAWKER BAe.125 Series BAe.125 BAe 125 Series (Honeywell TFE731)
BEECHCRAFT 800B
HAWKER BH.125 Series BH.125 BAe 125 Series (Honeywell TFE731)
BEECHCRAFT 400A
HAWKER BH.125 Series BH.125 BAe 125 Series (Honeywell TFE731)
BEECHCRAFT 600A
HAWKER DH.125 Series DH.125 BAe 125 Series (Honeywell TFE731)
BEECHCRAFT 1A
BEECHCRAFT 3A
BEECHCRAFT 3A/RA
BEECHCRAFT 400A
HAWKER HS.125 Series HS.125 BAe 125 Series (Honeywell TFE731)
BEECHCRAFT 400A
BEECHCRAFT 600A
BEECHCRAFT 700A
BEECHCRAFT 700B
BEECHCRAFT F3B
HAWKER HS.125 series HS.125 BAe 125 Series (Honeywell TFE731)
BEECHCRAFT F3B/RA
BEECHCRAFT F400B
BEECHCRAFT F403B

(Part-66)
GROUP 1 AEROPLANES
HAWKER HS.125 series HS.125 BAe 125 Series (Honeywell TFE731)
BEECHCRAFT F600B
HAWKER Hawker 800 BAe 125 Series (Honeywell TFE731)
BEECHCRAFT
HAWKER HS.125 series ‘Hawker BAe 125 Series (RR Viper)
BEECHCRAFT F400 Siddeley’
HAWKER HS.125 series ‘Hawker BAe 125 Series (RR Viper)
BEECHCRAFT F600 Siddeley’
HAWKER BH.125 Series BH.125 BAe 125 Series (RR Viper)
BEECHCRAFT 400A
HAWKER BH.125 Series BH.125 BAe 125 Series (RR Viper)
BEECHCRAFT 600A
HAWKER DH.125 Series DH.125 BAe 125 Series (RR Viper)
BEECHCRAFT 1A
BEECHCRAFT 1A/R-522
BEECHCRAFT 1A/S-522
BEECHCRAFT 1A-522
BEECHCRAFT 3A/R
BEECHCRAFT 400A
HAWKER HS.125 Series HS.125 BAe 125 Series (RR Viper)
BEECHCRAFT 1B
BEECHCRAFT 1B/R-522
BEECHCRAFT 1B/S-522
BEECHCRAFT 1B-522
BEECHCRAFT 3B
BEECHCRAFT 3B/R
BEECHCRAFT 3B/RA
BEECHCRAFT 3B/RB
BEECHCRAFT 3B/RC
BEECHCRAFT 400A
BEECHCRAFT 400B
BEECHCRAFT 400B/1

(Part-66)
GROUP 1 AEROPLANES
BEECHCRAFT 401B
BEECHCRAFT 403A(C)
BEECHCRAFT 403B
BEECHCRAFT 600A
BEECHCRAFT 600B
BEECHCRAFT 600B/1
BEECHCRAFT 600B/2
BEECHCRAFT 600B/3
HAWKER BAe.125 Series BAe.125 BAe 125 Series 1000 (PWC PW305)
BEECHCRAFT 1000A
HAWKER BAe.125 Series BAe.125 BAe 125 Series 1000 (PWC PW305)
BEECHCRAFT 1000B
HAWKER Hawker 1000 BAe 125 Series 1000 (PWC PW305)
BEECHCRAFT
HAWKER Hawker 750 Hawker 750 BAe 125 Series
BEECHCRAFT 750/800XP/850XP/900XP
(Honeywell TFE731)
HAWKER Hawker 800XP Hawker 800XP BAe 125 Series
(Honeywell TFE731)
(Honeywell TFE731)
(Honeywell TFE731)
HAWKER 400T (TX) Beechjet Beech 400/Mitsubishi MU-300
BEECHCRAFT (PWC JT15)
HAWKER 400 Beechjet Beech 400/Mitsubishi MU-300
BEECHCRAFT (PWC JT15)
HAWKER 400A Beechjet Beech 400/Mitsubishi MU-300
BEECHCRAFT (Hawker (PWC JT15)
400XP)
HAWKER MU-300 Diamond I Beech 400/Mitsubishi MU-300
BEECHCRAFT (Diamond I) Diamond IA (PWC JT15)
HAWKER MU-300-10 Diamond II Beech 400/Mitsubishi MU-300
BEECHCRAFT (Diamond II) (PWC JT15)
HONDA HA-420 HondaJet Honda Aircraft HA-420 (HF120)
AIRCRAFT
COMPANY LLC.

(Part-66)
GROUP 1 AEROPLANES
ISRAEL IAI 1123 Commodore IAI 1121/1123 (GE CJ610)
AIRCRAFT Jet
INDUSTRIES
ISRAEL IAI 1121 Jetcommander IAI 1121/1123 (GE CJ610)
AIRCRAFT
INDUSTRIES
ISRAEL IAI 1121A Jetcommander IAI 1121/1123 (GE CJ610)
AIRCRAFT
INDUSTRIES
ISRAEL IAI 1121B Jetcommander IAI 1121/1123 (GE CJ610)
AIRCRAFT
INDUSTRIES
ISRAEL IAI 1124 Westwind IAI 1124 (Honeywell TFE731)
AIRCRAFT
INDUSTRIES
ISRAEL IAI 1124A Westwind IAI 1124 (Honeywell TFE731)
AIRCRAFT
INDUSTRIES
JSC Sukhoi Civil RRJ-95B Superjet 100 RRJ-95 (PowerJet SaM146)
Aircraft
LEARJET 23 (Learjet) Learjet 23 (GE CJ610)
LEARJET 24 Learjet 24/25 (GE CJ610)
LEARJET 25 Learjet 24/25 (GE CJ610)
LEARJET 24A Learjet 24/25 (GE CJ610)
LEARJET 24B Learjet 24/25 (GE CJ610)
LEARJET 24B-A Learjet 24/25 (GE CJ610)
LEARJET 24D Learjet 24/25 (GE CJ610)
LEARJET 24D-A Learjet 24/25 (GE CJ610)
LEARJET 24F Learjet 24/25 (GE CJ610)
LEARJET 24F-A Learjet 24/25 (GE CJ610)
LEARJET 25B Learjet 24/25 (GE CJ610)
LEARJET 25C Learjet 24/25 (GE CJ610)
LEARJET 25D Learjet 24/25 (GE CJ610)
LEARJET 25F Learjet 24/25 (GE CJ610)
LEARJET 31 Learjet 31 (Honeywell TFE731)
LEARJET 31A Learjet 31 (Honeywell TFE731)
LEARJET 35 Learjet 35/36 (Honeywell TFE731)
LEARJET 36 Learjet 35/36 (Honeywell TFE731)
LEARJET 35A Learjet 35/36 (Honeywell TFE731)
LEARJET 36A Learjet 35/36 (Honeywell TFE731)
LEARJET Learjet Model Learjet 45 Learjet 45 (Honeywell TFE731)
45 Learjet 40
Learjet 75
Learjet 70
LEARJET 55 Learjet 55 (Honeywell TFE731)
LEARJET 55B Learjet 55 (Honeywell TFE731)

(Part-66)
GROUP 1 AEROPLANES
LEARJET 55C Learjet 55 (Honeywell TFE731)
LEARJET 60 Learjet 60 Learjet 60 (PWC PW305)
LOCKHEED 1329-25 JetStar II Lockheed 1329 (Honeywell TFE731)
MARTIN
Corporation
LOCKHEED 1329-23D JetStar Lockheed 1329 PW (PW JT12)
MARTIN
Corporation
LOCKHEED 188A Electra Lockheed 188 (RR Corp 501)
MARTIN
Corporation
LOCKHEED 188C Electra Lockheed 188 (RR Corp 501)
MARTIN
Corporation
LOCKHEED 382G Hercules Lockheed 382 (RR Corp 501)
MARTIN
Corporation
LOCKHEED L-1011-385-1 TriStar Lockheed L-1011 (RR RB211)
MARTIN
Corporation
LOCKHEED L-1011-385-1- TriStar Lockheed L-1011 (RR RB211)
MARTIN 15
Corporation
LOCKHEED L-1011-385-3 TriStar Lockheed L-1011 (RR RB211)
MARTIN
Corporation
M7 AEROSPACE SA226-AT Fairchild SA226 Series
(Honeywell TPE331)
M7 AEROSPACE SA226-T Fairchild SA226 Series
(Honeywell TPE331)
M7 AEROSPACE SA226-T(B) Fairchild SA226 Series
(Honeywell TPE331)
M7 AEROSPACE SA226-TC Fairchild SA226 Series
(Honeywell TPE331)
M7 AEROSPACE SA227-AC Swearingen Fairchild SA227 Series
Metro (Honeywell TPE331)
M7 AEROSPACE SA227-BC Swearingen Fairchild SA227 Series
Metro (Honeywell TPE331)
M7 AEROSPACE SA227-AT Fairchild SA227 Series
(Honeywell TPE331)
M7 AEROSPACE SA227-CC Fairchild SA227 Series
(Honeywell TPE331)
M7 AEROSPACE SA227-DC Fairchild SA227 Series
(Honeywell TPE331)
M7 AEROSPACE SA227-TT Fairchild SA227 Series
(Honeywell TPE331)
M7 AEROSPACE SA227-PC Swearingen Fairchild SA227 Series (PWC PT6)
Metro

(Part-66)
GROUP 1 AEROPLANES
M7 AEROSPACE SA26AT Fairchild SA26AT (Honeywell TPE331)
M7 AEROSPACE SA-26-T Fairchild SA26-T (PWC PT6)
McDONNELL DC-10-10 DC-10/MD-10 (GE CF6)
DOUGLAS
Corporation
BOEING
COMPANY
McDONNELL DC-10-30 DC-10/MD-10 (GE CF6)
DOUGLAS
Corporation
BOEING
COMPANY
McDONNELL DC-10-30F DC-10/MD-10 (GE CF6)
DOUGLAS
Corporation
BOEING
COMPANY
McDONNELL DC-8-71 DC-8-70 DC-8 (CFM56)
DOUGLAS
Corporation
BOEING
COMPANY
McDONNELL DC-8-71F DC-8-70 DC-8 (CFM56)
DOUGLAS
Corporation
BOEING
COMPANY
DOUGLAS
Corporation
BOEING
COMPANY
DOUGLAS
Corporation
BOEING
COMPANY
McDONNELL DC-8-73F DC-8-70 DC-8 (CFM56)
DOUGLAS
Corporation
BOEING
COMPANY
McDONNELL DC-8-52 DC-8 DC-8 (PW JT3D)
DOUGLAS
Corporation
BOEING
COMPANY
DOUGLAS
Corporation

(Part-66)
GROUP 1 AEROPLANES
BOEING
COMPANY
DOUGLAS
Corporation
BOEING
COMPANY
McDONNELL DC-8F-54 DC-8 DC-8 (PW JT3D)
DOUGLAS
Corporation
BOEING
COMPANY
McDONNELL DC-8F-55 DC-8 DC-8 (PW JT3D)
DOUGLAS
Corporation
BOEING
COMPANY
McDONNELL DC-8-61 DC-8-60 DC-8 (PW JT3D)
DOUGLAS
Corporation
BOEING
COMPANY
McDONNELL DC-8-61F DC-8-60 DC-8 (PW JT3D)
DOUGLAS
Corporation
BOEING
COMPANY
DOUGLAS
Corporation
BOEING
COMPANY
DOUGLAS
Corporation
BOEING
COMPANY
DOUGLAS
Corporation
BOEING
COMPANY
DOUGLAS
Corporation
BOEING
COMPANY
McDONNELL DC-8-33 DC-8 DC-8 (PW JT4A)
DOUGLAS
Corporation

(Part-66)
GROUP 1 AEROPLANES
BOEING
COMPANY
DOUGLAS
Corporation
BOEING
COMPANY
DOUGLAS
Corporation
BOEING
COMPANY
DOUGLAS
Corporation
BOEING
COMPANY
DOUGLAS
Corporation
BOEING
COMPANY
McDONNELL DC-9-33F DC-9 DC-9 (PW JT8D)
DOUGLAS
Corporation
BOEING
COMPANY
DOUGLAS
Corporation
BOEING
COMPANY
McDONNELL DC-9-34F DC-9 DC-9 (PW JT8D)
DOUGLAS
Corporation
BOEING
COMPANY
DOUGLAS
Corporation
BOEING
COMPANY
DOUGLAS
Corporation
BOEING
COMPANY
McDONNELL 717-200 717 MD 717-200 (RRD BR700-715)
DOUGLAS
Corporation

(Part-66)
GROUP 1 AEROPLANES
BOEING
COMPANY
McDONNELL MD-11 MD-11 MD-11 (GE CF6)
DOUGLAS
Corporation
BOEING
COMPANY
McDONNELL MD-11F MD-11 MD-11 (GE CF6)
DOUGLAS
Corporation
BOEING
COMPANY
McDONNELL MD-11 MD-11 MD-11 (PW 4000)
DOUGLAS
Corporation
BOEING
COMPANY
McDONNELL MD-11F MD-11 MD-11 (PW 4000)
DOUGLAS
Corporation
BOEING
COMPANY
McDONNELL DC-9-81 (MD- MD-81 MD-80 Series (PW JT8D)
DOUGLAS 81)
Corporation
BOEING
COMPANY
DOUGLAS 82)
Corporation
BOEING
COMPANY
DOUGLAS 83)
Corporation
BOEING
COMPANY
DOUGLAS 87)
Corporation
BOEING
COMPANY
McDONNELL MD-88 MD-80 Series (PW JT8D)
DOUGLAS
Corporation
BOEING
COMPANY
McDONNELL MD-90 Series MD-90 (IAE V2500)
DOUGLAS
Corporation

(Part-66)
GROUP 1 AEROPLANES
BOEING
COMPANY
MITSUBISHI MU-2B Mitsubishi MU-2B (Honeywell
Heavy Industries TPE331)
MITSUBISHI MU-2B-10 Mitsubishi MU-2B (Honeywell
Heavy Industries (USA) TPE331)
MITSUBISHI MU-2B-26A Mitsubishi MU-2B (Honeywell
Nomad TC Pty N22 Nomad N22/24 Series (RR Corp 250)
Ltd
Nomad TC Pty N22B Nomad N22/24 Series (RR Corp 250)
Ltd
Nomad TC Pty N22C Nomad N22/24 Series (RR Corp 250)
Ltd
Nomad TC Pty N22S Nomad N22/24 Series (RR Corp 250)
Ltd
Nomad TC Pty N24 Nomad N22/24 Series (RR Corp 250)
Ltd
Nomad TC Pty N24A Nomad N22/24 Series (RR Corp 250)
Ltd
PIAGGIO Aero P.166 DP1 Piaggio P166 (PWC PT6)
Industries

(Part-66)
GROUP 1 AEROPLANES
PIAGGIO Aero P180 Avanti Piaggio P180 Avanti/Avanti II
Industries (PWC PT6)
PIAGGIO Aero P180 Avanti II Piaggio P180 Avanti/Avanti II
Industries (PWC PT6)
PILATUS PC-12 Pilatus PC-12 (PWC PT6)
AIRCRAFT
PILATUS PC-12/45 Pilatus PC-12 (PWC PT6)
AIRCRAFT
PILATUS PC-12/47 Pilatus PC-12 (PWC PT6)
AIRCRAFT
PILATUS PC-12/47E Pilatus PC-12 (PWC PT6)
AIRCRAFT
PILATUS PC-24 Pilatus PC-24 (Williams FJ44)
AIRCRAFT
PIPER AIRCRAFT PA-31T Cheyenne / Piper PA-31T Series (PWC PT6)
(Cheyenne/ Cheyenne II
Cheyenne II)
PIPER AIRCRAFT PA-31T1 Cheyenne I / Piper PA-31T Series (PWC PT6)
(Chey. I/ Cheyenne 1A
Cheyenne IA)
PIPER AIRCRAFT PA-31T2 Cheyenne IIXL Piper PA-31T Series (PWC PT6)
(Cheyenne
IIXL)
PIPER AIRCRAFT PA-31T3 T-1040 Piper PA-31T Series (PWC PT6)
PIPER AIRCRAFT PA-42-1000 Cheyenne Piper PA-42 (Honeywell TPE-331)
(Cheyenne 400LS
400LS)
PIPER AIRCRAFT PA-42 Cheyenne III Piper PA-42 (PWC PT6)
(Cheyenne III)
PIPER AIRCRAFT PA-42-720R Cheyenne III Piper PA-42 (PWC PT6)
PIPER AIRCRAFT PA-42-720 Cheyenne IIIA Piper PA-42 (PWC PT6)
(Cheyenne
IIIA)
PIPER AIRCRAFT PA-46-600TP M600 Piper PA-46-500TP/600TP (PWC PT6)
PIPER AIRCRAFT PA-46-500TP Malibu Piper PA-46-500TP/600TP (PWC PT6)
Meridian
POLSKIE PZL M28 00 PZL M 28 (PWC PT6)
ZAKLADY
LOTNICZE
ZAKLADY
LOTNICZE
ZAKLADY
LOTNICZE
PT. CN-235 CASA CN-235 (GE CT7)
DIRGANTARA
INDONESIA

(Part-66)
GROUP 1 AEROPLANES
PT. CN-235-100 CASA CN-235 (GE CT7)
DIRGANTARA
INDONESIA
PT. CN-235-110 CASA CN-235 (GE CT7)
DIRGANTARA
INDONESIA
RUAG Dornier 228- Dornier 228 (Honeywell TPE331)
Aerospace 100
GmbH
(DORNIER)
Aerospace 101
GmbH
(DORNIER)
Aerospace 200
GmbH
(DORNIER)
Aerospace 201
GmbH
(DORNIER)
Aerospace 202
GmbH
(DORNIER)
Aerospace 212
GmbH
(DORNIER)
RUAG Do 28 D-6 Dornier Do 28 Series (PWC PT6)
Aerospace
GmbH
(DORNIER)
RUAG Dornier 128-6 Dornier Do 28 Series (PWC PT6)
Aerospace
GmbH
(DORNIER)
SAAB AB, SAAB Saab SF340A Saab-Fairchild Saab (SF) 340 (GE CT7)
Aerosystems 340A
SAAB AB, SAAB Saab 340B Saab (SF) 340 (GE CT7)
Aerosystems
SAAB AB, SAAB Saab 2000 Saab 2000 (RR Corp AE2100)
Aerosystems
SHORT SC7 Series 3 Skyvan Shorts SC7 (Honeywell TPE331)
BROTHERS PLC
SHORT SD3-30 Variant 200 Shorts SD3 Series-30/SD3-60
BROTHERS PLC (PWC PT6)

(Part-66)
GROUP 1 AEROPLANES
BROTHERS PLC SHERPA (PWC PT6)
SHORT SD3-SHERPA Variant 200 Shorts SD3 Series-30/SD3-60
Textron Aviation Model 3000 Textron Defense 3000 (PWC PT6) Pending
Defense LLC (PM Series) OSD
approval.
TEXTRON 1900 Airliner Beech 1900 (PWC PT6)
AVIATION Inc.
TEXTRON 1900C Airliner Beech 1900 (PWC PT6)
AVIATION Inc.
TEXTRON 1900D Airliner Beech 1900 (PWC PT6)
AVIATION Inc.
TEXTRON 200C Beech 200 Series (PWC PT6)
AVIATION Inc.
TEXTRON 200CT Beech 200 Series (PWC PT6)
AVIATION Inc.
TEXTRON 200T Beech 200 Series (PWC PT6)
AVIATION Inc.
TEXTRON A200 Beech 200 Series (PWC PT6)
AVIATION Inc.
TEXTRON A200C Beech 200 Series (PWC PT6)
AVIATION Inc.
TEXTRON A200CT Beech 200 Series (PWC PT6)
AVIATION Inc.
TEXTRON B200 Beech 200 Series (PWC PT6)
AVIATION Inc.
TEXTRON B200C Beech 200 Series (PWC PT6)
AVIATION Inc.
TEXTRON B200CGT Beech 200 Series (PWC PT6)
AVIATION Inc.
TEXTRON B200CT Beech 200 Series (PWC PT6)
AVIATION Inc.
TEXTRON B200GT Beech 200 Series (PWC PT6)
AVIATION Inc.
TEXTRON B200T Beech 200 Series (PWC PT6)
AVIATION Inc.
TEXTRON 300 Super King Air Beech 300 Series (PWC PT6)
AVIATION Inc.
TEXTRON B300 Super King Air Beech 300 Series (PWC PT6)
AVIATION Inc. 350
TEXTRON B300C Super King Air Beech 300 Series (PWC PT6)
AVIATION Inc. 350 C
TEXTRON 390 Premier I Beech 390 (Williams FJ44)
AVIATION Inc. (RB s/n 1-101
and 103-134).

(Part-66)
GROUP 1 AEROPLANES
Premier IA
(avionics and
interior
upgrades s/n
102 and 135).
TEXTRON 65-90 King Air Beech 90 Series (PWC PT6)
AVIATION Inc.
TEXTRON 65-A90 King Air Beech 90 Series (PWC PT6)
AVIATION Inc.
TEXTRON 65-A90-1 King Air Beech 90 Series (PWC PT6)
AVIATION Inc.
AVIATION Inc.
AVIATION Inc.
AVIATION Inc.
TEXTRON B90 King Air Beech 90 Series (PWC PT6)
AVIATION Inc.
TEXTRON C90 King Air Beech 90 Series (PWC PT6)
AVIATION Inc.
TEXTRON C90A King Air Beech 90 Series (PWC PT6)
AVIATION Inc.
TEXTRON C90GT King Air Beech 90 Series (PWC PT6)
AVIATION Inc.
TEXTRON C90GTi King Air Beech 90 Series (PWC PT6)
AVIATION Inc.
TEXTRON E90 King Air Beech 90 Series (PWC PT6)
AVIATION Inc.
TEXTRON H90 King Air Beech 90 Series (PWC PT6)
AVIATION Inc.
TEXTRON A100-1 King Air Beech 99/100 Series (PWC PT6)
AVIATION Inc.
TEXTRON 402C Businessliner Cessna 400 Series (Continental)
AVIATION Inc. Utiliner
TEXTRON 414A Chancellor Cessna 400 Series (Continental)
AVIATION Inc.
TEXTRON 421B Golden Eagle Cessna 400 Series (Continental)
AVIATION Inc.
TEXTRON 421C Golden Eagle Cessna 400 Series (Continental)
AVIATION Inc.
TEXTRON 404 Titan Cessna 400 Series (Continental)
AVIATION Inc.
TEXTRON 401 Cessna 400 Series (Continental)
AVIATION Inc.
AVIATION Inc.

(Part-66)
GROUP 1 AEROPLANES
AVIATION Inc.
AVIATION Inc.
AVIATION Inc.
TEXTRON 401A Cessna 400 Series (Continental)
AVIATION Inc.
TEXTRON 401B Cessna 400 Series (Continental)
AVIATION Inc.
AVIATION Inc.
TEXTRON 402B Cessna 400 Series (Continental)
AVIATION Inc.
AVIATION Inc.
AVIATION Inc.
TEXTRON 425 Corsair / Cessna 425 (PWC PT6)
AVIATION Inc. Conquest I
TEXTRON 441 Conquest Cessna 441 (Honeywell TPE331)
AVIATION Inc.
TEXTRON 560 Citation V Cessna 500/550/560 (PWC JT15D)
AVIATION Inc. Citation Ultra
TEXTRON 500 Citation / Cessna 500/550/560 (PWC JT15D)
AVIATION Inc. Citation I
TEXTRON 550 Citation II Cessna 500/550/560 (PWC JT15D)
AVIATION Inc.
TEXTRON S550 Citation S/II C Cessna 500/550/560 (PWC JT15D)
AVIATION Inc.
TEXTRON 501 Citation I Cessna 501/551 (PWC JT15D)
AVIATION Inc.
TEXTRON 551 Citation II Cessna 501/551 (PWC JT15D)
AVIATION Inc.
TEXTRON 510 Citation Cessna 510 (PWC PW615)
AVIATION Inc. Mustang
TEXTRON 525 Citation Jet Cessna 525/525A/525B
AVIATION Inc. (CJ) (s/n 1 - (Williams FJ44)
359);
Citation Jet 1
(CJ1) (s/n 360 -
599);
Citation Jet1+
(CJ1+) (s/n
600 - 684 and
686 - 701);
M2 (s/n 800 –
and up).

(Part-66)
GROUP 1 AEROPLANES
TEXTRON 525A Citation Jet Cessna 525/525A/525B
AVIATION Inc. CJ2 (Williams FJ44)
TEXTRON 525B Citation Jet Cessna 525/525A/525B
AVIATION Inc. CJ3 (Williams FJ44)
TEXTRON 525C Citation Jet Cessna 525C (Williams FJ44)
AVIATION Inc. CJ4
TEXTRON 550 Citation Bravo Cessna 550/560 (PWC PW530/535)
AVIATION Inc.
TEXTRON 560 Citation Cessna 550/560 (PWC PW530/535)
AVIATION Inc. Encore
Citation
Encore +
TEXTRON 560XL Citation Excel Cessna 560XL/XLS (PWC PW545)
AVIATION Inc. Citation XLS
Citation XLS+
TEXTRON 650 Citation III Cessna 650 (Honeywell TFE731)
AVIATION Inc. Citation VI
Citation VII
TEXTRON 680 Citation Cessna 680 (PWC PW306)
AVIATION Inc. Sovereign
Citation
Sovereign +
TEXTRON 680A Latitude Cessna 680 (PWC PW306)
AVIATION Inc.
TEXTRON 750 Citation X Cessna 750 (RR AE3007C)
AVIATION Inc.
TEXTRON 4000 Hawker 4000 Hawker 4000 (PWC PW308)
AVIATION Inc.
TUPOLEV PSC TU 204-120CE Tupolev TU 204 (RR RB211)
Turkish TT32 HÜRKUŞ TAI TT32 (PWC PT6)
Aerospace
Industries, Inc.
(TAI)
TWIN 681 Twin Twin Commander 680/681/690/695
COMMANDER Commander Series (Honeywell TPE331)
AIRCRAFT
Corporation
AIRCRAFT
Corporation
AIRCRAFT
Corporation
TWIN 680T Twin Twin Commander 680/681/690/695
AIRCRAFT
Corporation

(Part-66)
GROUP 1 AEROPLANES
TWIN 680V Twin Twin Commander 680/681/690/695
AIRCRAFT
Corporation
TWIN 680W Twin Twin Commander 680/681/690/695
AIRCRAFT
Corporation
TWIN 690A Twin Twin Commander 680/681/690/695
AIRCRAFT
Corporation
TWIN 690B Twin Twin Commander 680/681/690/695
AIRCRAFT
Corporation
TWIN 690C Twin Twin Commander 680/681/690/695
AIRCRAFT
Corporation
TWIN 690D Twin Twin Commander 680/681/690/695
AIRCRAFT
Corporation
TWIN 695A Twin Twin Commander 680/681/690/695
AIRCRAFT
Corporation
TWIN 695B Twin Twin Commander 680/681/690/695
AIRCRAFT
Corporation
VIKING AIR DHC-6 Series Twin Otter De Havilland DHC-6 (PWC PT6) OSD
(Bombardier) 400 approved
(De Havilland) on
28.2.2017.
VIKING AIR DHC-6 Series 1 Twin Otter De Havilland DHC-6 (PWC PT6)
(Bombardier)
(De Havilland)
VIKING AIR DHC-6 Series Twin Otter De Havilland DHC-6 (PWC PT6)
(Bombardier) 100
(De Havilland)
(Bombardier) 110
(De Havilland)
(Bombardier) 200
(De Havilland)

(Part-66)
GROUP 1 AEROPLANES
(Bombardier) 210
(De Havilland)
(Bombardier) 300
(De Havilland)
(Bombardier) 310
(De Havilland)
(Bombardier) 320
(De Havilland)
VIKING AIR DHC-7-100 De Havilland DHC-7 (PWC PT6)
(Bombardier)
(De Havilland)
(Bombardier)
(De Havilland)
(Bombardier)
(De Havilland)
(Bombardier)
(De Havilland)
(Bombardier)
(De Havilland)
(Bombardier)
(De Havilland)
VULCANAIR AP68TP-300 Spartacus Vulcanair AP68TP Series
‘Spartacus’ (RR Corp 250)
VULCANAIR AP68TP-600 Viator Vulcanair AP68TP Series
‘Viator’ (RR Corp 250)
VULCANAIR SF600 Vulcanair SF600 (RR Corp 250)
VULCANAIR SF600A Vulcanair SF600 (RR Corp 250)

(Part-66)
STCs in GROUP 1 AEROPLANES

GROUP 1 AEROPLANES (STC)

STC holder Model Com. des. Part-66 type rating endorsement Note
AEROSERVIS s.r.o. L 410 UVP-E Let-410 (PWC PT6) STC not yet
released.
AEROSERVIS s.r.o. L 410 UVP-E9 Let-410 (PWC PT6) STC not yet
released.
AEROSERVIS s.r.o. L 410 UVP-E20 Let-410 (PWC PT6) STC not yet
released.
GOMOLZIG FLUGZEUG- Dornier DO 28 Dornier Do 28 (Walter M601) STC No
UND MASCHINENBAU D-2 10015031
(STC)
JET AVIATION AG (STC) Fan Jet Falcon E Falcon 20E (Honeywell TFE731)
NEXTANT AEROSPACE Beech 400A Beech 400A (Williams FJ44) STC No
L.L.C. (STC) 10042353
Sierra Industries Ltd. 501 Citation Cessna 501 (Williams FJ44) STC No
EASA.IM.A.
S.01937
THE MONROE Cessna 550 Cessna 550/S550 (Williams FJ 44) STC No
COMPANY, LLC (STC) 10053014
THE MONROE Cessna S550 Cessna 550/S550 (Williams FJ 44) STC No
COMPANY, LLC (STC) 10053014
GROUP 1 HELICOPTERS
GROUP 1 HELICOPTERS
AGUSTA AB 204 B Agusta AB204, AB205 / Bell 204, 205
(Honeywell T53)
AGUSTA AB 205 A-1 Agusta AB204, AB205 / Bell 204, 205
(Honeywell T53)
AGUSTA AS-61N Agusta AS61N/Sikorsky S-61N
(GE CT58)
AGUSTA AS-61N1 Agusta AS61N/Sikorsky S-61N
(GE CT58)
AIRBUS AS 332 C SUPER PUMA Eurocopter AS 332
HELICOPTERS Mk I (Turbomeca Makila 1A/1A1)
AIRBUS AS 332 C1 SUPER PUMA Eurocopter AS 332
AIRBUS AS 332 L SUPER PUMA Eurocopter AS 332
AIRBUS AS 332 L1 SUPER PUMA Eurocopter AS 332
AIRBUS AS 332 L2 Eurocopter AS 332 L2
HELICOPTERS (Turbomeca Makila 1A2)
AIRBUS AS 355 E Ecureuil II / Eurocopter AS 355 (RR Corp 250)
HELICOPTERS TwinStar

(Part-66)
GROUP 1 HELICOPTERS
AIRBUS AS 355 F Ecureuil II / Eurocopter AS 355 (RR Corp 250)
AIRBUS AS 355 F1 Ecureuil II / Eurocopter AS 355 (RR Corp 250)
AIRBUS AS 355 F2 Ecureuil II / Eurocopter AS 355 (RR Corp 250)
AIRBUS AS 355 N Ecureuil II / Eurocopter AS 355
HELICOPTERS TwinStar (Turbomeca Arrius 1)
AIRBUS AS 355 NP Ecureuil II / Eurocopter AS 355
HELICOPTERS TwinStar (Turbomeca Arrius 1)
AIRBUS AS 365 N3 Dauphin Eurocopter AS 365 N3
HELICOPTERS (Turbomeca Arriel 2C)
AIRBUS EC 155 B Eurocopter EC 155
HELICOPTERS (Turbomeca Arriel 2)
AIRBUS EC 155 B1 Eurocopter EC 155
AIRBUS EC 175 B Eurocopter EC 175 (PWC PT6C)
HELICOPTERS
AIRBUS EC 225 LP SUPER PUMA Eurocopter EC 225
HELICOPTERS Mk II+ or LP (Turbomeca Makila 2A)
AIRBUS SA 330 J Eurocopter SA 330
HELICOPTERS (Turbomeca Turmo)
AIRBUS SA 365 C1 Dauphin Eurocopter SA 365 C Series
AIRBUS AS 365 N2 Dauphin Eurocopter SA 365 N/N1, AS 365 N2
AIRBUS SA 365 N1 Dauphin Eurocopter SA 365 N/N1, AS 365 N2
AIRBUS SA 365 N Eurocopter SA 365 N/N1, AS 365 N2
AIRBUS EC135 P3H AIRBUS HELICOPTERS EC135 P3H
HELICOPTERS (PWC PW206)
DEUTSCHLAND
GmbH
AIRBUS EC635 P3H AIRBUS HELICOPTERS EC135 P3H
HELICOPTERS (PWC PW206)
DEUTSCHLAND
GmbH
AIRBUS EC135 T3H AIRBUS HELICOPTERS EC135 T3H
HELICOPTERS (Turbomeca Arrius 2B)
DEUTSCHLAND
GmbH

(Part-66)
GROUP 1 HELICOPTERS
AIRBUS EC635 T3H AIRBUS HELICOPTERS EC135 T3H
DEUTSCHLAND
GmbH
AIRBUS BO 105 A BO 105 series (RR Corp 250)
HELICOPTERS
DEUTSCHLAND
GmbH
AIRBUS BO 105 C BO 105 series (RR Corp 250)
HELICOPTERS
DEUTSCHLAND
GmbH
AIRBUS BO 105 D BO 105 series (RR Corp 250)
HELICOPTERS
DEUTSCHLAND
GmbH
AIRBUS BO 105 LS A-1 BO 105 series (RR Corp 250)
HELICOPTERS
DEUTSCHLAND
GmbH
AIRBUS BO 105 LS A-3 BO 105 series (RR Corp 250)
HELICOPTERS
DEUTSCHLAND
GmbH
AIRBUS BO 105 S BO 105 series (RR Corp 250)
HELICOPTERS
DEUTSCHLAND
GmbH
AIRBUS EC135 P1 Eurocopter EC 135 (PWC PW206)
HELICOPTERS (CDS)
DEUTSCHLAND
GmbH
HELICOPTERS (CPDS)
DEUTSCHLAND
GmbH
HELICOPTERS (CPDS)
DEUTSCHLAND
GmbH
AIRBUS EC135 P2+ Eurocopter EC 135 (PWC PW206)
HELICOPTERS
DEUTSCHLAND
GmbH
HELICOPTERS (CPDS)
DEUTSCHLAND
GmbH

(Part-66)
GROUP 1 HELICOPTERS
AIRBUS EC635 P2+ Eurocopter EC 135 (PWC PW206)
HELICOPTERS
DEUTSCHLAND
GmbH
HELICOPTERS (CPDS)
DEUTSCHLAND
GmbH
AIRBUS EC 135 T2+ Eurocopter EC 135
DEUTSCHLAND
GmbH
AIRBUS EC135 T1 Eurocopter EC 135
HELICOPTERS (CDS) (Turbomeca Arrius 2B)
DEUTSCHLAND
GmbH
HELICOPTERS (CPDS) (Turbomeca Arrius 2B)
DEUTSCHLAND
GmbH
DEUTSCHLAND
GmbH
DEUTSCHLAND
GmbH
DEUTSCHLAND
GmbH
AIRBUS EC635 T2+ Eurocopter EC 135
DEUTSCHLAND
GmbH
DEUTSCHLAND
GmbH
AIRBUS MBB-BK117 Eurocopter MBB-BK 117 A/B
HELICOPTERS A-1 (Honeywell LTS 101)
DEUTSCHLAND
GmbH
DEUTSCHLAND
GmbH

(Part-66)
GROUP 1 HELICOPTERS
DEUTSCHLAND
GmbH
HELICOPTERS B-1 (Honeywell LTS 101)
DEUTSCHLAND
GmbH
HELICOPTERS B-2 (Honeywell LTS 101)
DEUTSCHLAND
GmbH
AIRBUS MBB-BK117 Eurocopter MBB-BK 117 C1
HELICOPTERS C-1 (Turbomeca Arriel 1)
DEUTSCHLAND
GmbH
AIRBUS MBB-BK117 EC145 Eurocopter MBB-BK 117 C2
HELICOPTERS C-2 (Turbomeca Arriel 1)
DEUTSCHLAND
GmbH
AIRBUS MBB-BK117 EC145 Eurocopter MBB-BK 117 C2
HELICOPTERS C-2e (Turbomeca Arriel 1)
DEUTSCHLAND
GmbH
AIRBUS MBB-BK117 EC145 T2 Eurocopter MBB-BK 117 D2
HELICOPTERS D-2 (Turbomeca Arriel 2)
DEUTSCHLAND
GmbH
AIRBUS MBB-BK117 H145 Eurocopter MBB-BK 117 D2
HELICOPTERS D-2m (Turbomeca Arriel 2)
DEUTSCHLAND
GmbH
BELL 222 Bell 222 (Honeywell LTS 101)
HELICOPTER
CANADA
BELL 222B Bell 222 (Honeywell LTS 101)
HELICOPTER
CANADA
BELL 222U Bell 222 (Honeywell LTS 101)
HELICOPTER
CANADA
BELL 230 230 Executive Bell 230 (RR Corp 250)
HELICOPTER 230 Utility
CANADA 230 EMS
BELL 427 Bell 427 (PWC PW207D)
HELICOPTER
CANADA
BELL 429 Bell 429 (PWC PW207D)
HELICOPTER
CANADA

(Part-66)
GROUP 1 HELICOPTERS
BELL 430 Bell 430 (RR Corp 250)
HELICOPTER
CANADA
BELL 204B Agusta AB204, AB205 / Bell 204, 205
HELICOPTER (Honeywell T53)
TEXTRON, INC.
BELL 205A-1 Agusta AB204, AB205 / Bell 204, 205
HELICOPTER (Honeywell T53)
TEXTRON, INC.
BELL 212 Bell 212 / Agusta AB212 (PWC PT6)
HELICOPTER
TEXTRON, INC.
BELL 214B Bell 214 (Honeywell T5508)
HELICOPTER
TEXTRON, INC.
BELL 214B-1 Bell 214 (Honeywell T5508)
HELICOPTER
TEXTRON, INC.
BELL 214ST Bell 214ST (GE CT7)
HELICOPTER
TEXTRON, INC.
BELL 412 Bell 412 / Agusta AB412 (PWC PT6)
HELICOPTER
TEXTRON, INC.
BELL 412EP Bell 412 / Agusta AB412 (PWC PT6)
HELICOPTER
TEXTRON, INC.
ERICKSON AIR- S-64F Erickson S-64 (PW JFTD 12)
CRANE
KAMAN K-1200 Kaman K-1200 (Honeywell T5317)
AEROSPACE
CORPORATION
KAMOV Ka-32A11BC Kamov Ka 32 (Klimov)
LEONARDO A109K2 Agusta A109 (Turbomeca Arriel 1)
S.p.A.
LEONARDO A109S Grand Agusta A109 Series (PWC PW206/207)
S.p.A. AW109S
LEONARDO AW109SP GrandNew Agusta A109 Series (PWC PW206/207)
S.p.A.
LEONARDO A109N Nexus Agusta A109 Series (PWC PW206/207)
S.p.A. AW109N
LEONARDO A109E Power Agusta A109 Series (PWC PW206/207)
S.p.A. AW109E
LEONARDO A109 Agusta A109 Series (RR Corp 250)
S.p.A.
LEONARDO A109A Agusta A109 Series (RR Corp 250)
S.p.A.
LEONARDO A109AII Agusta A109 Series (RR Corp 250)
S.p.A.

(Part-66)
GROUP 1 HELICOPTERS
LEONARDO A109C Agusta A109 Series (RR Corp 250)
S.p.A.
LEONARDO A109LUH AW109LUH Agusta A109 Series
S.p.A. (Turbomeca Arrius 2)
LEONARDO A109E Power Agusta A109 Series
S.p.A. AW109E (Turbomeca Arrius 2)
LEONARDO AB139 Agusta AB139 / AW139 (PWC PT6)
S.p.A.
LEONARDO AW139 Agusta AB139 / AW139 (PWC PT6)
S.p.A.
LEONARDO EH 101-300 Agusta/Westland EH-101 (GE CT7)
S.p.A.
S.p.A.
S.p.A.
LEONARDO AW169 AW169 (PWC 210)
S.p.A.
LEONARDO AW189 AW189 (GE CT7)
S.p.A.
LEONARDO AB 212 Bell 212 / Agusta AB212 (PWC PT6)
S.p.A.
LEONARDO AB 412 Bell 412 / Agusta AB412 (PWC PT6)
S.p.A.
LEONARDO AB 412 EP Bell 412 / Agusta AB412 (PWC PT6)
S.p.A.
MD MD900 MD Helicopters MD900
HELICOPTERS, (PWC PW206/207)
Inc.
Philippine P-BO 105 C BO 105 series (RR Corp 250)
Aerospace
Development
Corp
Philippine P-BO 105 S BO 105 series (RR Corp 250)
Aerospace
Development
Corp
PZL-ŚWIDNIK W-3A PZL-Swidnik W-3A/W-3AS
(Rzeszow PZL-10W)
PZL-ŚWIDNIK W-3AS PZL-Swidnik W-3A/W-3AS
(Rzeszow PZL-10W)
SIKORSKY S-61N Agusta AS61N/Sikorsky S-61N
AIRCRAFT (GE CT58)
SIKORSKY S-61NM Agusta AS61N/Sikorsky S-61N
AIRCRAFT (GE CT58)
SIKORSKY S-58BT Sikorsky S-58 (PWC PT6T)
AIRCRAFT

(Part-66)
GROUP 1 HELICOPTERS
SIKORSKY S-58DT Sikorsky S-58 (PWC PT6T)
AIRCRAFT
SIKORSKY S-58ET Sikorsky S-58 (PWC PT6T)
AIRCRAFT
SIKORSKY S-58FT Sikorsky S-58 (PWC PT6T)
AIRCRAFT
SIKORSKY S-58HT Sikorsky S-58 (PWC PT6T)
AIRCRAFT
SIKORSKY S-58JT Sikorsky S-58 (PWC PT6T)
AIRCRAFT
SIKORSKY S-76A S-76A+ Sikorsky S-76 (Turbomeca Arriel 1)
AIRCRAFT S-76A++
SIKORSKY S-76A Sikorsky S-76A (RR Corp 250)
AIRCRAFT
SIKORSKY S-76B S-76B Sikorsky S-76B (PWC PT6)
AIRCRAFT
SIKORSKY S-76C Sikorsky S-76C (Turbomeca Arriel 1)
AIRCRAFT
SIKORSKY S-76C S-76C+ Sikorsky S-76C (Turbomeca Arriel 2)
AIRCRAFT S-76C++
SIKORSKY S-76D Sikorsky S-76D (PW210S)
AIRCRAFT
SIKORSKY S-92A Sikorsky S-92A (GE CT7-8)
AIRCRAFT
STCs in GROUP 1 HELICOPTERS

GROUP 1 HELICOPTERS
STC Holder Model Com. des. Part-66 type rating endorsement Note
Heli-Air Inc. (STC) Bell 222 Bell 222 (RR Corp 250)
GROUP 1 GAS AIRSHIPS (other than ELA2)

GROUP 1 GAS AIRSHIPS (other than ELA2)

TC Holder Model Com. des. Part-66 type rating endorsement NOTE
Skyship Services Skyship 600 Skyship (Porsche)
Worldwide Aeros Aeros 40B Worldwide Aeros (Continental)
Corporation
Zeppelin LZ N07-100 Zeppelin LZ N07 (Lycoming)
Luftschifftechnik
GmbH & Co KG
Zeppelin LZ N07-101 Zeppelin LZ N07 (Lycoming)
Luftschifftechnik
GmbH & Co KG

(Part-66)
SUBGROUP 2a: SINGLE TURBO-PROPELLER ENGINE AEROPLANES (other than those in Group 1)
SUBGROUP 2a: SINGLE TURBO-PROPELLER ENGINE AEROPLANES (Other than those in Group 1)
TC holder Model Com. des. Part-66 type rating endorsement Note
AERO VODOCHODY Ae 270 Aero Ae-270 (PWC PT6)
AIR TRACTOR, INC. AT-302 Air Tractor AT-302 (Lycoming LTP101)
AIR TRACTOR, INC. AT-400 Air Tractor AT-400/500/600 Series
(PWC PT6)
AIR TRACTOR, INC. AT-400A Air Tractor AT-400/500/600 Series
(PWC PT6)
(PWC PT6)
(PWC PT6)
AIR TRACTOR, INC. AT-402B Air Tractor AT-400/500/600 Series
(PWC PT6)
(PWC PT6)
(PWC PT6)
AIR TRACTOR, INC. AT-502B Air Tractor AT-400/500/600 Series
(PWC PT6)
(PWC PT6)
(PWC PT6)
(PWC PT6)
ALLIED AG CAT G-164D Grumman G-164 (PWC PT6)
Productions
ALLIED AG CAT G-164D with 73' Grumman G-164 (PWC PT6)
Productions wing gap
EADS PZL PZL-106 BT-601 EADS PZL PZL-106 BT (Walter M601)
‘WARSZAWA-OKECIE’ TURBO KRUK
EADS PZL PZL-106 BTU-34 EADS PZL PZL-106 BTU (PWC PT6)
‘WARSZAWA-OKECIE’ TURBO KRUK
GROB Aircraft AG G 120TP-A Grob G 120TP (RR Corp 250)
LEONARDO S.p.A. SF260TP Aermacchi SF260 (RR M250) ELA1
PACIFIC AEROSPACE 750XL PAC 750XL (PWC PT6)
Corporation
PILATUS AIRCRAFT PC-6/B1-H2 Pilatus PC-6 (PWC PT6) ELA2
PILATUS AIRCRAFT PC-6/B-H2 Pilatus PC-6 (PWC PT6) ELA2
PILATUS AIRCRAFT PC-6/C1-H2 Pilatus PC-6 Series ELA2
(Honeywell TPE 331)
PILATUS AIRCRAFT PC-6/C-H2 Pilatus PC-6 Series ELA2
(Honeywell TPE 331)

(Part-66)
SUBGROUP 2a: SINGLE TURBO-PROPELLER ENGINE AEROPLANES (Other than those in Group 1)
TC holder Model Com. des. Part-66 type rating endorsement Note
PILATUS AIRCRAFT PC-6/A Pilatus PC-6 Series ELA2
(Turbomeca Astazou)
PILATUS AIRCRAFT PC-6/A1-H2 Pilatus PC-6 Series ELA2
(Turbomeca Astazou)
PILATUS AIRCRAFT PC-6/A2-H2 Pilatus PC-6 Series ELA2
(Turbomeca Astazou)
PILATUS AIRCRAFT PC-6/A-H1 Pilatus PC-6 Series ELA2
(Turbomeca Astazou)
PILATUS AIRCRAFT PC-6/A-H2 Pilatus PC-6 Series ELA2
(Turbomeca Astazou)
Quest Aircraft Design Kodiak 100 Quest Kodiak 100 (PWC PT6)
LLC
SST FLUGTECHNIK EA 400-500 EXTRA 500 Extra EA-400-500 (RR Corp 250)
GmbH
TEXTRON AVIATION 208 Caravan I Cessna 208 Series (PWC PT6)
Inc.
TEXTRON AVIATION 208B Caravan II Cessna 208 Series (PWC PT6)
Inc.
THRUSH AIRCRAFT S2R-H80 Thrush S2R Series (GEAC H80)
THRUSH AIRCRAFT 600 S-2D Thrush S2R Series (PWC PT6)
THRUSH AIRCRAFT S2RHG-T34 Thrush S2R Series (PWC PT6)
THRUSH AIRCRAFT S2RHG-T65 Thrush S2R Series (PWC PT6)
THRUSH AIRCRAFT S2R-T11 Thrush S2R Series (PWC PT6)
THRUSH AIRCRAFT S2R-G1 Thrush S2R Series (TPE331)
VIKING AIR DHC-2 MK III Turbo- De Havilland DHC-2 (PWC PT6)
(Bombardier) (De (Turbo-Beaver) Beaver
Havilland)
ZLIN AIRCRAFT Z 137 T Zlin Z-37 T Series (Walter M601)
ZLIN AIRCRAFT Z 37 T Zlin Z-37 T Series (Walter M601)

(Part-66)
STCs in SUBGROUP 2a AEROPLANES

SUBGROUP 2a: SINGLE TURBO-PROPELLER ENGINE AEROPLANES (Other than those in Group 1) (STC)
AERO TWIN, Inc. Cessna 208 Cessna 208 Cessna 208/208B STC No
(STC) (Honeywell TPE331) 10033295
AERO TWIN, Inc. Cessna 208B Cessna 208B Cessna 208/208B STC No
(STC) (Honeywell TPE331) 10033295
Eichenberger P210N Cessna P210N (RR Corp 250) ELA2. STC FAA
Aviation AG (STC) SA1003NE
LBA ref.:
0779/625b
EASA ref.:
10060053
JETPROP, LLC. (STC) PA-46-350P Mirage Piper PA-46 Pressurised (PWC PT6) ELA2. STC Nos
10015707,
10016000.
JETPROP, LLC. (STC) PA-46-310P Piper PA-46 Pressurised (PWC PT6) ELA2. STC Nos
10015707,
10016000.
SOLOY, LLC (STC) 206H Cessna 206 (RR Corp 250) ELA2. STC No
10027209
SOLOY, LLC (STC) T206H Cessna 206 (RR Corp 250) ELA2. STC No
10027209
SOLOY, LLC (STC) TU206G Cessna 206 (RR Corp 250) ELA2. STC No
10027209
SOLOY, LLC (STC) U206G Cessna 206 (RR Corp 250) ELA2. STC No
10027209
SOLOY, LLC (STC) 207 Cessna 207 (RR Corp 250) ELA2. STC
SOLOY, LLC (STC) 207A Cessna 207 (RR Corp 250) ELA2. STC
SOLOY, LLC (STC) T207 Cessna 207 (RR Corp 250) ELA2. STC
SOLOY, LLC (STC) T207A Cessna 207 (RR Corp 250) ELA2. STC
SUPERVAN Cessna 208 Cessna 208 Cessna 208/208B STC No
SYSTEMS, Ltd. (STC) (Honeywell TPE331) 10033267
SUPERVAN Cessna 208B Cessna 208B Cessna 208/208B STC No
SYSTEMS, Ltd. (STC) (Honeywell TPE331) 10033267
Tradewind Beech A36 Beech 36 Series (RR Corp 250) ELA2. STC LBA
Turbines/Soloy (STC) ref.: SA 1034.
FAA STC
SA3523NM.
Tradewind Beech A36TC Beech 36 Series (RR Corp 250) ELA2. STC LBA
Turbines/Soloy (STC) ref.: SA 1034.
FAA STC
SA3523NM.
Turbine Conversions, 206 Cessna 206 (PWC PT6) ELA2. STC No
LTD (STC) 10061949
Turbine Conversions, 206H Cessna 206 (PWC PT6) ELA2. STC No
LTD (STC) 10061949
Turbine Conversions, P206 Cessna 206 (PWC PT6) ELA2. STC No
LTD (STC) 10061949

(Part-66)
Turbine Conversions, P206A Cessna 206 (PWC PT6) ELA2. STC No
LTD (STC) 10061949
Turbine Conversions, P206B Cessna 206 (PWC PT6) ELA2. STC No
LTD (STC) 10061949
Turbine Conversions, P206C Cessna 206 (PWC PT6) ELA2. STC No
LTD (STC) 10061949
Turbine Conversions, P206D Cessna 206 (PWC PT6) ELA2. STC No
LTD (STC) 10061949
Turbine Conversions, P206E Cessna 206 (PWC PT6) ELA2. STC No
LTD (STC) 10061949
Turbine Conversions, T206H Cessna 206 (PWC PT6) ELA2. STC No
LTD (STC) 10061949
Turbine Conversions, TP206A Cessna 206 (PWC PT6) ELA2. STC No
LTD (STC) 10061949
Turbine Conversions, TP206B Cessna 206 (PWC PT6) ELA2. STC No
LTD (STC) 10061949
Turbine Conversions, TP206C Cessna 206 (PWC PT6) ELA2. STC No
LTD (STC) 10061949
Turbine Conversions, TP206D Cessna 206 (PWC PT6) ELA2. STC No
LTD (STC) 10061949
Turbine Conversions, TP206E Cessna 206 (PWC PT6) ELA2. STC No
LTD (STC) 10061949
Turbine Conversions, TU206A Cessna 206 (PWC PT6) ELA2. STC No
LTD (STC) 10061949
Turbine Conversions, TU206B Cessna 206 (PWC PT6) ELA2. STC No
LTD (STC) 10061949
Turbine Conversions, TU206C Cessna 206 (PWC PT6) ELA2. STC No
LTD (STC) 10061949
Turbine Conversions, TU206D Cessna 206 (PWC PT6) ELA2. STC No
LTD (STC) 10061949
Turbine Conversions, TU206E Cessna 206 (PWC PT6) ELA2. STC No
LTD (STC) 10061949
Turbine Conversions, TU206F Cessna 206 (PWC PT6) ELA2. STC No
LTD (STC) 10061949
Turbine Conversions, TU206G Cessna 206 (PWC PT6) ELA2. STC No
LTD (STC) 10061949
Turbine Conversions, U206 Cessna 206 (PWC PT6) ELA2. STC No
LTD (STC) 10061949
Turbine Conversions, U206A Cessna 206 (PWC PT6) ELA2. STC No
LTD (STC) 10061949
Turbine Conversions, U206B Cessna 206 (PWC PT6) ELA2. STC No
LTD (STC) 10061949
Turbine Conversions, U206C Cessna 206 (PWC PT6) ELA2. STC No
LTD (STC) 10061949
Turbine Conversions, U206D Cessna 206 (PWC PT6) ELA2. STC No
LTD (STC) 10061949
Turbine Conversions, U206E Cessna 206 (PWC PT6) ELA2. STC No
LTD (STC) 10061949

(Part-66)
Turbine Conversions, U206F Cessna 206 (PWC PT6) ELA2. STC No
LTD (STC) 10061949
Turbine Conversions, U206G Cessna 206 (PWC PT6) ELA2. STC No
LTD (STC) 10061949
WEST PACIFIC AIR, B36TC Beech 36TC (PWC PT6) ELA2. STC No
LLC (STC) 10030059
SUBGROUP 2b: SINGLE TURBINE-ENGINE HELICOPTERS (other than those in Group 1)


AIRBUS AS 350 D Eurocopter AS 350 (Lycoming LTS101)
HELICOPTERS
AIRBUS AS 350 B Écureuil Eurocopter AS 350 (Turbomeca Arriel 1)
HELICOPTERS
AIRBUS AS 350 B1 Écureuil Eurocopter AS 350 (Turbomeca Arriel 1)
HELICOPTERS
HELICOPTERS
AIRBUS AS 350 BA Écureuil Eurocopter AS 350 (Turbomeca Arriel 1)
HELICOPTERS
AIRBUS AS 350 BB Écureuil Eurocopter AS 350 (Turbomeca Arriel 1)
HELICOPTERS
HELICOPTERS
AIRBUS EC 120 B Colibri Eurocopter EC 120
HELICOPTERS (Turbomeca Arrius 2F)
AIRBUS EC 130 B4 Eurocopter EC 130 (Turbomeca Arriel 2)
HELICOPTERS
AIRBUS EC 130 T2 Eurocopter EC 130 (Turbomeca Arriel 2)
HELICOPTERS
AIRBUS SA 315 B Alouette III Eurocopter SA 315B
HELICOPTERS Lama (Turbomeca Artouste)
AIRBUS SA 316 B Alouette III Eurocopter SA 316 B/SA 316 C
HELICOPTERS (Turbomeca Artouste)
AIRBUS SA 316 C Alouette III Eurocopter SA 316 B/SA 316 C
AIRBUS SE 3160 Alouette III Eurocopter SA 316 B/SA 316 C
AIRBUS SA 318 B Alouette- Eurocopter SA 318
HELICOPTERS Astazou (Turbomeca Astazou)
AIRBUS SA 318 C Alouette- Eurocopter SA 318
AIRBUS SA 3180 Alouette- Eurocopter SA 318
AIRBUS SA 319 B Alouette III Eurocopter SA 319
HELICOPTERS (Turbomeca Astazou XIV)

(Part-66)

AIRBUS SA 341 G Gazelle Eurocopter SA 341
HELICOPTERS (Turbomeca Astazou)
AIRBUS SA 342 J Gazelle Eurocopter SA 342 J
HELICOPTERS (Turbomeca Astazou XIV)
BELL HELICOPTER 407 Bell 407 (RR Corp 250)
CANADA
BELL HELICOPTER 206A Agusta AB206 / Bell 206 (RR Corp 250)
TEXTRON CANADA
LIMITED
BELL HELICOPTER 206A-1 Agusta AB206 / Bell 206 (RR Corp 250)
TEXTRON CANADA
LIMITED
BELL HELICOPTER 206B Agusta AB206 / Bell 206 (RR Corp 250)
TEXTRON CANADA
LIMITED
BELL HELICOPTER 206L Agusta AB206 / Bell 206 (RR Corp 250)
TEXTRON CANADA
LIMITED
BELL HELICOPTER 206L-1 Agusta AB206 / Bell 206 (RR Corp 250)
TEXTRON CANADA
LIMITED
TEXTRON CANADA
LIMITED
TEXTRON CANADA
LIMITED
BELL HELICOPTER 505 Bell 505 (Safran Arrius 2R)
TEXTRON CANADA
LIMITED
LEONARDO S.p.A. A119 Koala Agusta A119/ Agusta AW119MkII
(PWC PT6)
LEONARDO S.p.A. AW119MkII Koala Agusta A119/ Agusta AW119MkII
enhanced (PWC PT6)
AW119Ke
LEONARDO S.p.A. AB206 A Agusta AB206 / Bell 206 (RR Corp 250)
LEONARDO S.p.A. AB206 B Agusta AB206 / Bell 206 (RR Corp 250)
MD HELICOPTERS 369D MD Helicopters 369 Series /
INC. (MDHI) SEI NH-500D (RR Corp 250)
MD HELICOPTERS 369E MD Helicopters 369 Series /
MD HELICOPTERS 369FF MD Helicopters 369 Series /
MD HELICOPTERS 369H MD Helicopters 369 Series /
MD HELICOPTERS 369HE MD Helicopters 369 Series /

(Part-66)

MD HELICOPTERS 369HM MD Helicopters 369 Series /
MD HELICOPTERS 369HS MD Helicopters 369 Series /
MD HELICOPTERS 600N HU60 MD Helicopters 500N/600N AMD500N
INC. (MDHI) (RR Corp 250)
MD HELICOPTERS 500N MD Helicopters 500N/600N AMD500N
INC. (MDHI) (RR Corp 250)
Mecaer Aviation NH-500D MD Helicopters 369 Series /
Group SEI NH-500D (RR Corp 250)
Mecaer Aviation NH-AMD500N MD Helicopters 500N/600N AMD500N
Group (RR Corp 250)
PZL-ŚWIDNIK SW-4 PZL SW-4 (RR Corp 250)
ROBINSON R 66 Robinson R66 (RR Corp 250)
HELICOPTER
COMPANY
Schweizer RSG LLC 269D Schweizer 269D (RR Corp 250)
THE ENSTROM 480 Enstrom 480 (RR Corp 250)
HELICOPTER
CORPORATION
THE ENSTROM 480B Enstrom 480 (RR Corp 250)
HELICOPTER
CORPORATION
SUBGROUP 2c: SINGLE PISTON-ENGINE HELICOPTERS (other than those in Group 1)


TC Holder Model Comm. Des. Part-66 type rating endorsement Note
ANTARES SH-4 Silvercraft SH-4 (Franklin)
INTERNATIONAL
(Aircraft with SAS)
BRANTLY B-2 Military YHO Brantly B2 (Lycoming)
INTERNATIONAL, INC. 3BR
BRANTLY 305 Brantly B2 (Lycoming)
INTERNATIONAL, INC.
BRANTLY B-2A Brantly B2 (Lycoming)
INTERNATIONAL, INC.
BRANTLY B-2B Brantly B2 (Lycoming)
INTERNATIONAL, INC.
HELICOPTÈRES CABRI G2 Cabri Cabri G2 (Lycoming)
GUIMBAL
Mecaer Aviation NH-300C Model 300C Mecaer 269/300 (Lycoming)
Group
ROBINSON R 22 Robinson R22/R44 Series (Lycoming)
HELICOPTER
COMPANY

(Part-66)

ROBINSON R 44 Astro Raven Robinson R22/R44 Series (Lycoming)
HELICOPTER
COMPANY
ROBINSON R22 Alpha Robinson R22/R44 Series (Lycoming)
HELICOPTER
COMPANY
ROBINSON R22 Beta Robinson R22/R44 Series (Lycoming)
HELICOPTER
COMPANY
ROBINSON R22 Robinson R22/R44 Series (Lycoming)
HELICOPTER Mariner
COMPANY
ROBINSON R44 II Raven II Robinson R22/R44 Series (Lycoming)
HELICOPTER
COMPANY
SIKORSKY AIRCRAFT S-58B Sikorsky S-58 (Wright Cyclone)
SIKORSKY AIRCRAFT S-58C Sikorsky S-58 (Wright Cyclone)
SIKORSKY AIRCRAFT S-58D Sikorsky S-58 (Wright Cyclone)
SIKORSKY AIRCRAFT S-58E Sikorsky S-58 (Wright Cyclone)
SIKORSKY AIRCRAFT S-58F Sikorsky S-58 (Wright Cyclone)
SIKORSKY AIRCRAFT S-58G Sikorsky S-58 (Wright Cyclone)
SIKORSKY AIRCRAFT S-58H Sikorsky S-58 (Wright Cyclone)
SIKORSKY AIRCRAFT S-58J Sikorsky S-58 (Wright Cyclone)
Schweizer RSG LLC 269A Model 300C Schweizer 269/300 (Lycoming)
Schweizer RSG LLC 269B Model 300C Schweizer 269/300 (Lycoming)
Schweizer RSG LLC 269C Model 300C Schweizer 269/300 (Lycoming)
Schweizer RSG LLC 269C-1 Model 300C Schweizer 269/300 (Lycoming)
THE ENSTROM 280 Enstrom F-28/280 (Lycoming)
HELICOPTER
CORPORATION
THE ENSTROM 280C Enstrom F-28/280 (Lycoming)
HELICOPTER
CORPORATION
THE ENSTROM 280F Enstrom F-28/280 (Lycoming)
HELICOPTER
CORPORATION
THE ENSTROM 280FX Enstrom F-28/280 (Lycoming)
HELICOPTER
CORPORATION
THE ENSTROM F-28A Enstrom F-28/280 (Lycoming)
HELICOPTER
CORPORATION
THE ENSTROM F-28C Enstrom F-28/280 (Lycoming)
HELICOPTER
CORPORATION
THE ENSTROM F-28C-2 Enstrom F-28/280 (Lycoming)
HELICOPTER
CORPORATION

(Part-66)

THE ENSTROM F-28F Enstrom F-28/280 (Lycoming)
HELICOPTER
CORPORATION
THE ENSTROM F-28F-R Enstrom F-28/280 (Lycoming)
HELICOPTER
CORPORATION
GROUP 3: PISTON-ENGINE AEROPLANES (other than those in Group 1)


Type of Part-66 MTOM
TC Holder Model Note
structure type rating endorsement ≤2T >2T
AD Holdings, Inc T-211 Metal Thorp T-211 (Continental) ELA1 X
AD Holdings, Inc T-211 Metal Thorp T-211 (Jabiru) ELA1 X
AERO Sp.z.o.o AT-3 R100 Metal Aero AT-3 (Rotax) ELA1 X
AEROCLUBUL IAR-46 Metal IAR-46 (Rotax) ELA1 X
ROMANIEI
AEROCLUBUL IAR-46S Metal IAR-46 (Rotax) ELA1 X
ROMANIEI
Aerospool, spol. s Club Composite Aerospool Club (Rotax) ELA1 X
r. o.
AEROSTAR PA-60-601P Metal + Piper PA-60/61 Pressurised X
AIRCRAFT (Aerostar Pressurised (Lycoming)
Corporation 601P)
Corporation 602P)
Corporation 700P)
AEROSTAR PA-60-600 Metal Piper PA-60/61 Series X
AIRCRAFT (Aerostar (Lycoming)
Corporation 600)
AEROSTAR PA-60-601 Metal Piper PA-60/61 Series X
AIRCRAFT (Aerostar (Lycoming)
Corporation 601)
AIR TRACTOR, AT-250 Metal Air Tractor AT-250/300 X
INC. (PW R985)
AIR TRACTOR, AT-300 Metal Air Tractor AT-250/300 X
INC. (PW R985)
AIR TRACTOR, AT-301 Metal Air Tractor AT-301/401/501 X
INC. (PW R1340)
INC. (PW R1340)
AIR TRACTOR, AT-401B Metal Air Tractor AT-301/401/501 X
INC. (PW R1340)

(Part-66)

INC. (PW R1340)
AIR TRACTOR, AT-401A Metal Air Tractor AT-401 (PZL-3S) X
INC.
AIRBUS DEFENCE Bölkow 207 Wood Bölkow BO 207 (Lycoming) ELA1 X
AND SPACE
GmbH
AIRBUS DEFENCE Bölkow 207T Wood Bölkow BO 207 (Lycoming) ELA1 X
AND SPACE
GmbH
AIRBUS DEFENCE Bölkow BO Metal Bölkow BO 208 (Continental) ELA1 X
AND SPACE 208 C Junior
GmbH
AIRBUS DEFENCE Bölkow Metal Bölkow BO 208 (Continental) ELA1 X
AND SPACE Junior
GmbH
AIRBUS DEFENCE Bölkow BO Metal Bölkow BO 209 (Continental) ELA1 X
AND SPACE 209 S
GmbH
AIRBUS DEFENCE Bölkow BO Metal Bölkow BO 209 (Lycoming) ELA1 X
AND SPACE 209 Monsun
GmbH
AIRBUS DEFENCE 223 A1 Metal SIAT 223 (Lycoming) ELA1 X
AND SPACE
GmbH
AIRBUS DEFENCE 223 K1 Metal SIAT 223 (Lycoming) ELA1 X
AND SPACE
GmbH
AIRBUS DEFENCE 223 V Metal SIAT 223 (Lycoming) ELA1 X
AND SPACE
GmbH
AIRCRAFT Design D4 Composite (WD) D4 Fascination (Rotax) ELA1 X
and Certification Fascination
AIRCRAFT L-200 A Metal Let L 200 (LOM) ELA2 X
INDUSTRIES
AIRCRAFT L-200 D Metal Let L 200 (LOM) ELA2 X
INDUSTRIES
AIRCRAFT Z-37-2 Metal tubing Let Z-37 Series (LOM) ELA2 X
INDUSTRIES Fabric
AIRCRAFT Z-37A Metal tubing Let Z-37 Series (LOM) ELA2 X
INDUSTRIES Fabric
AIRCRAFT Z-37A-2 Metal tubing Let Z-37 Series (LOM) ELA2 X
INDUSTRIES Fabric
ALEXANDRIA 17-30 Wood + Bellanca 17-30 (Continental) ELA2 X
Aircraft LLC Metal tubing
Fabric

(Part-66)

ALEXANDRIA 17-30A Wood + Bellanca 17-30 (Continental) ELA2 X
Aircraft LLC Metal tubing
Fabric
ALEXANDRIA 17-31 Wood + Bellanca 17-31 Series ELA2 X
Aircraft LLC Metal tubing (Lycoming)
Fabric
ALEXANDRIA 17-31A Wood + Bellanca 17-31 Series ELA2 X
Fabric
ALEXANDRIA 17-31ATC Wood + Bellanca 17-31 Series ELA2 X
Fabric
ALEXANDRIA 17-31TC Wood + Bellanca 17-31 Series ELA2 X
Fabric
ALLIED AG CAT G-164 Metal Grumman G-164 (Continental) ELA2 X
Productions
ALLIED AG CAT G-164B Metal Grumman G-164 (Continental) ELA2 X
Productions
ALLIED AG CAT G-164B with Metal Grumman G-164 (Continental) ELA2 X
Productions 73’ wing gap
ALLIED AG CAT G-164B-15T Metal Grumman G-164 (Continental) ELA2 X
Productions
Productions
Productions
ALLIED AG CAT G-164 Metal Grumman G-164 (Jacobs) ELA2 X
Productions
ALLIED AG CAT G-164 Metal Grumman G-164 ELA2 X
Productions (PW R Series)
ALLIED AG CAT G-164A Metal Grumman G-164 ELA2 X
ALLIED AG CAT G-164B Metal Grumman G-164 ELA2 X
ALLIED AG CAT G-164B with Metal Grumman G-164 ELA2 X
Productions 73’ wing gap (PW R Series)
ALLIED AG CAT G-164B-15T Metal Grumman G-164 ELA2 X
ALLIED AG CAT G-164C Metal Grumman G-164 ELA2 X
ALPHA AVIATION HR 200-100 Metal Robin HR 200/ R 2000 series ELA1 X
(Lycoming)

(Part-66)

S (Lycoming)
(Lycoming)
B (Lycoming)
(Lycoming)
ALPHA AVIATION R 2100 Metal Robin HR 200/ R 2000 series ELA1 X
(Lycoming)
ALPHA AVIATION R 2100A Metal Robin HR 200/ R 2000 series ELA1 X
(Lycoming)
(Lycoming)
ALPHA AVIATION R 2120U Metal Robin HR 200/ R 2000 series ELA1 X
(Lycoming)
(Lycoming)
ALPHA AVIATION R 2160D Metal Robin HR 200/ R 2000 series ELA1 X
(Lycoming)
ALPHA AVIATION R 2160i Metal Robin HR 200/ R 2000 series ELA1 X
(Lycoming)
AMERICAN 7GCAA Wood + Champion 7 (Superior) ELA1 X
CHAMPION Metal tubing
Aircraft Corp. Fabric
AMERICAN 7GCBC Wood + Champion 7 (Superior) ELA1 X
CHAMPION (180HP) Metal tubing
AMERICAN 7ECA Wood + Champion 7 (Lycoming) ELA1 X
AMERICAN 7GCAA Wood + Champion 7 (Lycoming) ELA1 X
AMERICAN 7GCBC Wood + Champion 7 (Lycoming) ELA1 X
CHAMPION (160HP) Metal tubing
AMERICAN 8GCBC Wood + Champion 8 Series (Lycoming) ELA1 X
AMERICAN 8KCAB Wood + Champion 8 Series (Lycoming) ELA1 X
AQUILA Aviation AQUILA Composite Aquila AT01 (Rotax) ELA1 X
by Excellence AG AT01
AQUILA Aviation AQUILA Composite Aquila AT01 (Rotax) ELA1 X
by Excellence AG AT01-100

(Part-66)

AUGUSTAIR, INC. VARGA 2180 Metal Varga (Lycoming) ELA1 X
AUGUSTAIR, INC. VARGA Metal Varga (Lycoming) ELA1 X
2150A
AUGUSTAIR, INC. VARGA 2150 Metal Varga (Lycoming) ELA1 X
AVIAT AIRCRAFT A-1 Metal Aviat Husky A (Lycoming) ELA1 X
INC
AVIAT AIRCRAFT A-1A Metal Aviat Husky A (Lycoming) ELA1 X
INC
AVIAT AIRCRAFT A-1B Metal Aviat Husky A (Lycoming) ELA1 X
INC
AVIAT AIRCRAFT A-1C-180 Metal Aviat Husky A (Lycoming) ELA1 X
INC
AVIAT AIRCRAFT S-1S Wood + Pitts S-1 Series (Lycoming) ELA1 X
INC Metal tubing
Fabric
AVIAT AIRCRAFT S-2A Wood + Pitts S-2 Series (Lycoming) ELA1 X
INC Metal tubing
Fabric
AVIAT AIRCRAFT S-2B Wood + Pitts S-2 Series (Lycoming) ELA1 X
INC Metal tubing
Fabric
AVIAT AIRCRAFT S-2C Wood + Pitts S-2 Series (Lycoming) ELA1 X
INC Metal tubing
Fabric
AVIAT AIRCRAFT S-2S Wood + Pitts S-2 Series (Lycoming) ELA1 X
INC Metal tubing
Fabric
BEECHCRAFT 19A Metal Beech 19 Series (Lycoming) ELA2 X
Corporation
BEECHCRAFT B19 Metal Beech 19 Series (Lycoming) ELA2 X
Corporation
BEECHCRAFT M19A Metal Beech 19 Series (Lycoming) ELA2 X
Corporation
BEECHCRAFT 23 Metal Beech 23 Series (Lycoming) ELA2 X
Corporation
BEECHCRAFT A23-19 Metal Beech 23 Series (Lycoming) ELA2 X
Corporation
BEECHCRAFT A23-24 Metal Beech 23 Series (Lycoming) ELA2 X
Corporation
BEECHCRAFT B23 Metal Beech 23 Series (Lycoming) ELA2 X
Corporation
BEECHCRAFT C23 Metal Beech 23 Series (Lycoming) ELA2 X
Corporation
BEECHCRAFT A24 Metal Beech 24 Series (Lycoming) ELA2 X
Corporation
BEECHCRAFT A24R Metal Beech 24 Series (Lycoming) ELA2 X
Corporation

(Part-66)

BEECHCRAFT B24R Metal Beech 24 Series (Lycoming) ELA2 X
Corporation
BEECHCRAFT C24R Metal Beech 24 Series (Lycoming) ELA2 X
Corporation
BEECHCRAFT 50 Metal Beech 50 Series (Lycoming) X
Corporation
BEECHCRAFT B50 Metal Beech 50 Series (Lycoming) X
Corporation
BEECHCRAFT C50 Metal Beech 50 Series (Lycoming) X
Corporation
BEECHCRAFT D50 Metal Beech 50 Series (Lycoming) X
Corporation
BEECHCRAFT D50A Metal Beech 50 Series (Lycoming) X
Corporation
BEECHCRAFT D50B Metal Beech 50 Series (Lycoming) X
Corporation
BEECHCRAFT D50C Metal Beech 50 Series (Lycoming) X
Corporation
BEECHCRAFT D50E Metal Beech 50 Series (Lycoming) X
Corporation
BEECHCRAFT D50E-5990 Metal Beech 50 Series (Lycoming) X
Corporation
BEECHCRAFT E50 Metal Beech 50 Series (Lycoming) X
Corporation
BEECHCRAFT F50 Metal Beech 50 Series (Lycoming) X
Corporation
BEECHCRAFT G50 Metal Beech 50 Series (Lycoming) X
Corporation
BEECHCRAFT H50 Metal Beech 50 Series (Lycoming) X
Corporation
BEECHCRAFT J50 Metal Beech 50 Series (Lycoming) X
Corporation
BEECHCRAFT 58P Metal + Beech 58P (Continental) X
Corporation Pressurised
BEECHCRAFT 58PA Metal + Beech 58P (Continental) X
Corporation Pressurised
BEECHCRAFT 58TC Metal Beech 58TC (Continental) X
Corporation
BEECHCRAFT 58TCA Metal Beech 58TC (Continental) X
Corporation
BEECHCRAFT 60 Metal Beech 60 Series (Lycoming) X
Corporation
BEECHCRAFT A60 Metal Beech 60 Series (Lycoming) X
Corporation
BEECHCRAFT B60 Metal Beech 60 Series (Lycoming) X
Corporation

(Part-66)

BEECHCRAFT 76 Metal Beech 76 (Lycoming) ELA2 X
Corporation
BEECHCRAFT 77 Metal Beech 77 (Lycoming) ELA2 X
Corporation
BEECHCRAFT A23 Metal Beech A23 (Continental) ELA2 X
Corporation
BEECHCRAFT A23A Metal Beech A23 (Continental) ELA2 X
Corporation
BERIEV Be 103 Metal Beriev Be-103 (Continental) X
Bernd R 90-230RG Composite Ruschmeyer R90-230RG ELA2 X
Hager/Anatoli (Lycoming)
Stobbe GbR
BLACKSHAPE BS 115 Composite Blackshape (Rotax) ELA1 X
S.p.A.
B-N GROUP Ltd. BN.2A MARK Metal Britten-Norman BN.2A Mark III X
(Britten-Norman) III (Lycoming)
(Britten-Norman) III-1 (Lycoming)
B-N GROUP Ltd. BN2 Metal Britten-Norman BN2A Series X
(Britten-Norman) (Lycoming)
B-N GROUP Ltd. BN2A Metal Britten-Norman BN2A Series X
B-N GROUP Ltd. BN2A-2 Metal Britten-Norman BN2A Series X

(Part-66)

B-N GROUP Ltd. BN2B-20 Metal Britten-Norman BN2B Series X
Breezer Aircraft B600 Metal Breezer B600 (Rotax) ELA1 X
GmbH & Co. KG
CEAPR CAP10 Wood CAP 10 (Lycoming) ELA1 X
CEAPR CAP10B Wood CAP 10 (Lycoming) ELA1 X
CEAPR CAP20 Wood CAP 20/21 (Lycoming) ELA1 X
CEAPR CAP20L/S20 Wood CAP 20/21 (Lycoming) ELA1 X
0
CEAPR CAP21 Wood CAP 20/21 (Lycoming) ELA1 X
CEAPR CAP231 Wood CAP 230 Series (Lycoming) ELA1 X
CEAPR CAP231EX Composite + CAP 230 Series (Lycoming) ELA1 X
Wood
CEAPR CAP232 Composite + CAP 230 Series (Lycoming) ELA1 X
Wood
CEAPR CAP230 Wood CAP 230 Series (Lycoming) ELA1 X
CEAPR ATL Wood + Robin ATL / ATL S (JPX 4T60) ELA1 X
Composite
CEAPR ATL S Wood + Robin ATL / ATL S ELA1 X
Composite (JPX 4T60)
CEAPR ATL L Wood + Robin ATL L ELA1 X
Composite (Limbach L2000)
CEAPR DR 200 Wood Robin DR 200 series (Potez) ELA1 X
CEAPR DR 220 Wood Robin DR 220 series ELA1 X
(Continental)
CEAPR DR 220 A Wood Robin DR 220 series ELA1 X
(Continental)
CEAPR DR 220 AB Wood Robin DR 220 series ELA1 X
(Continental)
CEAPR DR 220 B Wood Robin DR 220 series ELA1 X
(Continental)
CEAPR DR 221 Wood Robin DR 221 series (Lycoming) ELA1 X
CEAPR DR 221 B Wood Robin DR 221 series (Lycoming) ELA1 X
CEAPR DR 250 B- Wood Robin DR 250 series (Lycoming) ELA1 X
160
CEAPR DR 250-160 Wood Robin DR 250 series (Lycoming) ELA1 X

(Part-66)

CEAPR DR 300/108 Wood Robin DR 300 series (Lycoming) ELA1 X
R
CEAPR DR 400/125 i Wood Robin DR 400 series ELA1 X
(Continental)
CEAPR DR 400/200 I Wood Robin DR 400 series (Lycoming) ELA1 X
A
D
B
D
R
S
CEAPR DR 400/2+2 Wood Robin DR 400 series (Lycoming) ELA1 X
R
CEAPR DR 400/NGL Wood Robin DR 400 series (Lycoming) ELA1 X
CEAPR DR 400/RP Wood Robin DR 400RP (Porsche) ELA1 X
CEAPR HR 100-210 Metal Robin HR 100 series ELA1 X
(Continental)
D (Continental)
C (Continental)

(Part-66)

TIARA (Continental)
CEAPR HR 100-200 Metal Robin HR 100 series (Lycoming) ELA1 X
B
TR
CEAPR R 1180 T Metal Robin R 1180 series (Lycoming) ELA1 X
CEAPR R 1180 TD Metal Robin R 1180 series (Lycoming) ELA1 X
CEAPR R 3000/100 Metal Robin R 3000 series (Lycoming) ELA1 X
D
S
CESSNA AIRCRAFT F177RG Metal Cessna 177 Series (Lycoming) ELA2 X
Company
CESSNA AIRCRAFT F150F Metal Cessna/Reims-Cessna ELA1 X
Company 150/F150 Series (Continental)
CESSNA AIRCRAFT F150G Metal Cessna/Reims-Cessna ELA1 X
CESSNA AIRCRAFT F150H Metal Cessna/Reims-Cessna ELA1 X
CESSNA AIRCRAFT F150J Metal Cessna/Reims-Cessna ELA1 X
CESSNA AIRCRAFT F150K Metal Cessna/Reims-Cessna ELA1 X
CESSNA AIRCRAFT F150L Metal Cessna/Reims-Cessna ELA1 X
CESSNA AIRCRAFT F150M Metal Cessna/Reims-Cessna ELA1 X
CESSNA AIRCRAFT FA150K Metal Cessna/Reims-Cessna ELA1 X
CESSNA AIRCRAFT FA150L Metal Cessna/Reims-Cessna ELA1 X
CESSNA AIRCRAFT FA150M Metal Cessna/Reims-Cessna ELA1 X
CESSNA AIRCRAFT FRA150L Metal Cessna/Reims-Cessna ELA1 X
CESSNA AIRCRAFT FRA150M Metal Cessna/Reims-Cessna ELA1 X
CESSNA AIRCRAFT F152 Metal Cessna/Reims-Cessna ELA1 X
Company 152/F152 Series (Lycoming)

(Part-66)

CESSNA AIRCRAFT FA152 Metal Cessna/Reims-Cessna ELA1 X
CESSNA AIRCRAFT F172D Metal Cessna/Reims-Cessna ELA1 X
CESSNA AIRCRAFT F172E Metal Cessna/Reims-Cessna ELA1 X
CESSNA AIRCRAFT F172F Metal Cessna/Reims-Cessna ELA1 X
CESSNA AIRCRAFT F172G Metal Cessna/Reims-Cessna ELA1 X
CESSNA AIRCRAFT F172H Metal Cessna/Reims-Cessna ELA1 X
CESSNA AIRCRAFT F172K Metal Cessna/Reims-Cessna ELA1 X
CESSNA AIRCRAFT FP172D Metal Cessna/Reims-Cessna ELA1 X
CESSNA AIRCRAFT FR172E Metal Cessna/Reims-Cessna ELA2 X
CESSNA AIRCRAFT FR172F Metal Cessna/Reims-Cessna ELA2 X
CESSNA AIRCRAFT FR172G Metal Cessna/Reims-Cessna ELA2 X
CESSNA AIRCRAFT FR172H Metal Cessna/Reims-Cessna ELA2 X
CESSNA AIRCRAFT FR172J Metal Cessna/Reims-Cessna ELA2 X
CESSNA AIRCRAFT FR172K Metal Cessna/Reims-Cessna ELA2 X
CESSNA AIRCRAFT F172L Metal Cessna/Reims-Cessna ELA1 X
CESSNA AIRCRAFT F172M Metal Cessna/Reims-Cessna ELA1 X
CESSNA AIRCRAFT F172N Metal Cessna/Reims-Cessna ELA1 X
CESSNA AIRCRAFT F172P Metal Cessna/Reims-Cessna ELA1 X
CESSNA AIRCRAFT F182P Metal Cessna/Reims-Cessna ELA2 X
CESSNA AIRCRAFT F182Q Metal Cessna/Reims-Cessna ELA2 X
CESSNA AIRCRAFT FR182 Metal Cessna/Reims-Cessna ELA2 X
CESSNA AIRCRAFT F337E Metal Cessna/Reims-Cessna 337 X
Company Series (Continental)
(not pressurised)

(Part-66)

CESSNA AIRCRAFT F337F Metal Cessna/Reims-Cessna 337 X
(not pressurised)
CESSNA AIRCRAFT F337G Metal Cessna/Reims-Cessna 337 X
(not pressurised)
CESSNA AIRCRAFT F337H Metal Cessna/Reims-Cessna 337 X
(not pressurised)
CESSNA AIRCRAFT FT337E Metal Cessna/Reims-Cessna 337 X
(not pressurised)
CESSNA AIRCRAFT FT337F Metal Cessna/Reims-Cessna 337 X
(not pressurised)
CESSNA AIRCRAFT FT337GP Metal + Cessna/Reims-Cessna 337 X
Company Pressurised Series (Continental)
(pressurised)
CESSNA AIRCRAFT FT337HP Metal + Cessna/Reims-Cessna 337 X
Company Pressurised Series (Continental)
(pressurised)
CIRRUS Design SR20 Composite Cirrus SR20 / SR22 / SR22T ELA2 X
Corporation Series (Continental)
CIRRUS Design SR22 Composite Cirrus SR20 / SR22 / SR22T ELA2 X
CIRRUS Design SR22T Composite Cirrus SR20 / SR22 / SR22T ELA2 X
COMMANDER 112 Metal Commander 112 (Lycoming) ELA1 X
PREMIER
AIRCRAFT CO.
COMMANDER 112B Metal Commander 112 (Lycoming) ELA1 X
PREMIER
AIRCRAFT CO.
COMMANDER 112TC Metal Commander 112 (Lycoming) ELA1 X
PREMIER
AIRCRAFT CO.
COMMANDER 112TCA Metal Commander 112 (Lycoming) ELA1 X
PREMIER
AIRCRAFT CO.
COMMANDER 114 Metal Commander 114 (Lycoming) ELA2 X
PREMIER
AIRCRAFT CO.
COMMANDER 114A Metal Commander 114 (Lycoming) ELA2 X
PREMIER
AIRCRAFT CO.
COMMANDER 114B Metal Commander 114 (Lycoming) ELA2 X
PREMIER
AIRCRAFT CO.

(Part-66)

COMMANDER 114TC Metal Commander 114 (Lycoming) ELA2 X
PREMIER
AIRCRAFT CO.
CUB CRAFTERS, CC19-180 Metal tubing Cub Crafters 19-180 (Lycoming) ELA1 X
Inc. Fabric
Czech Sport PS-28 Metal Czech Sport PS-28 (Rotax) ELA1 X
Aircraft a.s. Cruiser
DAHER MS 880 B Metal SOCATA MS 880/885 ELA1 X
AEROSPACE (Continental)
DAHER MS 880 B-D Metal SOCATA MS 880/885 ELA1 X
DAHER MS 885 Metal SOCATA MS 880/885 ELA1 X
DAHER MS 881 Metal SOCATA MS 881 (Potez) ELA1 X
AEROSPACE
DAHER MS 884 Metal SOCATA MS 884/894/PZL ELA1 X
AEROSPACE Koliber (Franklin)
DAHER MS 894 A Metal SOCATA MS 884/894/PZL ELA1 X
DAHER MS 894 C Metal SOCATA MS 884/894/PZL ELA1 X
DAHER MS 894 E Metal SOCATA MS 884/894/PZL ELA1 X
DAHER MS 890 A Metal SOCATA MS 890 (Continental) ELA1 X
AEROSPACE
DAHER MS 890 B Metal SOCATA MS 890 (Continental) ELA1 X
AEROSPACE
DAHER MS 883 Metal SOCATA MS 892/883/886/887 ELA1 X
AEROSPACE (Lycoming)
AEROSPACE A.150 (Lycoming)
AEROSPACE B.150 (Lycoming)
AEROSPACE E.150 (Lycoming)
DAHER MS 892 E- Metal SOCATA MS 892/883/886/887 ELA1 X
AEROSPACE D.150 (Lycoming)
DAHER MS 893 A Metal SOCATA MS 892/883/886/887 ELA1 X
DAHER MS 893 B Metal SOCATA MS 892/883/886/887 ELA1 X
DAHER MS 893 E Metal SOCATA MS 892/883/886/887 ELA1 X

(Part-66)

DAHER MS 893 E-D Metal SOCATA MS 892/883/886/887 ELA1 X
DAHER RALLYE 100 Metal SOCATA Rallye Series ELA1 X
AEROSPACE S (Continental)
AEROSPACE S-D (Continental)
AEROSPACE ST (Continental)
AEROSPACE ST-D (Continental)
AEROSPACE ST (Lycoming)
AEROSPACE ST (Lycoming)
AEROSPACE ST-D (Lycoming)
AEROSPACE SV (Lycoming)
AEROSPACE SVS (Lycoming)
AEROSPACE T (Lycoming)
AEROSPACE T-D (Lycoming)
AEROSPACE T (Lycoming)
AEROSPACE T-D (Lycoming)
AEROSPACE TS (Lycoming)
AEROSPACE A (Lycoming)
AEROSPACE C (Lycoming)
AEROSPACE E (Lycoming)
AEROSPACE E-D (Lycoming)
AEROSPACE F (Lycoming)
DAHER TB 10 Metal SOCATA TB Series (Lycoming) ELA1 X
AEROSPACE
AEROSPACE
AEROSPACE

(Part-66)

AEROSPACE
AEROSPACE
DE HAVILLAND Beagle series Metal Beagle B.121 series 1 ELA1 X
Support (Aircraft 1. (Continental)
with SAS)
DE HAVILLAND Beagle series Metal Beagle B.121 series 2/3 ELA1 X
Support (Aircraft 2/3. (Lycoming)
with SAS)
DECOURT DMS 884-1 Wood Decourt DMS 884 (Franklin) ELA1 X
(Aircraft with
SAS)
DIAMOND DA 42 M-NG Composite Diamond DA42 Series (Austro ELA2. X
MTOM >2T
AIRCRAFT Engine)
with MÄM
Industries 42-659 and
MÄM 42-
678 and
OÄM 42-
260. Ref.:
TCDS
DIAMOND DA 42 NG Composite Diamond DA42 Series (Austro ELA2. X
MTOM >2T
AIRCRAFT Engine)
with MÄM
Industries 42-659 and
MÄM 42-
678 and
OÄM 42-
260. Ref.:
TCDS
DIAMOND DA 42 Composite Diamond DA42 Series ELA2 X
AIRCRAFT (Technify)
Industries
DIAMOND DA 42 M Composite Diamond DA42 Series ELA2 X
AIRCRAFT (Technify)
Industries
DIAMOND DA20-C1 Composite Diamond DA20 (Continental) ELA1 X
AIRCRAFT
Industries
DIAMOND DA20-A1 Composite Diamond DA20/DV20 (Rotax) ELA1 X
AIRCRAFT
Industries
DIAMOND DV 20 Composite Diamond DA20/DV20 (Rotax) ELA1 X
AIRCRAFT
Industries
DIAMOND DV 20 E Composite Diamond DA20/DV20 (Rotax) ELA1 X
AIRCRAFT
Industries
DIAMOND DA 40 NG Composite Diamond DA40 (Austro Engine) ELA2 X
AIRCRAFT
Industries

(Part-66)

DIAMOND DA 40 Composite Diamond DA40 (Lycoming) ELA2 X
AIRCRAFT
Industries
DIAMOND DA 40 F Composite Diamond DA40 (Lycoming) ELA2 X
AIRCRAFT
Industries
DIAMOND DA 40 D Composite Diamond DA40 D (Technify) ELA2 X
AIRCRAFT
Industries
DIAMOND DA 62 Composite Diamond DA62 (Austro Engine) X
AIRCRAFT
Industries
DYNAC Aero Metal Aerocommander 100 ELA1 X
AEROSPACE Commander (Lycoming)
Corporation 100
E.I.S Aircraft RS 180 Wood + RS 180 (Lycoming) ELA1 X
GmbH Composite
E.I.S. HOLDING RS 180 Wood + Sportavia Putzer RS180 ELA1 X
GmbH Composite (Lycoming)
EADS PZL PZL-106 Metal PZL-106 Series (PZL) X
‘WARSZAWA- series
OKECIE’ (Aircraft
with SAS)
EVEKTOR EV-97 VLA Metal Evektor EV-97 (Rotax) ELA1 X
EVEKTOR SportStar Metal SportStar RTC (Rotax) ELA1 X
RTC
EXTRA EA 300 Composite Extra EA-300 Series (Lycoming) ELA1 X
Flugzeugprodukti
ons- und
Vertriebs-GmbH
EXTRA EA 300/200 Composite Extra EA-300 Series (Lycoming) ELA1 X
Flugzeugprodukti
ons- und
Vertriebs-GmbH
EXTRA EA 300/L Composite Extra EA-300 Series (Lycoming) ELA1 X
Flugzeugprodukti
ons- und
Vertriebs-GmbH
EXTRA EA 300/LC Composite Extra EA-300 Series (Lycoming) ELA1 X
Flugzeugprodukti
ons- und
Vertriebs-GmbH
EXTRA EA 300/LT Composite Extra EA-300 Series (Lycoming) ELA1 X
Flugzeugprodukti
ons- und
Vertriebs-GmbH
EXTRA EA 300/S Composite Extra EA-300 Series (Lycoming) ELA1 X
Flugzeugprodukti

(Part-66)

ons- und
Vertriebs-GmbH
EXTRA EA 300/SC Composite Extra EA-300 Series (Lycoming) ELA1 X
Flugzeugprodukti
ons- und
Vertriebs-GmbH
FFT GYROFLUG SC01 Series Composite SC01 Series (Lycoming) ELA1 X
(Aircraft with
SAS)
Flight Design CTLS-ELA Composite CTLS-ELA (Rotax) ELA1 X
GmbH
FLS AEROSPACE Club Sprint Metal Club Sprint/Sprint 160 ELA1 X
(Aircraft with Sprint 160 (Lycoming)
SAS)
FLS AEROSPACE OA7 Series Metal OA7 Optica Series (Lycoming) ELA2 X
(Aircraft with
SAS)
FUJI Heavy FA-200-160 Metal Fuji FA-200 Series (Lycoming) ELA1 X
Industries
FUJI Heavy FA-200-180 Metal Fuji FA-200 Series (Lycoming) ELA1 X
Industries
FUJI Heavy FA-200- Metal Fuji FA-200 Series (Lycoming) ELA1 X
Industries 180AO
GA8 Airvan Pty GA8 Metal Gippsland GA8 (Lycoming) ELA2 X
Ltd
GA8 Airvan Pty GA8-TC 320 Metal Gippsland GA8 (Lycoming) ELA2 X
Ltd
Game Composite GB1 Composite GameBird1 (Lycoming) ELA1 X
LLC GameBird
GARDAN (Aircraft GY80 Series Metal Gardan GY 80 (Lycoming) ELA1 X
with SAS)
GENERAL AVIA F.20 Pegaso Metal General Avia F.20 Series X
Costruzioni (Continental)
Aeronautiche
(Aircraft with
SAS)
GENERAL AVIA F.22 series Metal General Avia F.22 (Lycoming) ELA1 X
Costruzioni
Aeronautiche
(Aircraft with
SAS)
GOMOLZIG AS202/15 Metal AS202 Series (Lycoming) ELA1 X
FLUGZEUG- UND
MASCHINENBAU
GmbH
GOMOLZIG AS202/15-1 Metal AS202 Series (Lycoming) ELA1 X
FLUGZEUG- UND

(Part-66)

MASCHINENBAU
GmbH
GOMOLZIG AS202/18A Metal AS202 Series (Lycoming) ELA1 X
FLUGZEUG- UND
MASCHINENBAU
GmbH
GOMOLZIG AS202/18A1 Metal AS202 Series (Lycoming) ELA1 X
FLUGZEUG- UND
MASCHINENBAU
GmbH
FLUGZEUG- UND
MASCHINENBAU
GmbH
FLUGZEUG- UND
MASCHINENBAU
GmbH
FLUGZEUG- UND
MASCHINENBAU
GmbH
GROB Aircraft AG G 115 Composite Grob G115/120 Series ELA1 X
(Lycoming)
GROB Aircraft AG G 115A Composite Grob G115/120 Series ELA1 X
(Lycoming)
GROB Aircraft AG G 115B Composite Grob G115/120 Series ELA1 X
(Lycoming)
GROB Aircraft AG G 115C Composite Grob G115/120 Series ELA1 X
(Lycoming)
GROB Aircraft AG G 115C2 Composite Grob G115/120 Series ELA1 X
(Lycoming)
GROB Aircraft AG G 115D Composite Grob G115/120 Series ELA1 X
(Lycoming)
GROB Aircraft AG G 115D2 Composite Grob G115/120 Series ELA1 X
(Lycoming)
GROB Aircraft AG G 115E Composite Grob G115/120 Series ELA1 X
(Lycoming)
GROB Aircraft AG G 115EG Composite Grob G115/120 Series ELA1 X
(Lycoming)
GROB Aircraft AG G 115TA Composite Grob G115/120 Series ELA2 X
(Lycoming)
GROB Aircraft AG G 120A Composite Grob G115/120 Series ELA2 X
(Lycoming)
GROB Aircraft AG G 120A-I Composite Grob G115/120 Series ELA2 X
(Lycoming)
Hoffmann GmbH H 40 Composite H 40 (Lycoming) ELA1 X
& Co. KG

(Part-66)

INSTYTUT I-23 Composite Instytut Lotnictwa I-23 ELA1 X
LOTNICTWA ‘Manager’ Manager (Lycoming)
INTERCEPTOR 200D Metal Aerocommander 200 ELA2 X
AIRCRAFT (Continental)
Corporation
ISSOIRE APM 20 Composite Issoire APM 20/30 (Rotax) ELA1 X
AVIATION
ISSOIRE APM 30 Composite Issoire APM 20/30 (Rotax) ELA1 X
AVIATION
ISSOIRE APM 40 Composite Issoire APM 40 (Continental) ELA1 X
AVIATION
LAVIA PA-25 Metal Piper PA-25 Series (Lycoming) ELA2 X
ARGENTINA S.A.
(LAVIASA)
LAVIA PA-25-235 Metal Piper PA-25 Series (Lycoming) ELA2 X
ARGENTINA S.A.
(LAVIASA)
LAVIA PA-25-260 Metal Piper PA-25 Series (Lycoming) ELA2 X
ARGENTINA S.A.
(LAVIASA)
LEONARDO S.p.A. F260 Metal Aermacchi F260 Series ELA1 X
(Lycoming)
LEONARDO S.p.A. F260B Metal Aermacchi F260 Series ELA1 X
(Lycoming)
LEONARDO S.p.A. F260C Metal Aermacchi F260 Series ELA1 X
(Lycoming)
LEONARDO S.p.A. F260D Metal Aermacchi F260 Series ELA1 X
(Lycoming)
LEONARDO S.p.A. F260E Metal Aermacchi F260 Series ELA1 X
(Lycoming)
LEONARDO S.p.A. F260F Metal Aermacchi F260 Series ELA1 X
(Lycoming)
LEONARDO S.p.A. S205-22/R Metal SIAI-Marchetti S.205 (Franklin) ELA2 X
LEONARDO S.p.A. S205-18/F Metal SIAI-Marchetti S.205/S.208 ELA1 X
(Lycoming)
LEONARDO S.p.A. S205-18/R Metal SIAI-Marchetti S.205/S.208 ELA1 X
(Lycoming)
LEONARDO S.p.A. S205-20/F Metal SIAI-Marchetti S.205/S.208 ELA2 X
(Lycoming)
LEONARDO S.p.A. S205-20/R Metal SIAI-Marchetti S.205/S.208 ELA2 X
(Lycoming)
LEONARDO S.p.A. S208 Metal SIAI-Marchetti S.205/S.208 ELA2 X
(Lycoming)
LEONARDO S.p.A. S208A Metal SIAI-Marchetti S.205/S.208 ELA2 X
(Lycoming)

(Part-66)

LIBERTY XL-2 Composite Liberty XL-2 (Continental) ELA1 X
AEROSPACE
Incorporated
Light Wing AG LightWing Metal tubing Lightwing AC4 (Rotax) ELA1 X
AC4 Fabric
Magnaghi Sky Arrow Composite III Sky Arrow 650/710 (Rotax) ELA1 X
Aeronautica 650 TC
S.p.A. (INIZIATIVE
INDUSTRIALI
ITALIANE)
Aeronautica 650 TCN
S.p.A. (INIZIATIVE
INDUSTRIALI
ITALIANE)
Aeronautica 650 TCNS
S.p.A. (INIZIATIVE
INDUSTRIALI
ITALIANE)
Aeronautica 650 TCS
S.p.A. (INIZIATIVE
INDUSTRIALI
ITALIANE)
Aeronautica 710 RG
S.p.A. (INIZIATIVE
INDUSTRIALI
ITALIANE)
MAULE Bee Dee M-4 Metal tubing Maule M4 (Continental) ELA1 X
AEROSPACE Fabric
TECHNOLOGY
MAULE M-4 Metal tubing Maule M4 (Continental) ELA1 X
AEROSPACE Fabric
TECHNOLOGY
MAULE M-4-210 Metal tubing Maule M4 (Continental) ELA1 X
AEROSPACE Fabric
TECHNOLOGY
MAULE M-4-210C Metal tubing Maule M4 (Continental) ELA1 X
AEROSPACE Fabric
TECHNOLOGY
MAULE M-4C Metal tubing Maule M4 (Continental) ELA1 X
AEROSPACE Fabric
TECHNOLOGY
MAULE M-4S Metal tubing Maule M4 (Continental) ELA1 X
AEROSPACE Fabric
TECHNOLOGY

(Part-66)

MAULE M-4T Metal tubing Maule M4 (Continental) ELA1 X
AEROSPACE Fabric
TECHNOLOGY
MAULE M-4-220 Metal tubing Maule M4 (Franklin) ELA1 X
AEROSPACE Fabric
TECHNOLOGY
MAULE M-4-220C Metal tubing Maule M4 (Franklin) ELA1 X
AEROSPACE Fabric
TECHNOLOGY
MAULE M-4-220S Metal tubing Maule M4 (Franklin) ELA1 X
AEROSPACE Fabric
TECHNOLOGY
MAULE M-4-180V Metal tubing Maule M4 (Lycoming) ELA1 X
AEROSPACE Fabric
TECHNOLOGY
MAULE M-5-180C Metal tubing Maule M5 (Lycoming) ELA1 X
AEROSPACE Fabric
TECHNOLOGY
AEROSPACE Fabric
TECHNOLOGY
AEROSPACE Fabric
TECHNOLOGY
MAULE M-6-235 Metal tubing Maule M6 (Lycoming) ELA1 X
AEROSPACE Fabric
TECHNOLOGY
MAULE M-7-235 Metal tubing Maule M7 Series (Lycoming) ELA1 X
AEROSPACE Fabric
TECHNOLOGY
MAULE M-7-235B Metal tubing Maule M7 Series (Lycoming) ELA2 X
AEROSPACE Fabric
TECHNOLOGY
MAULE MT-7-235 Metal tubing Maule M7 Series (Lycoming) ELA1 X
AEROSPACE Fabric
TECHNOLOGY
MAULE MT-7-235C Metal tubing Maule M7 Series (Lycoming) ELA1 X
AEROSPACE Fabric
TECHNOLOGY
MAULE MX-7-160 Metal + Maule MX-7 (Lycoming) ELA1. Wing X
is metal,
AEROSPACE Metal tubing
fuselage is
TECHNOLOGY Fabric metal
tubing
with fabric.
is metal,
fuselage is
tubing
with fabric.

(Part-66)

MAULE MX-7-180A Metal + Maule MX-7 (Lycoming) ELA1. Wing X
is metal,
fuselage is
tubing
with fabric.
MAULE MX-7-180B Metal + Maule MX-7 (Lycoming) ELA1. Wing X
is metal,
fuselage is
tubing
with fabric.
MAULE MX-7-180C Metal + Maule MX-7 (Lycoming) ELA1. Wing X
is metal,
fuselage is
tubing
with fabric.
is metal,
fuselage is
tubing
with fabric.
MAULE MXT-7-160 Metal tubing Maule MX-7 (Lycoming) ELA1 X
AEROSPACE Fabric
TECHNOLOGY
MAULE MXT-7-180 Metal tubing Maule MX-7 (Lycoming) ELA1 X
AEROSPACE Fabric
TECHNOLOGY
MAULE MXT-7-180A Metal tubing Maule MX-7 (Lycoming) ELA1 X
AEROSPACE Fabric
TECHNOLOGY
MOONEY M20K Metal Mooney M20 (Continental) ELA2 X
AIRPLANE
Company
MOONEY M20R Metal Mooney M20 (Continental) ELA2 X
AIRPLANE
Company
MOONEY M20S Metal Mooney M20 (Continental) ELA2 X
AIRPLANE
Company
MOONEY M20 Metal + Mooney M20/M20A ELA2 X
AIRPLANE Wood (Lycoming)
Company
MOONEY M20A Metal + Mooney M20/M20A ELA2 X
AIRPLANE Wood (Lycoming)
Company
MOONEY M20B Metal Mooney M20B to M20S/M22 ELA2 X
AIRPLANE (Lycoming)
Company

(Part-66)

MOONEY M20C Metal Mooney M20B to M20S/M22 ELA2 X
AIRPLANE (Lycoming)
Company
MOONEY M20D Metal Mooney M20B to M20S/M22 ELA2 X
AIRPLANE (Lycoming)
Company
MOONEY M20E Metal Mooney M20B to M20S/M22 ELA2 X
AIRPLANE (Lycoming)
Company
MOONEY M20F Metal Mooney M20B to M20S/M22 ELA2 X
AIRPLANE (Lycoming)
Company
MOONEY M20G Metal Mooney M20B to M20S/M22 ELA2 X
AIRPLANE (Lycoming)
Company
MOONEY M20J Metal Mooney M20B to M20S/M22 ELA2 X
AIRPLANE (Lycoming)
Company
MOONEY M20M Metal Mooney M20B to M20S/M22 ELA2 X
AIRPLANE (Lycoming)
Company
MOONEY M22 Metal Mooney M20B to M20S/M22 ELA2 X
AIRPLANE (Lycoming)
Company
MOONEY M20L Metal Mooney M20L (Porsche) ELA2 X
AIRPLANE
Company
OMA SUD SPA SKYCAR Metal SKYCAR (Lycoming) ELA2 X
Sky Technologies
PIAGGIO Aero P.166 Metal Piaggio P166 (Lycoming) X
Industries
PIAGGIO Aero P.166 B Metal Piaggio P166 (Lycoming) X
Industries
PIAGGIO Aero P.166 C Metal Piaggio P166 (Lycoming) X
Industries
PIAGGIO Aero P.166 DL3 Metal Piaggio P166 (Lycoming) X
Industries
PIAGGIO Aero P.166 S Metal Piaggio P166 (Lycoming) X
Industries
PILATUS PC-6 Metal Pilatus PC-6 Series (Lycoming) ELA2 X X
AIRCRAFT
PILATUS PC-6/350 Metal Pilatus PC-6 Series (Lycoming) ELA2 X X
AIRCRAFT
PILATUS PC-6/350-H1 Metal Pilatus PC-6 Series (Lycoming) ELA2 X X
AIRCRAFT
PILATUS PC-6/350-H2 Metal Pilatus PC-6 Series (Lycoming) ELA2 X X
AIRCRAFT

(Part-66)

PILATUS PC-6-H1 Metal Pilatus PC-6 Series (Lycoming) ELA2 X X
AIRCRAFT
PILATUS PC-6-H2 Metal Pilatus PC-6 Series (Lycoming) ELA2 X X
AIRCRAFT
PIPER AIRCRAFT PA-23-235 Metal Piper PA-23 Aztec (Lycoming) ELA2 X
PIPER AIRCRAFT PA-23-250 Metal Piper PA-23 Aztec (Lycoming) ELA2 X
PIPER AIRCRAFT PA-E23-250 Metal Piper PA-23 Aztec (Lycoming) X
PIPER AIRCRAFT PA-24 Metal Piper PA-24 Series (Lycoming) ELA1 X
PIPER AIRCRAFT PA-24-250 Metal Piper PA-24 Series (Lycoming) ELA2 X
PIPER AIRCRAFT PA-28-201T Metal Piper PA-28 Series ELA1 X
(Turbo (Continental)
Dakota)
PIPER AIRCRAFT PA-28R-201T Metal Piper PA-28 Series ELA2 X
(Turbo (Continental)
Arrow III)
PIPER AIRCRAFT PA-28RT- Metal Piper PA-28 Series ELA2 X
201T (Turbo (Continental)
Arrow IV)
(Cherokee
Cruiser)
(Cherokee)
(Cherokee
Warrior)
(Cherokee)
(Warrior II)
(Warrior III)
(Archer)
(Cherokee)
(Archer II)
(Archer III)
(Cher.
Pathfinder)

(Part-66)

(Dakota)
PIPER AIRCRAFT PA-28R-180 Metal Piper PA-28 Series (Lycoming) ELA1 X
(Arrow)
(Arrow II)
(Arrow)
(Arrow III)
PIPER AIRCRAFT PA-28RT-201 Metal Piper PA-28 Series (Lycoming) ELA2 X
(Arrow IV)
PIPER AIRCRAFT PA-28S-160 Metal Piper PA-28 Series (Lycoming) ELA1 X
(Cherokee)
(Cherokee)
PIPER AIRCRAFT PA-30 Metal Piper PA-30 Series (Lycoming) ELA2 X
PIPER AIRCRAFT PA-31 Metal Piper PA-31 Series (Lycoming) X
PIPER AIRCRAFT PA-31-300 Metal Piper PA-31 Series (Lycoming) X
(Chieftain)
PIPER AIRCRAFT PA-31P Metal + Piper PA-31P (Lycoming) X
(Pressurized Pressurised
Navajo)
PIPER AIRCRAFT PA-31P-350 Metal + Piper PA-31P (Lycoming) X
(Mojave) Pressurised
(Cherokee
Six 260)
(Cherokee
Six 300)
(Saratoga)
PIPER AIRCRAFT PA-32-301FT Metal Piper PA-32 Series (Lycoming) ELA2 X
(Piper 6X)
PIPER AIRCRAFT PA-32-301T Metal Piper PA-32 Series (Lycoming) ELA2 X
(Turbo
Saratoga)
PIPER AIRCRAFT PA-32- Metal Piper PA-32 Series (Lycoming) ELA2 X
301XTC
(Piper 6XT)
(Lance)

(Part-66)

(Saratoga II
HP)
(Saratoga
SP)
PIPER AIRCRAFT PA-32R-301T Metal Piper PA-32 Series (Lycoming) ELA2 X
(Saratoga II
TC)
(Turbo
SaratogaSP)
PIPER AIRCRAFT PA-32RT-300 Metal Piper PA-32 Series (Lycoming) ELA2 X
(Lance II)
PIPER AIRCRAFT PA-32RT- Metal Piper PA-32 Series (Lycoming) ELA2 X
300T (Turbo
Lance II)
(Cher.Six
Seaplane)
PIPER AIRCRAFT PA-34-200T Metal Piper PA-34 Series X
(Seneca II) (Continental)
(Seneca III) (Continental)
(Seneca IV) (Continental)
(Seneca V) (Continental)
(Seneca)
PIPER AIRCRAFT PA-36-285 Metal Piper PA-36 Series ELA2 X
(Normal (Continental)
category)
(Normal
category)
(Normal
category)
PIPER AIRCRAFT PA-39 Metal Piper PA-39/40 Series ELA2 X
(Lycoming)
PIPER AIRCRAFT PA-40 Metal Piper PA-39/40 Series ELA2 X
(Lycoming)
(Seminole)

(Part-66)

PIPER AIRCRAFT PA-44-180T Metal Piper PA-44 Series (Lycoming) ELA2 X
(Turbo
Seminole)
PIPER AIRCRAFT PA-46-310P Metal + Piper PA-46 Pressurised ELA2 X
Pressurised (Continental)
PIPER AIRCRAFT PA-46-350P Metal + Piper PA-46 Pressurised ELA2 X
(Mirage) Pressurised (Lycoming)
(Matrix)
Pipistrel Vertical Virus SW Composite Pipistrel Virus (Rotax) ELA1 X
Solutions d.o.o. 121
Polskie Zakłady PZL M18 Metal PZL M 18 (PZL) X
Lotnicze Sp. z o.o.
Polskie Zakłady PZL M18A Metal PZL M 18 (PZL) X
Lotnicze Sp. z o.o.
Polskie Zakłady PZL M18AS Metal PZL M 18 (PZL) X
Lotnicze Sp. z o.o.
Polskie Zakłady PZL M18B Metal PZL M 18 (PZL) X
Lotnicze Sp. z o.o.
Polskie Zakłady PZL M18BS Metal PZL M 18 (PZL) X
Lotnicze Sp. z o.o.
Polskie Zakłady PZL M26 01 Metal PZL M 26 (Lycoming) ELA2 X
Lotnicze Sp. z o.o.
Polskie Zakłady PZL M20 Metal PZL M 20 (PZL) X
Lotnicze Sp. z o.o.
(Aircrat with SAS)
PZL PZL-104M Metal PZL-104 Wilga (Lycoming) ELA2 X
WARSZAWAOKEC Wilga 2000
IE S.A.
PZL PZL-104MA Metal PZL-104 Wilga (Lycoming) ELA2 X
IE S.A.
PZL PZL-104MF Metal PZL-104 Wilga (Lycoming) ELA2 X
IE S.A.
PZL PZL-104MN Metal PZL-104 Wilga (Lycoming) ELA2 X
IE S.A.
PZL PZL-104 Metal PZL-104 Wilga Series ELA2 X
WARSZAWAOKEC Wilga 32 (Continental)
IE S.A.
PZL PZL-104 Metal PZL-104 Wilga Series ELA2 X
WARSZAWAOKEC Wilga 32A (Continental)
IE S.A.
PZL PZL-104 Metal PZL-104A Wilga (Ivchenko) ELA2 X
IE S.A.

(Part-66)

WARSZAWAOKEC Wilga 35A
IE S.A.
IE S.A.
PZL PZL-110 Metal PZL-110 Koliber (Franklin) ELA1 X
WARSZAWAOKEC KOLIBER
IE S.A.
PZL PZL-KOLIBER Metal PZL-Koliber 150 Series ELA1 X
WARSZAWAOKEC 150 (Lycoming)
IE S.A.
PZL PZL-KOLIBER Metal PZL-Koliber 150 Series ELA1 X
WARSZAWAOKEC 150A (Lycoming)
IE S.A.
PZL PZL-KOLIBER Metal PZL-Koliber 160 (Lycoming) ELA1 X
WARSZAWAOKEC 160A
IE S.A.
Reims Aviation FTB337G Metal Cessna/Reims-Cessna 337 Ref.: X
(Aircraft with Series (Continental) SAS.A.11
SAS) (not pressurised) 5.
Reims Aviation FTB337GA Metal Cessna/Reims-Cessna 337 Ref.: X
(Aircraft with Series (Continental) SAS.A.11
SAS) (not pressurised) 5.
REVO, Inc LA-4A Metal REVO C/LA-4 Series (Lycoming) ELA1 X
REVO, Inc LA-4P Metal REVO C/LA-4 Series (Lycoming) ELA1 X
REVO, Inc Lake 250 Metal REVO C/LA-4 Series (Lycoming) ELA2 X
REVO, Inc. LA-4-200 Metal Lake C/LA Series (Lycoming) ELA1 X
RUAG Do 28 A-1 Metal Do 28 Series (Lycoming) X
AEROSPACE
Services GmbH
RUAG Do 28 A-1[R] Metal Do 28 Series (Lycoming) X
AEROSPACE
Services GmbH
RUAG Do 28 B-1 Metal Do 28 Series (Lycoming) X
AEROSPACE
Services GmbH
RUAG Do 28 D Metal Do 28 Series (Lycoming) X
AEROSPACE
Services GmbH
RUAG Do 28 D-1 Metal Do 28 Series (Lycoming) X
AEROSPACE
Services GmbH
RUAG Do 28 D-2 Metal Do 28 Series (Lycoming) X
AEROSPACE
Services GmbH

(Part-66)

SCHEIBE SF 23 A Wood + SF 23 Series (Continental) ELA1 X
Flugzeugbau Metal tubing
Fabric
SCHEIBE SF 23 A1 Wood + SF 23 Series (Continental) ELA1 X
Fabric
SCHEIBE SF 23 B Wood + SF 23 Series (Continental) ELA1 X
Fabric
SCHEIBE SF 23 C Wood + SF 23 Series (Lycoming) ELA1 X
(Aircraft with Fabric
SAS)
SEASTAR CORP TSC-1A Composite TSC Series (Lycoming) ELA1 X
SEASTAR CORP TSC-1A1 Composite TSC Series (Lycoming) ELA1 X
SEASTAR CORP TSC-1A2 Composite TSC Series (Lycoming) ELA1 X
Skyfox Aviation CA25 Wood + CA25 Series (Rotax) ELA1 X
Ltd Metal tubing
Fabric
Skyfox Aviation CA25N Wood + CA25 Series (Rotax) ELA1 X
Ltd Metal tubing
Fabric
SLINGSBY T67A Wood Slingsby T67A (Lycoming) ELA1 X
Aviation
SLINGSBY T67B Firefly Composite Slingsby T67B/T67C/T67M ELA1 X
Aviation Series (Lycoming)
SLINGSBY T67C Firefly Composite Slingsby T67B/T67C/T67M ELA1 X
SLINGSBY T67M Firefly Composite Slingsby T67B/T67C/T67M ELA1 X
SLINGSBY T67M200 Composite Slingsby T67B/T67C/T67M ELA1 X
Aviation Firefly Series (Lycoming)
SLINGSBY T67M260 Composite Slingsby T67B/T67C/T67M ELA1 X
SLINGSBY T67M260- Composite Slingsby T67B/T67C/T67M ELA1 X
Aviation T3A Firefly Series (Lycoming)
SLINGSBY T67M-MKII Composite Slingsby T67B/T67C/T67M ELA1 X
SOCATA(Aircraft RALLYE 235 Metal SOCATA Rallye Series ELA2 X
with SAS) CA (Lycoming)
SOCATA (Aircraft RALLYE 235 Metal SOCATA Rallye Series ELA2 X
with SAS) CA-M (Lycoming)
SOCATA (Aircraft ST10 Metal SOCATA ST10 (Lycoming) ELA2 X
with SAS)
SONACA S200 Metal SONACA 200 (Rotax) ELA1 X
AIRCRAFT S.A.

(Part-66)

SONACA S201 Metal SONACA 200 (Rotax) ELA1 X
AIRCRAFT S.A.
SST FLUGTECHNIK EA 400 Composite Extra EA-400 (Continental) ELA2 X
GmbH
STEMME AG S15-1 Composite Stemme ASP S15-1 (Rotax) ELA1 X
SUKHOI (Aircraft Su-29 Composite Sukhoi SU-29 (Vedeneyev) ELA2 X
with SAS)
SUKHOI (Aircraft Su-31 Composite Sukhoi SU-31 (Vedeneyev) ELA1 X
with SAS)
SYMPHONY OMF-100- Metal Symphony OMF-100-160 ELA1 X
AIRCRAFT 160 (Lycoming)
INDUSTRIES
TAYLORCRAFT 19 Wood + Taylorcraft 19 Series ELA1 X
2000 Metal tubing (Continental)
Fabric
TAYLORCRAFT F19 Wood + Taylorcraft 19 Series ELA1 X
2000 Metal tubing (Continental)
Fabric
TAYLORCRAFT F21 Wood + Taylorcraft F21/F22 Series ELA1 X
2000 Metal tubing (Lycoming)
Fabric
TAYLORCRAFT F21A Wood + Taylorcraft F21/F22 Series ELA1 X
Fabric
TAYLORCRAFT F21B Wood + Taylorcraft F21/F22 Series ELA1 X
Fabric
TAYLORCRAFT F22 Wood + Taylorcraft F21/F22 Series ELA1 X
Fabric
TAYLORCRAFT F22A Wood + Taylorcraft F21/F22 Series ELA1 X
Fabric
TAYLORCRAFT F22B Wood + Taylorcraft F21/F22 Series ELA1 X
Fabric
TAYLORCRAFT F22C Wood + Taylorcraft F21/F22 Series ELA1 X
Fabric
TECNAM P2006T Metal Tecnam P2006T (Rotax) ELA1 X
Costruzioni
Aeronautiche
TECNAM P92-JS Metal Tecnam P92 (Rotax) ELA1 X
Costruzioni
Aeronautiche
TECNAM P2002-JF Metal Tecnam P2002 (Rotax) ELA1 X
Costruzioni
Aeronautiche

(Part-66)

TECNAM P2002-JR Metal Tecnam P2002 (Rotax) ELA1 X
Costruzioni
Aeronautiche
TECNAM P2008 JC Composite + Tecnam P2008 (Rotax) ELA1 X
Costruzioni Metal
Aeronautiche
TECNAM P2010 Composite + Tecnam P2010 (Lycoming) ELA1 X
Costruzioni Metal
Aeronautiche
TECNAM P2012 Metal Tecnam P2012 (Lycoming) X
Costruzioni Traveller
Aeronautiche
TECNAM P92-J Metal Tecnam P92 (Rotax) ELA1 X
Costruzioni
Aeronautiche
TEXTRON E33 Metal Beech 33 Series (Continental) ELA2 X
AVIATION Inc.
TEXTRON E33A Metal Beech 33 Series (Continental) ELA2 X
AVIATION Inc.
TEXTRON E33C Metal Beech 33 Series (Continental) ELA2 X
AVIATION Inc.
TEXTRON F33 Metal Beech 33 Series (Continental) ELA2 X
AVIATION Inc.
TEXTRON F33A Metal Beech 33 Series (Continental) ELA2 X
AVIATION Inc.
TEXTRON F33C Metal Beech 33 Series (Continental) ELA2 X
AVIATION Inc.
TEXTRON G33 Metal Beech 33 Series (Continental) ELA2 X
AVIATION Inc.
TEXTRON 35-33 Metal Beech 35 Series (Continental) ELA2 X
AVIATION Inc.
TEXTRON 35-A33 Metal Beech 35 Series (Continental) ELA2 X
AVIATION Inc.
TEXTRON 35-B33 Metal Beech 35 Series (Continental) ELA2 X
AVIATION Inc.
TEXTRON 35-C33 Metal Beech 35 Series (Continental) ELA2 X
AVIATION Inc.
TEXTRON 35-C33A Metal Beech 35 Series (Continental) ELA2 X
AVIATION Inc.
TEXTRON H35 Metal Beech 35 Series (Continental) ELA2 X
AVIATION Inc.
TEXTRON J35 Metal Beech 35 Series (Continental) ELA2 X
AVIATION Inc.
TEXTRON K35 Metal Beech 35 Series (Continental) ELA2 X
AVIATION Inc.
TEXTRON M35 Metal Beech 35 Series (Continental) ELA2 X
AVIATION Inc.

(Part-66)

TEXTRON N35 Metal Beech 35 Series (Continental) ELA2 X
AVIATION Inc.
TEXTRON P35 Metal Beech 35 Series (Continental) ELA2 X
AVIATION Inc.
TEXTRON S35 Metal Beech 35 Series (Continental) ELA2 X
AVIATION Inc.
TEXTRON V35 Metal Beech 35 Series (Continental) ELA2 X
AVIATION Inc.
TEXTRON V35A Metal Beech 35 Series (Continental) ELA2 X
AVIATION Inc.
TEXTRON V35B Metal Beech 35 Series (Continental) ELA2 X
AVIATION Inc.
TEXTRON 36 Metal Beech 36 Series (Continental) ELA2 X
AVIATION Inc.
TEXTRON A36 Metal Beech 36 Series (Continental) ELA2 X
AVIATION Inc.
TEXTRON A36TC Metal Beech 36 Series (Continental) ELA2 X
AVIATION Inc.
TEXTRON B36TC Metal Beech 36 Series (Continental) ELA2 X
AVIATION Inc.
TEXTRON G36 Metal Beech 36 Series (Continental) ELA2 X
AVIATION Inc.
TEXTRON D55 Metal Beech 55 Series (Continental) X
AVIATION Inc.
TEXTRON D55A Metal Beech 55 Series (Continental) X
AVIATION Inc.
TEXTRON E55 Metal Beech 55 Series (Continental) X
AVIATION Inc.
TEXTRON E55A Metal Beech 55 Series (Continental) X
AVIATION Inc.
TEXTRON 56TC Metal Beech 56 Series (Lycoming) X
AVIATION Inc.
TEXTRON A56TC Metal Beech 56 Series (Lycoming) X
AVIATION Inc.
TEXTRON 58 Metal Beech 58 Series (Continental) X
AVIATION Inc.
TEXTRON 58A Metal Beech 58 Series (Continental) X
AVIATION Inc.
TEXTRON G58 Metal Beech 58 Series (Continental) X
AVIATION Inc.
TEXTRON 65 Metal Beech 65-80 Series (Lycoming) X
AVIATION Inc.
TEXTRON 70 Metal Beech 65-80 Series (Lycoming) X
AVIATION Inc.
TEXTRON 65-80 Metal Beech 65-80 Series (Lycoming) X
AVIATION Inc.

(Part-66)

TEXTRON 65-88 Metal Beech 65-80 Series (Lycoming) X
AVIATION Inc.
TEXTRON 65-A80 Metal Beech 65-80 Series (Lycoming) X
AVIATION Inc.
TEXTRON 65-A80-8800 Metal Beech 65-80 Series (Lycoming) X
AVIATION Inc.
TEXTRON 65-B80 Metal Beech 65-80 Series (Lycoming) X
AVIATION Inc.
TEXTRON A65 Metal Beech 65-80 Series (Lycoming) X
AVIATION Inc.
TEXTRON A65-8200 Metal Beech 65-80 Series (Lycoming) X
AVIATION Inc.
TEXTRON 95-B55 Metal Beech 95 Series (Continental) X
AVIATION Inc.
TEXTRON 95-B55A Metal Beech 95 Series (Continental) X
AVIATION Inc.
TEXTRON 95-B55B Metal Beech 95 Series (Continental) X
AVIATION Inc.
TEXTRON 95-C55 Metal Beech 95 Series (Continental) X
AVIATION Inc.
TEXTRON 95-C55A Metal Beech 95 Series (Continental) X
AVIATION Inc.
TEXTRON 95 Metal Beech 95 Series (Lycoming) ELA2 X
AVIATION Inc
TEXTRON 95-55 Metal Beech 95 Series (Lycoming) X
AVIATION Inc
TEXTRON 95-A55 Metal Beech 95 Series (Lycoming) X
AVIATION Inc
TEXTRON B95 Metal Beech 95 Series (Lycoming) ELA2 X
AVIATION Inc
TEXTRON B95A Metal Beech 95 Series (Lycoming) ELA2 X
AVIATION Inc
TEXTRON D95A Metal Beech 95 Series (Lycoming) ELA2 X
AVIATION Inc
TEXTRON E95 Metal Beech 95 Series (Lycoming) ELA2 X
AVIATION Inc
TEXTRON 175 Metal Cessna 175 Series (Continental) ELA1 X
AVIATION Inc.
TEXTRON 175A Metal Cessna 175 Series (Continental) ELA1 X
AVIATION Inc.
TEXTRON 175B Metal Cessna 175 Series (Continental) ELA1 X
AVIATION Inc.
TEXTRON 175C Metal Cessna 175 Series (Continental) ELA1 X
AVIATION Inc.
TEXTRON 177 Metal Cessna 177 Series (Lycoming) ELA1 X
AVIATION Inc.

(Part-66)

TEXTRON 177A Metal Cessna 177 Series (Lycoming) ELA1 X
AVIATION Inc.
TEXTRON 177B Metal Cessna 177 Series (Lycoming) ELA1 X
AVIATION Inc.
TEXTRON 177RG Metal Cessna 177 Series (Lycoming) ELA2 X
AVIATION Inc.
AVIATION Inc.
AVIATION Inc.
AVIATION Inc.
AVIATION Inc.
TEXTRON 180D Metal Cessna 180 Series (Continental) ELA2 X
AVIATION Inc.
TEXTRON 180E Metal Cessna 180 Series (Continental) ELA2 X
AVIATION Inc.
TEXTRON 180F Metal Cessna 180 Series (Continental) ELA2 X
AVIATION Inc.
TEXTRON 180G Metal Cessna 180 Series (Continental) ELA2 X
AVIATION Inc.
TEXTRON 180H Metal Cessna 180 Series (Continental) ELA2 X
AVIATION Inc.
TEXTRON 180J Metal Cessna 180 Series (Continental) ELA2 X
AVIATION Inc.
TEXTRON 180K Metal Cessna 180 Series (Continental) ELA2 X
AVIATION Inc.
AVIATION Inc.
AVIATION Inc.
AVIATION Inc.
AVIATION Inc.
AVIATION Inc.
AVIATION Inc.
TEXTRON A185E Metal Cessna 185 Series (Continental) ELA2 X
AVIATION Inc.
TEXTRON A185F Metal Cessna 185 Series (Continental) ELA2 X
AVIATION Inc.
TEXTRON 188 Metal Cessna 188 (Continental) ELA2 X
AVIATION Inc.

(Part-66)

TEXTRON 188A Metal Cessna 188 (Continental) ELA2 X
AVIATION Inc.
TEXTRON 188B Metal Cessna 188 (Continental) ELA2 X
AVIATION Inc.
TEXTRON A188 Metal Cessna 188 (Continental) ELA2 X
AVIATION Inc.
TEXTRON A188A Metal Cessna 188 (Continental) ELA2 X
AVIATION Inc.
TEXTRON A188B Metal Cessna 188 (Continental) ELA2 X
AVIATION Inc.
TEXTRON T188C Metal Cessna 188 (Continental) ELA2 X
AVIATION Inc.
AVIATION Inc.
TEXTRON P206 Metal Cessna 206 Series (Continental) ELA2 X
AVIATION Inc.
TEXTRON P206A Metal Cessna 206 Series (Continental) ELA2 X
AVIATION Inc.
TEXTRON P206B Metal Cessna 206 Series (Continental) ELA2 X
AVIATION Inc.
TEXTRON P206C Metal Cessna 206 Series (Continental) ELA2 X
AVIATION Inc.
TEXTRON P206D Metal Cessna 206 Series (Continental) ELA2 X
AVIATION Inc.
TEXTRON P206E Metal Cessna 206 Series (Continental) ELA2 X
AVIATION Inc.
TEXTRON TP206A Metal Cessna 206 Series (Continental) ELA2 X
AVIATION Inc.
TEXTRON TP206B Metal Cessna 206 Series (Continental) ELA2 X
AVIATION Inc.
TEXTRON TP206C Metal Cessna 206 Series (Continental) ELA2 X
AVIATION Inc.
TEXTRON TP206D Metal Cessna 206 Series (Continental) ELA2 X
AVIATION Inc.
TEXTRON TP206E Metal Cessna 206 Series (Continental) ELA2 X
AVIATION Inc.
TEXTRON TU206A Metal Cessna 206 Series (Continental) ELA2 X
AVIATION Inc.
TEXTRON TU206B Metal Cessna 206 Series (Continental) ELA2 X
AVIATION Inc.
TEXTRON TU206C Metal Cessna 206 Series (Continental) ELA2 X
AVIATION Inc.
TEXTRON TU206D Metal Cessna 206 Series (Continental) ELA2 X
AVIATION Inc.
TEXTRON TU206E Metal Cessna 206 Series (Continental) ELA2 X
AVIATION Inc.

(Part-66)

TEXTRON TU206F Metal Cessna 206 Series (Continental) ELA2 X
AVIATION Inc.
TEXTRON TU206G Metal Cessna 206 Series (Continental) ELA2 X
AVIATION Inc.
TEXTRON U206 Metal Cessna 206 Series (Continental) ELA2 X
AVIATION Inc.
TEXTRON U206A Metal Cessna 206 Series (Continental) ELA2 X
AVIATION Inc.
TEXTRON U206B Metal Cessna 206 Series (Continental) ELA2 X
AVIATION Inc.
TEXTRON U206C Metal Cessna 206 Series (Continental) ELA2 X
AVIATION Inc.
TEXTRON U206D Metal Cessna 206 Series (Continental) ELA2 X
AVIATION Inc.
TEXTRON U206E Metal Cessna 206 Series (Continental) ELA2 X
AVIATION Inc.
TEXTRON U206F Metal Cessna 206 Series (Continental) ELA2 X
AVIATION Inc.
TEXTRON U206G Metal Cessna 206 Series (Continental) ELA2 X
AVIATION Inc.
TEXTRON 206H Metal Cessna 206 Series (Lycoming) ELA2 X
AVIATION Inc.
TEXTRON T206H Metal Cessna 206 Series (Lycoming) ELA2 X
AVIATION Inc.
AVIATION Inc.
AVIATION Inc.
TEXTRON T207 Metal Cessna 207 Series (Continental) ELA2 X
AVIATION Inc.
TEXTRON T207A Metal Cessna 207 Series (Continental) ELA2 X
AVIATION Inc.
AVIATION Inc.
TEXTRON 210-5 (205) Metal Cessna 210 Series (Continental) ELA2 X
AVIATION Inc.
TEXTRON 210-5A Metal Cessna 210 Series (Continental) ELA2 X
AVIATION Inc. (205A)
AVIATION Inc.
AVIATION Inc.
AVIATION Inc.
AVIATION Inc.

(Part-66)

AVIATION Inc.
TEXTRON 210F Metal Cessna 210 Series (Continental) ELA2 X
AVIATION Inc.
TEXTRON 210G Metal Cessna 210 Series (Continental) ELA2 X
AVIATION Inc.
TEXTRON 210H Metal Cessna 210 Series (Continental) ELA2 X
AVIATION Inc.
TEXTRON 210J Metal Cessna 210 Series (Continental) ELA2 X
AVIATION Inc.
TEXTRON 210K Metal Cessna 210 Series (Continental) ELA2 X
AVIATION Inc.
TEXTRON 210L Metal Cessna 210 Series (Continental) ELA2 X
AVIATION Inc.
TEXTRON 210M Metal Cessna 210 Series (Continental) ELA2 X
AVIATION Inc.
TEXTRON 210N Metal Cessna 210 Series (Continental) ELA2 X
AVIATION Inc.
TEXTRON 210R Metal Cessna 210 Series (Continental) ELA2 X
AVIATION Inc.
TEXTRON 310 Metal Cessna 310/320 Series X
AVIATION Inc. (Continental)
TEXTRON 320 Metal Cessna 310/320 Series X
TEXTRON 310B Metal Cessna 310/320 Series X
TEXTRON 310C Metal Cessna 310/320 Series X
TEXTRON 310D Metal Cessna 310/320 Series X
TEXTRON 310F Metal Cessna 310/320 Series X
TEXTRON 310G Metal Cessna 310/320 Series X
TEXTRON 310H Metal Cessna 310/320 Series X
TEXTRON 310I Metal Cessna 310/320 Series X
TEXTRON 310J Metal Cessna 310/320 Series X
TEXTRON 310J-1 Metal Cessna 310/320 Series X
TEXTRON 310K Metal Cessna 310/320 Series X
TEXTRON 310L Metal Cessna 310/320 Series X

(Part-66)

TEXTRON 310N Metal Cessna 310/320 Series X
TEXTRON 310P Metal Cessna 310/320 Series X
TEXTRON 310Q Metal Cessna 310/320 Series X
TEXTRON 310R Metal Cessna 310/320 Series X
TEXTRON 320-1 Metal Cessna 310/320 Series X
TEXTRON 320A Metal Cessna 310/320 Series X
TEXTRON 320B Metal Cessna 310/320 Series X
TEXTRON 320C Metal Cessna 310/320 Series X
TEXTRON 320D Metal Cessna 310/320 Series X
TEXTRON 320E Metal Cessna 310/320 Series X
TEXTRON 320F Metal Cessna 310/320 Series X
TEXTRON E310H Metal Cessna 310/320 Series X
TEXTRON E310J Metal Cessna 310/320 Series X
TEXTRON T310P Metal Cessna 310/320 Series X
TEXTRON T310Q Metal Cessna 310/320 Series X
TEXTRON T310R Metal Cessna 310/320 Series X
AVIATION Inc.
TEXTRON 335 Metal Cessna 335 (Continental) X
AVIATION Inc.
AVIATION Inc.
TEXTRON 340 Metal + Cessna 340 (Continental) X
AVIATION Inc. Pressurised
TEXTRON 340A Metal + Cessna 340 (Continental) X
TEXTRON LC40-550FG Composite Cessna C300/C350/C400 ELA2 X

(Part-66)

TEXTRON T240 Composite Cessna C300/C350/C400 ELA2 X
TEXTRON P210N Metal + Cessna P210 (Continental) ELA2 X
TEXTRON P210R Metal + Cessna P210 (Continental) ELA2 X
TEXTRON T210F Metal Cessna T210 (Continental) ELA2 X
AVIATION Inc.
TEXTRON T210G Metal Cessna T210 (Continental) ELA2 X
AVIATION Inc.
TEXTRON T210H Metal Cessna T210 (Continental) ELA2 X
AVIATION Inc.
TEXTRON T210J Metal Cessna T210 (Continental) ELA2 X
AVIATION Inc.
TEXTRON T210K Metal Cessna T210 (Continental) ELA2 X
AVIATION Inc.
TEXTRON T210L Metal Cessna T210 (Continental) ELA2 X
AVIATION Inc.
TEXTRON T210M Metal Cessna T210 (Continental) ELA2 X
AVIATION Inc.
TEXTRON T210N Metal Cessna T210 (Continental) ELA2 X
AVIATION Inc.
TEXTRON T210R Metal Cessna T210 (Continental) ELA2 X
AVIATION Inc.
TEXTRON T303 Metal Cessna T303 (Continental) X
AVIATION Inc.
TEXTRON 150 Metal Cessna/Reims-Cessna ELA1 X
AVIATION Inc. 150/F150 Series (Continental)
TEXTRON 150A Metal Cessna/Reims-Cessna ELA1 X
TEXTRON 150B Metal Cessna/Reims-Cessna ELA1 X
TEXTRON 150C Metal Cessna/Reims-Cessna ELA1 X
TEXTRON 150D Metal Cessna/Reims-Cessna ELA1 X
TEXTRON 150E Metal Cessna/Reims-Cessna ELA1 X
TEXTRON 150F Metal Cessna/Reims-Cessna ELA1 X
TEXTRON 150G Metal Cessna/Reims-Cessna ELA1 X
TEXTRON 150H Metal Cessna/Reims-Cessna ELA1 X

(Part-66)

TEXTRON 150J Metal Cessna/Reims-Cessna ELA1 X
TEXTRON 150K Metal Cessna/Reims-Cessna ELA1 X
TEXTRON 150L Metal Cessna/Reims-Cessna ELA1 X
TEXTRON 150M Metal Cessna/Reims-Cessna ELA1 X
TEXTRON A150K Metal Cessna/Reims-Cessna ELA1 X
TEXTRON A150L Metal Cessna/Reims-Cessna ELA1 X
TEXTRON A150M Metal Cessna/Reims-Cessna ELA1 X
AVIATION Inc. 152/F152 Series (Lycoming)
TEXTRON A152 Metal Cessna/Reims-Cessna ELA1 X
TEXTRON P172D Metal Cessna/Reims-Cessna ELA1 X
TEXTRON R172E Metal Cessna/Reims-Cessna ELA1 X
TEXTRON R172F Metal Cessna/Reims-Cessna ELA1 X
TEXTRON R172G Metal Cessna/Reims-Cessna ELA1 X
TEXTRON R172H Metal Cessna/Reims-Cessna ELA1 X

(Part-66)

TEXTRON R172J Metal Cessna/Reims-Cessna ELA1 X
TEXTRON R172K Metal Cessna/Reims-Cessna ELA1 X
TEXTRON 172I Metal Cessna/Reims-Cessna ELA1 X
TEXTRON 172N Metal Cessna/Reims-Cessna ELA1 X
TEXTRON 172P Metal Cessna/Reims-Cessna ELA1 X
TEXTRON 172Q Metal Cessna/Reims-Cessna ELA1 X
TEXTRON 172R Metal Cessna/Reims-Cessna ELA1 X
TEXTRON 172RG Metal Cessna/Reims-Cessna ELA2 X
TEXTRON 172S Metal Cessna/Reims-Cessna ELA1 X
TEXTRON 182J Metal Cessna/Reims-Cessna ELA2 X

(Part-66)

TEXTRON 182N Metal Cessna/Reims-Cessna ELA2 X
TEXTRON 182P Metal Cessna/Reims-Cessna ELA2 X
TEXTRON 182Q Metal Cessna/Reims-Cessna ELA2 X
TEXTRON 182R Metal Cessna/Reims-Cessna ELA2 X
TEXTRON R182 Metal Cessna/Reims-Cessna ELA2 X
TEXTRON T182T Metal Cessna/Reims-Cessna ELA2 X
TEXTRON 182S Metal Cessna/Reims-Cessna ELA2 X
TEXTRON 182T Metal Cessna/Reims-Cessna ELA2 X
TEXTRON T337H-SP Metal Cessna/Reims-Cessna 337 X
AVIATION Inc. Series (Continental)
(not pressurised)
TEXTRON 337 Metal Cessna/Reims-Cessna 337 ELA2 X
(not pressurised)
TEXTRON 337A Metal Cessna/Reims-Cessna 337 ELA2 X
(not pressurised)
TEXTRON 337B Metal Cessna/Reims-Cessna 337 ELA2 X
(not pressurised)
TEXTRON 337C Metal Cessna/Reims-Cessna 337 ELA2 X
(not pressurised)
TEXTRON 337D Metal Cessna/Reims-Cessna 337 ELA2 X
(not pressurised)
TEXTRON 337E Metal Cessna/Reims-Cessna 337 X
(not pressurised)
TEXTRON 337F Metal Cessna/Reims-Cessna 337 X
(not pressurised)
TEXTRON 337G Metal Cessna/Reims-Cessna 337 X
(not pressurised)

(Part-66)

TEXTRON 337H Metal Cessna/Reims-Cessna 337 X
(not pressurised)
TEXTRON M337B Metal Cessna/Reims-Cessna 337 ELA2 X
(not pressurised)
TEXTRON T337B Metal Cessna/Reims-Cessna 337 ELA2 X
(not pressurised)
TEXTRON T337C Metal Cessna/Reims-Cessna 337 X
(not pressurised)
TEXTRON T337D Metal Cessna/Reims-Cessna 337 X
(not pressurised)
TEXTRON T337E Metal Cessna/Reims-Cessna 337 X
(not pressurised)
TEXTRON T337F Metal Cessna/Reims-Cessna 337 X
(not pressurised)
TEXTRON T337G Metal Cessna/Reims-Cessna 337 X
(not pressurised)
TEXTRON T337H Metal Cessna/Reims-Cessna 337 X
(not pressurised)
TEXTRON P337H Metal + Cessna/Reims-Cessna 337 X
AVIATION Inc. Pressurised Series (Continental)
(not pressurised)
TEXTRON T182 Metal Cessna/Reims-Cessna T182 ELA2 X
AVIATION Inc. Series (Lycoming)
TEXTRON TR182 Metal Cessna/Reims-Cessna T182 ELA2 X
AVIATION Inc. Series (Lycoming)
THRUSH S2R Metal Thrush S2R Series The Model X
S2R also
AIRCRAFT (PW R1340)
designated
as S-2R or
S2-R.
THRUSH S2R-R3S Metal Thrush S2R (Wsk PZL-3S) X
AIRCRAFT
THRUSH S2R-R1340 Metal Thrush S2R Series X
AIRCRAFT (PW R1340)
THRUSH S2R-R1820 Metal Thrush S2R Series X
AIRCRAFT (Wright R-1820)
TOMARK, s.r.o. Viper SD-4 Metal Tomark Viper SD-4 (Rotax) ELA1. X
Restricted
RTC
TC.

(Part-66)

TOMARK, s.r.o. Viper SD-4 Metal Tomark Viper SD-4 (Rotax) ELA1. X
Restricted
Night-VFR
TC.
TRUE FLIGHT AA-1 Metal Grumman/American AA-1 ELA1 X
Holdings Series (Lycoming)
TRUE FLIGHT AA-1A Metal Grumman/American AA-1 ELA1 X
TRUE FLIGHT AA-1B Metal Grumman/American AA-1 ELA1 X
TRUE FLIGHT AA-1C Metal Grumman/American AA-1 ELA1 X
TRUE FLIGHT AA-5 Metal Grumman/American AA-5 ELA1 X
TRUE FLIGHT AA-5A Metal Grumman/American AA-5 ELA1 X
TRUE FLIGHT AA-5B Metal Grumman/American AA-5 ELA1 X
TRUE FLIGHT AG-5B Metal Grumman/American AA-5 ELA1 X
TWIN 500A Metal Twin Commander 500 Series X
COMMANDER (Continental)
AIRCRAFT
Corporation
TWIN 500 Metal Twin Commander 500 Series X
COMMANDER (Lycoming)
AIRCRAFT
Corporation
AIRCRAFT
Corporation
AIRCRAFT
Corporation
TWIN 500B Metal Twin Commander 500 Series X
AIRCRAFT
Corporation
TWIN 500S Metal Twin Commander 500 Series X
AIRCRAFT
Corporation
TWIN 500U Metal Twin Commander 500 Series X
AIRCRAFT
Corporation
TWIN 560A Metal Twin Commander 500 Series X

(Part-66)

AIRCRAFT
Corporation
TWIN 560E Metal Twin Commander 500 Series X
AIRCRAFT
Corporation
TWIN 685 Metal + Twin Commander 600 Series X
COMMANDER Pressurised (Continental)
AIRCRAFT
Corporation
AIRCRAFT
Corporation
TWIN 560F Metal Twin Commander 600 Series X
AIRCRAFT
Corporation
TWIN 680E Metal Twin Commander 600 Series X
AIRCRAFT
Corporation
TWIN 680F Metal Twin Commander 600 Series X
AIRCRAFT
Corporation
TWIN 680FL Metal Twin Commander 600 Series X
AIRCRAFT
Corporation
COMMANDER Pressurised (Lycoming)
AIRCRAFT
Corporation
TWIN 680FL(P) Metal + Twin Commander 600 Series X
AIRCRAFT
Corporation
AIRCRAFT
Corporation
VULCANAIR P.68 Metal Vulcanair P.68 Series X
‘Observer 2’ (Lycoming)
VULCANAIR P.68 Metal Vulcanair P.68 Series ELA2 X
‘Observer’ (Lycoming)
VULCANAIR P.68 ‘Victor’ Metal Vulcanair P.68 Series ELA2 X
(Lycoming)

(Part-66)

VULCANAIR P.68B Metal Vulcanair P.68 Series ELA2 X
‘Victor’ (Lycoming)
VULCANAIR P.68C Metal Vulcanair P.68 Series ELA2 X
(Lycoming)
VULCANAIR P.68C-TC Metal Vulcanair P.68 Series ELA2 X
(Lycoming)
VULCANAIR P.68R Metal Vulcanair P.68 Series ELA2 X
‘Victor’ (Lycoming)
VULCANAIR P.68TC Metal Vulcanair P.68 Series ELA2 X
‘Observer’ (Lycoming)
VULCANAIR P.64 ‘Oscar’ Metal Vulcanair P.64 ELA1 X
series/V1.0/V1.1 (Lycoming)
VULCANAIR P.64B ‘Oscar Metal Vulcanair P.64 ELA1 X
200’ series/V1.0/V1.1 (Lycoming)
B 1155’ series/V1.0/V1.1 (Lycoming)
B’ series/V1.0/V1.1 (Lycoming)
VULCANAIR VULCANAIR Metal Vulcanair P.64 ELA1
V1.0 series/V1.0/V1.1 (Lycoming)
(formerly
P.64B
‘OSCAR B
1155’)
VULCANAIR VULCANAIR Metal Vulcanair P.64 ELA1
V1.1 series/V1.0/V1.1 (Lycoming)
(formerly
P.64B ‘Oscar
200’
VULCANAIR P.66B ‘Oscar Metal Vulcanair P.66 series/ ELA1 X
100’ V1.100L/V1.150L/V1.CL
(Lycoming)
150’ series/V1.100L/V1.150L/V1.CL
(Lycoming)
VULCANAIR P.66C Metal Vulcanair P.66 series/ ELA1 X
‘CHARLIE’ V1.100L/V1.150L/V1.CL
(Lycoming)
VULCANAIR VULCANAIR Metal Vulcanair P.66 series/ ELA1
V1.100L V1.100L/V1.150L/V1.CL
(formerly (Lycoming)
P.66B ‘Oscar
100’)
V1.150L V1.100L/V1.150L/V1.CL
P.66B ‘Oscar
150’)

(Part-66)

V1.CL V1.100L/V1.150L/V1.CL
P.66C
‘Charlie’)
WACO Aircraft YMF F5 Wood + Waco YMF (Jacobs) ELA2 X
Company Metal tubing
Fabric
WACO Aircraft YMF F5C Wood + Waco YMF (Jacobs) ELA2 X
Company Metal tubing
Fabric
WACO Classic 2T-1A-1 Wood + Waco 2T Series (Lycoming) ELA1 X
Aircraft Corp Metal tubing
Fabric
WACO Classic 2T-1A-2 Wood + Waco 2T Series (Lycoming) ELA1 X
Aircraft Corp Metal tubing
Fabric
WASSMER CE 43 Metal CERVA CE43 (Lycoming) ELA2 X
(Aircraft with
SAS)
WASSMER WA 4/21 Wood + WA4/21 Series (Lycoming) ELA2 X
(Aircraft with Metal tubing
SAS) Fabric
WASSMER WA Wood + WA4/21 Series (Lycoming) ELA2 X
(Aircraft with 4/21/250 Metal tubing
SAS) ‘Super 4/21’ Fabric
WASSMER WA 40 A Wood + WA40 Series (Lycoming) ELA1 X
(Aircraft with Metal tubing
SAS) Fabric
WASSMER WA 40 Wood + WA40 Series (Lycoming) ELA1 X
(Aircraft with ‘SUPER IV’ Metal tubing
SAS) Fabric
WASSMER WA 40 B Wood + WA40 Series (Lycoming) ELA1 X
(Aircraft with ‘Super IV Metal tubing
SAS) Sancy’ Fabric
WASSMER WA 41 Wood + WA41 (Lycoming) ELA1 X
(Aircraft with ‘Baladou’ Metal tubing
SAS) Fabric
WITHOUT TC RF 3 Wood RF 3 (Rectimo) ELA1 X
HOLDER -
ORPHANED (ex
Fournier, René)
WITHOUT TC RF 4 Wood RF 4 (VW) ELA1 X
HOLDER -
ORPHANED (ex
Fournier, René)
WITHOUT TC RF 47 Wood RF 47 (Limbach) ELA1 X
HOLDER -

(Part-66)

ORPHANED (ex
Fournier, René)
WITHOUT TC RF.6.B. 100 Wood RF 6B (Continental) ELA1 X
HOLDER -
ORPHANED (ex
Fournier, René)
WITHOUT TC RF.6.B. 120 Wood RF 6B (Lycoming) ELA1 X
HOLDER -
ORPHANED (ex
Fournier, René)
WITHOUT TC RF.6.B. 90 Wood RF 6B (Lycoming) ELA1 X
HOLDER -
ORPHANED (ex
Fournier, René)
XtremeAir GmbH XA41 Composite XtremeAir XA42 (Lycoming) ELA1 X
XtremeAir GmbH XA42 Composite XtremeAir XA42 (Lycoming) ELA1 X
YAKOVLEV YAK-18T Metal Yakovlev YAK-18T (Vedeneyev) ELA2 X
(Aircraft with
SAS)
ZAKŁADY EM-11C Composite EM-11 (Lycoming) ELA2 X
LOTNICZE ORKA
ZENAIR LTD CH 2000 Metal Zenair CH2000 (Lycoming) ELA1 X
ZLIN AIRCRAFT Z 143 L Metal Zlin Z-143 L (Lycoming) ELA1 X
(MORAVAN
AVIATION)
ZLIN AIRCRAFT Z 143 Lsi Metal Zlin Z-143 L (Lycoming) ELA1 X
(MORAVAN
AVIATION)
(MORAVAN
AVIATION)
ZLIN AIRCRAFT Z 126 Metal Zlin Z-26 Series ELA1 X
(MORAVAN (Walter Minor/AVIA)
AVIATION)
ZLIN AIRCRAFT Z 126 T Metal Zlin Z-26 Series (Walter ELA1 X
(MORAVAN Minor/AVIA)
AVIATION)
ZLIN AIRCRAFT Z 226 A Metal Zlin Z-26 Series (Walter ELA1 X
AVIATION)
ZLIN AIRCRAFT Z 226 B Metal Zlin Z-26 Series (Walter ELA1 X
AVIATION)
ZLIN AIRCRAFT Z 226 M Metal Zlin Z-26 Series (Walter ELA1 X
AVIATION)

(Part-66)

ZLIN AIRCRAFT Z 226 MS Metal Zlin Z-26 Series (Walter ELA1 X
AVIATION)
ZLIN AIRCRAFT Z 226 T Metal Zlin Z-26 Series (Walter ELA1 X
AVIATION)
ZLIN AIRCRAFT Z 326 Metal Zlin Z-26 Series (Walter ELA1 X
AVIATION)
ZLIN AIRCRAFT Z 326 A Metal Zlin Z-26 Series (Walter ELA1 X
AVIATION)
ZLIN AIRCRAFT Z 326 M Metal Zlin Z-26 Series (Walter ELA1 X
AVIATION)
ZLIN AIRCRAFT Z 526 Metal + Zlin Z-26 Series (Walter ELA1 X
(MORAVAN Metal tubing Minor/AVIA)
AVIATION) & fabric
ZLIN AIRCRAFT Z 526 A Metal + Zlin Z-26 Series (Walter ELA1 X
AVIATION) & fabric
ZLIN AIRCRAFT Z 526 AFS Metal + Zlin Z-26 Series (Walter ELA1 X
AVIATION) & fabric
ZLIN AIRCRAFT Z 526 AFS-V Metal + Zlin Z-26 Series (Walter ELA1 X
AVIATION) & fabric
ZLIN AIRCRAFT Z 526 F Metal + Zlin Z-26 Series (Walter ELA1 X
AVIATION) & fabric
ZLIN AIRCRAFT Z 526 M Metal + Zlin Z-26 Series (Walter ELA1 X
AVIATION) & fabric
ZLIN AIRCRAFT Z 726 Metal + Zlin Z-26 Series (Walter ELA1 X
AVIATION) & fabric
ZLIN AIRCRAFT Z 726 K Metal + Zlin Z-26 Series (Walter ELA1 X
AVIATION) & fabric
ZLIN AIRCRAFT Z 142 Metal Zlin Z-42 Series (LOM) ELA1 X
(MORAVAN
AVIATION)
ZLIN AIRCRAFT Z 142 C Metal Zlin Z-42 Series (LOM) ELA1 X
(MORAVAN
AVIATION)
ZLIN AIRCRAFT Z 42 M Metal Zlin Z-42 Series (LOM) ELA1 X
(MORAVAN
AVIATION)

(Part-66)

ZLIN AIRCRAFT Z 42 MU Metal Zlin Z-42 Series (LOM) ELA1 X
(MORAVAN
AVIATION)
ZLIN AIRCRAFT Z 43 Metal Zlin Z-43 Series (LOM) ELA1 X
(MORAVAN
AVIATION)
ZLIN AIRCRAFT Z 50 M Metal Zlin Z-50 Series (LOM) ELA1 X
(MORAVAN
AVIATION)
ZLIN AIRCRAFT Z 50 L Metal Zlin Z-50L Series (Lycoming) ELA1 X
(MORAVAN
AVIATION)
ZLIN AIRCRAFT Z 50 LA Metal Zlin Z-50L Series (Lycoming) ELA1 X
(MORAVAN
AVIATION)
ZLIN AIRCRAFT Z 50 LS Metal Zlin Z-50L Series (Lycoming) ELA1 X
(MORAVAN
AVIATION)
ZLIN AIRCRAFT Z 50 LX Metal Zlin Z-50L Series (Lycoming) ELA1 X
(MORAVAN
AVIATION)
(MORAVAN
AVIATION)
STCs in GROUP 3 AEROPLANES

GROUP 3: PISTON-ENGINE AEROPLANES (other than those in Group 1) (STC)

STC holder Model Note
BARBARA AND 150 Metal Cessna 150 Series (Lycoming) ELA1. X
ROBERT WILLIAMS STC No
(STC) 10015952
BARBARA AND 150A Metal Cessna 150 Series (Lycoming) ELA1. X
(STC) 10015952
BARBARA AND 150B Metal Cessna 150 Series (Lycoming) ELA1. X
(STC) 10015952
BARBARA AND 150C Metal Cessna 150 Series (Lycoming) ELA1. X
(STC) 10015952
BARBARA AND 150D Metal Cessna 150 Series (Lycoming) ELA1. X
(STC) 10015952

(Part-66)

BARBARA AND 150E Metal Cessna 150 Series (Lycoming) ELA1. X
(STC) 10015952
BARBARA AND 150F Metal Cessna 150 Series (Lycoming) ELA1. X
(STC) 10015952
BARBARA AND 150G Metal Cessna 150 Series (Lycoming) ELA1. X
(STC) 10015952
BARBARA AND 150H Metal Cessna 150 Series (Lycoming) ELA1. X
(STC) 10015952
BARBARA AND 150J Metal Cessna 150 Series (Lycoming) ELA1. X
(STC) 10015952
BARBARA AND 150K Metal Cessna 150 Series (Lycoming) ELA1. X
(STC) 10015952
BARBARA AND 150L Metal Cessna 150 Series (Lycoming) ELA1. X
(STC) 10015952
BARBARA AND 150M Metal Cessna 150 Series (Lycoming) ELA1. X
(STC) 10015952
BARBARA AND A150K Metal Cessna 150 Series (Lycoming) ELA1. X
(STC) 10015952
BARBARA AND A150L Metal Cessna 150 Series (Lycoming) ELA1. X
(STC) 10015952
CEAPR (STC) DR Wood Robin DR 400 (Thielert) ELA1. X
400/120 D STC No
10014219
400/140 B STC No
10014219
400/180 R STC No
10014219
400/200 R STC No
10014219
CEAPR (STC) DR 400/RP Wood Robin DR 400 (Thielert) ELA1. X
STC No
10014219
HOFFMANN GmbH 150 Metal Cessna 150/A150/F150/FA150 ELA1. STC X
& Co. KG (STC) (Rotax)

(Part-66)

HOFFMANN GmbH A150 Metal Cessna 150/A150/F150/FA150 ELA1. STC X
HOFFMANN GmbH F150 Metal Cessna 150/A150/F150/FA150 ELA1. STC X
HOFFMANN GmbH FA150 Metal Cessna 150/A150/F150/FA150 ELA1. STC X
LTB SAMMET 150D Metal Cessna 150 (Rotax) ELA1. X
GmbH (STC) STC No
10015134
LTB SAMMET 150E Metal Cessna 150 (Rotax) ELA1. X
GmbH (STC) STC No
10015134
LTB SAMMET 150F Metal Cessna 150 (Rotax) ELA1. X
GmbH (STC) STC No
10015134
LTB SAMMET 150G Metal Cessna 150 (Rotax) ELA1. X
GmbH (STC) STC No
10015134
LTB SAMMET 150H Metal Cessna 150 (Rotax) ELA1. X
GmbH (STC) STC No
10015134
LTB SAMMET 150J Metal Cessna 150 (Rotax) ELA1. X
GmbH (STC) STC No
10015134
LTB SAMMET 150K Metal Cessna 150 (Rotax) ELA1. X
GmbH (STC) STC No
10015134
LTB SAMMET 150L Metal Cessna 150 (Rotax) ELA1. X
GmbH (STC) STC No
10015134
LTB SAMMET 150M Metal Cessna 150 (Rotax) ELA1. X
GmbH (STC) STC No
10015134
LTB SAMMET A150L Metal Cessna 150 (Rotax) ELA1. X
GmbH (STC) STC No
10015134
LTB SAMMET F150G Metal Cessna 150 (Rotax) ELA1. X
GmbH (STC) STC No
10015134
LTB SAMMET F150H Metal Cessna 150 (Rotax) ELA1. X
GmbH (STC) STC No
10015134
LTB SAMMET F150J Metal Cessna 150 (Rotax) ELA1. X
GmbH (STC) STC No
10015134
LTB SAMMET F150K Metal Cessna 150 (Rotax) ELA1. X
GmbH (STC) STC No
10015134

(Part-66)

LTB SAMMET F150L Metal Cessna 150 (Rotax) ELA1. X
GmbH (STC) STC No
10015134
LTB SAMMET F150M Metal Cessna 150 (Rotax) ELA1. X
GmbH (STC) STC No
10015134
LTB SAMMET FA150K Metal Cessna 150 (Rotax) ELA1. X
GmbH (STC) STC No
10015134
PORSCHE AG (STC) 182Q Metal Cessna 182Q/F182Q (Porsche) ELA2. STC X
PORSCHE AG (STC) F182Q Metal Cessna 182Q/F182Q (Porsche) ELA2. STC X
SAFRAN ENGINES 182M Metal Cessna 182/F182 Series (SMA) ELA2.
SAS (STC) STC No
10013975
SAFRAN ENGINES 182N Metal Cessna 182/F182 Series (SMA) ELA2.
SAS (STC) STC No
10013975
SAFRAN ENGINES 182P Metal Cessna 182/F182 Series (SMA) ELA2.
SAS (STC) STC No
10013975
SAFRAN ENGINES 182Q Metal Cessna 182/F182 Series (SMA) ELA2.
SAS (STC) STC No
10013975
SAFRAN ENGINES 182R Metal Cessna 182/F182 Series (SMA) ELA2.
SAS (STC) STC No
10013975
SAFRAN ENGINES F182P Metal Cessna 182/F182 Series (SMA) ELA2.
SAS (STC) STC No
10013975
SAFRAN ENGINES F182Q Metal Cessna 182/F182 Series (SMA) ELA2.
SAS (STC) STC No
10013975
SMA ENGINES INC. 182Q Metal Cessna 182/F182 Series (SMA) ELA2. X
(STC) STC No
10016495
SMA ENGINES INC. 182R Metal Cessna 182/F182 Series (SMA) ELA2. X
(STC) STC No
10016495
SPERL TECHNIK & 150 Metal Cessna 150/A150/F150/FA150 ELA1. STC X
ENTWICKLUNGEN (Rotax)
(STC)
SPERL TECHNIK & A150 Metal Cessna 150/A150/F150/FA150 ELA1. STC X
(STC)
SPERL TECHNIK & F150 Metal Cessna 150/A150/F150/FA150 ELA1. STC X
(STC)

(Part-66)

SPERL TECHNIK & FA150 Metal Cessna 150/A150/F150/FA150 ELA1. STC X
(STC)
TECHNIFY MOTORS 172F Metal Cessna 172/F172 (Technify) ELA1. X
GmbH (STC) STC No
10014287
TECHNIFY MOTORS 172G Metal Cessna 172/F172 (Technify) ELA1. X
GmbH (STC) STC No
10014287
TECHNIFY MOTORS 172H Metal Cessna 172/F172 (Technify) ELA1. X
GmbH (STC) STC No
10014287
TECHNIFY MOTORS 172I Metal Cessna 172/F172 (Technify) ELA1. X
GmbH (STC) STC No
10014287
TECHNIFY MOTORS 172K Metal Cessna 172/F172 (Technify) ELA1. X
GmbH (STC) STC No
10014287
TECHNIFY MOTORS 172L Metal Cessna 172/F172 (Technify) ELA1. X
GmbH (STC) STC No
10014287
TECHNIFY MOTORS 172M Metal Cessna 172/F172 (Technify) ELA1. X
GmbH (STC) STC No
10014287
TECHNIFY MOTORS 172N Metal Cessna 172/F172 (Technify) ELA1. X
GmbH (STC) STC No
10014287
TECHNIFY MOTORS 172P Metal Cessna 172/F172 (Technify) ELA1. X
GmbH (STC) STC No
10014287
TECHNIFY MOTORS 172R Metal Cessna 172/F172 (Technify) ELA1. X
GmbH (STC) STC No
10014287
TECHNIFY MOTORS 172S Metal Cessna 172/F172 (Technify) ELA1. X
GmbH (STC) STC No
10014287
TECHNIFY MOTORS F172F Metal Cessna 172/F172 (Technify) ELA1. X
GmbH (STC) STC No
10014287
TECHNIFY MOTORS F172G Metal Cessna 172/F172 (Technify) ELA1. X
GmbH (STC) STC No
10014287
TECHNIFY MOTORS F172H Metal Cessna 172/F172 (Technify) ELA1. X
GmbH (STC) STC No
10014287
TECHNIFY MOTORS F172K Metal Cessna 172/F172 (Technify) ELA1. X
GmbH (STC) STC No
10014287

(Part-66)

TECHNIFY MOTORS F172L Metal Cessna 172/F172 (Technify) ELA1. X
GmbH (STC) STC No
10014287
TECHNIFY MOTORS F172M Metal Cessna 172/F172 (Technify) ELA1. X
GmbH (STC) STC No
10014287
TECHNIFY MOTORS F172N Metal Cessna 172/F172 (Technify) ELA1. X
GmbH (STC) STC No
10014287
TECHNIFY MOTORS F172P Metal Cessna 172/F172 (Technify) ELA1. X
GmbH (STC) STC No
10014287
TECHNIFY MOTORS T206H Metal Cessna 206 (Technify) ELA2. X
GmbH (STC) STC No
10014500
TECHNIFY MOTORS TU206F Metal Cessna 206 (Technify) ELA2. X
GmbH (STC) STC No
10014500
TECHNIFY MOTORS TU206G Metal Cessna 206 (Technify) ELA2. X
GmbH (STC) STC No
10014500
TECHNIFY MOTORS U206F Metal Cessna 206 (Technify) ELA2. X
GmbH (STC) STC No
10014500
TECHNIFY MOTORS U206G Metal Cessna 206 (Technify) ELA2. X
GmbH (STC) STC No
10014500
TECHNIFY MOTORS U206H Metal Cessna 206 (Technify) ELA2. X
GmbH (STC) STC No
10014500
TECHNIFY MOTORS SR22 Composite Cirrus SR22 (Technify) ELA2. STC X
GmbH (STC)
TECHNIFY MOTORS PA-28-140 Metal Piper PA-28-140/150/151/160/ ELA1. X
GmbH (STC) 161/180/181 (Technify) STC No
10014364
10014364
10014364
10014364
10014364

(Part-66)

10014364
10014364
GROUP 4 SAILPLANES
GROUP 4 SAILPLANES
TC Holder Model Type of structure Note
AEROCLUBUL ROMANIEI IS-28B2 metal
AEROCLUBUL ROMANIEI IS-29D metal
AEROCLUBUL ROMANIEI IS-29D2 metal
AEROCLUBUL ROMANIEI IS-30 metal
AEROCLUBUL ROMANIEI IS-32A metal
AIRBUS DEFENCE AND SPACE GmbH FS 24 "Phoenix T" composite
AIRBUS DEFENCE AND SPACE GmbH FS 24 "Phoenix T0" composite
AIRBUS DEFENCE AND SPACE GmbH FS 24 "Phoenix" composite
AIRBUS DEFENCE AND SPACE GmbH Phoebus A0 composite
AIRBUS DEFENCE AND SPACE GmbH Phoebus A1 composite
AIRBUS DEFENCE AND SPACE GmbH Phoebus B1 composite
AIRBUS DEFENCE AND SPACE GmbH Phoebus C composite
ALEXANDER SCHLEICHER AS 12 composite
ALEXANDER SCHLEICHER ASG 32 composite The model has also
powered variants.
ALEXANDER SCHLEICHER ASG 32 MI composite
ALEXANDER SCHLEICHER ASH 25 composite
ALEXANDER SCHLEICHER ASH 26 composite
ALEXANDER SCHLEICHER AS-K 13 metal-tube, wood
ALEXANDER SCHLEICHER ASK 18 metal-tube, wood
ALEXANDER SCHLEICHER ASK 18 B metal-tube, wood
ALEXANDER SCHLEICHER ASK 21 composite
ALEXANDER SCHLEICHER ASK 21 B composite
ALEXANDER SCHLEICHER ASK 23 composite
ALEXANDER SCHLEICHER ASK 23 B composite
ALEXANDER SCHLEICHER ASW 12 composite
ALEXANDER SCHLEICHER ASW 12 BV composite
ALEXANDER SCHLEICHER ASW 15 B composite

(Part-66)
GROUP 4 SAILPLANES
ALEXANDER SCHLEICHER ASW 20 BL composite
ALEXANDER SCHLEICHER ASW 20 C composite
ALEXANDER SCHLEICHER ASW 20 CL composite
ALEXANDER SCHLEICHER ASW 20 L composite
ALEXANDER SCHLEICHER ASW 22 BE composite
ALEXANDER SCHLEICHER ASW 22 BL composite
ALEXANDER SCHLEICHER ASW 27-18 composite
ALEXANDER SCHLEICHER ASW 28-18 composite
ALEXANDER SCHLEICHER K 10 A wood
ALEXANDER SCHLEICHER K7 metal-tube, wood
ALEXANDER SCHLEICHER K8 metal-tube, wood
ALEXANDER SCHLEICHER K8B metal-tube, wood
ALEXANDER SCHLEICHER K8C metal-tube, wood
ALEXANDER SCHLEICHER Ka 6 BR wood
ALEXANDER SCHLEICHER Ka 6 BR-Pe wood
ALEXANDER SCHLEICHER Ka 6 C wood
ALEXANDER SCHLEICHER Ka 6 CR wood
ALEXANDER SCHLEICHER Ka 6 CR-PE wood
ALEXANDER SCHLEICHER Ka 6 E wood
ALEXANDER SCHLEICHER Ka 6/0 wood
ALLSTAR PZL GLIDER SP. Z.O.O. SZD-48-3 Jantar Standard composite
3
ALLSTAR PZL GLIDER SP. Z.O.O. SZD-50-3 "Puchacz" composite
ALLSTAR PZL GLIDER SP. Z.O.O. SZD-51-1 "Junior" composite
ALLSTAR PZL GLIDER SP. Z.O.O. SZD-55-1 composite
ALLSTAR PZL GLIDER SP. Z.O.O. SZD-59 "Acro" composite
AVIACOM.PL SP. ZO.O. B1-PW-5 composite
AVIACOM.PL SP. ZO.O. B1-PW-5D composite
AVIONIC SPOLKA JAWNA SZD-56-1 "Diana" composite
AVIONIC SPOLKA JAWNA SZD-56-2 "Diana 2" composite
BARRY AVIATION, LLC KR-03A metal
BLANIK AIRCRAFT CZ s.r.o. L - 33 SÓLO metal
BLANIK AIRCRAFT CZ s.r.o. L 13 A Blanik metal
BLANIK AIRCRAFT CZ s.r.o. L 23 SUPER-BLANÍK metal
BLANIK AIRCRAFT CZ s.r.o. L-13 "BLANÍK" metal
BLANIK AIRCRAFT CZ s.r.o. L-13 AC BLANÍK metal

(Part-66)
GROUP 4 SAILPLANES
DG FLUGZEUGBAU GMBH DG-100 composite
DG FLUGZEUGBAU GMBH DG-100 ELAN composite
DG FLUGZEUGBAU GMBH DG-100 G composite
DG FLUGZEUGBAU GMBH DG-100 G ELAN composite
DG FLUGZEUGBAU GMBH DG-1000S composite
DG FLUGZEUGBAU GMBH DG-200/17 composite
DG FLUGZEUGBAU GMBH DG-200/17 C composite
DG FLUGZEUGBAU GMBH DG-300 CLUB ELAN composite
DG FLUGZEUGBAU GMBH DG-300 CLUB ELAN ACRO composite
DG FLUGZEUGBAU GMBH DG-300 ELAN composite
DG FLUGZEUGBAU GMBH DG-300 ELAN ACRO composite
DG FLUGZEUGBAU GMBH DG-500 ELAN ORION composite
DG FLUGZEUGBAU GMBH DG-500 ELAN TRAINER composite
DG FLUGZEUGBAU GMBH DG-500/20 ELAN composite
DG FLUGZEUGBAU GMBH DG-500/22 ELAN composite
DG FLUGZEUGBAU GMBH DG-600/18 composite
DG FLUGZEUGBAU GMBH DG-800 S composite
DG FLUGZEUGBAU GMBH DG-808 S composite
DG FLUGZEUGBAU GMBH LS 1-0 composite
DG FLUGZEUGBAU GMBH LS 10-a composite
DG FLUGZEUGBAU GMBH LS 1-b composite
DG FLUGZEUGBAU GMBH LS 1-c composite
DG FLUGZEUGBAU GMBH LS 1-d composite
DG FLUGZEUGBAU GMBH LS 1-e composite
DG FLUGZEUGBAU GMBH LS 1-f composite
DG FLUGZEUGBAU GMBH LS 1-f (45) composite
DG FLUGZEUGBAU GMBH LS 3 composite
DG FLUGZEUGBAU GMBH LS 3-17 composite
DG FLUGZEUGBAU GMBH LS 6-18w composite
DG FLUGZEUGBAU GMBH LS 6-c composite
DG FLUGZEUGBAU GMBH LS 6-c18 composite
DG FLUGZEUGBAU GMBH LS 7-WL composite

(Part-66)
GROUP 4 SAILPLANES
DG FLUGZEUGBAU GMBH LS10-s composite
DG FLUGZEUGBAU GMBH LS8 composite
DG FLUGZEUGBAU GMBH LS8-18 composite
DG FLUGZEUGBAU GMBH LS8-a composite
DG FLUGZEUGBAU GMBH LS8-b composite
DG FLUGZEUGBAU GMBH LS8-s composite
DG FLUGZEUGBAU GMBH LS8-sb composite
ECOFLY GMBH FK 3 metal
EICHELSDOERFER GMBH mistral-c composite
EICHELSDOERFER GMBH SB 5 B wood
EICHELSDOERFER GMBH SB 5 E wood
FIBERGLAS TECHNIK R. LINDNER ASTIR CS composite
FIBERGLAS TECHNIK R. LINDNER ASTIR CS 77 composite
FIBERGLAS TECHNIK R. LINDNER ASTIR CS Jeans composite
FIBERGLAS TECHNIK R. LINDNER CLUB ASTIR II composite
FIBERGLAS TECHNIK R. LINDNER GROB G 103 "TWIN II" composite
FIBERGLAS TECHNIK R. LINDNER GROB G 103 A "TWIN II composite
ACRO"
FIBERGLAS TECHNIK R. LINDNER GROB G 103 C "TWIN III composite
ACRO"
FIBERGLAS TECHNIK R. LINDNER GROB G 103 C "TWIN III" composite
FIBERGLAS TECHNIK R. LINDNER GROB G102 "CLUB ASTIR composite
III b"
FIBERGLAS TECHNIK R. LINDNER GROB G102 "CLUB ASTIR composite
III"
FIBERGLAS TECHNIK R. LINDNER GROB G102 "STANDARD composite
ASTIR III"
FIBERGLAS TECHNIK R. LINDNER SPEED ASTIR II composite
FIBERGLAS TECHNIK R. LINDNER SPEED ASTIR II B composite
FIBERGLAS TECHNIK R. LINDNER STANDARD ASTIR II composite
FIBERGLAS TECHNIK R. LINDNER TWIN ASTIR composite
FIBERGLAS TECHNIK R. LINDNER TWIN ASTIR TRAINER composite
GLASFASER-FLUGZEUG-SERVICE BS 1 composite
GLASFASER-FLUGZEUG-SERVICE Club Libelle 205 composite
GLASFASER-FLUGZEUG-SERVICE Glasflügel 304 composite
GLASFASER-FLUGZEUG-SERVICE Glasflügel 604 composite
GLASFASER-FLUGZEUG-SERVICE H 301 "Libelle" composite
GLASFASER-FLUGZEUG-SERVICE H 301 B composite
GLASFASER-FLUGZEUG-SERVICE H 301 serial No. 1 composite
GLASFASER-FLUGZEUG-SERVICE Hornet composite
GLASFASER-FLUGZEUG-SERVICE Hornet C composite
GLASFASER-FLUGZEUG-SERVICE Kestrel composite
GLASFASER-FLUGZEUG-SERVICE Mosquito composite
GLASFASER-FLUGZEUG-SERVICE Mosquito B composite
GLASFASER-FLUGZEUG-SERVICE Standard Libelle composite

(Part-66)
GROUP 4 SAILPLANES
GLASFASER-FLUGZEUG-SERVICE Standard Libelle 201 B composite
GLASFASER-FLUGZEUG-SERVICE Standard Libelle 203 composite
HPH SPOL SRO Glasflügel 304 C composite
HPH SPOL SRO Glasflügel 304 CZ composite
HPH SPOL SRO Glasflügel 304 CZ-17 composite
HPH SPOL SRO Glasflügel 304 S composite
M & D FLUGZEUGBAU GMBH JS-MD 1C composite The model has also
powered variants.
PILATUS AIRCRAFT LTD. B4-PC11 metal
PILATUS AIRCRAFT LTD. B4-PC11A metal
PILATUS AIRCRAFT LTD. B4-PC11AF metal
SCHEIBE AIRCRAFT GMBH Bergfalke II metal-tube, wood
SCHEIBE AIRCRAFT GMBH Bergfalke II-55 metal-tube, wood
SCHEIBE AIRCRAFT GMBH Bergfalke III metal-tube, wood
SCHEIBE AIRCRAFT GMBH Bergfalke IV metal-tube, wood
SCHEIBE AIRCRAFT GMBH L-Spatz metal-tube, wood
SCHEIBE AIRCRAFT GMBH L-Spatz 55 metal-tube, wood
SCHEIBE AIRCRAFT GMBH L-Spatz III metal-tube, wood
SCHEIBE AIRCRAFT GMBH Mü 13 E "Bergfalke" metal-tube, wood
SCHEIBE AIRCRAFT GMBH SF 26 A "Standard" metal-tube, wood
SCHEIBE AIRCRAFT GMBH SF 27 A metal-tube, wood
SCHEIBE AIRCRAFT GMBH SF 27 B metal-tube, wood
SCHEIBE AIRCRAFT GMBH SF 30 A “Club-Spatz” metal-tube, wood
SCHEIBE AIRCRAFT GMBH SF 34 composite
SCHEIBE AIRCRAFT GMBH SF 34 B composite
SCHEIBE AIRCRAFT GMBH Spatz 55 composite
SCHEIBE AIRCRAFT GMBH Spatz A metal-tube, wood
SCHEIBE AIRCRAFT GMBH Spatz B metal-tube, wood
SCHEIBE AIRCRAFT GMBH Specht metal-tube, wood
SCHEIBE AIRCRAFT GMBH Sperber metal-tube, wood
SCHEIBE AIRCRAFT GMBH Zugvogel I metal-tube, wood
SCHEIBE AIRCRAFT GMBH Zugvogel II metal-tube, wood
SCHEIBE AIRCRAFT GMBH Zugvogel III metal-tube, wood
SCHEIBE AIRCRAFT GMBH Zugvogel III A metal-tube, wood
SCHEIBE AIRCRAFT GMBH Zugvogel III B metal-tube, wood
SCHEIBE AIRCRAFT GMBH Zugvogel IV metal-tube, wood
SCHEIBE AIRCRAFT GMBH Zugvogel IV A metal-tube, wood
SCHEMPP HIRTH FLUGZEUGBAU Arcus composite
SCHEMPP HIRTH FLUGZEUGBAU Cirrus composite
SCHEMPP HIRTH FLUGZEUGBAU Cirrus-VTC composite
SCHEMPP HIRTH FLUGZEUGBAU Discus a composite
SCHEMPP HIRTH FLUGZEUGBAU Discus b composite
SCHEMPP HIRTH FLUGZEUGBAU Discus CS composite
SCHEMPP HIRTH FLUGZEUGBAU Discus-2a composite

(Part-66)
GROUP 4 SAILPLANES
SCHEMPP HIRTH FLUGZEUGBAU Discus-2b composite
SCHEMPP HIRTH FLUGZEUGBAU Discus-2c composite
SCHEMPP HIRTH FLUGZEUGBAU Duo Discus composite
SCHEMPP HIRTH FLUGZEUGBAU Duo Discus C composite
SCHEMPP HIRTH FLUGZEUGBAU Janus composite
SCHEMPP HIRTH FLUGZEUGBAU Janus B composite
SCHEMPP HIRTH FLUGZEUGBAU Janus C composite
SCHEMPP HIRTH FLUGZEUGBAU Janus Ce composite
SCHEMPP HIRTH FLUGZEUGBAU Mini Nimbus B composite
SCHEMPP HIRTH FLUGZEUGBAU Mini Nimbus C composite
SCHEMPP HIRTH FLUGZEUGBAU Mini Nimbus HS 7 composite
SCHEMPP HIRTH FLUGZEUGBAU Nimbus-2 composite
SCHEMPP HIRTH FLUGZEUGBAU Nimbus-2B composite
SCHEMPP HIRTH FLUGZEUGBAU Nimbus-2C composite
SCHEMPP HIRTH FLUGZEUGBAU Nimbus-3/24,5 composite
SCHEMPP HIRTH FLUGZEUGBAU Nimbus-3D composite
SCHEMPP HIRTH FLUGZEUGBAU Nimbus-4D composite
SCHEMPP HIRTH FLUGZEUGBAU S wood
SCHEMPP HIRTH FLUGZEUGBAU SH wood
SCHEMPP HIRTH FLUGZEUGBAU SH 1 wood
SCHEMPP HIRTH FLUGZEUGBAU SHK 1 wood
SCHEMPP HIRTH FLUGZEUGBAU Standard Cirrus composite
SCHEMPP HIRTH FLUGZEUGBAU Standard Cirrus B composite
SCHEMPP HIRTH FLUGZEUGBAU Standard Cirrus CS 11-75L composite
SCHEMPP HIRTH FLUGZEUGBAU Standard Cirrus G composite
SCHEMPP HIRTH FLUGZEUGBAU Ventus a composite
SCHEMPP HIRTH FLUGZEUGBAU Ventus a/16.6 composite
SCHEMPP HIRTH FLUGZEUGBAU Ventus b composite
SCHEMPP HIRTH FLUGZEUGBAU Ventus b/16.6 composite
SCHEMPP HIRTH FLUGZEUGBAU Ventus c composite
SCHEMPP HIRTH FLUGZEUGBAU Ventus-2a composite
SCHEMPP HIRTH FLUGZEUGBAU Ventus-2b composite
SCHEMPP HIRTH FLUGZEUGBAU Ventus-2c composite
SCHEMPP HIRTH VÝROBA LETADEL VSO 10 composite
SCHEMPP HIRTH VÝROBA LETADEL VSO 10 C composite
SN CENTRAIR 101 composite
SN CENTRAIR 101 A composite
SN CENTRAIR 101 AP composite
SN CENTRAIR 101 B composite
SN CENTRAIR 101 BC composite
SN CENTRAIR 101 D composite
SN CENTRAIR 101 P composite

(Part-66)
GROUP 4 SAILPLANES
SN CENTRAIR 201 A composite
SN CENTRAIR 201 B composite
SN CENTRAIR 201 B1 composite
SN CENTRAIR ASW 20 F composite
SN CENTRAIR ASW 20 FL composite
SN CENTRAIR SNC 34C composite
SPORTINE AVIACIJA IR KO LAK-12 composite
SPORTINE AVIACIJA IR KO LAK-17A composite
SPORTINE AVIACIJA IR KO LAK-19 composite
WITHOUT TC HOLDER - ORPHANED 905 A wood
WITHOUT TC HOLDER - ORPHANED 905 S wood
WITHOUT TC HOLDER - ORPHANED 905 SA wood
WITHOUT TC HOLDER - ORPHANED Avia Strotel AC-4c composite
WITHOUT TC HOLDER - ORPHANED Carman-Morelli M200 wood
WITHOUT TC HOLDER - ORPHANED Diamant 16.5 composite
WITHOUT TC HOLDER - ORPHANED Diamant 18 composite
WITHOUT TC HOLDER - ORPHANED Elfe S3 metal, wood,
composite
WITHOUT TC HOLDER - ORPHANED Elfe S4 metal, wood,
composite
WITHOUT TC HOLDER - ORPHANED Elfe S4A metal, wood,
composite
WITHOUT TC HOLDER - ORPHANED Glasflügel 304 B composite
WITHOUT TC HOLDER - ORPHANED H 101 "Salto" composite
WITHOUT TC HOLDER - ORPHANED HBV-Diamant composite
WITHOUT TC HOLDER - ORPHANED JP 15-36 A composite
WITHOUT TC HOLDER - ORPHANED JP 15-36 AR composite
WITHOUT TC HOLDER - ORPHANED Kenilworth Me7 composite
WITHOUT TC HOLDER - ORPHANED PIK 20 composite
WITHOUT TC HOLDER - ORPHANED PIK 20B composite
WITHOUT TC HOLDER - ORPHANED PIK-20D composite
WITHOUT TC HOLDER - ORPHANED Siren "Edelweiss" C30S wood
WITHOUT TC HOLDER - ORPHANED Slingsby T51 Dart 15 wood
WITHOUT TC HOLDER - ORPHANED Slingsby T51 Dart 17 wood
WITHOUT TC HOLDER - ORPHANED Slingsby T51 Dart 17R wood
WITHOUT TC HOLDER - ORPHANED Slingsby T53B composite
WITHOUT TC HOLDER - ORPHANED Slingsby T59D composite
WITHOUT TC HOLDER - ORPHANED Standard Cirrus 75 VTC composite
WITHOUT TC HOLDER - ORPHANED Standard Cirrus G/81 composite
WITHOUT TC HOLDER - ORPHANED T.65 "Vega" composite
WITHOUT TC HOLDER - ORPHANED WA 26 CM wood, composite
WITHOUT TC HOLDER - ORPHANED WA 26 P wood, composite
WITHOUT TC HOLDER - ORPHANED WA 28 composite
WITHOUT TC HOLDER - ORPHANED WA 28 E composite

(Part-66)
GROUP 4 SAILPLANES
WITHOUT TC HOLDER - ORPHANED WA 28 EF composite
WITHOUT TC HOLDER - ORPHANED WA 28 F composite
ZAKLAD SZYBOWCOWY JEZOW PW-5 "Smyk" composite
ZAKLAD SZYBOWCOWY JEZOW PW-6U composite
ZAKLAD SZYBOWCOWY JEZOW SZD-22B "Mucha- wood
Standard"
ZAKLAD SZYBOWCOWY JEZOW SZD-22C "Mucha- wood
Standard"
ZAKLAD SZYBOWCOWY JEZOW SZD-24 C "Foka" wood
ZAKLAD SZYBOWCOWY JEZOW SZD-24-4A wood
ZAKLAD SZYBOWCOWY JEZOW SZD-25A Lis metal-tube, wood
ZAKLAD SZYBOWCOWY JEZOW SZD-30 "Pirat" wood
ZAKLAD SZYBOWCOWY JEZOW SZD-30C "Pirat" wood
ZAKLAD SZYBOWCOWY JEZOW SZD-32A "Foka 5" wood
ZAKLAD SZYBOWCOWY JEZOW SZD-36A "Cobra 15" wood, composite
ZAKLAD SZYBOWCOWY JEZOW SZD-38A "Jantar 1" composite
ZAKLAD SZYBOWCOWY JEZOW SZD-41A "Jantar composite
Standard"
ZAKLAD SZYBOWCOWY JEZOW SZD-42 "Jantar 2" composite
ZAKLAD SZYBOWCOWY JEZOW SZD-42-1 "Jantar 2" composite
ZAKLAD SZYBOWCOWY JEZOW SZD-42-2 "Jantar 2B" composite
ZAKLAD SZYBOWCOWY JEZOW SZD-48 "Jantar Standard composite
2"
ZAKLAD SZYBOWCOWY JEZOW SZD-48-1 "Jantar Standard composite
2"
ZAKLAD SZYBOWCOWY JEZOW SZD-48-1M "Jantar composite
Standard 2M"
ZAKLAD SZYBOWCOWY JEZOW SZD-48-3M "Brawo" composite
ZAKLAD SZYBOWCOWY JEZOW SZD-48-3M1 "Brawo" composite
ZAKLAD SZYBOWCOWY JEZOW SZD-48M "Jantar Standard composite
2M"
ZAKLAD SZYBOWCOWY JEZOW SZD-52-3 “Krokus S” composite
ZAKLAD SZYBOWCOWY JEZOW SZD-52-4 “Krokus C” composite
ZAKLAD SZYBOWCOWY JEZOW SZD-9 bis 1 D "Bocian" wood
ZAKLAD SZYBOWCOWY JEZOW SZD-9 bis 1 E "Bocian" wood
ZAKLADY LOTNICZE MDM-1 “Fox” composite
ZAKLADY LOTNICZE MDM-1P “Fox-P” composite
ZAKLADY LOTNICZE Swift S-1 composite

(Part-66)
GROUP 4 POWERED SAILPLANES


AEROCLUBUL ROMANIEI IS-28M2 metal
AEROCLUBUL ROMANIEI IS-28M2/80HP metal
AEROCLUBUL ROMANIEI IS-28M2/G metal
AEROCLUBUL ROMANIEI IS-28M2/GR metal
AEROMOT - INDUSTRIA MECANICO AMT-100 composite
AEROMOT - INDUSTRIA MECANICO AMT-200 composite
AEROMOT - INDUSTRIA MECANICO AMT-200S composite
ALEXANDER SCHLEICHER ASG 32 El composite
ALEXANDER SCHLEICHER ASH 25 E composite
ALEXANDER SCHLEICHER ASH 25 M composite
ALEXANDER SCHLEICHER ASH 30 Mi composite
ALEXANDER SCHLEICHER ASH 31 Mi composite
ALEXANDER SCHLEICHER ASK 16 B metal-tube, wood
ALEXANDER SCHLEICHER ASK 21 Mi composite
ALEXANDER SCHLEICHER ASW 22 BLE composite
ALEXANDER SCHLEICHER ASW 22 BLE 50R composite
ALEXANDER SCHLEICHER ASW 22 M composite
ALEXANDER SCHLEICHER ASW 24 E composite
ALEXANDER SCHLEICHER ASW 27-18 E composite
ALEXANDER SCHLEICHER ASW 28-18 E composite
AMS-FLIGHT D.O.O. CARAT A composite
BINDER MOTORENBAU GMBH ASH 25 EB composite
BINDER MOTORENBAU GMBH ASH 25 EB 28 composite
BINDER MOTORENBAU GMBH EB 28 composite
BINDER MOTORENBAU GMBH EB 28 Edition composite
BINDER MOTORENBAU GMBH EB 29 composite
BINDER MOTORENBAU GMBH EB 29D composite
BINDER MOTORENBAU GMBH EB29DR composite
BINDER MOTORENBAU GMBH EB29R composite
DG FLUGZEUGBAU GMBH DG-1000M composite
DG FLUGZEUGBAU GMBH DG-1000T composite
DG FLUGZEUGBAU GMBH DG-500 M composite
DG FLUGZEUGBAU GMBH DG-500 MB composite
DG FLUGZEUGBAU GMBH DG-600/18 M composite
DG FLUGZEUGBAU GMBH DG-600M composite
DG FLUGZEUGBAU GMBH DG-800 A composite
DG FLUGZEUGBAU GMBH DG-800 B composite

(Part-66)

DG FLUGZEUGBAU GMBH DG-800 LA composite
DG FLUGZEUGBAU GMBH DG-808 C composite
DG FLUGZEUGBAU GMBH LS10-st composite
DG FLUGZEUGBAU GMBH LS8-t composite
DG FLUGZEUGBAU GMBH LS9 composite
DIAMOND AIRCRAFT INDUSTRIES H 36 "Dimona" composite
DIAMOND AIRCRAFT INDUSTRIES HK 36 "Super Dimona" composite
DIAMOND AIRCRAFT INDUSTRIES HK 36 R "Super Dimona" composite
DIAMOND AIRCRAFT INDUSTRIES HK 36 TC composite
DIAMOND AIRCRAFT INDUSTRIES HK 36 TS composite
DIAMOND AIRCRAFT INDUSTRIES HK 36 TTC composite
DIAMOND AIRCRAFT INDUSTRIES HK 36 TTC-ECO composite
DIAMOND AIRCRAFT INDUSTRIES HK 36-TTS composite
E.I.S. HOLDING GmbH Fournier RF 3 wood
E.I.S. HOLDING GmbH Fournier RF 4 D wood
E.I.S. HOLDING GmbH Fournier RF 5 B "Sperber" wood
E.I.S. HOLDING GmbH SFS 31 "Milan" wood
EICHELSDOERFER GMBH KIWI composite
EVEKTOR, SPOL. S R.O. L 13 SDL Vivat metal
EVEKTOR, SPOL. S R.O. L 13 SDM Vivat metal
EVEKTOR, SPOL. S R.O. L 13 SE Vivat metal
EVEKTOR, SPOL. S R.O. L 13 SEH Vivat metal
EVEKTOR, SPOL. S R.O. L 13 SL Vivat metal
EVEKTOR, SPOL. S R.O. L 13 SW Vivat metal
FIBERGLAS TECHNIK R. LINDNER G 103 C TWIN III SL composite
FISCHER UND ENTWICKLUNGEN ASTIR CS 77 TOP composite
FISCHER UND ENTWICKLUNGEN ASTIR CS Jeans TOP composite
FISCHER UND ENTWICKLUNGEN ASTIR CS TOP composite
FISCHER UND ENTWICKLUNGEN ASW 20 TOP composite
FISCHER UND ENTWICKLUNGEN ASW 20B TOP composite
FISCHER UND ENTWICKLUNGEN ASW 20BL TOP composite
FISCHER UND ENTWICKLUNGEN ASW 20C TOP composite
FISCHER UND ENTWICKLUNGEN ASW 20CL TOP composite
FISCHER UND ENTWICKLUNGEN ASW 20L TOP composite
FISCHER UND ENTWICKLUNGEN ASW 24 TOP composite
FISCHER UND ENTWICKLUNGEN Standard Cirrus B TOP composite
FISCHER UND ENTWICKLUNGEN Standard Cirrus TOP composite
FOURNIER, RENE RF 9 wood
GANTENBRINK, BRUNO Eta composite
GROB AIRCRAFT AG G109 composite
GROB AIRCRAFT AG G109 B composite
HB-FLUGTECHNIK GMBH HB 21 metal-tube, wood

(Part-66)

HB-FLUGTECHNIK GMBH HB 21 V1 metal-tube, wood
HB-FLUGTECHNIK GMBH HB 21 V2 metal-tube, wood
HB-FLUGTECHNIK GMBH HB 21/2400 metal-tube, wood
HB-FLUGTECHNIK GMBH HB 21/2400 B metal-tube, wood
HB-FLUGTECHNIK GMBH HB 23/2400 metal-tube, wood
HB-FLUGTECHNIK GMBH HB 23/2400 Scanliner metal-tube, wood
HB-FLUGTECHNIK GMBH HB 23/2400 SP metal-tube, wood
HB-FLUGTECHNIK GMBH HB 23/2400 V2 metal-tube, wood
HPH SPOL SRO Glasflügel 304 eS composite
HPH SPOL SRO Glasflügel 304 MS composite
KORFF LUFTFAHRT Taifun 17 E composite
KORFF LUFTFAHRT Taifun 17 E II composite
LANGE AVIATION GMBH E1 Antares composite
M & D FLUGZEUGBAU GMBH AVO 68 - R "Samburo" metal-tube, wood
M & D FLUGZEUGBAU GMBH AVO 68 - R 100 "Samburo" metal-tube, wood
M & D FLUGZEUGBAU GMBH AVO 68 - R 115 "Samburo" metal-tube, wood
M & D FLUGZEUGBAU GMBH AVO 68 - s "Samburo" metal-tube, wood
M & D FLUGZEUGBAU GMBH AVO 68 - v "Samburo" metal-tube, wood
SCHEIBE AIRCRAFT GMBH SF 25 A metal-tube, wood
SCHEIBE AIRCRAFT GMBH SF 25 B metal-tube, wood
SCHEIBE AIRCRAFT GMBH SF 25 C metal-tube, wood
SCHEIBE AIRCRAFT GMBH SF 25 D metal-tube, wood
SCHEIBE AIRCRAFT GMBH SF 25 E metal-tube, wood
SCHEIBE AIRCRAFT GMBH SF 25 K metal-tube, wood
SCHEIBE AIRCRAFT GMBH SF 28 A “Tandem-Falke” metal-tube, wood
SCHEIBE AIRCRAFT GMBH SF 36 A composite
SCHEIBE AIRCRAFT GMBH SF 36 R composite
SCHEMPP HIRTH FLUGZEUGBAU ARCUS M composite
SCHEMPP HIRTH FLUGZEUGBAU Arcus T composite
SCHEMPP HIRTH FLUGZEUGBAU Discus bM composite
SCHEMPP HIRTH FLUGZEUGBAU Discus bT composite
SCHEMPP HIRTH FLUGZEUGBAU Discus-2cFES composite
SCHEMPP HIRTH FLUGZEUGBAU Discus-2cT composite
SCHEMPP HIRTH FLUGZEUGBAU Discus-2T composite
SCHEMPP HIRTH FLUGZEUGBAU Duo Discus T composite
SCHEMPP HIRTH FLUGZEUGBAU Janus CM composite
SCHEMPP HIRTH FLUGZEUGBAU Janus CT composite
SCHEMPP HIRTH FLUGZEUGBAU Nimbus-2M composite
SCHEMPP HIRTH FLUGZEUGBAU Nimbus-3DM composite
SCHEMPP HIRTH FLUGZEUGBAU Nimbus-3DT composite
SCHEMPP HIRTH FLUGZEUGBAU Nimbus-3T composite
SCHEMPP HIRTH FLUGZEUGBAU Nimbus-4DM composite
SCHEMPP HIRTH FLUGZEUGBAU Nimbus-4DT composite
SCHEMPP HIRTH FLUGZEUGBAU Nimbus-4M composite

(Part-66)

SCHEMPP HIRTH FLUGZEUGBAU Nimbus-4T composite
SCHEMPP HIRTH FLUGZEUGBAU Ventus bT composite
SCHEMPP HIRTH FLUGZEUGBAU Ventus cM composite
SCHEMPP HIRTH FLUGZEUGBAU Ventus cT composite
SCHEMPP HIRTH FLUGZEUGBAU Ventus-2cM composite
SCHEMPP HIRTH FLUGZEUGBAU Ventus-2cT composite
SCHEMPP HIRTH FLUGZEUGBAU Ventus-3T composite
SPORTINE AVIACIJA IR KO LAK-17AT composite
SPORTINE AVIACIJA IR KO LAK-17B FES composite
SPORTINE AVIACIJA IR KO LAK-19T composite
STEMME AG S6 composite
STEMME AG S6-RT composite
STEMME AG Stemme S10 composite
STEMME AG Stemme S10-V composite
STEMME AG Stemme S10-VT composite
STEMME AG Stemme S12 composite
TECHNOFLUG LEICHTFLUGZEUGBAU CARAT composite
TECHNOFLUG LEICHTFLUGZEUGBAU Piccolo composite
TECHNOFLUG LEICHTFLUGZEUGBAU Piccolo B composite
WITHOUT TC HOLDER - ORPHANED PIK 20 E II F composite
WITHOUT TC HOLDER - ORPHANED PIK 30 composite
WITHOUT TC HOLDER - ORPHANED PIK-20 E composite
WITHOUT TC HOLDER - ORPHANED PIK-20 E II composite
WITHOUT TC HOLDER - ORPHANED RF-5 AJ-1 Serrania wood
ZAKLAD SZYBOWCOWY JEZOW SZD-45A "Ogar" composite
GROUP 4 GAS BALLOONS


BALLONBAU WÖRNER GMBH K-STU/1000 ELA1
BALLONBAU WÖRNER GMBH NL-STU/1000 ELA1

(Part-66)

CAMERON BALLOONS LIMITED GB 1000 ELA1
LINDSTRAND TECHNOLOGIES LTD. 105G ELA1
LINDSTRAND TECHNOLOGIES LTD. 14M ELA1
WITHOUT TC HOLDER — ORPHANED K-1050/3-Ri ELA1
AERONAUTICAL CENTER AUGUR AL-30 ELA2 (Tethered gas balloon)
AEROPHILE SAS AEROPHILE 5500 ELA2 (Tethered gas balloon)
BALLONBAU WÖRNER GMBH FK-5500/STU ELA2 (Tethered gas balloon)
BALLONBAU WÖRNER GMBH FKP-STU/280 ELA1 (Tethered gas balloon)
BALLONBAU WÖRNER GMBH FK-STU/280 ELA1 (Tethered gas balloon)
LINDSTRAND TECHNOLOGIES LTD. 203T ELA2 (Tethered gas balloon)
LINDSTRAND TECHNOLOGIES LTD. 9T ELA1 (Tethered gas balloon)
LINDSTRAND TECHNOLOGIES LTD. LBL 203P ELA2 (Tethered gas balloon)
GROUP 4 HOT-AIR BALLOONS


AEROSTAR INTERNATIONAL CELL ELA2
AEROSTAR INTERNATIONAL RX-6 ELA2
AEROSTAR INTERNATIONAL RXS-8 ELA2
AEROSTAR INTERNATIONAL S-49A ELA2
AEROSTAR INTERNATIONAL S-57S ELA2
AEROSTAR INTERNATIONAL W100LB ELA2

(Part-66)

BALLONS CHAIZE CS 1600 F12 ELA1
BALLONS CHAIZE DC 1800 F16 ELA1
BALLONS CHAIZE DC-Type ELA1
BALLONS CHAIZE JZ 18 F12 ELA1
BALLONS CHAIZE JZX 18 F12 ELA1

(Part-66)

BALLONS LIBERT S.P.R.L. L12-2600 ELA1
BALLONS LIBERT S.P.R.L. L12-3000 ELA1
BALLONS LIBERT S.P.R.L. L1800 ELA1
BALLONS LIBERT S.P.R.L. L3000+ ELA1
BALLONS LIBERT S.P.R.L. L4000+ ELA2
BALLONS LIBERT S.P.R.L. LC Replica ELA1
BALLONS LIBERT S.P.R.L. LC2000 ELA1
BALLONSERVICE UND TECHNIK Schön-Mars ELA2
BALLONSERVICE UND TECHNIK Schön-Neptun ELA2
BALLONSERVICE UND TECHNIK Schön-Saturn ELA2
BALLONSERVICE UND TECHNIK Schön-Venus ELA2
BALÓNY KUBÍČEK SPOL. S.R.O. AB 2 ELA1
BALÓNY KUBÍČEK SPOL. S.R.O. AB 2a ELA1
BALÓNY KUBÍČEK SPOL. S.R.O. AB 8 ELA1
BALÓNY KUBÍČEK SPOL. S.R.O. AB 8 N30 ELA1
BALÓNY KUBÍČEK SPOL. S.R.O. AB N22 ELA1
BALÓNY KUBÍČEK SPOL. S.R.O. AB N30 ELA1
BALÓNY KUBÍČEK SPOL. S.R.O. AB O22 ELA1
BALÓNY KUBÍČEK SPOL. S.R.O. BALL ELA1
BALÓNY KUBÍČEK SPOL. S.R.O. BB D-Type ELA2
BALÓNY KUBÍČEK SPOL. S.R.O. BB ED-Type ELA1
BALÓNY KUBÍČEK SPOL. S.R.O. BB E-Type ELA1
BALÓNY KUBÍČEK SPOL. S.R.O. BB GP-Type ELA1
BALÓNY KUBÍČEK SPOL. S.R.O. BB N-Type ELA2
BALÓNY KUBÍČEK SPOL. S.R.O. BB O-Type ELA1
BALÓNY KUBÍČEK SPOL. S.R.O. BB P-Type ELA1
BALÓNY KUBÍČEK SPOL. S.R.O. BB Series ELA1
BALÓNY KUBÍČEK SPOL. S.R.O. BB XR-Type ELA1
BALÓNY KUBÍČEK SPOL. S.R.O. BB Z-Type ELA2
BALÓNY KUBÍČEK SPOL. S.R.O. BB100Z ELA2
BALÓNY KUBÍČEK SPOL. S.R.O. BB12 ELA1
BALÓNY KUBÍČEK SPOL. S.R.O. BB120P ELA2

(Part-66)

BALÓNY KUBÍČEK SPOL. S.R.O. BB142P ELA2
BALÓNY KUBÍČEK SPOL. S.R.O. BB17GP ELA1
BALÓNY KUBÍČEK SPOL. S.R.O. BB17XR ELA1
BALÓNY KUBÍČEK SPOL. S.R.O. BB20E ELA1
BALÓNY KUBÍČEK SPOL. S.R.O. BB20GP ELA1
BALÓNY KUBÍČEK SPOL. S.R.O. BB22N ELA1
BALÓNY KUBÍČEK SPOL. S.R.O. BEAR ELA1
BALÓNY KUBÍČEK SPOL. S.R.O. BEMB ELA2
BALÓNY KUBÍČEK SPOL. S.R.O. BURGER KING ELA1
BALÓNY KUBÍČEK SPOL. S.R.O. CUBE ELA1
BALÓNY KUBÍČEK SPOL. S.R.O. DHL ELA1
BALÓNY KUBÍČEK SPOL. S.R.O. FISH ELA1
BALÓNY KUBÍČEK SPOL. S.R.O. FORKLIFT ELA1
BALÓNY KUBÍČEK SPOL. S.R.O. GNOME ELA1
BALÓNY KUBÍČEK SPOL. S.R.O. HEART ELA1
BALÓNY KUBÍČEK SPOL. S.R.O. ICE ELA1

(Part-66)

BALÓNY KUBÍČEK SPOL. S.R.O. JAG ELA1
BALÓNY KUBÍČEK SPOL. S.R.O. JAGER ELA1
BALÓNY KUBÍČEK SPOL. S.R.O. JAGER 28 ELA1
BALÓNY KUBÍČEK SPOL. S.R.O. JUPOL ELA1
BALÓNY KUBÍČEK SPOL. S.R.O. KATZENKOPF ELA1
BALÓNY KUBÍČEK SPOL. S.R.O. KRIGL ELA1
BALÓNY KUBÍČEK SPOL. S.R.O. MONTGOLFIERE ELA1
BALÓNY KUBÍČEK SPOL. S.R.O. PHARE ELA1
BALÓNY KUBÍČEK SPOL. S.R.O. RABBIT ELA2
BALÓNY KUBÍČEK SPOL. S.R.O. REPLIKA ELA1
BALÓNY KUBÍČEK SPOL. S.R.O. SANTA ELA2
BALÓNY KUBÍČEK SPOL. S.R.O. SHIP ELA2
BALÓNY KUBÍČEK SPOL. S.R.O. SILO ELA1
BALÓNY KUBÍČEK SPOL. S.R.O. SKYBALLS ELA1
BALÓNY KUBÍČEK SPOL. S.R.O. VOSTOK ELA2
BALÓNY KUBÍČEK SPOL. S.R.O. WERA ELA2
BALÓNY KUBÍČEK SPOL. S.R.O. WURST ELA2
CAMERON BALLOONS LIMITED 105-24 ELA1
CAMERON BALLOONS LIMITED 105A ELA1

(Part-66)

CAMERON BALLOONS LIMITED 4 Pack-90 (Four Pack-1) ELA1
CAMERON BALLOONS LIMITED 56B ELA1
CAMERON BALLOONS LIMITED A Type Cloudhopper Series Ref.: Models LBL 21A to
LBL 35A
CAMERON BALLOONS LIMITED A Type Series Ref.: Models LBL 42A to
LBL 500A
CAMERON BALLOONS LIMITED A-105 ELA1
CAMERON BALLOONS LIMITED A-340HL ELA2
CAMERON BALLOONS LIMITED A-425LW ELA2
CAMERON BALLOONS LIMITED AML-105 ELA1

(Part-66)

CAMERON BALLOONS LIMITED Andrelon Bottle (Bottle-8) ELA1
CAMERON BALLOONS LIMITED Apple-120 ELA1
CAMERON BALLOONS LIMITED Apple-90 ELA1
CAMERON BALLOONS LIMITED AX10-150 S2 ELA2
CAMERON BALLOONS LIMITED AX10-160Z ELA2
CAMERON BALLOONS LIMITED AX5-42Bolt ELA1
CAMERON BALLOONS LIMITED AX56-Series 1/SP1 ELA1
CAMERON BALLOONS LIMITED AX6-56A ELA1
CAMERON BALLOONS LIMITED AX7-77A ELA1
CAMERON BALLOONS LIMITED B Type Series Ref.: Models LBL 56B to
LBL 105B
CAMERON BALLOONS LIMITED Ball-70 ELA1
CAMERON BALLOONS LIMITED Ball-77 (Ball-4) ELA1
CAMERON BALLOONS LIMITED Baltika-77 (Cylinder-14) ELA1
CAMERON BALLOONS LIMITED Battery LR2 (Cylinder-6) ELA1
CAMERON BALLOONS LIMITED Bear-72 ELA1
CAMERON BALLOONS LIMITED Bearskin ELA1

(Part-66)

CAMERON BALLOONS LIMITED Beer Crate-120 (Box-20) ELA1
CAMERON BALLOONS LIMITED Bertie Bassett-90 (St. Fig.10) ELA1
CAMERON BALLOONS LIMITED Bibendum -110 (St. Fig.-12) ELA1
CAMERON BALLOONS LIMITED Bic Chic-90 (Figure-6) ELA1
CAMERON BALLOONS LIMITED Bottle-100 (Bottle-2) ELA1
CAMERON BALLOONS LIMITED Bottle-77 (Bottle-6) ELA1
CAMERON BALLOONS LIMITED Bowler-90 (Hat-1) ELA1
CAMERON BALLOONS LIMITED Bradford/Bingley-90 (Box-9) ELA1
CAMERON BALLOONS LIMITED Brandenburger Tor (Box-3) ELA1
CAMERON BALLOONS LIMITED Britannia Pig-90 (Quadruped-8) ELA1
CAMERON BALLOONS LIMITED Buddy-90 (Figure-7) ELA1
CAMERON BALLOONS LIMITED Bulb-65 Light (Bulb-1) ELA1
CAMERON BALLOONS LIMITED Bull-110 (Quadruped-12) ELA1
CAMERON BALLOONS LIMITED Bunch-100 ELA1
CAMERON BALLOONS LIMITED Bunny-90 (Standing Figure-7) ELA1
CAMERON BALLOONS LIMITED Burger King (Burger-1) ELA1
CAMERON BALLOONS LIMITED Bus-90 ELA1
CAMERON BALLOONS LIMITED C Type Series Ref.: Models LBL 400C to
600C
CAMERON BALLOONS LIMITED C-100 ELA1
CAMERON BALLOONS LIMITED Cabin ELA1
CAMERON BALLOONS LIMITED Calling Card-110 (Box-10) ELA1
CAMERON BALLOONS LIMITED CameronBox 105 (Telef.häuschen) ELA1
CAMERON BALLOONS LIMITED Can-120 (Cylinder-16) ELA1
CAMERON BALLOONS LIMITED Can-60 (Barrel-60) ELA1
CAMERON BALLOONS LIMITED Can-77 (Cylinder-10) ELA1
CAMERON BALLOONS LIMITED Carrots-80 ELA1
CAMERON BALLOONS LIMITED Cart (Box-6) ELA1
CAMERON BALLOONS LIMITED Chateau-84 (House-1) ELA1
CAMERON BALLOONS LIMITED Cheese-82 (Horizontal Cylinder) ELA1
CAMERON BALLOONS LIMITED Chicken-105 (Bird-2) ELA1
CAMERON BALLOONS LIMITED Cider Bottle-120 (Cylinder- 9) ELA1
CAMERON BALLOONS LIMITED Clown Standing (Figure-6) ELA1
CAMERON BALLOONS LIMITED Club-90 ELA1
CAMERON BALLOONS LIMITED Cockerel-130 (Bird-7) ELA2 (Volume 3 681 m3)
CAMERON BALLOONS LIMITED Coffee Jug-90 (Jug-1) ELA1
CAMERON BALLOONS LIMITED Cola Can-90 (Cylinder-12) ELA1
CAMERON BALLOONS LIMITED Colt ‘Bullet‘ Type Ref.: Models 56B to 77B
CAMERON BALLOONS LIMITED Colt 56 Satzenbrau Bottle ELA1
CAMERON BALLOONS LIMITED Colt A Type Ref.: Models 17A to 400A

(Part-66)

CAMERON BALLOONS LIMITED Colt Ariel Bottle (Bottle-1) ELA1
CAMERON BALLOONS LIMITED Colt Beer Glass ELA1
CAMERON BALLOONS LIMITED Colt Beetle-105 (Car-3) ELA1
CAMERON BALLOONS LIMITED Colt Bottle-10 ELA1
CAMERON BALLOONS LIMITED Colt Bottle-90 (Bottle-5) ELA1
CAMERON BALLOONS LIMITED Colt Can-110 (Cylinder -15) ELA1
CAMERON BALLOONS LIMITED Colt Clown (Standing Figure-2) ELA1
CAMERON BALLOONS LIMITED Colt Cylinder One ELA1
CAMERON BALLOONS LIMITED Colt Film Can (Cylinder-5) ELA1
CAMERON BALLOONS LIMITED Colt Flying Book (Box-2) ELA1
CAMERON BALLOONS LIMITED Colt Flying Head ELA1
CAMERON BALLOONS LIMITED Colt Flying Hut ELA1
CAMERON BALLOONS LIMITED Colt Flying Jeans ELA1
CAMERON BALLOONS LIMITED Colt Flying Kiwi ELA1
CAMERON BALLOONS LIMITED Colt Flying Lager (Bottle 2) ELA1
CAMERON BALLOONS LIMITED Colt Flying Mitt ELA1
CAMERON BALLOONS LIMITED Colt Flying Open Book (Box-5) ELA1
CAMERON BALLOONS LIMITED Colt Flying Pig (Quadruped-6) ELA1
CAMERON BALLOONS LIMITED Colt Flying Shuttlecock (Cone- ELA1
CAMERON BALLOONS LIMITED Colt Flying Whiskey (Bottle 3) ELA1
CAMERON BALLOONS LIMITED Colt Flying Yacht ELA1
CAMERON BALLOONS LIMITED Colt Golf Ball-90 (Ball-2) ELA1
CAMERON BALLOONS LIMITED Colt Jumbo-2 ELA1
CAMERON BALLOONS LIMITED Colt Mickey Mouse (Wimi-3) ELA1
CAMERON BALLOONS LIMITED Colt Pils Bottle (Bottle-12) ELA1
CAMERON BALLOONS LIMITED Colt Santa Claus (St. Fig.-4) ELA1
CAMERON BALLOONS LIMITED Colt World-90 ELA1
CAMERON BALLOONS LIMITED Condom-105 (Cylinder-18) ELA1
CAMERON BALLOONS LIMITED Cooling Tower-80 (Cylinder-2) ELA1
CAMERON BALLOONS LIMITED Cork-105 ELA1
CAMERON BALLOONS LIMITED Cow-105 (Quadruped-2) ELA1
CAMERON BALLOONS LIMITED Cow-110 (Quadruped-5) ELA2 (Volume 5 947 m3)
CAMERON BALLOONS LIMITED Cube-105 ELA1
CAMERON BALLOONS LIMITED Cup-110 (Urn-1) ELA1
CAMERON BALLOONS LIMITED Cup-90 (F.A.) ELA1
CAMERON BALLOONS LIMITED Dinosaur-80 (Quadruped-1) ELA1
CAMERON BALLOONS LIMITED Dodo-105 (Bird 8) ELA1
CAMERON BALLOONS LIMITED Doll-105 Standing (Figure-8) ELA1

(Part-66)

CAMERON BALLOONS LIMITED Doll-90 (Cylinder-3) ELA1
CAMERON BALLOONS LIMITED Donald-97 (Head-10) ELA1
CAMERON BALLOONS LIMITED Double Cow -110 (Quadruped-10) ELA1
CAMERON BALLOONS LIMITED Douglas-110 (Figure-5) ELA2 (Volume 3 541 m3)
CAMERON BALLOONS LIMITED Dragon (Quadruped-4) ELA1
CAMERON BALLOONS LIMITED Drop-180 ELA2 (Volume 5 098 m3)
CAMERON BALLOONS LIMITED Drop-95 ELA1
CAMERON BALLOONS LIMITED Dude-90 ELA1
CAMERON BALLOONS LIMITED Eagle -110 (Bird-5) ELA1
CAMERON BALLOONS LIMITED Eagle-95 (Bird-4) ELA1
CAMERON BALLOONS LIMITED EB-90 (Glass-3) ELA1
CAMERON BALLOONS LIMITED Egg-120 ELA1
CAMERON BALLOONS LIMITED Elephant-77 ELA1
CAMERON BALLOONS LIMITED F.R. Ball ELA1
CAMERON BALLOONS LIMITED Film Can-90 (Cylinder-7) ELA1
CAMERON BALLOONS LIMITED Fire Truck-100 ELA1
CAMERON BALLOONS LIMITED Fire-90 (Cylinder-11) ELA1
CAMERON BALLOONS LIMITED Flame-95 ELA1
CAMERON BALLOONS LIMITED Flying Beer Glass (Cylinder-4) ELA1
CAMERON BALLOONS LIMITED Flying Castle ELA1
CAMERON BALLOONS LIMITED Flying Coffee Jar (Cylinder-8) ELA1
CAMERON BALLOONS LIMITED Flying Cow-110 (Quadruped-11) ELA1
CAMERON BALLOONS LIMITED Flying Ice Cream Cone (Cone-2) ELA1
CAMERON BALLOONS LIMITED Flying Lager Bottle (Bottle-4) ELA1
CAMERON BALLOONS LIMITED Flying Piggy Bank (House-2) ELA1
CAMERON BALLOONS LIMITED Flying Windmill ELA1
CAMERON BALLOONS LIMITED Football-120 (Sphere-120) ELA1
CAMERON BALLOONS LIMITED Fork Lift-105 ELA1
CAMERON BALLOONS LIMITED Freddo-105 (Standing Figure-13) ELA1
CAMERON BALLOONS LIMITED Frog-90 (Quadruped-7) ELA1
CAMERON BALLOONS LIMITED Furness 56 Building ELA1
CAMERON BALLOONS LIMITED Golf Ball-76 (Ball-1) ELA1
CAMERON BALLOONS LIMITED GosserMug90/Bierkrug90 ELA1
CAMERON BALLOONS LIMITED GP-65 ELA1
CAMERON BALLOONS LIMITED GP-70 ELA1
CAMERON BALLOONS LIMITED G-Rail-90 (Standing Figure 16) ELA1
CAMERON BALLOONS LIMITED Grand Illusion (Figure-3) ELA2 (Volume 3 535 m3)
CAMERON BALLOONS LIMITED Graz Box-110 (Box-19) ELA1
CAMERON BALLOONS LIMITED Grolsch-105 (Bottle-7) ELA1
CAMERON BALLOONS LIMITED H-20 ELA1

(Part-66)

CAMERON BALLOONS LIMITED Hard Hat-90 (Hat-2) ELA1
CAMERON BALLOONS LIMITED Harley-78 (Motor Bike-1) ELA1
CAMERON BALLOONS LIMITED Head 2-120 ELA1
CAMERON BALLOONS LIMITED Head One-105 ELA1
CAMERON BALLOONS LIMITED Head-90 (Head-15) ELA1
CAMERON BALLOONS LIMITED Heart-100 ELA1
CAMERON BALLOONS LIMITED Heart-120 ELA1
CAMERON BALLOONS LIMITED Helmet-120 (Head-16) ELA1
CAMERON BALLOONS LIMITED Hex Glass-84 (Glass-2) ELA1
CAMERON BALLOONS LIMITED Home Special-105 (House-3) ELA1
CAMERON BALLOONS LIMITED Horse-90 (Quadruped-3) ELA1
CAMERON BALLOONS LIMITED House-60 ELA1
CAMERON BALLOONS LIMITED Ikea-120 (Heart/Box-120) ELA1
CAMERON BALLOONS LIMITED Inverted Balloon-105 ELA1
CAMERON BALLOONS LIMITED Inverted Balloon-78 ELA1
CAMERON BALLOONS LIMITED Katalog-82 (Box-4) ELA1
CAMERON BALLOONS LIMITED Kindernet Dog-100 (St. Fig.-14) ELA1
CAMERON BALLOONS LIMITED Kookaburra-120 (Bird-6) ELA1
CAMERON BALLOONS LIMITED Krush Bottle-106 (Bottle-7) ELA1
CAMERON BALLOONS LIMITED L Type Series Refers to Model LBL 48L
CAMERON BALLOONS LIMITED LBL 105A ELA1
CAMERON BALLOONS LIMITED LBL 105B ELA1
CAMERON BALLOONS LIMITED LBL 210S ELA2
CAMERON BALLOONS LIMITED LBL 400C ELA2

(Part-66)

CAMERON BALLOONS LIMITED LBL 48L ELA1
CAMERON BALLOONS LIMITED LBL 60X ELA1
CAMERON BALLOONS LIMITED LBL Armchair ELA1
CAMERON BALLOONS LIMITED LBL Baby Bel ELA1
CAMERON BALLOONS LIMITED LBL Bananas ELA1
CAMERON BALLOONS LIMITED LBL Battery ELA1
CAMERON BALLOONS LIMITED LBL Bear ELA1
CAMERON BALLOONS LIMITED LBL Box ELA1
CAMERON BALLOONS LIMITED LBL Bulb ELA1
CAMERON BALLOONS LIMITED LBL Cake ELA1
CAMERON BALLOONS LIMITED LBL Cornetto ELA1
CAMERON BALLOONS LIMITED LBL Dog ELA1
CAMERON BALLOONS LIMITED LBL Dreher Bottle ELA1
CAMERON BALLOONS LIMITED LBL Drinks Can ELA1
CAMERON BALLOONS LIMITED LBL Flowers ELA1
CAMERON BALLOONS LIMITED LBL Flying M ELA1
CAMERON BALLOONS LIMITED LBL Flying Pig ELA1
CAMERON BALLOONS LIMITED LBL Four ELA1
CAMERON BALLOONS LIMITED LBL Fruit Bottle ELA1
CAMERON BALLOONS LIMITED LBL House ELA1
CAMERON BALLOONS LIMITED LBL Ice Cream Cone ELA1
CAMERON BALLOONS LIMITED LBL J and B Bottle ELA1
CAMERON BALLOONS LIMITED LBL Lion ELA1
CAMERON BALLOONS LIMITED LBL Lozenge ELA1
CAMERON BALLOONS LIMITED LBL Man ELA1
CAMERON BALLOONS LIMITED LBL Motorbike ELA2 (Volume 4 816 m3)
CAMERON BALLOONS LIMITED LBL Newspaper ELA1
CAMERON BALLOONS LIMITED LBL Octopus ELA1

(Part-66)

CAMERON BALLOONS LIMITED LBL Oriental Duck ELA1
CAMERON BALLOONS LIMITED LBL Pharmacist ELA1
CAMERON BALLOONS LIMITED LBL Pink Panther ELA1
CAMERON BALLOONS LIMITED LBL Pop Can ELA1
CAMERON BALLOONS LIMITED LBL Racing Car ELA1
CAMERON BALLOONS LIMITED LBL RR21 ELA1
CAMERON BALLOONS LIMITED LBL Salami ELA1
CAMERON BALLOONS LIMITED LBL Saloon Car ELA1
CAMERON BALLOONS LIMITED LBL Stove ELA1
CAMERON BALLOONS LIMITED LBL Sun ELA1
CAMERON BALLOONS LIMITED LBL Syrup Bottle ELA1
CAMERON BALLOONS LIMITED LBL Telewest Sphere ELA1
CAMERON BALLOONS LIMITED LBL Triangle ELA1
CAMERON BALLOONS LIMITED LBL Tulips ELA1
CAMERON BALLOONS LIMITED Light Bulb-110 (Light Bulb-2) ELA1
CAMERON BALLOONS LIMITED Lindstrand X Type Ref.: Models LBL 60X to
LBL 77X
CAMERON BALLOONS LIMITED Lips-90 ELA1
CAMERON BALLOONS LIMITED Loco-105 (Locomotive-1) ELA1
CAMERON BALLOONS LIMITED LTSB-90 (Box-14) ELA1
CAMERON BALLOONS LIMITED Macaw-90 (Bird-1) ELA1
CAMERON BALLOONS LIMITED Maple Leaf-95 ELA1
CAMERON BALLOONS LIMITED Mickey-90 (Wimi-1) ELA1
CAMERON BALLOONS LIMITED Mikey-90 (Head-13) ELA1
CAMERON BALLOONS LIMITED Minion-105 (Cylinder 19) ELA1
CAMERON BALLOONS LIMITED Modified Sugar Box-90 (Box-21) ELA1
CAMERON BALLOONS LIMITED Monster -110 (Head-12) ELA1
CAMERON BALLOONS LIMITED Monster Truck-105 ELA1
CAMERON BALLOONS LIMITED Mountie-120 (Quadruped-9) ELA1
CAMERON BALLOONS LIMITED Mug-90 (Cylinder-13) ELA1
CAMERON BALLOONS LIMITED N-100 ELA1
CAMERON BALLOONS LIMITED N-120 Fox ELA1
CAMERON BALLOONS LIMITED N120MW ELA1
CAMERON BALLOONS LIMITED N-120SP (Robijn) ELA1

(Part-66)

CAMERON BALLOONS LIMITED N-90 Nail ELA1
CAMERON BALLOONS LIMITED N-90 Nivea ELA1
CAMERON BALLOONS LIMITED Newspaper-90 (Cone-3) ELA1
CAMERON BALLOONS LIMITED Nissan Micra (Car-1) ELA1
CAMERON BALLOONS LIMITED Nudie-90 (Standing Figure-15) ELA1
CAMERON BALLOONS LIMITED O-105 ELA1
CAMERON BALLOONS LIMITED Obelix-90 (Figure-8) ELA1
CAMERON BALLOONS LIMITED Onion-105 ELA1
CAMERON BALLOONS LIMITED Orange Box-115 (Box-17) ELA1
CAMERON BALLOONS LIMITED Orange-120 ELA2 (Volume 3 436 m3)
CAMERON BALLOONS LIMITED Otti-34 ELA1
CAMERON BALLOONS LIMITED Pack-130 (Box-18) ELA2 (Volume 3 681 m3)
CAMERON BALLOONS LIMITED Paint Can-115 (Cylinder-17) ELA1
CAMERON BALLOONS LIMITED Parachutist-110 (Figure-4) ELA1
CAMERON BALLOONS LIMITED Peacock-90 (Bird-3) ELA1
CAMERON BALLOONS LIMITED Pipe-105 (Standing Figure-9) ELA1
CAMERON BALLOONS LIMITED PM-80 (Bottle-9) ELA1
CAMERON BALLOONS LIMITED Pot-180 (Cylinder-20) ELA2 (Volume 5 098 m3)
CAMERON BALLOONS LIMITED Pot-90 ELA1
CAMERON BALLOONS LIMITED Printer-105 (Box-15) ELA1
CAMERON BALLOONS LIMITED Pylon-80 (Figure-2) ELA1
CAMERON BALLOONS LIMITED R-200 ELA2 (Mixed Gas / Hot-Air
Balloons)
Balloons)
Balloons)
Balloons)

(Part-66)

Balloons)
Balloons)
Balloons)
CAMERON BALLOONS LIMITED Racing Car-110 (Car-4) ELA1
CAMERON BALLOONS LIMITED Raindrop-77 ELA1
CAMERON BALLOONS LIMITED Robijn N-133 ELA2 (Volume 3 767 m3)
CAMERON BALLOONS LIMITED Ronald-105 (Standing Figure-11) ELA1
CAMERON BALLOONS LIMITED RTW-120 ELA1
CAMERON BALLOONS LIMITED Rugby-90 (Ball-3) ELA1
CAMERON BALLOONS LIMITED Rupert Bear-90 (Standing Figure-5) ELA1
CAMERON BALLOONS LIMITED RX-100 ELA1
CAMERON BALLOONS LIMITED RX-105 ELA1
CAMERON BALLOONS LIMITED RX-120 Replica ELA1
CAMERON BALLOONS LIMITED S Can-100 ELA1
CAMERON BALLOONS LIMITED S Type Series Ref.: LBL 210S to 317S
CAMERON BALLOONS LIMITED Sarotti-105 (Standing Figure-3) ELA1
CAMERON BALLOONS LIMITED Saturn-110 (Sphere-110) ELA1
CAMERON BALLOONS LIMITED Saucer-80 ELA1
CAMERON BALLOONS LIMITED Ship-90 ELA1
CAMERON BALLOONS LIMITED Shoe-90 (Shoe-1) ELA1
CAMERON BALLOONS LIMITED Shopping Bag-120 (Box-7) ELA1
CAMERON BALLOONS LIMITED Sign-90 (Box-11) ELA1
CAMERON BALLOONS LIMITED Sim Card-120 ELA1
CAMERON BALLOONS LIMITED Sky-16 Series Ref.: Sky Models 25-16 to
80-16
317-24
500-28
CAMERON BALLOONS LIMITED Skywhale-110 ELA1
CAMERON BALLOONS LIMITED Smurf-2 (Head-11) ELA1
CAMERON BALLOONS LIMITED Snacpac-90 ELA1
CAMERON BALLOONS LIMITED Sonic-90 (Figure 1) ELA1
CAMERON BALLOONS LIMITED Spaceship-110 ELA1
CAMERON BALLOONS LIMITED Sparkasse Box-90 (Box-12) ELA1
CAMERON BALLOONS LIMITED Special Shape Hot Air Balloons Ref.: Cameron special shape
models - 4 Pack-90 (Four
Pack-1), etc.
CAMERON BALLOONS LIMITED Special Shape Hot Air Balloons LBL Ref.: LBL Special shape
models - Armchair, etc.
CAMERON BALLOONS LIMITED Sphere-105 ELA1
CAMERON BALLOONS LIMITED Sport-50 ELA1

(Part-66)

CAMERON BALLOONS LIMITED Sports Car-110 (Car-2) ELA1
CAMERON BALLOONS LIMITED Standing Bear-105 ELA1
CAMERON BALLOONS LIMITED Startac-105 ELA1
CAMERON BALLOONS LIMITED Sugar Box-90 (Box-16) ELA1
CAMERON BALLOONS LIMITED Sultan-80 (Standing Figure-1) ELA1
CAMERON BALLOONS LIMITED Super FMG-100 ELA1
CAMERON BALLOONS LIMITED Thomas-110 (Locomotive-2) ELA1
CAMERON BALLOONS LIMITED Thunder ‘Bolt’ Type Ref.: Models AX5-42Bolt to
AX7-77Bolt
CAMERON BALLOONS LIMITED Thunder A Type Ref.: Models AX6-56A and
AX7-77A
CAMERON BALLOONS LIMITED Thunder AX-Series S1 Ref.: Models AX5-42S1 to
AX10-180S1
CAMERON BALLOONS LIMITED Thunder AX-Series S2 Ref.: Models AX8-90S2 to
AX11-250S2
CAMERON BALLOONS LIMITED Thunder Forklift-90 ELA1
CAMERON BALLOONS LIMITED Thunder Z Type Ref.: Model AX4-31Z to
AX10-160Z
CAMERON BALLOONS LIMITED Tiger-90 ELA1
CAMERON BALLOONS LIMITED Tissue Pack-100 (Four Pack-2) ELA1
CAMERON BALLOONS LIMITED TR-60 ELA1
CAMERON BALLOONS LIMITED TR-84S1 ELA1
CAMERON BALLOONS LIMITED TR-84S2 ELA1
CAMERON BALLOONS LIMITED Trivial Pursuit (Box-1) ELA1
CAMERON BALLOONS LIMITED Truck-56 ELA1
CAMERON BALLOONS LIMITED Truck-72 ELA1
CAMERON BALLOONS LIMITED Tub-80 ELA1
CAMERON BALLOONS LIMITED Turtle-120 (Quadruped-13) ELA1
CAMERON BALLOONS LIMITED TV-80 (Box-8) ELA1
CAMERON BALLOONS LIMITED Tyre-100 (Horizontal Cylinder-2) ELA1
CAMERON BALLOONS LIMITED Unox -110 (Hat-3) ELA1
CAMERON BALLOONS LIMITED V-31 ELA1

(Part-66)

CAMERON BALLOONS LIMITED Van Gogh-110 Head-14 ELA1
CAMERON BALLOONS LIMITED Van-110 ELA1
CAMERON BALLOONS LIMITED Wallaby-42 ELA1
CAMERON BALLOONS LIMITED Watch-75 ELA1
CAMERON BALLOONS LIMITED Waving Flag-105 ELA1
CAMERON BALLOONS LIMITED Waving Flag-90 ELA1
CAMERON BALLOONS LIMITED Whisky Bottle-90 (Bottle-6) ELA1
CAMERON BALLOONS LIMITED Wimi Airbus-90 (Wimi-2) ELA1
CAMERON BALLOONS LIMITED Wine Box-90 (Box-13) ELA1
CAMERON BALLOONS LIMITED Z-105 ELA1
CAMERON BALLOONS LIMITED Z-425LW ELA2
CAMERON BALLOONS LIMITED Z-450Z ELA2
HEAD BALLOONS AX7-77 ELA2
HEAD BALLOONS AX7-77b ELA2
HEAD BALLOONS AX8-88b ELA2
JR AEROSPORTS LTD Firefly 10 ELA2

(Part-66)

JR AEROSPORTS LTD Firefly 11B ELA2
JR AEROSPORTS LTD Firefly 6B-15 ELA2
JR AEROSPORTS LTD Firefly 7-15 ELA2
JR AEROSPORTS LTD Firefly 8-24 ELA2
JR AEROSPORTS LTD Firefly B7 ELA2
JR AEROSPORTS LTD Firefly Bottle ELA2
JR AEROSPORTS LTD Firefly C7 ELA2
JR AEROSPORTS LTD Firefly C7B ELA2
JR AEROSPORTS LTD Firefly C8 ELA2
JR AEROSPORTS LTD Galaxy-7 ELA2
KAVANAGH INVESTMENT TRUST B-105 ELA1
KAVANAGH INVESTMENT TRUST C-56 ELA1
KAVANAGH INVESTMENT TRUST D-105 ELA1
KAVANAGH INVESTMENT TRUST E-120 ELA1

(Part-66)

KAVANAGH INVESTMENT TRUST EX-65 ELA1
KAVANAGH INVESTMENT TRUST G-450 ELA2
LINDSTRAND TECHNOLOGIES LTD. 70 ELA1
LINDSTRAND TECHNOLOGIES LTD. Lindstrand Racer Series ELA1
LINDSTRAND TECHNOLOGIES LTD. Lindstrand Series 1 ELA2
LINDSTRAND TECHNOLOGIES LTD. LTL Series Special ELA2
LINDSTRAND TECHNOLOGIES LTD. SR-56 ELA1
LINDSTRAND TECHNOLOGIES LTD. SR-65 ELA1
NOTHEISZ BALLOONS HUNGARY Kft. AX-10 ELA2
NOUVELLE MANUFACT. D’AEROSTATS MA 18 ELA1
SUP-AIR BALLON EGYESŰLET B-AX 8 ELA1
SUP-AIR BALLON EGYESŰLET C-AX 9 ELA2
SUP-AIR BALLON EGYESŰLET D-AX 5 ELA1
SUP-AIR BALLON EGYESŰLET E-AX-10 ELA2
SUP-AIR BALLON EGYESŰLET F-AX 7 ELA1
THEO SCHROEDER FIRE BALLOONS Auto ELA2
THEO SCHROEDER FIRE BALLOONS Bierglas ELA1
THEO SCHROEDER FIRE BALLOONS Cat ELA1
THEO SCHROEDER FIRE BALLOONS Clown-Kopf ELA1
THEO SCHROEDER FIRE BALLOONS Erdbeere ELA1
THEO SCHROEDER FIRE BALLOONS Fire Balloons G ELA2
THEO SCHROEDER FIRE BALLOONS Gasbehälter ELA1
THEO SCHROEDER FIRE BALLOONS Gasflasche ELA1
THEO SCHROEDER FIRE BALLOONS Gutfried ELA1
THEO SCHROEDER FIRE BALLOONS Kasper ELA2
THEO SCHROEDER FIRE BALLOONS Kater ELA1
THEO SCHROEDER FIRE BALLOONS Katze ELA1
THEO SCHROEDER FIRE BALLOONS Kopf ELA1
THEO SCHROEDER FIRE BALLOONS Kopfhörer ELA2

(Part-66)

THEO SCHROEDER FIRE BALLOONS Lefax ELA2
THEO SCHROEDER FIRE BALLOONS Maus ELA1
THEO SCHROEDER FIRE BALLOONS Ottifant ELA1
THEO SCHROEDER FIRE BALLOONS Pig 30 ELA1
THEO SCHROEDER FIRE BALLOONS Pig 36 ELA2
THEO SCHROEDER FIRE BALLOONS Pinguin ELA2
THEO SCHROEDER FIRE BALLOONS Schwartau ELA2
THEO SCHROEDER FIRE BALLOONS Sky Heart ELA2
THEO SCHROEDER FIRE BALLOONS Sunflower 36 ELA2
THEO SCHROEDER FIRE BALLOONS Teefix ELA1
THEO SCHROEDER FIRE BALLOONS Teekanne ELA1
THEO SCHROEDER FIRE BALLOONS Vase ELA1
ULTRAMAGIC, S.A. B-Series ELA1
ULTRAMAGIC, S.A. B-Series B-70 ELA1
ULTRAMAGIC, S.A. F-10 TXORI ELA1
ULTRAMAGIC, S.A. F-11 MONTGOLFIERE ELA1
ULTRAMAGIC, S.A. F-12 PAQUETE ELA1
ULTRAMAGIC, S.A. F-13 FAIRY ELA2
ULTRAMAGIC, S.A. F-14 JARRA DE CERVEZA ELA1
ULTRAMAGIC, S.A. F-15 BOTE-HUCHA ELA1
ULTRAMAGIC, S.A. F-16 CAJA 2 ELA1
ULTRAMAGIC, S.A. F-17 OVNI ELA1
ULTRAMAGIC, S.A. F-18 PIZZA ELA2
ULTRAMAGIC, S.A. F-19 CAVA ELA1
ULTRAMAGIC, S.A. F-20 BEETLE ELA1
ULTRAMAGIC, S.A. F-21 CEPSA ELA1
ULTRAMAGIC, S.A. F-22 TORRE ELA1
ULTRAMAGIC, S.A. F-24 FLYINGMAN ELA2
ULTRAMAGIC, S.A. F-25 FUTBOL ELA1
ULTRAMAGIC, S.A. F-26 HEART ELA1
ULTRAMAGIC, S.A. F-29 MOVISTAR ELA2
ULTRAMAGIC, S.A. F-30 EGG ELA1
ULTRAMAGIC, S.A. F-31 MAZORCA DEKALB ELA2
ULTRAMAGIC, S.A. F-32 BEIRAO BOTTLE ELA1
ULTRAMAGIC, S.A. F-33 PHAROX LAMP ELA2
ULTRAMAGIC, S.A. F-34 METTEN ELA2
ULTRAMAGIC, S.A. F-35 R4TS ELA2
ULTRAMAGIC, S.A. F-4 TXORI ELA1
ULTRAMAGIC, S.A. F-6 JAMBON ELA1
ULTRAMAGIC, S.A. F-7 BOTE ELA1
ULTRAMAGIC, S.A. F-8 LA CARTUJA ELA2
ULTRAMAGIC, S.A. F-9 BOTELLA DE AGUA ELA1
ULTRAMAGIC, S.A. F-Series ELA1
ULTRAMAGIC, S.A. G-Series ELA1

(Part-66)

ULTRAMAGIC, S.A. H-Series ELA1
ULTRAMAGIC, S.A. H-Series H-31 ELA1
ULTRAMAGIC, S.A. M-Series M-105 ELA1
ULTRAMAGIC, S.A. M-Series M-56C ELA1
ULTRAMAGIC, S.A. N-Series ELA2
ULTRAMAGIC, S.A. N-Series N-180 ELA2
ULTRAMAGIC, S.A. S-Series S-105 ELA1
ULTRAMAGIC, S.A. T-Series ELA2
ULTRAMAGIC, S.A. T-Series T-150 ELA2
ULTRAMAGIC, S.A. V-Series ELA1
ULTRAMAGIC, S.A. V-Series V-105 ELA1

(Part-66)

ULTRAMAGIC, S.A. Z Series ELA1
ULTRAMAGIC, S.A. Z-Series Z-90 ELA1
WITHOUT TC HOLDER — ORPHANED 105 A ELA1
WITHOUT TC HOLDER — ORPHANED FRX 65 ELA2
WITHOUT TC HOLDER — ORPHANED FS 57 A ELA2
WITHOUT TC HOLDER — ORPHANED FS 83 A ELA2
WITHOUT TC HOLDER — ORPHANED RX 6 ELA2
WITHOUT TC HOLDER — ORPHANED RXS 8 ELA2
WITHOUT TC HOLDER — ORPHANED S 40 A ELA2
WITHOUT TC HOLDER — ORPHANED SCB AX-6 ELA2
GROUP 4 GAS AIRSHIPS (other than those in Group 1)

GROUP 4 GAS AIRSHIPS

AMERICAN BLIMP CORPORATION A-1-50 ELA2
AMERICAN BLIMP CORPORATION A-1-70 ELA2
AMERICAN BLIMP CORPORATION A-60 ELA2
AMERICAN BLIMP CORPORATION A-60+ ELA2
CAMERON BALLOONS LIMITED DG-14 ELA2

(Part-66)
GROUP 4 GAS AIRSHIPS

WDL LUFTSCHIFFGESELLSCHAFT MBH P 4360 A ELA2
WDL LUFTSCHIFFGESELLSCHAFT MBH WDL I ELA2
WDL LUFTSCHIFFGESELLSCHAFT MBH WDL I B ELA2
GROUP 4 HOT-AIR AIRSHIPS

GROUP 4 HOT-AIR AIRSHIPS

CAMERON BALLOONS LIMITED AS 105 GD/4 ELA1
CAMERON BALLOONS LIMITED AS 105 GD/6 ELA2
CAMERON BALLOONS LIMITED AS 105 MkII ELA1
CAMERON BALLOONS LIMITED AS 80 GD ELA1
CAMERON BALLOONS LIMITED D-38 ELA1
CAMERON BALLOONS LIMITED DP-50 ELA1
LINDSTRAND HOT AIR BALLOONS HS-110 ELA1

(Part-66)
Appendix II — Aircraft Type Practical Experience and On-the-Job

Training - List of Tasks
Tasks are divided in categories of aircraft:

A) aeroplanes
B) sailplanes and powered sailplanes
C) balloons and airships
A. SPECIFIC TASKS FOR AEROPLANES
Time limits/Maintenance checks

100 hour check (general aviation aircraft).
‘B’ or ‘C’ check (transport category aircraft).
Assist carrying out a scheduled maintenance check i.a.w. AMM.
Review Aircraft maintenance log for correct completion.
Review records for compliance with Airworthiness Directives.
Review records for compliance with component life limits.
Procedure for inspection following heavy landing.
Procedure for inspection following lightning strike.
Dimensions/Areas
Locate component(s) by zone/station number.
Perform symmetry check.
Lifting and Shoring
Assist in:
Jack aircraft nose or tail wheel.
Jack complete aircraft.
Sling or trestle major component.
Levelling/Weighing
Level aircraft.
Weigh aircraft.
Prepare weight and balance amendment.
Check aircraft against equipment list.
Towing and Taxiing
Prepare for aircraft towing.
Tow aircraft.

(Part-66)
Be part of aircraft towing team.

Parking and mooring
Tie down aircraft.
Park, secure and cover aircraft.
Position aircraft in dock.
Secure rotor blades.
Placards and Markings
Check aircraft for correct placards.
Check aircraft for correct markings.
Servicing
Refuel aircraft.
Defuel aircraft.
Carry out tank to tank fuel transfer.
Check/adjust tire pressures.
Check/replenish oil level.
Check/replenish hydraulic fluid level.
Check/replenish accumulator pressure.
Charge pneumatic system.
Grease aircraft.
Connect ground power.
Service toilet/water system
Perform pre-flight/daily check.
Vibration and Noise Analysis

Analyse helicopter vibration problem.
Analyse noise spectrum.
Analyse engine vibration.
Air Conditioning
Replace combustion heater.
Replace flow control valve.
Replace outflow valve.
Replace safety valve.
Replace vapour cycle unit.
Replace air cycle unit.
Replace cabin blower.

(Part-66)
Replace heat exchanger.

Replace pressurisation controller.
Clean outflow valves.
Deactivate/reactivate cargo isolation valve.
Deactivate/reactivate avionics ventilation components.
Check operation of air conditioning/heating system.
Check operation of pressurisation system.
Troubleshoot faulty system.
Auto flight
Install servos.
Rig bridle cables Replace controller.
Replace amplifier.
Replacement of the auto flight system LRUs in case of fly-by-wire aircraft.
Check operation of auto-pilot.
Check operation of auto-throttle/auto-thrust.
Check operation of yaw damper.
Check and adjust servo clutch.
Perform autopilot gain adjustments.
Perform mach trim functional check.
Check autoland system.
Check flight management systems.
Check stability augmentation system.
Communications
Replace VHF COM unit.
Replace HF COM unit.
Replace existing antenna.
Replace static discharge wicks.
Check operation of radios.
Perform antenna VSWR check.
Perform SELCAL operational check.
Perform operational check of passenger address system.
Functionally check audio integrating system.
Repair coaxial cable.

(Part-66)
Check SATCOM.
Electrical Power
Charge lead/acid battery.
Charge Ni-Cad battery.
Check battery capacity.
Deep-cycle Ni-Cad battery.
Replace integrated drive/generator/alternator.
Replace switches.
Replace circuit breakers.
Adjust voltage regulator.
Change voltage regulator.
Amend electrical load analysis report.
Repair/replace electrical feeder cable.
Perform functional check of integrated drive/generator/alternator.
Perform functional check of voltage regulator.
Perform functional check of emergency generation system.
Equipment/Furnishings
Replace carpets
Replace crew seats.
Replace passenger seats.
Check inertia reels.
Check seats/belts for security.
Check emergency equipment.
Check ELT for compliance with regulations.
Repair toilet waste container.
Remove and install ceiling and sidewall panels.
Repair upholstery.
Change cabin configuration.
Replace cargo loading system actuator.
Test cargo loading system.
Replace escape slides/ropes.
Fire protection
Check fire bottle contents.
Check/test operation of fire/smoke detection and warning system.

(Part-66)
Check cabin fire extinguisher contents.

Check lavatory smoke detector system.
Check cargo panel sealing.
Install new fire bottle.
Replace fire bottle squib.
Inspect engine fire wire detection systems.
Flight Controls
Inspect primary flight controls and related components i.a.w. AMM.
Extending/retracting flaps & slats.
Replace horizontal stabiliser.
Replace spoiler/lift damper.
Replace elevator.
Deactivation/reactivation of aileron servo control.
Replace aileron.
Replace rudder.
Replace trim tabs.
Install control cable and fittings.
Replace slats.
Replace flaps.
Replace powered flying control unit.
Replace flat actuator.
Rig primary flight controls.
Adjust trim tab.
Adjust control cable tension.
Check control range and direction of movement.
Check for correct assembly and locking.
Functional test of primary flight controls.
Functional test of flap system.
Operational test of the side stick assembly.
Operational test of the THS.
THS system wear check.
Fuel
Water drain system (operation).

(Part-66)
Replace booster pump.

Replace fuel selector.
Replace fuel tank cells.
Replace/test fuel control valves.
Replace magnetic fuel level indicators.
Replace water drain valve.
Check/calculate fuel contents manually.
Check filters.
Flow check system.
Check calibration of fuel quantity gauges.
Check operation feed/selectors.
Check operation of fuel dump/jettison system.
Fuel transfer between tanks.
Pressure defuel.
Pressure refuel (manual control).
Deactivation/reactivation of the fuel valves (transfer defuel, X-feed, refuel).
Hydraulics
Replace engine driven pump.
Check/replace case drain filter.
Replace standby pump.
Replace hydraulic motor pump/generator.
Replace accumulator.
Check operation of shut off valve.
Check filters/clog indicators.
Check indicating systems.
Perform functional checks.
Pressurisation/depressurisation of the hydraulic system.
Power Transfer Unit (PTU) operation.
Replacement of PTU.
Ice and rain protection
Replace pump.
Replace timer.
Inspect repair propeller deice boot.

(Part-66)
Test propeller de-icing system.

Inspect/test wing leading edge de-icer boot.
Replace anti-ice/deice valve.
Install wiper motor.
Check operation of systems.
Operational test of the pitot-probe ice protection.
Operational test of the TAT ice protection.
Operational test of the wing ice protection system.
Assistance to the operational test of the engine air-intake ice protection (with engines operating).
Indicating/recording systems
Replace flight data recorder.
Replace cockpit voice recorder.
Replace clock.
Replace master caution unit.
Replace FDR.
Perform FDR data retrieval.
Implement ESDS procedures.
Inspect for HIRF requirements.
Start/stop EIS procedure.
Bite test of the CFDIU.
Ground scanning of the central warning system.
Landing Gear
Build up wheel.
Replace main wheel.
Replace nose wheel.
Replace steering actuator.
Replace truck tilt actuator.
Replace gear retraction actuator.
Replace uplock/downlock assembly.
Replace shimmy damper.
Rig nose wheel steering.
Functional test of the nose wheel steering system.
Replace shock strut seals.

(Part-66)
Replace brake unit.

Replace brake control valve.
Bleed brakes.
Replace brake fan.
Test anti-skid unit.
Test gear retraction.
Change bungees.
Adjust micro switches/sensors.
Charge struts with oil and air.
Test auto-brake system.
Replace rotorcraft skids.
Replace rotorcraft skid shoes.
Pack and check floats.
Flotation equipment.
Check/test emergency blowdown (emergency landing gear extension).
Operational test of the landing gear doors.
Lights
Repair/replace rotating beacon.
Repair/replace landing lights.
Repair/replace navigation lights.
Repair/replace interior lights.
Replace ice inspection lights.
Repair/replace logo lights.
Repair/replace emergency lighting system.
Perform emergency lighting system checks.
Troubleshoot faulty system
Instruments
Calibrate magnetic direction indicator.
Replace airspeed indicator.
Replace altimeter.
Replace air-data computer.
Replace ADI.
Replace HSI.

(Part-66)
Check pitot static system for leaks.

Check operation of directional gyro.
Check calibration of pitot static instruments.
Compass replacement direct/indirect.
Functional check flight director system.
Surveillance
Functional check weather radar.
Functional check doppler.
Functional check TCAS.
Functional check ATC transponder.
Check calibration of pressure altitude reporting system.
Navigation
Functional check inertial navigation system.
Complete quadrantal error correction of ADF system.
Check GPS.
Test AVM.
Check marker systems.
Functional check DME.
Oxygen
Inspect on board oxygen equipment.
Purge and recharge oxygen system.
Replace regulator.
Replace oxygen generator.
Test crew oxygen system.
Perform auto oxygen system deployment check.
Pneumatic systems
Replace filter.
Replace air shut off valve.
Replace pressure regulating valve.
Replace compressor.
Recharge dessicator.
Adjust regulator.
Check for leaks.

(Part-66)

Vacuum systems
Inspect the vacuum system i.a.w. AMM.
Replace vacuum pump.
Check/replace filters.
Adjust regulator.
Water/Waste
Replace water pump.
Replace tap.
Replace toilet pump.
Perform water heater functional check.
Inspect waste bin flap closure.
Central Maintenance System
Retrieve data from CMU.
Replace CMU.
Perform Bite check.
Airborne Auxiliary power
Install APU.
Inspect hot section.
Structures
Assessment of damage.
Sheet metal repair.
Fibre glass repair.
Wooden repair.
Fabric repair.
Recover fabric control surface.
Treat corrosion.
Apply protective treatment.
Doors
Inspect passenger door i.a.w. AMM.
Rig/adjust locking mechanism.

(Part-66)
Adjust air stair system.

Check operation of emergency exits.
Test door warning system.
Remove and install passenger door i.a.w. AMM.
Remove and install emergency exit i.a.w. AMM.
Inspect cargo door i.a.w. AMM.
Windows
Replace windshield.
Replace direct vision window.
Replace cabin window.
Repair transparency.
Wings
Skin repair.
Recover fabric wing.
Replace tip.
Replace rib.
Replace integral fuel tank panel.
Check incidence/rig.
Propeller
Assemble prop after transportation.
Replace propeller.
Replace governor.
Adjust governor.
Perform static functional checks.
Check operation during ground run.
Check track.
Check setting of micro switches.
Assessment of blade damage i.a.w. AMM.
Dynamically balance prop.
Main Rotors
Install rotor assembly.
Replace blades.
Replace damper assembly.

(Part-66)
Check track.
Check static balance.
Check dynamic balance.
Troubleshoot.
Rotor Drive
Replace mast.
Replace drive coupling.
Replace clutch/freewheel unit
Replace drive belt.
Install main gearbox.
Overhaul main gearbox.
Check gearbox chip detectors.
Tail Rotors
Install rotor assembly.
Replace blades.
Troubleshoot.
Tail Rotor Drive
Replace bevel gearbox.
Replace universal joints.
Overhaul bevel gearbox.
Install drive assembly.
Check chip detectors.
Check/install bearings and hangers.
Check/service/assemble flexible couplings.
Check alignment of drive shafts.
Install and rig drive shafts.
Rotorcraft flight controls
Install swash plate.
Install mixing box.
Adjust pitch links.
Rig collective system.
Rig cyclic system.
Rig anti-torque system.
Check controls for assembly and locking.
Check controls for operation and sense.

(Part-66)

Power Plant
Build up ECU.
Replace engine.
Repair cooling baffles.
Repair cowling.
Adjust cowl flaps.
Repair faulty wiring.
Troubleshoot.
Assist in dry motoring check.
Assist in wet motoring check.
Assist in engine start (manual mode).
Piston Engines
Remove/install reduction gear.
Check crankshaft run-out.
Check tappet clearance.
Check compression.
Extract broken stud.
Install helicoil.
Perform ground run.
Establish/check reference RPM.
Troubleshoot.
Turbine Engines
Replace module.
Replace fan blade.
Hot section inspection/boroscope check.
Carry out engine/compressor wash.
Carry out engine dry cycle.
Engine ground run.
Establish reference power.
Trend monitoring/gas path analysis.
Troubleshoot.
Fuel and control, piston
Adjust AMC.

(Part-66)
Adjust ABC.
Install carburettor/injector.
Adjust carburettor/injector.
Clean injector nozzles.
Replace primer line.
Check carburettor float setting.
Fuel and control, turbine
Replace FCU.
Replace Engine Electronic Control Unit (FADEC).
Replace Fuel Metering Unit (FADEC).
Clean/test fuel nozzles.
Clean/replace filters.
Adjust FCU.
Functional test of FADEC.
Ignition systems, piston
Change magneto.
Change ignition vibrator.
Change plugs.
Test plugs.
Check H.T. leads.
Install new leads.
Check timing.
Check system bonding.
Ignition systems, turbine
Perform functional test of the ignition system.
Check glow plugs/ignitors.
Check H.T. leads.
Check ignition unit.
Replace ignition unit.
Engine Controls

(Part-66)
Rig thrust lever.

Rig RPM control.
Rig mixture HP cock lever.
Rig power lever.
Check control sync (multi-eng).
Check controls for correct assembly and locking.
Check controls for range and direction of movement.
Adjust pedestal micro-switches.
Engine Indicating
Replace engine instruments(s).
Replace oil temperature bulb.
Replace thermocouples.
Check calibration.
Exhaust, piston
Replace exhaust gasket.
Inspect welded repair.
Pressure check cabin heater muff.
Exhaust, turbine
Change jet pipe.
Change shroud assembly.
Install trimmers.
Inspect/replace thrust reverser.
Replace thrust reverser component.
Deactivate/reactivate thrust reverser.
Operational test of the thrust reverser system.
Oil
Change oil.
Check filter(s).
Adjust pressure relief valve.
Replace oil tank.
Replace oil pump.
Replace oil cooler.

(Part-66)
Replace firewall shut off valve.

Perform oil dilution test.
Starting
Replace starter.
Replace start relay.
Replace start control valve.
Check cranking speed.
Turbines, piston engines
Replace PRT.
Replace turbo-blower.
Replace heat shields.
Replace waste gate.
Adjust density controller.
Engine water injection
Replace water/methanol pump.
Flow check water/methanol system.
Adjust water/methanol control unit.
Check fluid for quality.
Troubleshoot faulty system
Accessory gear boxes
Replace gearbox.
Replace drive shaft.
Inspect magnetic chip detector.
APU
Removal/installation of the APU.
Removal/installation of the inlet guide-vane actuator.
Operational test of the APU emergency shut-down test.
Operational test of the APU.

(Part-66)
B. SPECIFIC TASKS FOR SAILPLANES AND POWERED SAILPLANES

Structures Wooden/metal tube and
fabric/composite/metallic
General activities
Placards check or replace x
Weighing, weight & balance sheet x
Documentation of annual inspection, repair x
Review records for compliance with airworthiness directives x
Five annual inspections x
Inspection after an occurrence x
Dismantling/reinstallation of wings and empennages x
Leveling and weighing
Level the sailplane x
Weighing, weight & balance sheet x
Prepare a weight and balance amendment x
Check the list of equipment x
Flight controls and flight control systems
Aileron, flaps: Removal — Balancing — Reinstallation x
Elevator: Removal — Balancing — Reinstallation x
Rudder: Removal — Balancing — Reinstallation x
Rudder cable: Fabrication and installation x
Elevator pushrod: Installation x
Safeguarding of pins, screws, castellated nuts x
Sealing of gaps x
Electrical systems
Electrical components, wiring: Removal — Installation x
Batteries — Servicing x
Avionics systems
COM: Removal — Installation x
NAV: Removal — Installation x
XPDR: Removal — Installation x
Antenna/antenna cable: Removal — Installation x
Cabin equipment/systems
Belts/safety harnesses: Removal — Installation x
Oxygen system removal installation — Test x
Canopy replacement or repair x
Pitot/static system: Removal — Installation — Test x
Flight instruments: Removal — Installation x
Installation of approved equipment x
Compass: Installation — Compensation x
Tow release: Removal — Installation x
Water ballast system: Removal — Installation — Test x
Undercarriage: Removal — Installation x
Brake system: Replacement of components x
Fuel — Engine — Propeller — Engine — Instruments x

(Part-66)
Refer to the tasks related to propeller, piston engine, fuel and control, ignition,
engine indications and exhaust, which are contained in Table A ‘Specific tasks
for aeroplanes’
Verification and adjustment of folding system of powered sailplanes x
Wooden structures/Metal tubes and fabric
Inspection/testing for damages x
Rib structure repair x
Plywood skin repair x
Recover or repair structure with fabric x
Protective coating and finishing x
Install patch on fabric material x
Repair of fairings x
Composite structures
Laminate repair x
Sandwich structure repair x
Partial gel coat repair x
Complete gel coating x
Metal structures
Crack testing x
Repair of covering x
Drilling cracks x
Riveting jobs x
Bonding of structures x
Anti-corrosion treatment x
C. SPECIFIC TASKS FOR BALLOONS AND AIRSHIPS

Tasks Balloon Airship
Hot air Gas Tethered gas Hot air Gas
General activities:
Functionality test of aircraft (*) x x x x x
Placards check or replace x x x x x
Documentation annual inspection, repair, x x x x x
ADs, equipment (*)
Classification repair (*) x x x x x
Weighing:
Weighing and weighing report (*) x x x x x
Servicing:
Lubrication of controls when applicable x x x
Cleaning envelope, basket, burner x x x x x
Inspections:
Eight annual inspections (covering at least 3 x
different types) (*)
Five annual inspections (covering at least 2 x

(Part-66)
Three annual inspections (covering at least 2 x x

Two annual inspections (*) x
Strength test of envelope fabric (*) x x x x x
Flight control systems — Removal — Inspection — Reinstallation
Control surface cable x
Trim system x
Safeguarding of pins, screws, castellated nuts x x x
(*)
Stick and pedals x
Hydromechanical control systems x x
Ballonet control systems (*) x x x
Electrical control systems x x
Valves (gas valve, turning vent, parachute or x x x x x
rip panel) (*)
Control and shroud lines and pulleys x x x x x
Elevator – stabilizer (incl. balancing if x
applicable)
Rudder (incl. balancing if applicable) x
Drag rope x
Electrical system:
Removal – installation of electrical wires x x x
Removal – installation of electrical x x x
components
Servicing of batteries x x x x x
Communication system – Transponder:
Removal – installation of COM x x x x x
Removal – installation of NAV x
Removal – installation of XPDR x x x x x
Installation of antenna x x x x x
Replacement of antenna cable x x x x x
Cabin – Equipments:
Pitot / static systems – tubes removal - x
installation - replacement
Flight instruments removal - installation - x x x x x
replacement
Installation of an approved system x x x x x
Magnetic compass installation - x
compensation
Fire extinguisher x x x
Ballast - Replacement of:
Water ballast (when applicable) x
Sand/shot ballast (when applicable) x x x
Valves - inspection and rigging of valves x
Envelope:
Inspection and repair of envelope x x x x x
panels/gores/seams

(Part-66)
Inspection and repair of load tapes and x x x x x

attachment points
Inspection and repair of deflation system x x x
Inspection and repair of net x x
Inspection and repair of mooring system x
Electrostatic conductivity test (if type is x x
approved for hydrogen) (*)
Ballonet inspection and repair x x
Inspection and fabrication of a suspension x x x x x
cable or rope
Inspection and fabrication of a catena x x
Load ring/frame:
Crack detection (welded and machined parts) x x x x
(*)
Heater system:
Removal, inspection and re-installation x x
Inspection and cleaning of vaporizer and filter x x
(*)
Inspection and replacement of hoses (*) x x
Inspection and replacement of pilot flame x x
ignition unit (*)
Sealing of fittings (*) x x
Pressure and leak test (*) x x
Disassembly an assembly of fuel cell (*) x x
10-year inspection of fuel cell x x
Basket/gondola:
Removal, inspection and re-installation (as x x x x x
applicable)
Inspection and fabrication of a suspension x x
cable or rope (*)
Removal – installation of padding x x
Removal – installation of belts - safety x x
harness
Removal – installation of essential elements x x x x x
of the cabin
Inspection and fabrication of a basket wire x x x
Inspection of operational equipment and its x x x x x
fixation points
Crack detection and repair (welded parts and x x x x x
frames)
Landing gear:
Removal, inspection and re-installation of x x x
wheels
Removal, inspection and re-installation of x
brakes
Removal, inspection and re-installation of x
shock absorber
Fuel – Engine – Propeller – Engine instruments systems:
Refer to tasks in blocks for aeroplanes x x

(Part-66)
Wood structure:
Structure repair x x x
Protective coating
Composite structure:
Laminate repair x x
Sandwich structure repair x x
Metal structures:
Crack detection (welded and machined parts) x x x x x
Riveting jobs x x
Bonding of structures x x x x
Anti-corrosion treatment x x x
Repair of fairings x x
Engine:
Tasks for aeroplanes of comparable x x
certification level
Exhaust system:
certification level
Propeller:
certification level
Fuel system:
certification level
Hydraulic system:
certification level
Pneumatic system:
certification level
Winch system:
Witness winch inspection x

(Part-66)
Appendix III — Evaluation of the competence: assessment and

assessors
This Appendix applies to the competence assessment performed by the designated assessors (and
their qualifications).
1) What does ‘competence’ mean and areas of focus for assessment
The assessment should aim at measuring the competence by evaluating three major factors
associated to the learning objectives:
− Knowledge;
− Skills;
− Attitude;
Generally, knowledge is evaluated by examination. The purpose of this document is not to
describe the examination process: this material mainly addresses the evaluation of ‘skills’ and
‘attitude’ after training containing practical elements. Nevertheless, the trainee needs to
demonstrate to have sufficient knowledge to perform the required tasks.
‘Attitude’ is indivisible from the ‘skill’ as this greatly contributes to the safe performance of the
tasks.
The evaluation of the competence should be based on the learning objectives of the training, in
particular:
− the (observable) desired performance. This covers what the trainee is expected to be able
to do and how the trainee is expected to behave at the end of the training;
− the (measurable) performance standard that must be attained to confirm the trainee’s
level of competence in the form of tolerances, constraints, limits, performance rates or
qualitative statements; and
− the conditions under which the trainee will demonstrate competence. Conditions consist
of the training methods, the environmental, situational and regulatory factors.
The assessment should focus on the competencies relevant to the aircraft type and its
maintenance such as, but not limited to:
− Environment awareness (act safely, apply safety precautions and prevent dangerous
situations);
− Systems integration (demonstrate understanding of aircraft systems interaction –
identify, describe, explain, plan, execute);
− Knowledge and understanding of areas requiring special emphasis or novelty (areas
peculiar to the aircraft type, domains not covered by Part-66 Appendix I, practical training
elements that cannot be imparted through simulation devices, etc.);
− Using reports and indications (the ability to read and interpret);
− Aircraft documentation finding and handling (identify the appropriate aircraft
documentation, navigate, execute and obey the prescribed maintenance procedures);
− Perform maintenance actions (demonstrate safe handling of aircraft, engines,
components and tools);

(Part-66)
− Aircraft final/close-up and report (apply close up, initiate appropriate actions/follow-
up/records of testing, establish and sign maintenance records/logbooks).
2) How to assess
As far as feasible, the objectives of the assessment should be associated with the learning
objectives and the passing level; it means that observable criteria should be set in order to
measure the performance and should remain as objective as possible.
The general characteristics of effective assessment are: objective, flexible, acceptable,
comprehensive, constructive, organised and thoughtful. At the conclusion, the trainee should
have no doubt about what he/she did well, what he/she did poorly and how he/she can
improve.
The following is a non-exhaustive list of questions that may be posed to assist assessment:
− What are the success factors for the job?
− What are typical characteristics of a correct behaviour for the task?
− What criteria should be observed?
− What level of expertise is expected?
− Is there any standard available?
− What is the pass mark? For example:
− ‘Go-no go’ situation;
− How to allocate points? Minimum amount to succeed;
− ‘Must know or execute’ versus ‘Good to know or execute’ versus ‘Don’t expect the
candidate to be an expert’.
− Minimum or maximum time to achieve? Use time effectively and efficiently.
− What if the trainee fails? How many times is the trainee allowed to fail?
− When and how should the trainee be prepared for the assessment?
− What proportion of judgment by the instructor out of collaboration with the trainee is
needed during the evaluation stage?
The assessment may be:
− diagnostic (prior to a course), formative (re-orientate the course on areas where there is
a need to reinforce) or summative (partial or final evaluation);
− performed task-by-task, as a group of tasks or as a final assessment;
One method might be an initial assessment to be performed by the trainee himself, then
discussing areas where the perceptions of the trainee’s performance by the assessors differ in
order to:
− develop the self-assessment habits;
− make the assessment more acceptable and understandable to both parties.
A ‘box-ticking’ exercise would be pointless. Experience has shown that assessment sheets have
largely evolved over time into assessment of groups of ‘skills’ because in practice such things
eventually detracted from the training and assessment that it was intended to serve: evaluate

(Part-66)
at a point of time, encourage and orientate the training needs, improve safety and ultimately
qualify people for their duties.
In addition, many other aspects should be appropriately considered during the assessment
process such as stress and environmental conditions, difficulty of the test, history of evaluation
(such as tangible progresses or sudden and unexpected poor performance made by the trainee),
amount of time necessary to build competence, etc.
All these reasons place more emphasis on the assessor and highlight the function of the
organisation’s approval.
3) Who should assess
In order to qualify, the assessor should:
− Be proficient and have sufficient experience or knowledge in:
− human performance and safety culture;
− the aircraft type (necessary to have the certifying staff privileges in case of CRS
issuances);
− training/coaching/testing skills;
− instructional tools to use;
− Understand the objective and the content of the practical elements of the training that is
being assessed;
− Have interpersonal skills to manage the assessment process (professionalism, sincerity,
objectivity and neutrality, analysis skills, sense of judgement, flexibility, capability of
evaluating the supervisor’s or instructor’s reports, handling of trainee’s reactions to
failing assessment with the cultural environment, being constructive, etc.);
− Be ultimately designated by the organisation to carry out the assessment.
The roles may be combined for:
− the assessor and the instructor for the practical elements of the Type Rating Training; or
− the assessor and the supervisor for the On-the-Job Training.
provided that the objectives associated to each role are clearly understood and that the
competence and qualification criteria according to the company’s procedures are met for both
functions. Whenever possible (depending on the size of the organisation), it is recommended
to split the roles (two different persons) in order to avoid any conflicts of interests.
When the functions are not combined, the role of each function should be clearly understood.

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Easy Access Rules for Continuing Airworthiness Annex III (Part-66)

(Regulation (EU) No 1321/2014)

ANNEX III (PART-66)

66.1 Competent authority

AMC 66.1(a) Competent Authority

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SECTION A — TECHNICAL REQUIREMENTS

SUBPART A — AIRCRAFT MAINTENANCE LICENCE

66.A.3 Licence categories and subcategories

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GM 66.A.3 Licence categories

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66.A.5 Aircraft groups

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GM 66.A.5 Aircraft groups

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AMC 66.A.10 Application

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An applicant for an aircraft maintenance licence shall be at least 18 years of age.

(a) The following privileges shall apply:

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The category B2 licence does not include any A subcategory.

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1. The following definitions apply:

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AMC 66.A.20(a)(4) Privileges

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AMC 66.A.20(b)3 Privileges

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− The endorsement of group/subgroup ratings based on experience on a representative number

66.A.25 Basic knowledge requirements

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The holder of an aircraft maintenance licence in subcategory B1.2 or category B3 is deemed to

AMC 66.A.25 Basic knowledge requirements

1. For an applicant being a person qualified by holding an academic degree in an aeronautical,

GM 66.A.25(a) Basic knowledge requirements

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GM 66.A.25(b) Basic knowledge requirements

66.A.30 Basic experience requirements

(a) An applicant for an aircraft maintenance licence shall have acquired:

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(ii) as a derogation from point (i), 1 year of practical maintenance experience in

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AMC 66.A.30(a) Basic experience requirements

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− However, it is acceptable to combine the experience in a single 5-year period if the

AMC 66.A.30(c) Basic experience requirements

AMC 66.A.30(d) Basic experience requirements

AMC 66.A.30(e) Basic experience requirements

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66.A.40 Continued validity of the aircraft maintenance licence

GM 66.A.40 Continued validity of the aircraft maintenance licence

66.A.45 Endorsement with aircraft ratings

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− For category L, the relevant aircraft ratings are the following:

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GM 66.A.45 Endorsement with aircraft ratings