Hartzell Propeller LLC: One Propeller Place Piqua, Ohio 45356-2634 U.S.A. Telephone: 937.778.4200 Fax: 937.778.4215

HARTZELL PROPELLER LLC
One Propeller Place

Piqua, Ohio 45356-2634 U.S.A.
Telephone: 937.778.4200
Fax: 937.778.4215
MANUAL REVISION TRANSMITTAL

MANUAL 202A, VOLUME 7 (61-01-02)
Standard Practices Manual
REVISION 55 dated APRIL 2024
Remove Pages: Insert Pages:
COVER COVER
Cover and Inside Cover Cover and Inside Cover
REVISION HIGHLIGHTS REVISION HIGHLIGHTS
pages 1 thru 4 pages 1 thru 4
LIST OF EFFECTIVE PAGES LIST OF EFFECTIVE PAGES
pages 1 and 2 pages 1 and 2
INTRODUCTION INTRODUCTION
pages 1 thru 10 pages 1 thru 10
CONSUMABLE MATERIALS CONSUMABLE MATERIALS
pages 1-1 thru 1-16 pages 1-1 thru 1-16
pages 1-19 and 1-20 pages 1-19 and 1-20
VENDOR CROSS REFERENCE VENDOR CROSS REFERENCE
PACKAGING AND STORAGE PACKAGING AND STORAGE
pages 3-1 thru 3-20 pages 3-1 thru 3-20
NOTE 1: Record the removal of a Temporary Revision on the Record of Temporary

Revisions pages in this manual if applicable.
NOTE 2: When the manual revision has been inserted in the manual, record the information
required on the Record of Revisions page in this manual.
NOTE 3: Pages distributed in this revision may include pages from previous revisions if they
are on the opposite side of revised pages. This is done as a convenience to those
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Manual No. 202A, Volume 7
61-01-02
Revision 55
April 2024
Standard Practices Manual

Volume 7
Consumable Materials
Packaging and Storage
Hartzell Propeller LLC

One Propeller Place
Phone: 937.778.4200
Fax: 937.778.4215
HARTZELL STANDARD PRACTICES MANUAL 202A
VOLUME 7
© 2004, 2006, 2007, 2008, 2009, 2010, 2012, 2014, 2015, 2016, 2017, 2018, 2019, 2020, 2021, 2022, 2023,
2024 - Hartzell Propeller LLC - All rights reserved
COVER 61-01-02 Inside Cover

Rev. 55 Apr/24
VOLUME 7
202A, VOLUME 7 - REVISION 55 HIGHLIGHTS

Revision 55, dated April 2024, incorporates the following:
Front matter (Cover, Revision Highlights, etc.), has been revised to match this revision.
Removed references to "Hartzell Propeller Inc.". Revised to "Hartzell Propeller LLC"
where applicable.
Minor language/format changes and renumbering, if applicable are marked with a revision
bar, but are not listed below.
• CONSUMABLE MATERIALS
• Revised Table 1-1, "Consumable Materials"
REVISION HIGHLIGHTS 61-01-02 Page 1

Rev. 55 Apr/24
VOLUME 7
REVISION 55 HIGHLIGHTS
1. Introduction
A. General
(1) This is a list of current revisions that have been issued against this manual.
Please compare to the RECORD OF REVISIONS page to make sure that all
revisions have been added to the manual.
B. Components
(1) Revision No. indicates the revisions incorporated in this manual.
(2) Issue Date is the date of the revision.
(3) Comments indicates the level of the revision.
(a) New Issue is a new manual distribution. The manual is distributed in its
entirety. All the revision dates are the same and no change bars are used.
(b) Reissue is a revision to an existing manual that includes major content
and/or major format changes. The manual is distributed in its entirety. All
the revision dates are the same and no change bars are used.
(c) Major Revision is a revision to an existing manual that includes major
content or minor format changes over a large portion of the manual. The
manual is distributed in its entirety. All the revision dates are the same, but
change bars are used to indicate the changes incorporated in the latest
revision of the manual.
(d) Minor Revision is a revision to an existing manual that includes minor
content changes to the manual. Only the revised pages of the manual are
distributed. Each page retains the date and the change bars associated
with the last revision to that page.

Rev. 55 Apr/24
VOLUME 7
Revision No. Issue Date Comments

Original Mar/93 New
Revision 1 Jun/94 Minor Revision
Revision 2 Apr/95 Minor Revision
Revision 5 Nov/96 Minor Revision
Revision 6 Mar/97 Minor Revision
Revision 7 Oct/97 Minor Revision
Revision 8 Jan/98 Minor Revision
Revision 10 Dec/98 Minor Revision
Revision 11 Sep/99 Minor Revision
Revision 14 Feb/02 Minor Revision
Revision 15 May/02 Minor Revision
Revision 18 Aug/03 Minor Revision
Revision 27 Oct/04 Major Revision - Volume 7

Rev. 55 Apr/24
VOLUME 7
Revision No. Issue Date Comments

Revision 46 Jul/18 Minor Revision
Revision 54 Nov/23 Major Revision

Rev. 55 Apr/24
VOLUME 7
RECORD OF REVISIONS
This is a record of revisions inserted into this manual.
Revision 54 includes all prior revisions.
Revision Number Issue Date Date Inserted Inserted By
54 Nov/23 Nov/23 HPI
55 Apr/24 Apr/24 Hartzell
RECORD OF REVISIONS 61-01-02 Page 1

Rev. 54 Nov/23
VOLUME 7
RECORD OF REVISIONS 61-01-02 Page 2

Rev. 54 Nov/23
VOLUME 7
RECORD OF TEMPORARY REVISIONS

Update this page to show all temporary revisions inserted into this manual.
Revision 54 includes all prior temporary revisions, up to and including TR-024.
Temporary Section/ Issue Date Inserted Date Removed

Revision No. Page Date Inserted By Removed By
RECORD OF TEMPORARY REVISIONS 61-01-02 Page 1

Rev. 54 Nov/23
VOLUME 7
RECORD OF TEMPORARY REVISIONS

Update this page to show all temporary revisions inserted into this manual.
Revision 54 includes all prior temporary revisions, up to and including TR-024.
Temporary Section/ Issue Date Inserted Date Removed

Revision No. Page Date Inserted By Removed By
61-01-02
Page 2
RECORD OF TEMPORARY REVISIONS Rev. 54 Nov/23
VOLUME 7
SERVICE DOCUMENT LIST
CAUTION 1: DO NOT USE OBSOLETE OR OUTDATED INFORMATION. PERFORM

ALL INSPECTIONS OR WORK IN ACCORDANCE WITH THE MOST
RECENT REVISION OF THE SERVICE DOCUMENT. INFORMATION
CONTAINED IN A SERVICE DOCUMENT MAY BE SIGNIFICANTLY
CHANGED FROM EARLIER REVISIONS. FAILURE TO COMPLY WITH
INFORMATION CONTAINED IN A SERVICE DOCUMENT OR THE USE
OF OBSOLETE INFORMATION MAY CREATE AN UNSAFE CONDITION
THAT MAY RESULT IN DEATH, SERIOUS BODILY INJURY, AND/OR
SUBSTANTIAL PROPERTY DAMAGE.
CAUTION 2: THE INFORMATION FOR THE DOCUMENTS LISTED INDICATES

THE REVISION LEVEL AND DATE AT THE TIME THAT THE
DOCUMENT WAS INITIALLY INCORPORATED INTO THIS MANUAL.
INFORMATION CONTAINED IN A SERVICE DOCUMENT MAY BE
SIGNIFICANTLY CHANGED FROM EARLIER REVISIONS. REFER
TO THE APPLICABLE SERVICE DOCUMENT INDEX FOR THE MOST
RECENT REVISION LEVEL OF THE SERVICE DOCUMENT.
Service Document Incorporation Service Document Incorporation

Number Rev./Date Number Rev./Date
Service Bulletins: Service Letters:
SB 159A Orig., Mar/93 HC-SL-61-170 Rev. 11, Sep/99
SL 212 Rev. 41, Apr/16
Service Instructions: Service Advisories:

SI 209 Rev. 11, Sep/99 SA 19 Orig., Mar/93
SERVICE DOCUMENTS LIST 61-01-02 Page 1

Rev. 54 Nov/23
VOLUME 7
SERVICE DOCUMENT LIST
Service Document Incorporation Service Document Incorporation

Number Rev./Date Number Rev./Date
SERVICE DOCUMENTS LIST 61-01-02 Page 2

Rev. 54 Nov/23
VOLUME 7
LIST OF EFFECTIVE PAGES
Chapter Page Rev. Level Date
Cover/Inside Cover Cover/Inside Cover Rev. 55 Apr/24

Revision Highlights 1 thru 4 Rev. 55 Apr/24
Record of Revisions 1 and 2 Rev. 54 Nov/23
Record of Temporary Revisions 1 and 2 Rev. 54 Nov/23
Service Document List 1 and 2 Rev. 54 Nov/23
List of Effective Pages 1 and 2 Rev. 55 Apr/24
Table of Contents 1 and 2 Rev. 54 Nov/23
Introduction 1 thru 10 Rev. 55 Apr/24
Introduction
11 thru 18 Rev. 54 Nov/23
Consumable Materials 1-1 thru 1-4 Rev. 55 Apr/24
Consumable Materials 1-5 Rev. 54 Nov/23
Consumable Materials 1-6 thru 1-11 Rev. 55 Apr/24
Consumable Materials 1-12 and 1-13 Rev. 54 Nov/23
Consumable Materials 1-14 Rev. 55 Apr/24
Consumable Materials 1-15 Rev. 54 Nov/23
Consumable Materials 1-17 thru 1-19 Rev. 54 Nov/23
Consumable Materials 1-57 and 1-58 Rev. 54 Nov/23
Consumable Materials 1-59 and 1-60 Rev. 55 Apr/24
Vendor Cross Reference 2-1 and 2-2 Rev. 55 Apr/24
Packaging and Storage 3-1 Rev. 55 Apr/24
Packaging and Storage 3-2 Rev. 54 Nov/23
Packaging and Storage 3-5 thru 3-17 Rev. 55 Apr/24
LIST OF EFFECTIVE PAGES 61-01-02 Page 1

Rev. 55 Apr/24
VOLUME 7
LIST OF EFFECTIVE PAGES
Chapter Page Rev. Level Date

Packaging and Storage 3-20 thru 3-28 Rev. 54 Nov/23
Packaging and Storage 3-30 thru 3-32 Rev. 54 Nov/23
LIST OF EFFECTIVE PAGES 61-01-02 Page 2

Rev. 55 Apr/24
VOLUME 7
TABLE OF CONTENTS
Revision Highlights................................................................................................................. 1
Record of Revisions .............................................................................................................. 1
Record of Temporary Revisions............................................................................................. 1
Service Documents List.......................................................................................................... 1
List of Effective Pages............................................................................................................ 1
Table of Contents................................................................................................................... 1
Introduction............................................................................................................................. 1
Consumable Materials ........................................................................................................ 1-1
Vendor Cross Reference.......................................................................................... Relocated
Vendor cross reference information has been relocated to Hartzell Propeller Inc.
Standard Practices Manual 202A, Volume 6 (61-01-02).
Packaging and Storage....................................................................................................... 3-1
TABLE OF CONTENTS 61-01-02 Page 1

Rev. 54 Nov/23
VOLUME 7
TABLE OF CONTENTS 61-01-02 Page 2

Rev. 54 Nov/23
VOLUME 7
INTRODUCTION - CONTENTS
1. General...................................................................................................................3
A. Statement of Purpose.......................................................................................3
2. Reference Publications...........................................................................................4
A. Hartzell Propeller Publications..........................................................................4
B. Vendor Publications..........................................................................................5
3. Personnel Requirements........................................................................................6
A. Service and Maintenance Procedures..............................................................6
4. Special Tooling and Consumable Materials............................................................6
A. Special Tooling..................................................................................................6
B. Consumable Materials......................................................................................6
5. Safe Handling of Paints and Chemicals.................................................................7
A. Instructions for Use...........................................................................................7
6. Component Life......................................................................................................7
A. Component Life.................................................................................................7
7. Propeller Critical Parts............................................................................................8
A. Propeller Critical Parts......................................................................................8
8. Hartzell Propeller Contact Information....................................................................9
A. Product Support Department............................................................................9
B. Technical Publications Department...................................................................9
C. Recommended Facilities...................................................................................9
9. Definitions.............................................................................................................10
10. Abbreviations........................................................................................................17
INTRODUCTION 61-01-02 Page 1

Rev. 55 Apr/24
VOLUME 7

Rev. 55 Apr/24
VOLUME 7
1. General
A. Statement of Purpose
(1) This manual has been reviewed and accepted by the FAA. Additionally, this
manual contains data that has been approved in a manner acceptable to the
FAA Administrator.
(2) This manual is to be used in propeller repair stations by personnel that are
trained and experienced with Hartzell Propeller LLC products.
(a) This manual does not provide complete information for an inexperienced
technician to attempt propeller overhaul without supervision.
(3) The information in this manual revision supersedes data in all previously
published revisions of this manual.
(4) Where possible, this manual is written in the format specified by
ATA iSpec 2200.

Rev. 55 Apr/24
VOLUME 7
2. Reference Publications
A. Hartzell Propeller Publications

(1) Information published in Service Bulletins, Service Letters, Service Advisories,
and Service Instructions may supersede information published in this manual.
The reader must consult active Service Bulletins, Service Letters, Service
Advisories, and Service Instructions for information that may have not yet been
incorporated into the latest revision of this manual.
(2) The Hartzell Propeller Standard Practices Manual 202A has several volumes. A
complete set consists of the following:
Volume Number Chapter Number Chapter Name
Volume 1 1 Cleaning
2 Paint and Finish
Volume 2 1 Eddy Current Inspection
2 Magnetic Particle Inspection
3 Penetrant Inspection
Volume 3 1 Aluminum Hub Overhaul
Volume 4 1 Steel Hub Overhaul
Volume 5 1 Blade Clamp Overhaul
Volume 6 1 Special Inspections
2 Parts Identification and Marking
3 Part Retirement Procedures
4 Vendor Cross Reference
Volume 7
1 Consumable Materials
3 Packaging and Storage
(Available on the Hartzell Propeller
website at www.hartzellprop.com)
Volume 8
1 Standard Repairs and Instructions
2 Special Adhesive and Bonding
Procedures
Volume 9 1 Shot Peening
2 Approved Facilities
Volume 10 1 Hard Chrome Re-plating
2 Cadmium Replating
3 Chromic Acid Anodizing
Volume 11
1 Propeller Lubrication
2 Static and Dynamic Balance
(Available on the Hartzell Propeller
website at www.hartzellprop.com)

Rev. 55 Apr/24
VOLUME 7
(3) In addition to this manual, one or more of the following publications are required
for information regarding specific recommendations and procedures to maintain
propeller assemblies that are included in this manual.
Manual No. Available at

Hartzell Propeller Manual Title
(ATA No.) www.hartzellprop.com
n/a Yes Active Hartzell Propeller Service Bulletins,
Service Letters, Service Instructions, and
Service Advisories
Manual 130B - Mechanically Actuated Governors and
(61-23-30) Accessories Maintenance Manual
Manual 159 Yes Application Guide
(61-02-59)
Manual 165A Yes Illustrated Tool and Equipment Manual
(61-00-65)
Manual 180 Yes Ice Protection System Manual
(30-61-80)
B. Vendor Publications
None.

Rev. 55 Apr/24
VOLUME 7
3. Personnel Requirements (Rev. 2)
A. Service and Maintenance Procedures in this Manual

(1) Personnel performing the service and maintenance procedures in this manual
are expected to have the required equipment/tooling, training, and certifications
(when required by the applicable Aviation Authority) to accomplish the work in
a safe and airworthy manner.
(2) Compliance to the applicable regulatory requirements established by the
Federal Aviation Administration (FAA) or international equivalent is mandatory
for anyone performing or accepting responsibility for the inspection and/or
repair of any Hartzell Propeller LLC product.
(a) Maintenance records must be kept in accordance with the requirements
established by the Federal Aviation Administration (FAA) or international
equivalent.
(b) Refer to Federal Aviation Regulation (FAR) Part 43 for additional
information about general aviation maintenance requirements.
4. Special Tooling and Consumable Materials (Rev. 2)
A. Special Tooling
(1) Special tooling may be required for procedures in this manual. For further
tooling information, refer to Hartzell Propeller Illustrated Tool and Equipment
Manual 165A (61-00-65).
(a) Tooling reference numbers appear with the prefix “TE” directly following
the tool name to which they apply. For example, a template that is
reference number 133 will appear as: template TE133.
B. Consumable Materials
(1) Consumable materials are referenced in certain sections throughout this
manual. Specific approved materials are listed in the Consumable Materials
chapter of Hartzell Propeller Standard Practices Manual 202A (61‑01‑02).
(a) Consumable material reference numbers appear with the prefix “CM”
directly following the material to which they apply. For example, an
adhesive that is reference number 16 will appear as: adhesive CM16.
Only the material(s) specified can be used.

Rev. 55 Apr/24
VOLUME 7
5. Safe Handling of Paints and Chemicals (Rev.1)
A. Instructions for Use

(1) Always use caution when handling or being exposed to paints and/or chemicals
during propeller overhaul and maintenance procedures.
(2) Before using paint or chemicals, always read the manufacturer’s label on
the container(s) and follow specified instructions and procedures for storage,
preparation, mixing, and/or application.
(3) Refer to the product’s Material Safety Data Sheet (MSDS) for detailed
information about the physical properties, health, and physical hazards of any
paint or chemical.
6. Component Life
WARNING: CERTAIN PROPELLER COMPONENTS USED IN NON-AVIATION

APPLICATIONS ARE MARKED WITH DIFFERENT PART NUMBERS
TO DISTINGUISH THEM FROM COMPONENTS USED IN AVIATION
APPLICATIONS. DO NOT ALTER THE PART NUMBERS SHOWN
ON PARTS DESIGNATED FOR NON-AVIATION APPLICATIONS
OR OTHERWISE APPLY THOSE PARTS FOR USE ON AVIATION
APPLICATIONS.
A. Component Life
(1) Component life is expressed in terms of hours of service (Time Since New, TSN)
and in terms of hours of service since overhaul (Time Since Overhaul, TSO).
NOTE: TSN/TSO is considered as the time accumulated between rotation
and landing, i.e., flight time.
(2) Time Since New (TSN) and Time Since Overhaul (TSO) records for the
propeller hub and blades must be maintained in the propeller logbook.
(3) Both TSN and TSO are necessary for defining the life of the component.
Certain components, or in some cases an entire propeller, may be "life limited",
which means that they must be replaced after a specified period of use (TSN).
(a) It is a regulatory requirement that a record of the Time Since New (TSN)
be maintained for all life limited parts.
(b) Refer to the Airworthiness Limitations chapter in the applicable Hartzell
Propeller Owner's Manual for a list of life limited components.
(4) When a component or assembly undergoes an overhaul, the TSO is returned to
zero hours.
(a) Time Since New (TSN) can never be returned to zero.
(b) Repair without overhaul does not affect TSO or TSN.

Rev. 55 Apr/24
VOLUME 7
(5) Blades and hubs are sometimes replaced while in service or at overhaul.
(a) Maintaining separate TSN and TSO histories for a replacement hub or
blade is required.
(b) Hub replacement
1 If the hub is replaced, the replacement hub serial number must be
recorded (the entry signed and dated) in the propeller logbook.
2 The propeller will be identified with the serial number of the
replacement hub.
NOTE: Propeller assembly serial numbers are impression stamped
on the hub. For stamping information, refer to the Parts
Identification and Marking chapter of Hartzell Propeller
Standard Practices Manual 202A (61-01-02).
3 The TSN and TSO of the replacement hub must be recorded and
maintained in the propeller logbook.
4 If tracking any component(s) other than the hub/blades, maintain
these TSN/TSO records separately in the propeller logbook.
NOTE: Hub replacement does not affect the TSN/TSO of any other
propeller components.
7. Propeller Critical Parts (Rev. 2)
A. Propeller Critical Parts

(1) Procedures in this manual may involve Propeller Critical Parts (PCP).
(a) These procedures have been substantiated based on Engineering
analysis that expects this product will be operated and maintained using
the procedures and inspections provided in the Instructions for Continued
Airworthiness (ICA) for this product.
(b) Refer to the Illustrated Parts List chapter in the applicable Hartzell
Propeller maintenance manual to identify the Propeller Critical Parts.
(2) Numerous propeller system parts can produce a propeller Major or Hazardous
effect, even though those parts may not be considered as Propeller Critical
Parts.
(a) The operating and maintenance procedures and inspections provided in
the ICA for this product are, therefore, expected to be accomplished for all
propeller system parts.

Rev. 55 Apr/24
VOLUME 7
8. Hartzell Propeller Contact Information (Rev. 3)
A. Product Support Department

(1) Contact the Hartzell Propeller Product Support Department about any
maintenance problems or to request information not included in this publication.
NOTE: When calling from outside the United States, dial (001) before dialing
the telephone numbers below.
(a) The Product Support Department may be reached during business hours
(8:00 a.m. through 5:00 p.m., United States Eastern Time) at
(937) 778-4379 or at (800) 942-7767, toll free from the United States
and Canada.
(b) The Product Support Department can also be reached by fax at
(937) 778-4215, and by e-mail at techsupport@hartzellprop.com.
(c) After business hours, you may leave a message on our 24 hour product
support line at (937) 778-4376 or at (800) 942-7767, toll free from the
United States and Canada.
1 A technical representative will contact you during normal business
hours.
2 Urgent AOG support is also available 24 hours per day, seven days
per week via this message service.
(d) Additional information is available on the Hartzell Propeller website at
www.hartzellprop.com.
B. Technical Publications Department
(1) For Hartzell Propeller service literature and revisions, contact:

Hartzell Propeller LLC Telephone: 937.778.4200
Attn: Technical Publications Department Fax: 937.778.4215
One Propeller Place E-mail: manuals@hartzellprop.com
C. Recommended Facilities
(1) Hartzell Propeller LLC recommends using Hartzell-approved distributors and
repair facilities for the purchase, repair, and overhaul of Hartzell propeller
assemblies or components.
(2) Information about the Hartzell Propeller LLC worldwide network of aftermarket
distributors and approved repair facilities is available on the Hartzell website at
www.hartzellprop.com.

Rev. 55 Apr/24
VOLUME 7
9. Definitions (Rev. 5)
A basic understanding of the following terms will assist in maintaining and operating
Hartzell propeller systems.
Term Definition
Annealed Softening of material due to overexposure to heat
Aviation Certified Intended for FAA or international equivalent type
certificated aircraft applications. A TC and PC number
must be stamped on the hub, and a PC number must be
stamped on blades.
Aviation Experimental Intended for aircraft/propeller applications not certified
by the FAA or international equivalent. Products marked
with an “X” at or near the end of the model number or
part number are not certified by the FAA or international
equivalent and are not intended to use on certificated
aircraft.
Beta Operation A mode of pitch control that is directed by the pilot rather
than by the propeller governor
Beta Range Blade angles between low pitch and maximum reverse
blade angle
Beta System Parts and/or equipment related to operation (manual
control) of propeller blade angle between low pitch blade
angle and full reverse blade angle
Blade Angle Measurement of blade airfoil location described as the
angle between the blade airfoil and the surface described
by propeller rotation
Blade Centerline An imaginary reference line through the length of a blade
around which the blade rotates
Blade Station Refers to a location on an individual blade for blade
inspection purposes. It is a measurement from the blade
“zero” station to a location on a blade, used to apply blade
specification data in blade overhaul manuals.
Note: Do not confuse blade station with reference blade
radius; they may not originate at the same location.
Blemish An imperfection with visible attributes, but having no
impact on safety or utility
Brinelling A depression caused by failure of the material in
compression

Rev. 55 Apr/24
VOLUME 7
Term Definition
Bulge An outward curve or bend
Camber The surface of the blade that is directed toward the front
of the aircraft. It is the low pressure, or suction, side of the
blade. The camber side is convex in shape over the entire
length of the blade.
Chord A straight line distance between the leading and trailing
edges of an airfoil
Chordwise A direction that is generally from the leading edge to the
trailing edge of an airfoil
Co-bonded The act of bonding a composite laminate and
simultaneously curing it to some other prepared surface
Composite Material Kevlar®, carbon, or fiberglass fibers bound together with,
or encapsulated within an epoxy resin
Compression Rolling A process that provides improved strength and resistance
to fatigue
Constant Force A force that is always present in some degree when the
propeller is operating
Constant Speed A propeller system that employs a governing device to
maintain a selected engine RPM
Corrosion (Aluminum) The chemical or electrochemical attack by an acid or
alkaline that reacts with the protective oxide layer and
results in damage of the base aluminum. Part failure can
occur from corrosion due to loss of structural aluminum
converted to corrosion product, pitting, a rough etched
surface finish, and other strength reduction damage
caused by corrosion.
Corrosion (Steel) Typically, an electrochemical process that requires the
simultaneous presence of iron (component of steel),
moisture and oxygen. The iron is the reducing agent (gives
up electrons) while the oxygen is the oxidizing agent (gains
electrons). Iron or an iron alloy such as steel is oxidized
in the presence of moisture and oxygen to produce rust.
Corrosion is accelerated in the presence of salty water or
acid rain. Part failure can occur from corrosion due to loss
of structural steel converted to corrosion product, pitting,
a rough etched surface finish and other strength reduction
damage caused by corrosion.

Rev. 54 Nov/23
VOLUME 7
Term Definition
Corrosion Product A white or dull gray powdery material that has an
(Aluminum) increased volume appearance (compared to non-corroded
aluminum). Corrosion product is not to be confused with
damage left in the base aluminum such as pits, worm
holes, and etched surface finish.
Corrosion Product When iron or an iron alloy such as steel corrodes, a
(Steel) corrosion product known as rust is formed. Rust is an
iron oxide which is reddish in appearance and occupies
approximately six times the volume of the original material.
Rust is flakey and crumbly and has no structural integrity.
Rust is permeable to air and water, therefore the interior
metallic iron (steel) beneath a rust layer continues to
corrode. Corrosion product is not to be confused with
damage left in the base steel such as pits and etched
surface finish.
Crack Irregularly shaped separation within a material, sometimes
visible as a narrow opening at the surface
Debond Separation of two materials that were originally bonded
together in a separate operation
Defect An imperfection that affects safety or utility
Delamination Internal separation of the layers of composite material
Dent The permanent deflection of the cross section that is
visible on both sides with no visible change in cross
sectional thickness
Depression Surface area where the material has been compressed but
not removed
Distortion Alteration of the original shape or size of a component
Edge Alignment Distance from the blade centerline to the leading edge of
the blade
Erosion Gradual wearing away or deterioration due to action of the
elements
Exposure Leaving material open to action of the elements

Rev. 54 Nov/23
VOLUME 7
Term Definition
Face The surface of the blade that is directed toward the rear
of the aircraft. The face side is the high pressure, or
thrusting, side of the blade. The blade airfoil sections are
normally cambered or curved such that the face side of the
blade may be flat or even concave in the midblade and tip
region.
Face Alignment Distance from the blade centerline to the highest point on
the face side perpendicular to the chord line
Feathering The capability of blades to be rotated parallel to the
relative wind, thus reducing aerodynamic drag
Fraying A raveling or shredding of material
Fretting Damage that develops when relative motion of small
displacement takes place between contacting parts,
wearing away the surface
Galling To fret or wear away by friction
Gouge Surface area where material has been removed
Hazardous Propeller The hazardous propeller effects are defined in Title 14 CFR
Effect section 35.15(g)(1)
Horizontal Balance Balance between the blade tip and the center of the hub
Impact Damage Damage that occurs when the propeller blade or hub
assembly strikes, or is struck by, an object while in flight or
on the ground
Inboard Toward the butt of the blade
Intergranular Corrosion Corrosion that attacks along the grain boundaries of metal
alloys
Jog A term used to describe movement up/down, left/right, or
on/off in short incremental motions
Laminate To unite composite material by using a bonding material,
usually with pressure and heat
Lengthwise A direction that is generally parallel to the pitch axis
Loose Material Material that is no longer fixed or fully attached
Low Pitch The lowest blade angle attainable by the governor for
constant speed operation

Rev. 54 Nov/23
VOLUME 7
Term Definition
Major Propeller Effect The major propeller effects are defined in Title 14 CFR
section 35.15(g)(2)
Minor Deformation Deformed material not associated with a crack or missing
material
Monocoque A type of construction in which the outer skin carries all or
a major part of the load
Nick Removal of paint and possibly a small amount of material
Non-Aviation Certified Intended for non-aircraft application, such as Hovercraft or
Wing in Ground Effect (WIG) applications. These products
are certificated by an authority other than FAA. The hub
and blades will be stamped with an identification that is
different from, but comparable to TC and PC.
Non-Aviation Experimental Intended for non-aircraft application, such as Hovercraft
or Wing-In-Ground effect (WIG) applications. Products
marked with an “X” at or near the end of the model number
or part number are not certified by any authority and are
not intended for use on certificated craft.
Onspeed Condition in which the RPM selected by the pilot through
the propeller control/condition lever and the actual engine
(propeller) RPM are equal
Open Circuit Connection of high or infinite resistance between points in
a circuit which are normally lower
Outboard Toward the tip of the blade
Overhaul The periodic disassembly, inspection, repair, refinish,
and reassembly of a propeller assembly to maintain
airworthiness
Overspeed Condition in which the RPM of the propeller or engine
exceeds predetermined maximum limits; the condition in
which the engine (propeller) RPM is higher than the RPM
selected by the pilot through the propeller control/condition
lever
Pitch Same as “Blade Angle”
Pitting Formation of a number of small, irregularly shaped cavities
in surface material caused by corrosion or wear

Rev. 54 Nov/23
VOLUME 7
Term Definition
Pitting (Linear) The configuration of the majority of pits forming a pattern
in the shape of a line
Porosity An aggregation of microvoids. See “voids”.
Propeller Critical Parts A part on the propeller whose primary failure can result in
a hazardous propeller effect, as determined by the safety
analysis required by Title 14 CFR section 35.15
Reference Blade Radius Refers to the propeller reference blade radius in an
assembled propeller, e.g., 30-inch radius. A measurement
from the propeller hub centerline to a point on a blade,
used for blade angle measurement in an assembled
propeller. An adhesive stripe (blade angle reference tape
CM160) is usually located at the reference blade radius
location.
Note: Do not confuse reference blade radius with blade
station; they may not originate at the same point.
Reversing The capability of rotating blades to a position to generate
reverse thrust to slow the aircraft or back up
Scratch Same as “Nick”
Short Circuit Connection of low resistance between points on a circuit
between which the resistance is normally much greater
Shot Peening Process where steel shot is impinged on a surface to
create compressive surface stress, that provides improved
strength and resistance to fatigue
Single Acting Hydraulically actuated propeller that utilizes a single oil

supply for pitch control
Split Delamination of blade extending to the blade surface,
normally found near the trailing edge or tip
Station Line See "Blade Station"
Synchronizing Adjusting the RPM of all the propellers of a multi-engine
aircraft to the same RPM
Synchrophasing A form of propeller sychronization in which not only the
RPM of the engines (propellers) are held constant, but
also the position of the propellers in relation to each other
Ticking A series of parallel marks or scratches running
circumferentially around the diameter of the blade

Rev. 54 Nov/23
VOLUME 7
Term Definition
Track In an assembled propeller, a measurement of the location
of the blade tip with respect to the plane of rotation, used
to verify face alignment and to compare blade tip location
with respect to the locations of the other blades in the
assembly
Trailing Edge The aft edge of an airfoil over which the air passes last
Trimline Factory terminology referring to where the part was
trimmed to length
Underspeed The condition in which the actual engine (propeller) RPM
is lower than the RPM selected by the pilot through the
propeller control/condition lever
Unidirectional Material A composite material in which the fiber are substantially
oriented in the same direction.
Variable Force A force that may be applied or removed during propeller
operation
Vertical Balance Balance between the leading and trailing edges of a two-
blade propeller with the blades positioned vertically
Voids Air or gas that has been trapped and cured into a laminate
Windmilling The rotation of an aircraft propeller caused by air flowing
through it while the engine is not producing power
Woven Fabric A material constructed by interlacing fiber to form a fabric
pattern
Wrinkle (aluminum blade) A wavy appearance caused by high and low material
displacement
Wrinkle (composite blade) Overlap or fold within the material

Rev. 54 Nov/23
VOLUME 7
10. Abbreviations (Rev. 2)
Abbreviation Term
AD Airworthiness Directives
AMM Aircraft Maintenance Manual
AOG Aircraft on Ground
AR As Required
ATA Air Transport Association
CSU Constant Speed Unit
FAA Federal Aviation Administration
FH Flight Hour
FM Flight Manual
FMS Flight Manual Supplement
Ft-Lb Foot-Pound
HMI Human Machine Interface
ICA Instructions for Continued Airworthiness
ID Inside Diameter
In-Lb Inch-Pound
IPL Illustrated Parts List
IPS Inches Per Second
kPa Kilopascals
Lb(s) Pound(s)
Max. Maximum
Min. Minimum
MIL-X-XXX Military Specification
MPI Major Periodic Inspection (Overhaul)
MS Military Standard
MSDS Material Safety Data Sheet
N Newtons

Rev. 54 Nov/23
VOLUME 7
Abbreviation Term
N/A Not Applicable
NAS National Aerospace Standards
NASM National Aerospace Standards, Military
NDT Nondestructive Testing
NIST National Institute of Standards and Technology
N•m Newton-Meters
OD Outside Diameter
OPT Optional
PC Production Certificate
PCP Propeller Critical Part
PLC Programmable Logic Controller
PMB Plastic Media Blasting (Cleaning)
POH Pilot’s Operating Handbook
PSI Pounds per Square Inch
RF Reference
RPM Revolutions per Minute
SAE Society of Automotive Engineers
STC Supplemental Type Certificate
TBO Time Between Overhaul
TC Type Certificate
TSI Time Since Inspection
TSN Time Since New
TSO Time Since Overhaul
UID Unique Identification
WIG Wing-In-Ground-Effect

Rev. 54 Nov/23
VOLUME 7
CONSUMABLE MATERIALS - CONTENTS
1. Introduction..........................................................................................................1-3
A. General..........................................................................................................1-3
B. Material Control Requirements......................................................................1-3
C. Date Code Formats........................................................................................1-5
D. Consumable Material Management Procedures............................................1-5
E. Revisions........................................................................................................1-5
F. Hartzell Propeller Overhaul Kits.....................................................................1-6
G. Approved Lubricants....................................................................................1-10
LIST OF FIGURES
Lubrication Labels...............................................................Figure 1-1....................1-10
LIST OF TABLES
Consumable Materials........................................................Table 1-1......................1-12
CONSUMABLE MATERIALS 61-01-02 Page 1-1

Rev. 55 Apr/24
VOLUME 7

Rev. 55 Apr/24
VOLUME 7
1. Introduction
CAUTION: INSTRUCTIONS AND PROCEDURES IN THIS CHAPTER

MAY INVOLVE PROPELLER CRITICAL PARTS. REFER TO
THE INTRODUCTION CHAPTER OF THIS MANUAL FOR
INFORMATION ABOUT PROPELLER CRITICAL PARTS. REFER
TO THE ILLUSTRATED PARTS LIST CHAPTER OF THE
APPLICABLE OVERHAUL MANUAL(S) FOR THE IDENTIFICATION
OF PROPELLER CRITICAL PARTS.
A. General
(1) This section contains information on materials most commonly used for
cleaning, repair, painting, etc.
(2) If there is a need to use a material not listed in this section, contact Hartzell
Propeller LLC for approval and applicable control requirements.
(3) To order Sherwin-Williams paints that are specified in this manual, contact
Hartzell Propeller LLC Aftermarket Sales or refer to the Sherwin-Williams
Product Finishes Global Finishes Group website at
http://oem.sherwin-williams.com to find the location of the nearest distributor.
(a) The last four digits of a Sherwin-Williams part number, i.e., the 4311 in the
following number F63TXB9629-4311, indicates the local Sherwin-Williams
office and is not a part of the part number.
B. Material Control Requirements
(1) Table 1-1 lists the supply basis, cure time, pot life, storage temperature, and
shelf life for consumables including adhesives, sealants, lubricants, paints,
primers, and other miscellaneous materials.
(2) The listed specifications describe limitations for shelf life and temperature
control.
(a) The following terms are used to define shelf life:
1 DOM: Date of Manufacture
2 DOS: Date of Shipment from supplier
3 mos: Months
4 MD: Use Manufaturer’s Expiration Date - Hartzell Accepts
Manufacturer’s Expiration Date As-Is

Rev. 55 Apr/24
VOLUME 7
(b) The following terms are used to define temperature control:

1 F: Frozen, Store below 0°F (-17° C)
2 F1 = Frozen, -40°F (-40°C) maximum
3 R: Refrigerate, 40° - 60°F (4° - 15°C)
4 RT: Controlled room temperature, 60° - 80°F (15° - 26°C)
5 UC: No special Hartzell Propeller LLC requirement, follow
manufacturer’s requirements
6 SV: Store Vertically. Modifer code used as a suffix indicating liquids
must be stored vertically in their container in order for the shelf life
to be valid. Example, RTSV - controlled room temperature 60°-80°F,
store vertically.
(3) Supply basis codes have been assigned to each consumable material to
indicate if the item can be purchased from Hartzell Propeller LLC. The following
supply basis codes have been assigned:
(a) Y = customer can get the consumable material either from Hartzell or from
a local source
(b) N = Hartzell does not sell the consumable material, the customer must
purchase it locally
(c) HPI = Hartzell is the only supplier of the consumable material, the
customer must purchase the consumable material from Hartzell
(d) S = Customer can get the consumable material from any supplier as long
as the material meets the requirements of the specification
(4) For materials purchased directly from Hartzell Propeller LLC, the expiration
date control information required by Hartzell Propeller LLC in Table 1-1
will be added to the package or container in a location different than the
manufacturer’s label. The Hartzell Propeller control information takes
precedence over any conflicting information from the consumable manufacturer.
(5) Materials purchased directly from Hartzell Propeller LLC will not have storage
temperature control information added to the package or container. The
temperature control information contained in Table 1-1 in this chapter takes
precedence over any conflicting information from the manufacturer.
(6) For materials purchased from other sources, the purchaser is required to
record the expiration date control information required by Hartzell Propeller LLC
on the package or container in accordance with Table 1-1 in this chapter.
Storage temperature control information in Table 1-1 must be observed.

Rev. 55 Apr/24
VOLUME 7
C. Date Code Formats

(1) The expiration date may be recorded using the letters “Exp” followed by a
month and year. In this case, the shelf life of that material extends through the
last day of the month and year recorded.
(2) The cure date for elastomeric products such as O-rings, gaskets, and hoses
is normally recorded on the packaging using the numbers 1 through 4, the
letter “Q,” and the last two numbers of the year. This marking indicates that the
material was cured during a particular “quarter”, i.e., three month period, of the
stated year.
(3) The cure date marking will suffice for control purposes. The actual date of
expiration will occur after the last day of the quarter in the year projected from
the cure date plus the allowable number of years for storage.
D. Consumable Material Management Procedures
(1) Rotate stock on a “first in-first out” basis.
(2) Epoxy and other materials normally require, at minimum, a room temperature
cure. Lower temperatures may greatly increase the cure time. Temperatures
below 60° F (15° C) may cause the epoxy to not cure at all.
(3) The maximum storage time for standard O-rings, gaskets, and diaphragms is
10 years from the date of cure.
(a) The maximum storage time for O-rings, part numbers 459413032,
459413112, 103043, and 103045 produced using Viton compound, is
20 years from the date of cure.
NOTE: Viton is a proprietary name for fluoroelastomer compound that
complies with certain AMS standards.
(b) Color identification is optional for individually packaged O-rings.
(4) The maximum storage time for hoses is 8 years from the date of cure.
(5) Before the use of consumable materials, technicians are responsible to
examine consumable material labels for specified shelf life and storage
requirements and discard any consumable materials found with expired shelf
life.
E. Revisions
(1) Alternate
(a) Alternate consumable materials are identified by the term "ALTERNATE is
CM ______". Alternate consumable materials are considered acceptable
for continued use and existing stock of consumable materials may be used
for maintenance and/or repair. The consumable materials may be used
interchangeably when ordering/stocking new consumable materials.

Rev. 54 Nov/23
VOLUME 7
(2) Supersedure
(a) Consumable material changes are identified by the terms “SUPERSEDES
CM _____” or “SUPERSEDED BY CM _____”. Superseded consumable
materials are considered acceptable for continued use and existing stock
of superseded consumable materials may be used for maintenance
and/or repair. Superseded consumable materials may no longer be
available, and the new consumable material number must be used when
ordering/stocking new consumable materials.
(3) Replacement
(a) Consumable material changes identified by the terms "REPLACES
CM _____” or “REPLACED BY CM _____” are considered acceptable for
continued use, but must be replaced with the new consumable material
at overhaul. Existing stock of consumable materials may not be used for
maintenance and/or repair of effected assemblies. Replaced consumable
materials may no longer be available, and the new consumable material
number must be used when ordering/stocking consumable materials.
F. Hartzell Propeller Overhaul Kits
NOTE: Specific Hartzell Propeller manuals and service documents are available
on the Hartzell Propeller website at www.hartzellprop.com. Refer to the
Required Publications section in the Introduction chapter of this manual for
the identification of these publications.
(1) Hartzell Propeller LLC has compiled propeller overhaul kits for the convenience
of its customers.
(2) Propeller overhaul intervals are published in Hartzell Propeller Service Letter
HC-SL-61-61Y. Use of propeller overhaul kits at the time of overhaul is
recommended, but is not required.
(3) A propeller overhaul kit part number is based on the propeller model number,
followed by the letters “OH”. For example, the part number for an overhaul kit
for a model HC-E4N-3G propeller is HC-E4N-3G-OH.
(a) Propeller overhaul kits for propeller models with more than 12 characters
will not contain the “OH” suffix.
(4) A Hartzell Propeller overhaul kit contains the following:
(a) All consumable parts (O-rings, seals, gaskets, etc.) except as noted in
Paragraph 1.F.(5)
(b) Duplicate parts that are propeller configuration specific, i.e. screws and
washers for mounting beta pick-ups, plastic spring retainers, etc.
(c) The standard size only part for any part that is dimensionally specific
or has an oversized alternate; i.e., dowel pins, bushings, blade needle
bearings, etc.

Rev. 55 Apr/24
VOLUME 7
(5) A Hartzell Propeller overhaul kit does not contain:

(a) Paint kit(s) and other consumable items, such as grease, sealants, and
thread locking compounds used in propeller assembly
1 Hazardous material shipping restrictions prohibit shipping of these
items
(b) De-ice boots, anti-icing boots, and any other de-ice hardware
1 Propeller de-ice hardware may be controlled by the airframe
manufacturer, airframe STC holder, or in some cases by Hartzell
Propeller LLC.
2 In all cases, the type certificate holder of the de-ice system is the
final authority to determine which de-ice items are to be replaced at
overhaul.
(c) Any part for which an overhaul procedure is provided for in the overhaul
manual
(d) Steel hub reciprocating propeller hydraulic and valve parts
(e) Unknown Quantity or Floor Stock Items
1 Balance weights and associated hardware
2 Compact propeller high pitch adjustment washers
3 Feathering spring spacers
(f) Application Specific Items
1 Spinner mounting hardware
a Refer to Hartzell Propeller Application Guide Manual 159
(61-02-59), Hartzell Propeller Metal Spinner Maintenance
Manual 127 (61-16-27), or Hartzell Propeller Composite Spinner
Maintenance Manual 148 (61-16-48) for application of specific
spinner mounting hardware.
2 Nuts and washers used to clamp the hub halves together and are
used for hub mounted bulkhead attachment
3 Mounting studs for F-flange or N-flange compact propellers
4 Compact propeller hub bolt-on extension hardware
5 Start lock mounting hardware
(61-02-59), Hartzell Propeller Metal Spinner Maintenance
Manual 127 (61-16-27), or Hartzell Propeller Composite Spinner
Maintenance Manual 148 (61-16-48) for application specific start
lock mounting hardware.

Rev. 55 Apr/24
VOLUME 7
6 Counterweight slug mounting hardware

(61-02-59) for application specific counterweight slug mounting
hardware.
(6) Propeller Overhaul Kit Expiration Date
(a) The cure date of a propeller overhaul kit is marked on the outside of the
package when the overhaul kit is assembled at Hartzell Propeller LLC.
1 The cure date of the propeller overhaul kit package is the oldest cure
date of all applicable parts contained in the propeller overhaul kit.
(b) The expiration date of a propeller overhaul kit is calculated using the cure
date that is identified on the outside of the package.
1 The actual date of expiration of the propeller overhaul kit will occur
after the last day of the quarter in the year projected from the cure
date, plus 10 years for storage, in accordance with this chapter.
(c) Using the cure date marked on the outside of the propeller overhaul kit
package, calculate the expiration date of the kit.
(d) Record the expiration date of the propeller overhaul kit on the outside of
the package.
(7) Options when a propeller overhaul kit has expired before use:
(a) Option 1:
1 Open the propeller overhaul kit package.
2 Identify and remove the part(s) that has expired.
a Using the cure date of each part in the propeller overhaul kit,
calculate its expiration date.
b The actual date of expiration of a part will occur after the last
day of the quarter in the year projected from its cure date, plus
10 years for storage, in accordance with this chapter.
3 Replace any expired part(s) with an unexpired part(s).
4 Revise the expiration date on the propeller overhaul kit package
to match the nearest upcoming expiration date of any parts in the
overhaul kit.
5 Reseal the propeller overhaul kit package.
(b) Option 2:
1 Remove all contents from the propeller overhaul kit.
2 Using the cure date of each part in the propeller overhaul kit,
calculate its expiration date in accordance with this chapter, if
applicable.
3 Remove any parts that have expired.
4 Disperse the remaining individual parts into normal parts stock.

Rev. 55 Apr/24
VOLUME 7
(8) All parts required to be replaced at overhaul are identified by a “Y” in the “OH”
column in the Illustrated Parts List chapter of the applicable Hartzell
Propeller Overhaul manual.
(a) Not all parts designated by the “Y” in the “OH” column of the Illustrated
Parts List chapter of the Hartzell Propeller Overhaul manuals are included
in the propeller overhaul kit.
(9) A list of the Hartzell propeller overhaul kits, including kit contents, and the
revision level of the kit, is contained on the Hartzell Propeller Technical
Documents Library on CD Rom.
(a) The list of propeller overhaul kits contained on the Hartzell Propeller
Technical Documents Library on CD Rom is to be used for reference only,
and does not include all mandatory overhaul replacement parts that are
defined in the Illustrated Parts List chapter of the applicable propeller
Overhaul Manual.
(b) The list of overhaul kits is updated each time a new revision of the Hartzell
Propeller Technical Documents Library on CD Rom is issued.
NOTE: A subscription to the Hartzell Propeller Technical Documents
Library on CD Rom may be purchased by contacting Hartzell
Propeller New Parts Sales at newpartssales@hartzellprop.com.
(c) The contents of an overhaul kit that is contained on the Hartzell
Propeller Technical Documents Library on CD Rom may not agree with the
contents listed on the shipping documents for the overhaul kit.
1 Compare the revision level of the overhaul kit on the shipping
paperwork with the revision level of the overhaul kit on the Hartzell
Propeller Technical Documents Library on CD Rom.
2 If the parts lists of the two sources do not agree, refer to the overhaul
kit information that has the most recent revision level.
3 If there is a question about a Hartzell propeller overhaul kit, contact
Hartzell Propeller LLC Aftermarket Sales.

Rev. 55 Apr/24
VOLUME 7
G. Approved Lubricants
CAUTION: USE ONLY HARTZELL PROPELLER LLC APPROVED GREASE.

DO NOT MIX DIFFERENT SPECIFICATIONS AND/OR BRANDS
OF GREASE EXCEPT AS NOTED IN THIS SECTION.
NOTE: A label (Refer to Figure 1-1) identifying the type of grease used for
previous lubrication (if used) is installed on the propeller piston or on
the blade clamp. If the propeller is to be lubricated with a different
type of grease, the propeller must be disassembled and cleaned of
old grease before relubricating.
THIS PROPELLER WAS

LUBRICATED WITH _____________
THIS GREASE MUST BE USED ON
ALL SUBSEQUENT LUBRICATIONS.
LABEL A-3594
Lubrication Labels
Figure 1-1

Rev. 55 Apr/24
VOLUME 7
(1) The following lubricants are approved for use in Hartzell Propeller LLC
propellers:
NOTE: Some propellers require a specified grease, refer to Hartzell

Propeller Manual 159.
NYCO GN-3058 - Operates across a broad temperature range from -66° F (-54° C)
to 247° F (175° C). Provides good stability resulting in
reduced leakage and oil separation. Provides improved water
washout and corrosion resistance.
Aeroshell 5 - Good high temperature qualities, very little oil separation
or leakage. Cannot be used in temperatures colder than
-40° F (-40° C). Aircraft serviced with this grease must be
placarded to indicate that flight is prohibited if the outside air
temperature is less than -40° F (-40° C).
Aeroshell 6 - “All purpose” grease. Used in most Hartzell Propeller LLC
propellers before January 6, 2020. Higher leakage/oil
separation than Aeroshell 5 at higher temperatures
(approximately 100° F [38° C]).
NOTE: Aeroshell 5 and Aeroshell 6 greases both have a mineral oil
base and the same thickening agent; therefore, mixing of these
two greases is permitted in Hartzell propellers.
WARNING: WHEN MIXING AEROSHELL 5 AND AEROSHELL 6

GREASES, THE AIRCRAFT MUST BE PLACARDED
TO INDICATE THAT FLIGHT IS PROHIBITED IF THE
OUTSIDE AIR TEMPERATURE IS LESS THAN -40° F
(-40° C). AEROSHELL 5 GREASE MUST BE INDICATED
ON THE LABEL.
Aeroshell 7 - Good low temperature grease, but high leakage/oil separation
at higher temperatures. This grease has been associated with
sporadic problems involving seal swelling.
Aeroshell 22 - Qualities similar to Aeroshell 7.
Royco 22CF - Not widely used. Qualities similar to Aeroshell 22.
(2) The following lubricants are approved for use in Hartzell Propeller LLC
A-38( ) bearings:
Exxon Andok 260 High speed bearing lubrication. Only approved use is to
grease the A-38( ) bearing.
Shell Gadus S2 High performance multipurpose grease. Only approved
V100 2 use is to grease the A-38( ) bearing.

Rev. 55 Apr/24
CM Hartzell Supply Manufacturer/Supplier Part Cure Pot Storage Shelf
No. Part No. Description Basis Number/Specification Time Life Temp. Life
1 n/a Oil, Vacuum, 5 gallon N Duoseal, 54996-252 --- --- UC 60 mos
DOS
2 n/a Hose, Vacuum x foot N UA-6407-02 --- --- UC ---
3 n/a Syringe, 30 cc, Disposable - N --- --- --- UC ---
0.03 - 0.05 inch (0.7 - 1.2 mm)
OD needle
4 n/a Electrolyte, Red, Quart N Chem-Etch/Kammerer, A-10 --- --- UC ---
5 n/a Cleaner, Electrolyte, Quart N Monode/Kammerer, MSC-1 --- --- UC ---
6 n/a Cleaner, Electrolyte, Oil N Kammerer, #90 --- --- UC ---
7 n/a Use CM 129 n/a --- --- --- --- ---
8 n/a Sealant N 3M, EC801 Tack free: --- UC 5 mos
Alternate is CM9 24 hours DOS
Full: 7 days
9 A-6741-9 Sealant, Industrial, 5 ounce Y 3M, Scotch Seal, EC800 10-15 --- RT MD
VOLUME 7
minutes
10 A-6741-10 Adhesive, Rubber, quart Y 3M, 1300L or 3M, EC-1300L; Tack: --- RT 15 mos
Alternate is CM79 Use Toluene formula ONLY. 8 minutes DOS
CONSUMABLE MATERIALS
Adhesive without toluene has Full: 3 days
NOT been Hartzell tested or
approved
SUPPLY BASIS SHELF LIFE STORAGE TEMP CLASSES

CODE DESCRIPTION CODE DESCRIPTION CODE DESCRIPTION
Y= Customer can get the consumable material either from Hartzell DOM= Date of Manufacture F= Frozen, store below 0°F (-17°C)
or from a local source. DOS= Date of Shipment from supplier F1= Frozen, -40°F (-40°C) maximum
N= Hartzell does not sell the consumable material, the customer
61-01-02
mos= Months R= Refrigerate, 40°-60°F (4°-15°C)
must purchase it locally.
MD= Manufacturer Expiration Date, use RT= Controlled Room Temperature - 60°-80°F
HPI= Hartzell is the only supplier of the consumable material, the (15°-26°C)
customer must purchase the consumable material from Hartzell. manufacturer’s expiration date -
Hartzell accepts manufacturer’s UC= Uncontrolled, no special Hartzell requirements
S= Customer can get the consumable material from any supplier as follow manufacturer’s requirements
long as the material meets the requirements of the specification. expiration date as-is
SV= Store Vertically (modifier code)
Rev. 54 Nov/23
Page 1-12
Table 1-1
10 A-6741-10-1 Adhesive, Rubber, gallon Y 3M, 1300L or 3M, EC-1300L; Tack: --- RT 15 mos
(cont) Alternate is CM79 Use Toluene formula ONLY. 8 minutes DOS
Adhesive without toluene has Full: 3 days
NOT been Hartzell tested or
approved
11 n/a Acetone, 5 gallon N --- --- --- UC ---
Alternate is CM173
n/a Alcohol, Denatured, gallon N Denatured Alcohol - --- --- UC ---
(preferred for composites) Denatured with Methanol Only
n/a Acetone, 55 gallons N --- --- --- UC ---
12 n/a Grease, 35 pound N Aeroshell, No. 5, 70025 --- --- UC MD
A-6741-12-1-1 Grease, 14.1 ounce tube N Aeroshell, No. 5, 70025 --- --- UC MD
A-6741-12-2 Grease, 55 gallon N Aeroshell, No. 6 --- --- UC MD
A-6741-12-2-1 Grease, 35 pound N Aeroshell, No. 6, 70026 --- --- UC MD
VOLUME 7
A-6741-12-2-2 Grease, 14 ounce N Aeroshell, No. 6, 70026 --- --- UC MD

61-01-02
N= Hartzell does not sell the consumable material, the customer R= Refrigerate, 40°-60°F (4°-15°C)
must purchase it locally. mos= Months
Rev. 54 Nov/23
Page 1-13
Table 1-1
12 A-6741-12-3-1 Grease, 14 ounce N Aeroshell, No.7, 70027 --- --- UC MD

n/a Grease, 55 gallon N Aeroshell, No. 22 --- --- UC MD
A-6741-12-4-1 Grease, 14.1 ounce tube Y Aeroshell, No. 22, 70022 --- --- UC MD
n/a Grease N Royco, No. 22C --- --- UC ---
n/a Grease N Exxon, 5114EP --- --- UC ---
A-6741-12-7 Grease, 400 pound drum N NYCO, GN3058, 400 Lb Drum --- --- UC MD
(Hartzell Propeller LLC SAE-AMS-3058
preferred grease.)
A-6741-12-7-1 Grease, 35 pound pail Y NYCO, GN3058, 35 Lb Pail --- --- UC MD
preferred grease.)
A-6741-12-7-2 Grease, 1 kg can Y NYCO, GN3058, 1 Kg Can --- --- UC MD
preferred grease.)
VOLUME 7
A-6741-12-7-3 Grease, 380 gram cartridge Y NYCO, GN3058, 380 Gram --- --- UC MD
(Hartzell Propeller LLC Cartridge SAE-AMS-3058
preferred grease.)

61-01-02
Rev. 55 Apr/24
Page 1-14
Table 1-1
13 n/a Ethyl Acetate, 5 gallon N --- --- --- UC ---
14 A-2328-21 Adhesive, Quart Kit HPI Henkel/Hysol, EA9330 Full: 5-7 days 60 mins @ RT 12 mos
Alternate for E13890K winding Handle: 77°F (25°C), DOS
repairs only is a combination of min. of 12 hrs 100 gm
CM192, CM193, and CM194 @77°F (25°C) mass
A-6741-14-1 Adhesive, EZ Pack, 25 grams HPI Henkel/Hysol, EA9330 Full: 5-7 days 60 mins @ RT 12 mos
Alternate for E13890K winding Handle: 77°F (25°C), DOS
repairs only is a combination of min. of 12 hrs 100 gm
CM192, CM193, and CM194 @77°F (25°C) mass
A-6741-14-2 Obsolete n/a --- --- --- --- ---

Use A-6741-14-1
15 n/a Adhesive, Quart Kit N Loctite, Henkel/Hysol, EA9430 Min. 4 hrs 50 mins @ UC 12 mos
@77°F (25°C) 77°F (25°C), DOM
250 gm
mass
VOLUME 7
16 A-6741-16 Epoxy Patch, Y Loctite, Henkel/Hysol, 0151 Full: 24 hours 60 minutes RT 36 mos
2.8 ounce Tube Kit @77°F (25°C) mixed DOM
or 2 hours
@140°F (60°C)

61-01-02
Rev. 54 Nov/23
Page 1-15
Table 1-1
17 n/a Media, Blast,Plastic, N A & B Deburring #PMB2-2030 --- --- UC ---
275 pound
18 Use CM59 n/a --- --- --- --- ---
19 A-6741-19 Mold Release, gallon Y Lilly-RAM Chemical Company, Flash Off --- RT MD
Alternate - CM362 LLC/RAM Composite Products,
#87-X26 Mold Release 225
A-6741-19-1 Mold Release, 4 ounce Y Lilly-RAM Chemical Company, Flash Off --- RT 12 mos
Alternate - CM362 LLC/RAM Composite Products, DOS
#87-X26 Mold Release 225
20 A-6741-20 Epoxy, Quart Kit Y Loctite, EA9309.3NA 12 hrs @70°F 35 min @ RT 12 mos
(21°C) or 77°F (25°C) DOS
2 hrs @140°F 450 gm
(60°C) mass
21 A-6741-21 Threadlocker, low strength, Y Loctite, 222 6 hrs @72°F --- RT 24 mos
250 cc (22°C) DOS
VOLUME 7
A-6741-21-1 Threadlocker, low strength, Y Loctite, 222 6 hrs @72°F --- RT 24 mos
50 cc (22°C) DOS
22 n/a Lacquer Thinner, 55 gallon N --- --- --- UC ---

61-01-02
Rev. 55 Apr/24
Page 1-16
Table 1-1
23 n/a Stoddard Solvent, gallon N Kwik Dry --- --- UC ---
Alternates - Naphtha Safety Solvent,
Petroleum Solvent, PD-680,
Varnoline, Spotting Naphtha,
Texsolve, Varsol, and Lotoxane
n/a Parts Cleaning Fluid N ERS Australia Pty Ltd. --- --- UC ---
n/a Solvent, Safety, Red N Enviro Solve UK Ltd, 103570R1 --- --- UC ---
24 A-6741-24 Wash Primer, gallon Y ASG/Randolph Paints --- --- UC 24 mos

Alternate - CM410 MIL-C-8514 DOM
A-6741-24-1 Wash Primer, quart Y ASG/Randolph Paints --- --- UC 24 mos

Alternate - CM410 MIL-C-8514 DOM
25 A-6741-25 Reducer, Wash Primer, gallon Y Randolph Paints, T-54 --- --- UC 24 mos
Alternate - CM412 DOS
A-6741-25-1 Reducer, Wash Primer, quart Y Randolph Paints, T-54 --- --- UC 24 mos
VOLUME 7
26 A-6741-26 Obsolete, use A-6741-26-1 n/a --- --- --- --- ---

A-6741-26-1 Acid Diluent, quart Y Randolph Paints, 120AC-1 --- --- UC 24 mos

61-01-02
Rev. 54 Nov/23
Page 1-17
Table 1-1
27 n/a Spray Fill, gallon N Sherwin-Williams, D61-A-23 --- --- UC 36 mos
Use with CM28 DOM
Alternate - CM84
28 n/a Catalyst n/a Sherwin-Williams, V66V27 --- --- --- 12 mos

Use with CM27 DOM
29 A-6741-29 Primer Sealer, Dark Y Sherwin-Williams, --- --- UC 36 mos

Gray, gallon E65XXA28960-4311 DOM
Alternate - CM318
A-6741-29-1 Primer Sealer, Dark Y Sherwin-Williams, --- --- UC 36 mos

Gray, quart E65XXA28960-4311 DOM
Alternate - CM318
30 A-6741-30 Catalyst, gallon Y Sherwin-Williams, V66V29 --- --- UC 24 mos

DOM
A-6741-30-1 Catalyst, quart Y Sherwin-Williams, V66V29 --- --- UC 24 mos

DOM
VOLUME 7
31 A-6741-31 Accelerator, gallon Y Sherwin-Williams, V66VB11 --- --- UC 12 mos

DOM
A-6741-31-1 Accelerator, quart Y Sherwin-Williams, V66VB11 --- --- UC 12 mos
DOM

61-01-02
Rev. 54 Nov/23
Page 1-18
Table 1-1
32 A-6741-32 Polane Reducer, gallon Y Sherwin-Williams, R7K69, --- --- UC 36 mos
superseded by DOM
Sherwin-Williams, K69
A-6741-32-1 Polane Reducer, quart Y Sherwin-Williams, R7K69, --- --- UC 36 mos

superseded by DOM
Sherwin-Williams, K69
33 A-6741-33 Paint, Polane, Black, gallon Y Sherwin Williams, --- --- UC 36 mos
F63TXB9629-4311 DOM
A-6741-33-1 Paint, Polane, Black, quart Y Sherwin Williams --- --- UC 36 mos
F63TXB9629-4311 DOM
34 A-6741-34 Paint, Polane, Gray, gallon Y Sherwin-Williams --- --- UC 36 mos

F63TXA9920-4311 DOM
A-6741-34-1 Paint, Polane, Gray, quart Y Sherwin-Williams --- --- UC 36 mos

F63TXA9920-4311 DOM
VOLUME 7
35 A-6741-35 Paint, Polane, Gray, Metallic, Y Sherwin-Williams --- --- UC 36 mos

gallon F63TXS9851-4311 DOM
A-6741-35-1 Paint, Polane, Gray, Metallic, Y Sherwin-Williams --- --- UC 36 mos
quart F63TXS9851-4311 DOM

61-01-02
Rev. 54 Nov/23
Page 1-19
Table 1-1
36 A-6741-36 Paint, Polane, Flat White, Y Sherwin Williams --- --- UC 36 mos
gallon F63TXW9627-4311 DOM
A-6741-36-1 Paint, Polane, Flat White, Y Sherwin Williams --- --- UC 36 mos
quart F63TXW9627-4311 DOM
37 n/a Use CM164 n/a --- --- --- --- ---
38 n/a Use CM164 n/a --- --- --- --- ---
39 n/a Use CM170 n/a --- --- --- --- ---
40 n/a Use CM170 n/a --- --- --- --- ---
41 A-6741-41 Toluene, gallon Y --- --- --- UC ---
A-6741-41-1 Toluene, quart Y --- --- --- UC ---
42 A-6741-42 Fiberglass, Fabric, 2 ounce, HPI B210241 --- --- UC ---

38 inch (965 mm) wide x foot
VOLUME 7
43 n/a Use TE209 n/a --- --- --- --- ---
44 n/a 1,1,1 Trichloroethane, pound N --- --- --- UC ---
45 A-6741-45 Vacuum Bag, 16 inch (406 mm) Y New Tech Plastics --- --- UC ---
Tube X 0.004 inch (0.10 mm)
Thick Polybutylene x foot

61-01-02
Rev. 55 Apr/24
Page 1-20
Table 1-1
46 A-6741-46 Gasket Sealant, 7 ounce Y Loctite, #1 Operational: --- RT 12 mos
Superseded by 2 hours, DOS
Henkel/Loctite, #1, P/N 30512 Full:
24 hours
Y Henkel/Loctite, #1, P/N 30512 Operational: --- RT 12 mos

Supersedes Loctite, #1 2 hours, DOS
Full:
24 hours
n/a Gasket Sealant N Permatex Form-A-Gasket No. 1 Operational: --- UC 12 mos

2 hours, DOS
Full:
24 hours
47 n/a Abrasive Pad, 1 each N 3M, Scotch Brite® Pad, white, --- --- UC ---
light duty
n/a Abrasive Pad, 1 each N 3M, Scotch Brite® Pad, very fine --- --- UC ---
VOLUME 7
n/a Abrasive Pad, 1 each N 3M, Scotch Brite® Pad, red, --- --- UC ---
very fine, #7447
48 n/a Use CM14 n/a --- --- --- --- ---

61-01-02
Rev. 54 Nov/23
Page 1-21
Table 1-1
49 A-6741-49 Sealer, quart Y 3M, EC No. 776 10 minutes @ --- RT 12 mos
77°F(25°C) DOS
50 A-6741-50 Nozzle, Mixing Y Nordson 7701487 --- --- UC ---
Alternate - 3M, 62-9742-9935-6
superseded by 3M,
62-9178-9150-9 or
MixTips, MAH-06-21T
51 n/a Sealant Tape, 0.5 inch N Cytec Solvay Group, RS200 --- --- UC ---
(12 mm), 1 case
n/a Sealant Tape, 0.5 inch N Northern Composites, NST-200 --- --- UC ---
(12 mm), 1 case, Alternate
52 n/a Brush, Acid, 0.5 inch (12 mm) N --- --- --- UC ---
53 n/a Use CM130 n/a --- --- --- --- ---
54 n/a Gel, Ultrasonic Inspection N Ultra II Gel or E-Z Gel --- --- UC 36 mos
DOS
VOLUME 7
n/a Gel, Ultrasonic Inspection N Sonotech, Inc. Thermasonic --- --- UC 36 mos
Mid-Temp Grade 60”, DOS
NSN : 6850-01-157-4348
55 A-6741-55 E-Glass 38 inch (965 mm) Y 7781 style cloth finished for --- --- UC ---
wide x foot an epoxy resin system per
AMS-3824A

61-01-02
Rev. 54 Nov/23
Page 1-22
Table 1-1
56 A-6741-56 Fiberglass, Milled, 0.062 in Y --- --- --- UC ---
(1.57 mm), pound
57 A-6741-57 Primer, Adhesive, quart Y Bostik, (L)1007M --- --- RT 9 mos

DOS
58 A-6741-58 Cloth, Bleeder, Teflon®, Y Northern Fiberglass, 200TFP-1 --- --- UC ---
yard (0.8 ounce/yard)
59 A-6741-59 Polyester Absorbent Cloth, Y --- --- --- UC ---

60 inch (1524 mm) x foot
60 n/a Oil, Turbine Engine N MIL-L-23699 --- --- UC ---
61 n/a Use CM 74 n/a --- --- --- --- ---
62 n/a Use CM129 n/a --- --- --- --- ---
63 A-6741-63 Paint, Polane, Cream, Y Sherwin-Williams --- --- UC 36 mos

gallon F63TXH12151-4311 DOM
VOLUME 7
A-6741-63-1 Paint, Polane, Cream, Y Sherwin-Williams --- --- UC 36 mos

quart F63TXH12151-4311 DOM
64 n/a Tape, Aluminum Foil, N 3M, No. 425 --- --- UC ---
1 inch square

61-01-02
Rev. 54 Nov/23
Page 1-23
Table 1-1
65 n/a Use CM118 n/a --- --- --- --- ---
66 n/a RTV, 2.8 ounce N GE, RTV102 Tack Free: Use while RT ---
Alternate - CM92, CM257 Superseded by 30 minutes tacky
Momentive, RTV102
n/a RTV, 2.8 ounce N Momentive, RTV102 Tack Free: Use while RT ---
Alternate - CM92, CM257 Supersedes GE, RTV102 20 minutes tacky
67 n/a Primer, Zinc Chromate, gallon

Randolph Products, N --- --- UC ---
P/N 1757B1C-Y-GL
(Sherwin Williams is an eligible
supplier, no specific p/n)
TT-P-1757, Type 1, Class C,
Yellow
n/a Primer, Zinc Phosphate, gallon N Sherwin-Williams, E90RC38 --- --- UC ---
Alternate TT-P-644D
n/a Primer, Zinc Molybdate, gallon N Sherwin-Williams, N42Y100 --- --- UC ---
VOLUME 7
Alternate TT-P-645B
n/a Primer, Epoxy N Akzo Nobel Advanced Coatings 30 min set 8 hours RT 24 mos
Alternate 37035A to touch, DOM
EFA Spec SP-J-513-A-0016 4 hours
Type 1, Class A hard dry

61-01-02
Rev. 54 Nov/23
Page 1-24
Table 1-1
67 n/a Primer, Epoxy N Akzo Nobel Advanced Coatings 2 hours 4 hours RT 24 mos
(cont.) Alternate 10P8-11 VOC dry topcoat, DOM
MIL-PRF-23377 Type 1, 7 days air
Class C2 performance dry full cure
n/a Primer, Zinc Chromate, N Aircraft Spruce, P/N 09-00895 --- --- RTSV 12 mos
16 ounce, spray can, Alternate TT-P-1757, Type 1, Class C DOM
n/a Primer, Zinc Phosphate, N Aircraft Spruce, A-702, --- --- RTSV 12 mos
16 ounce, spray can P/N 09-00895 DOM
Alternate TT-P-1757, Type 1, Class C
n/a Primer, Zinc Phosphate, N Aircraft Spruce, P/N A-702 --- --- RTSV 12 mos
12 ounce, spray can, Alternate TT-P-1757, Type 1, Class C DOM
68 A-6741-68 Epoxy, 5-minute, 1 to 1 Mix, Y Devcon, 14250 Handle: 3-4 min @ UC 12 mos
25 ml Tube 15 min 75°F(24°C) DOS
Full: 1 hr @ open
75°F(24°C) 48 mos
DOS
unopened
VOLUME 7
n/a Epoxy, 5-minute, 1 to 1 Mix, N Devcon, S-208, 20845 Handle: 3-4 min @ UC 12 mos
25 ml Tube - Alternate 15 min 75°F(24°C) DOS
Full: 1 hr @ open
75°F(24°C) 48 mos
DOS
unopened

61-01-02
Rev. 54 Nov/23
Page 1-25
Table 1-1
68 n/a Epoxy, 5-minute, 1 to 1 Mix, Y Devcon, 14630 Handle: 3-4 min @ UC 12 mos
(cont) gallon 15 min 75°F(24°C) DOS
Full: 1 hr @ open
75°F(24°C) 48 mos
DOS
unopened
69 n/a Ink, White Opaque, 4 ounce N Specialty Ink Co., 352 --- --- UC ---
70 n/a Ink, Black Opaque N --- --- --- UC ---
71 A-6741-71 Adhesive Super Bonder, Y Loctite, 495 Fixture (20% --- R 12 mos
1 ounce max): 20 sec DOS
Full: 8 hours
72 n/a Powder, Talc, 16 pound N Fiber Glast Development Corp., --- --- UC ---
1131-B
73 n/a Use CM129 n/a --- --- --- --- ---
74 A-6741-74 Retaining Compound, Y Loctite, RC675 (Green) --- --- RT 12 mos
VOLUME 7
8.5 ounce Alternate - CM140 DOS

75 A-6741-75 Coating, Rust Preventative, Y E. F Houghtin & Co., --- --- UC ---
5 gallon Rust Veto 342
A-6741-75-1 Coating, Rust Preventative, Y E. F Houghtin & Co., --- --- UC ---
gallon Rust Veto 342

61-01-02
Rev. 54 Nov/23
Page 1-26
Table 1-1
76 n/a Use CM24 n/a --- --- --- --- ---
77 n/a Obsolete n/a --- --- --- --- ---
78 n/a Obsolete n/a --- --- --- --- ---
79 n/a Obsolete n/a --- --- --- --- ---
A-6741-79-1 Adhesive, quart N Bostik, 1096MR, supersedes --- --- RT 9 mos

Bostik, 1096M DOM
80 n/a No. 4 Oil, 55 gallon N Petro Lube Inc, Way Pure 220 --- --- UC ---
n/a No. 4 Oil, 55 gallon, alternate N Mobil Vactra #4 --- --- UC ---
81 n/a Use CM164 n/a --- --- --- --- ---
82 n/a Use CM164 n/a --- --- --- --- ---
83 n/a Use CM164 n/a --- --- --- --- ---

VOLUME 7
84 A-6741-84 Spray Fill, gallon Y Sherwin-Williams, --- --- UC 24 mos

Use with CM85 D61XXH23316-431 DOM
Alternate - CM27
A-6741-84-1 Spray Fill, quart Y Sherwin-Williams, D61H75 --- --- UC 24 mos
Use with CM85 DOM
Alternate - CM27

61-01-02
Rev. 54 Nov/23
Page 1-27
Table 1-1
85 A-6741-85 Catalyst, gallon Y Sherwin-Williams, V66V44 --- --- UC 24 mos
Use with CM84 Superseded by DOM
Sherwin-Williams, V66V47
A-6741-85-1 Catalyst, quart Y Sherwin-Williams, V66V44 --- --- UC 24 mos

Use with CM84 Superseded by DOM
Sherwin-Williams, V66V47
86 n/a Adhesive, Industrial, 5 ounce N 3M, EC No. 847 --- --- RT 12 mos
DOS
87 n/a Use CM90 n/a --- --- --- --- ---
88 n/a Use CM90 n/a --- --- --- --- ---
89 n/a Use CM71 n/a --- --- --- --- ---
90 A-6741-90 Epoxy Adhesive, Gray, 48.5 ml Y 3M, DP-190 Handle: 8 hrs 90 min, RT 15 mos
or 50 ml @75°F (24°C), Full Bond DOS
Full: 24 hours in 24 hours
VOLUME 7
91 n/a Use CM9 n/a --- --- --- --- ---

61-01-02
Rev. 54 Nov/23
Page 1-28
Table 1-1
92 A-6741-92 RTV, 10.1 ounce Y GE, IS 802, Superseded by --- --- RT 12 mos
Alternate - CM66, CM257 Momentive, IS 802 DOS
A-6741-92 RTV, 3 ounce Y Momentive, IS 802 --- --- RT 12 mos
Alternate - CM66 Supersedes GE, IS 802 DOS
93 n/a RTV, 2.8 ounce N GE, RTV6703, Superseded by --- --- RT 12 mos
Alternates are A-6741-93( ) Momentive, RTV6703 DOS

N Momentive, RTV6703 --- --- RT 12 mos
Supersedes GE, RTV6703 DOS
A-6741-93-1 RTV, Black, 10 ounce Y GE, RTV123, Superseded by --- --- RT 12 mos
Alternates are A-6741-93( ) Momentive, RTV123 DOS

Y Momentive, RTV123 --- --- RT 12 mos
Supersedes GE, RTV123 DOS
A-6741-93-2 RTV, White, 10 ounce Y Momentive, RTV122 --- --- RT 12 mos
Alternates are A-6741-93( ) DOS
A-6741-93-3 RTV, Translucent, 10 ounce Y Momentive, RTV128 --- --- RT 12 mos
VOLUME 7
Alternates are A-6741-93( ) DOS

94 A-6741-94 Adhesive, quart Y Henkel/Hysol, EA9309.NA --- --- RT 12 mos
DOS
95 n/a Adhesive, quart N Henkel/Hysol, EA9346.5 --- 14 days F 12 mos
Replaced by CM314 DOS

61-01-02
Rev. 54 Nov/23
Page 1-29
Table 1-1
96 A-6741-96 Adhesive - Quick Set, Y Loctite, 404 --- --- R 12 mos
1/3 ounce DOS
97 n/a Adhesive, 50 ml N Loctite, 324 --- --- UC 12 mos

DOS
98 A-6741-98 Adhesive, Depend, 0.85 ounce Y Loctite, 330 Fixture: 5 min --- RT 12 mos
(2 part kit includes: Product Number 20251 Kit Full: 4 to 24 DOS
A-6741-98-1 and A-6741-98-2) hours
A-6741-98-1 Loctite, 330 Depend adhesive n/a Part 1 of 20251 Kit --- --- --- 12 mos
DOS
A-6741-98-2 Loctite, 7387 Depend activator n/a Part 2 of 20251 Kit --- --- --- 12 mos
DOS
99 n/a Oakite N Chemetall, Oakite 31, --- --- UC ---

TT-C-490C, Method VI,
MIL-C-10578CD Type V,
MIL-C-46487 Type II
VOLUME 7
100 n/a Coating, Chemical Conversion N Chemetall Oakite, --- --- UC ---
Chromicoat L-25
MIL-C-81706, MIL-C-5541,
Class1A & Class 3

61-01-02
Rev. 54 Nov/23
Page 1-30
Table 1-1
101 n/a Cleaner, Alkaline, pound N Turco, 4215NC-LT --- --- UC ---
102 n/a Obsolete n/a --- --- --- --- ---
Use CM17
103 n/a Solvent, gallon N Whitford Worldwide, 99 Solvent --- --- UC ---
104 n/a Solvent, gallon N Whitford Worldwide, 99B Solvent --- --- UC ---
105 n/a Coating, Xylan®, gallon N Xylan®, 1052/399 Olive --- --- UC 12 mos
DOM
A-6741-105-1 Coating, Xylan®, quart Y Xylan®, 1052DF/399 Olive --- --- UC 12 mos
Alternate - Xylan®, 1053/399A DOM
106 n/a Methyl-Ethyl-Ketone (MEK), N MEK --- --- RT 24 mos
5 gallon DOM
n/a Methyl-Ethyl-Ketone (MEK), N MEK --- --- RT 24 mos
55 gallon DOM
107 n/a Activator, Spray N Loctite, 7387 Depend Activator --- --- RT 24 mos
VOLUME 7
DOM
108 A-6741-108 Lubricant, gallon Y Starrett, M1 --- --- UC ---
A-6741-108-1 Lubricant, Aerosol, 12 ounce Y Starrett, M1 --- --- UC ---
109 n/a Spray Clean N --- --- --- UC ---
Alternate is CM128

61-01-02
Rev. 54 Nov/23
Page 1-31
Table 1-1
110 n/a Powder, Aluminum, 2.5 pound N Freeman Manufacturing --- --- UC ---
& Supply Co., 406383
n/a Powder, Aluminum, pound N Kindt-Collins Co., 9122A --- --- UC ---
n/a Powder, Aluminum, ounce N Freeman Manufacturing --- --- UC ---

& Supply Co., 406383
n/a Powder, Aluminum, ounce N Kindt-Collins Co., 9122A --- --- UC ---
111 A-6741-111 Cloth, Carbon, 38 inch HPI --- --- --- UC ---
(965 mm) wide x foot
112 n/a Steel Wool, #0000 N --- --- --- UC ---
113 A-6741-113 Kevlar®, Drycloth, #549, HPI --- --- --- UC ---
114 A-6741-114 Accelerator, Adhesive, Y Bostik, Boscodur, #9R --- --- RT 6 mos
4 ounce, DOS
superseded by A-6741-114-1
VOLUME 7
A-6741-114-1 Obsolete n/a --- --- --- --- ---
A-6741-114-2 Curing Agent, Adhesive, Y Bostik, Boscodur, 4L --- --- RT 12 mos
4 ounce, DOM
supersedes A-6741-114 and
A-6741-114-1

61-01-02
Rev. 54 Nov/23
Page 1-32
Table 1-1
115 n/a Obsolete n/a --- --- --- --- ---
116 A-6741-116 Threadlocker, Removable, Y Loctite, 242 --- --- RT MD

50 cc
117 n/a Use CM60 n/a --- --- --- --- ---
118 A-3338-4 Anti-Seize Compound, Y MIL-PRF-83483 --- --- UC ---

1/3 ounce
A-3338-7 Anti-Seize Compound, 8 ounce Y MIL-PRF-83483 --- --- UC ---
119 A-6741-119 Mat, Carbon Fiber, HPI --- --- --- UC ---
120 A-6741-120 Paint, Polane, Red, gallon Y Sherwin-Williams, --- --- UC 36 mos
F63TXR9853-4311 DOM
A-6741-120-1 Paint, Polane, Red, quart Y Sherwin-Williams, --- --- UC 36 mos

F63TXR9853-4311 DOM
VOLUME 7
121 A-6741-121 Lubricant, Metal Protect, Y Molykote by Dupont/Dow, --- --- UC ---
13.6 kg pail “Metal Protector Plus”
A-6741-121-1 Lubricant, Metal Protect, Y Molykote by Dupont/Dow, --- --- UC ---
quart “Metal Protector Plus”
122 A-6741-122 Leak Detector, 4 ounce Y Leak Tec, 372 --- --- UC ---

61-01-02
Rev. 54 Nov/23
Page 1-33
Table 1-1
123 n/a Use CM21 n/a --- --- --- --- ---
124 A-6741-124 Adhesive Promoter, pint Y 3M, 86A --- --- RT 24 mos
DOM
125 A-6741-125 Replication Putty, 2 pound Y Dynamold Inc. - p/n DMR-503 30 min. --- UC 12 mos
P.O. Box 9617 DOM
Fort Worth, TX
Phone: 817.335.0862
Fax: 817.877.5203
n/a Replication Putty N 3M Impregum F --- --- UC ---
126 n/a Coating, Chemical Conversion N Parker + Amchem --- --- UC ---
127 A-6741-127 Primer T, 4.5 ounce Y Loctite, Locquic, T7471 1 minute --- RSV 24 mos
Mil-S-22473E Grade T Form R, DOS
ASTM-D5363
A-6741-127-1 Primer T, 1 gallon Y Loctite, Locquic, T7471 1 minute --- R 24 mos

VOLUME 7
Mil-S-22473E Grade T Form R, DOS

ASTM-D5363
128 n/a Cleaner, Electronics, 12 ounce N Contax HP, 90393 --- --- UC ---
129 n/a Protective Spray, Clear, N Krylon 1301 Crystal Clear --- --- RTSV ---
11 ounce (preferred), Ace Polyurethane
1037795, or Semi-gloss Krylon 8118

61-01-02
Rev. 54 Nov/23
Page 1-34
Table 1-1
130 n/a Freeze Mist II, 10 ounce N Freeze Mist II --- --- UC ---
Spray, Freeze, 10 ounce N TechSpray, Envi-Ro-Tech™ 1672 --- --- UC ---
131 A-6741-131 Wire, Stainless Steel - Y MS20995C32 --- --- UC ---

0.032 inch (0.81 mm) diameter,
pound
132 A-6741-132 Wire, Stainless Steel - Y MS20995C20 --- --- UC ---

0.020 inch (0.50 mm) diameter,
pound
133 A-6741-133 Adhesive - Retaining N Loctite, RC 635 72 hrs @ room --- RT 12 MOS
Compound, 250 cc temperature DOS
134 A-6741-134 Sealant, Hydraulic, 250 cc Y Loctite, #569 24 hours --- RT 36 mos
DOS
A-6741-134-1 Sealant, Hydraulic, 50 ml Y Loctite, #569 24 hours --- RT 36 mos

DOS
VOLUME 7
135 A-6741-135 Adhesive, - Retaining Y Loctite, 272 6 hours, can --- RT 24 mos
Compound, 50 cc accelerate DOM
with Primer T
136 A-6741-136 Sealant - Gasket Eliminator, Y Loctite, 510 15 hours, can --- RT 36 mos
50 cc be accelerated DOS
to 6 hours
with Primer N

61-01-02
Rev. 54 Nov/23
Page 1-35
Table 1-1
137 B-6654-100 Tape, UHMW - 1 inch x 36 yard Y Saint-Gobain, 2302-5R x 1.00 --- --- UC ---
(25.4 x 32.92 M) roll
B-6654-100-1 Tape, UHMW - 1 inch x 36 inch Y Saint-Gobain, 2302-5R x 1.00 --- --- UC ---
(25.4 x 914.4 mm)
B-6654-150 Tape, UHMW - 1.5 inch x 36 yard Y Saint-Gobain, 2302-5R x 1.5 --- --- UC ---
(38.1 mm x 32.92 M) roll
138 n/a Cleaning Formula N Branson, p/n MC-3 --- --- UC ---
Eagle Road
Danbury, CT 06810-1961
Phone: 203.796.0400
Fax: 203.796.2240
139 A-6741-139-1 Grease, 2.5 pound HPI --- --- --- UC ---
superseded by A-6741-139-2
A-6741-139-2 Grease, 14 ounce Y Shell, Gadus S2 V100 2 --- --- UC ---

supersedes A-6741-139-1 Superseded by
VOLUME 7
Shell, Gadus S5 V100 2
140 n/a Adhesive - Retaining N Loctite, RC 609 --- --- UC ---

Compound, 250 ml
Alternate - CM74

61-01-02
Rev. 54 Nov/23
Page 1-36
Table 1-1
141 n/a Use CM132 n/a --- --- --- --- ---
142 n/a Use CM131 n/a --- --- --- --- ---
143 A-6741-143 Accelerator, Adhesive, N Loctite, N7649 --- --- UC ---
Locquic Primer N
144 n/a Solvent, Safety, Red, Manpower N Enviro Solve UK Ltd, 103570R1 --- --- UC ---
Alternate - CM23
145 A-6741-145-1 Paint, Touch-up, Y Sherwin-Williams, 1-2 hours --- UCSV 24 mos
Black, 12 ounce F75KXB9958-4311 DOM
A-6741-145-2 Paint, Touch-up, Black N Tempo, A-150 1 hour --- UC 24 mos
DOM
Gray, 12 ounce F75KXA10445-4311 DOM
A-6741-146-2 Paint, Touch-up, Gray N Tempo, A-151 1 hour --- UC 24 mos
DOM
VOLUME 7
White, 12 ounce F75KXW10309-4311 DOM
A-6741-147-2 Paint, Touch-up, White N Tempo, A-152 1 hour --- UC 24 mos
DOM
A-6741-147-3 Paint, Touch-up, White, Y Sherwin-Williams, 1-2 hours --- UCSV 24 mos
6 ounce F75KXW10309-4311 DOM

61-01-02
Rev. 54 Nov/23
Page 1-37
Table 1-1
Gray Metallic, 12 ounce F75KXS9754-4311 DOM
149 A-6741-149-1 Paint, Touch-up, Red, Y Sherwin-Williams, 1-2 hours --- UCSV 24 mos
12 ounce F75KXR12320-4311 DOM

A-6741-149-2 Paint, Touch-up, Red N Tempo, A-153 1 hour --- UC 24 mos
DOM
A-6741-149-3 Paint, Touch-up, Red, 6 ounce Y Sherwin-Williams, 1-2 hours --- UCSV 24 mos
F75KXR12320-4311 DOM
150 A-6741-150-1 Paint, Touch-up, Yellow, Y Sherwin-Williams, 1-2 hours --- UCSV 24 mos
12 ounce F75KXY11841-4311 DOM
A-6741-150-2 Paint, Touch-up, Yellow N Tempo, A-154 1 hour --- UC 24 mos
DOM
151 A-6741-151 Lubricant, Anti-seize, 1 pound Y Loctite, 767, MIL-A-907E --- --- UC 36 mos
DOM
152 A-6741-152 Threadlocker, 1.69 ounce Y Loctite, 26231 20 min.-fixture --- RT 12 mos
5 min.w/ primer DOS
VOLUME 7
24 hours-full

61-01-02
Rev. 54 Nov/23
Page 1-38
Table 1-1
153 n/a Use CM98 n/a --- --- --- --- ---
154 n/a Sealant - Form-a-Gasket N Loctite #30516 Aviation --- --- UC ---
Gasket Sealant
155 A-6741-155-2 Tape, Teflon® - 0.5 inch Y Datwyler Sealing Solutions USA, Inc. --- --- UC ---
wide X 0.010 inch thick X 100 TS 1/2 X 0.010 X 100
foot (12 X 0.25 X 30480 mm) PTFE (Teflon®) film per
roll - preferred thickness. AMS3652, 0.010 ± 0.0005 inch
Alternate is CM156 (0.25 ± 0.0125 mm) thick, etch
one side per AMS 2491
B-4256-2 Tape, Teflon® - 0.5 inch Y Datwyler Sealing Solutions USA, Inc. --- --- UC ---
wide X 0.010 inch thick X 10.62 VT00SX.500EFT
inch (12 X 0.25 X 269.7 mm) PTFE (Teflon®) film per
cut - preferred thickness. AMS3652, 0.010 ± 0.0005 inch
103842-2 Tape, Teflon® - 0.5 inch Y Datwyler Sealing Solutions USA, Inc. --- --- UC ---
VOLUME 7

cut - preferred thickness. AMS3652, 0.010 ± 0.0005 inch

61-01-02
Rev. 54 Nov/23
Page 1-39
Table 1-1
155 A-6741-155
Tape, Teflon® - 0.5 inch Y Datwyler Sealing Solutions USA, Inc. --- --- UC ---
(cont.)
wide X 0.005 inch thick X 100 TS 1/2 X 0.005 X 100
foot (12 X 0.12 X 30480 mm) PTFE (Teflon®) film per
roll AMS3652, 0.005 ± 0.0005 inch
B-4256 Tape, Teflon® - 0.5 inch Y Datwyler Sealing Solutions USA, Inc. --- --- UC ---
cut AMS3652, 0.005 ± 0.0005 inch
156 n/a Tape, Teflon® - 0.75 inch N Datwyler Sealing Solutions USA, Inc. --- --- UC ---
wide X 0.010 inch thick X 100 PTFE (Teflon®) film per
feet (19.0 X 0.25 X 30480 mm) AMS3652, 0.010 ± 0.0005 inch
long - preferred thickness. (0.25 ± 0.0125 mm) thick, etch
Alternate is CM155 one side per AMS 2491
VOLUME 7
n/a Tape, Teflon® - 0.75 inch N Datwyler Sealing Solutions USA, Inc. --- --- UC ---
wide X 0.005 inch thick X 100 PTFE (Teflon®) film per
feet (19.0 X 0.12 X 30480 mm) AMS3652, 0.005 ± 0.0005 inch
long (0.12 ± 0.0125 mm) thick, etch
Alternate is CM155 one side per AMS 2491

61-01-02
Rev. 54 Nov/23
Page 1-40
Table 1-1
157 n/a Oil, Hydraulic, gallon N Shell, 60421, MIL-PRF-5606 --- --- UC 24 mos
DOM
158 A-6741-158 Erosion Tape, Y 3M, 8672-2 --- --- RT 24 mos

Polyurethane, 108 foot roll DOS
A-6741-158-1 Erosion Tape, Y 3M, 8672-2 --- --- RT 24 mos

Polyurethane x foot DOS
159 n/a Cheesecloth S AMS 3819, Class 1, Grade A, --- --- UC ---
Form 1
CCP Industries, p/n CCR588043
P.O. Box 6500
Cleveland, Ohio 44101
Phone: 1-800-321-2840
Alternate - American Fiber &
Finishing, Inc., 588074C
160 A-6741-160 Tape, Reference Stripe, Yellow Y Material: 3M 7125 Vinyl, --- --- UC ---
- 1/8 inch X 2 inch (Available for Color: Pantone 109C
VOLUME 7
purchase from Hartzell

Propeller LLC only in multiples
of 100 each on a single sheet.)

61-01-02
Rev. 55 Apr/24
Page 1-41
Table 1-1
161 A-6741-161 Sealant, 6 ounce Kit Y PPG Aerospace Tack Free Less 30 minutes RT 9 mos
( (PRC-Desoto International) than 10 hours DOM
PR1422A-1/2AM654SK or 35A Durometer
PR1440A-1/2AM654SK Cure 30 hours
A-6741-161-2 Sealant, Pint Y PPG Aerospace Tack Free Less 30 minutes RT 9 mos
PR1422A-1/2AM012PT or 35A Durometer
PR1440A-1/2AM012PT Pint Cure 30 hours
A-6741-161-3 Sealant, Quart Y PPG Aerospace Tack Free Less 30 minutes RT 9 mos
PR1422A-1/2AM024QT or 35A Durometer
PR1440A-1/2AM024QT Quart Cure 30 hours
A-6741-161-1 Sealant, 6 ounce Kit Y PRC Aerospace Tack 2 hours 30 minutes RT 9 mos
(PRC-Desoto International) Cure 35 hours DOM
1422B-1/2AM654SK
A-6741-161-1-1 Sealant, 2.5 ounce Semkit Y PPG Aerospace Tack 2 hours 30 minutes RT 9 mos
(PRC-Desoto International) Cure 35 hours DOM
VOLUME 7
1422B-1/2AM655SK
162 A-6741-162-1 Pencil, Non-graphite, Y Sanford, SAN-02450 --- --- UC ---

Carmine Red, 1 dozen or Non-Graphite Equivalent
Alternate is Markal 96100
A-6741-162-2 Pencil, Non-graphite, Y Sanford, SAN-02460 --- --- UC ---

Silver, 1 dozen

61-01-02
Rev. 54 Nov/23
Page 1-42
Table 1-1
163 A-6741-163 Paint, Polane, Silver, Y Sherwin-Williams, --- --- UC 36 mos
A-6741-163-1 Paint, Polane, Silver, Y Sherwin-Williams, --- --- UC 36 mos

164 A-2328-30 Kit, Conductive Coating, Y PRC-Desoto 4 hours 4 hours RT 24 mos
2 gallon DOM
Contains: A-6741-164-(5, 6)
A-2328-13 Kit, Conductive Coating, quart Y PRC-Desoto 4 hours 4 hours RT 24 mos

Contains: A-6741-164-(5, 6) DOM
A-6741-5 528X310 Coating, Conductive - N PRC-Desoto, 528X310 4 hours 4 hours RT 24 mos

Base, Black DOM
Not sold separately.
A-6741-6 910X464 Coating, Conductive/ N PRC-Desoto, 910X464 4 hours 4 hours RT 24 mos

Anti-static- Activator DOM
Not sold separately.
165 A-6741-165 Paint, Polane, Yellow, gallon Y Sherwin-Williams, --- --- UC 36 mos
VOLUME 7
F63TXY9791-4311 DOM
A-6741-165-1 Paint, Polane, Yellow, quart Y Sherwin-Williams --- --- UC 36 mos

F63TXY9791-4311 DOM
166 A-6741-166 Use CM33 - A-6741-33 Y --- --- --- --- ---
A-6741-166-1 Use CM33 - A-6741-33-1 Y --- --- --- --- ---


61-01-02
Rev. 54 Nov/23
Page 1-43
Table 1-1
167 A-6741-167 Reducer, Acrylic Urethane, Y Sherwin-Williams, R7K 6202 --- --- UC 24 mos
gallon (Automotive Finishes) DOM
A-6741-167-1 Reducer, Acrylic Urethane, Y Sherwin-Williams, R7K 6202 --- --- UC 24 mos
8 ounce (Automotive Finishes) DOM
168 A-6741-168 Paint, Acrylic Urethane, Y Sherwin-Williams, J6-4802 Mixed: 1 hour --- UC 24 mos
Gold Metallic, gallon (Automotive Finishes) @140°F (60°C) DOM
or 16 hours
@75°F (24°C)
A-6741-168-1 Paint, Acrylic Urethane, Y Sherwin-Williams, J6-4802 Mixed: 1 hour --- UC 24 mos
Gold Metallic, pint (Automotive Finishes) @140°F (60°C) DOM
or 16 hours
@75°F (24°C)
169 A-6741-169 Catalyst, Acrylic Urethane, Y Sherwin-Williams, V6V769 --- --- UC 24 mos
quart (Automotive Finishes) DOM
A-6741-169-1 Catalyst, Acrylic Urethane, Y Sherwin-Williams, V6V769 --- --- UC 24 mos

VOLUME 7
4 ounce (Automotive Finishes) DOM

61-01-02
Rev. 54 Nov/23
Page 1-44
Table 1-1
170 A-2328-8 Paint, Comp Blade, Repair Kit, Y Spraylat, 599-A8574-1ABC --- --- UC 6 mos
Lightning DOM
A-6741-170-5 Catalyst, Coating, Conductive N PPG, 599-A8574-1A --- --- UC 6 mos

Solution - Lightning Guard, DOM
Part A - Not sold separately,
part of A-2328-8 Paint Kit
A-6741-170-6 Paint, Copper Filled, N PPG, 599-A8574-1B --- --- UC 6 mos

Lightning Guard, DOM
Part B - Not sold separately,
A-6741-170-7 Retardant, Coating, Conductive, N PPG, 599-A8574-1C --- --- UC 6 mos

Lightning Guard, DOM
Part C - Not sold separately,
173 n/a Acetone, 5 gallon N --- --- --- UC ---

VOLUME 7
175 n/a Shield, Erosion, Dome N PM-192 (PM Research), --- --- UC ---
SJ-8665 FP-408 (3M)

61-01-02
Rev. 54 Nov/23
Page 1-45
Table 1-1
178 A-6741-178 Adhesive, 0.70 ounce container Y Loctite 480, 48040 1 hour --- R MD
179 A-6741-179 Primer, 1.75 ounce container Y Loctite 770, 2759219 --- --- RT 36 mos
DOS
183 n/a 70% or higher Isopropyl Alcohol N --- --- --- UC ---
184 n/a Adhesive, Threadlocker, 50 ml N Loctite, 2760 24 hours --- RT 24 mos

can accelerate DOS
with Primer T
185 n/a Cleaning Agent N Radiaze L.F, Diverseylever --- --- UC ---
(Dubois Chemical)
n/a Cleaning Agent N Dubois Power Lift Cleaner --- --- UC ---
(Dubois Chemical)
187 n/a Threadlocker, 50 ml N Loctite, 290 24 hours --- RT 12 mos

Steel @ 77°F DOS
(25°C)
VOLUME 7
188 A-6741-188-1 Grease, silicon carbide, 400 grit N Loctite, 39523 - 1 pound --- --- RT ---
Alternate - Loctite, 39522 - 4 ounce --- ---
188 A-6741-188-2 Grease, silicon carbide, 600 grit N Loctite, 39549 - 1 pound --- --- RT ---
Alternate - Loctite, 39548 - 4 ounce --- ---

61-01-02
Rev. 54 Nov/23
Page 1-46
Table 1-1
190 A-6741-190-1 Paint, Touch-up, Silver, Y Sherwin-Williams, 1-2 hours --- UCSV 24 mos
12 ounce F75KXS13564-4311 DOM
192 n/a Resin N Shell Cherie/Glycidather 162 12 hours at 40 min at RT 6 mos

room temp. room temp. DOS
mixed with
CM193
193 n/a Hardener N Shell Cherie/Epikure 113 18 hours at 40 min at RT 6 mos

140° F (60°C) room temp. DOS
mixed with
CM192
194 n/a Fiber, roving N Saint Gobain Vetrotex: --- --- RT

EC2400P185 E Glass Roving
195 n/a Solder, 0.062 Dia., 63/37 alloy N Kester/Type 24-6337-0061 --- --- --- ---
196 n/a Solder, 0.062 Dia., 60/40 alloy N Kester/Type 24-6040-0061 --- --- --- ---
VOLUME 7
199 A-6741-199 Sealant, Electrically Conductive Y PRC-Desoto/PR-2200 Class B 6 hours at --- RT MD

Alternate is A-6741-199-1 room temp.
A-6741-199-1 Sealant, Electrically Conductive Y PRC-Desoto/PR-2201 Class B 5 hours at --- RT MD
Alternate is A-6741-199 room temp.

61-01-02
Rev. 54 Nov/23
Page 1-47
Table 1-1
200 A-6741-200 Paint, Bright Red Polane, Y Sherwin -Williams, --- --- UC 36 mos
gallon F63TXR16285-4311 DOM
A-6741-200-1 Paint, Bright Red Polane, Y Sherwin -Williams, --- --- UC 36 mos
quart F63TXR16285-4311 DOM
A-6741-200-5 Paint, Touch-up, Bright Red, Y Sherwin -Williams, 1-2 hours --- UCSV 24 mos
can F63TXR16285-4311 DOM
201 A-6741-201 Paint, Bright Yellow Polane, Y Sherwin -Williams, --- --- UC 36 mos
gallon F63TXY16286-4311 DOM
A-6741-201-1 Paint, Bright Yellow Polane, Y Sherwin -Williams, --- --- UC 36 mos
quart F63TXY16286-4311 DOM
A-6741-201-5 Paint, Touch-up, Bright Yellow, Y Sherwin -Williams, 1-2 hours --- UCSV 24 mos
can F63TXY16286-4311 DOM
203 A-6741-203 Paint Bright Silver Polane, Y Sherwin-Williams, --- --- UC 36 mos
VOLUME 7
A-6741-203-1 Paint Bright Silver Polane, Y Sherwin-Williams, --- --- UC 36 mos

A-6741-203-5 Paint, Touch up, Bright Silver, Y Sherwin-Williams, 1-2 hours --- UCSV 24 mos
can F63TXS16768-4311 DOM

61-01-02
Rev. 54 Nov/23
Page 1-48
Table 1-1
204 A-6741-204 Paint, Prop Gold Polane, Y Sherwin-Williams, --- --- UC 36 mos
A-6741-204-1 Paint, Prop Gold Polane, Y Sherwin-Williams, --- --- UC 36 mos

A-6741-204-5 Paint, Touch up, Prop Gold, Y Sherwin-Williams, 1-2 --- UCSV 24 mos
12 ounce F63TXS17221-4311 hours DOM
208 A-6741-208 Epoxy, Adhesive, Y 3M/DP110 Gray 48 hours 8-13 RT 15 mos

50 ml Duo Pak full cure minutes DOS
209 n/a Use TE209 n/a --- --- --- --- ---
210 n/a Oil Dye, Red N Innospec, Oil Dye Red B4 Liquid --- --- UC ---
5 gallon
A-6741-210-1 Oil Dye, Red Y Innospec, Oil Dye Red B4 Liquid --- --- UC ---
pint Cessna P/N A-4880-1PT
211 A-6741-211 Sealent, Thread, 250 CC Y Loctite, 565 Operational: --- RT ---
VOLUME 7
2 hours,
Full:
24 hours

61-01-02
Rev. 54 Nov/23
Page 1-49
Table 1-1
215 A-6741-215 5 Minute Epoxy Gel Adhesive Y Devcon 14240 12 hours 4-7 RT MD
full cure minutes
n/a 5 Minute Epoxy Gel Adhesive, N Devcon S-210 12 hours 4-7 RT MD

alternate full cure minutes
216 n/a Primer, Adhesive N Bostik, 9252 Primer --- --- RT 6 mos
DOS
217 n/a Adhesive N Bostik, 2402 Adhesive --- --- RT 6 mos

DOS
218 n/a Curing Agent, Adhesive N Bostikure D Curing Agent --- --- RT 9 mos
DOM
219 n/a Methyl Propyl Ketone (MPK) N --- --- --- UC ---
220 n/a Tape, Vinyl, 1/8 inch width N Defense Holdings Inc., AG104 --- --- RT ---
A part of PL Paint Kit
A-6741-233-1
VOLUME 7
221 n/a Tape, Vinyl, 1/4 inch width N Defense Holdings Inc., AG105 --- --- RT ---
A-6741-233-1

61-01-02
Rev. 54 Nov/23
Page 1-50
Table 1-1
222 n/a Funnel/Filter N Defense Holdings Inc., AG106 --- --- UC ---
A-6741-233-1
223 n/a Stick, Stir N Defense Holdings Inc., AG107 --- --- UC ---
A-6741-233-1
224 n/a Paint, Polane White, PL Base N Defense Holdings Inc., AG108 --- 4 hours RT 12 mos
A part of PL Paint Kit after DOM
A-6741-233-1 mixing
225 n/a Hardener, PL Base Coat N Defense Holdings Inc., AG109 --- 4 hours RT 12 mos
A-6741-233-1 mixing
226 n/a Paint, Photoluminescent N Defense Holdings Inc., AG110 --- 4 hours RT 12 mos
A-6741-233-1 mixing
VOLUME 7
227 n/a Hardener, Photoluminescent N Defense Holdings Inc., AG111 --- 4 hours RT 12 mos
A-6741-233-1 mixing

61-01-02
Rev. 54 Nov/23
Page 1-51
Table 1-1
228 n/a Reducer, Photoluminescent N Defense Holdings Inc., AG112 --- 4 hours RT 12 mos
A-6741-233-1 mixing
229 n/a Coating, PL Clear Coat N Defense Holdings Inc., AG113 --- 4 hours RT 12 mos
A-6741-233-1 mixing
230 n/a Reducer, PL Clear Coat N Defense Holdings Inc., AG114 --- 4 hours RT 12 mos
A-6741-233-1 mixing
231 n/a Hardener, PL Clear Coat N Defense Holdings Inc., AG115 --- 4 hours RT 12 mos
A-6741-233-1 mixing
232 n/a Rag, Tack N Defense Holdings Inc., AG116 --- --- UC ---
A-6741-233-1
VOLUME 7

61-01-02
Rev. 54 Nov/23
Page 1-52
Table 1-1
233 A-6741-233-1 Kit, Photoluminescent HPI Defense Holdings Inc., AGPK100 --- --- RT 12 mos
Includes: DOM
CM220
CM221
CM222
CM223
CM224
CM225
CM226
CM227
CM228
CM229
CM230
CM231
CM232
238 A-6741-238 RTV, Silicone Y GE RTV 627 --- --- RT 12 mos

DOS
VOLUME 7
244 n/a Lead Wool N Avril - GA, lead wool, --- --- UC ---
5 pound bag
257 A-6741-257 Sealant, Silicone, 430 gm Y ThreeBond, 1216E430G or Tack Free --- RT 9 mos
1216E455G/JCL-US 6 minutes DOM

61-01-02
Rev. 54 Nov/23
Page 1-53
Table 1-1
259 A-6741-259 Tape, Polyurethane, 36 yard Y 3M, 8681HS or 8671 --- --- UC 24 mos
roll DOM
282 A-6741-282 Paint, Matterhorn White, Y Sherwin-Williams, Acry Glo, --- --- RT 36 mos
gallon W00150 DOM
283 A-6741-283 Catalyst, Acry Glo, quart Y Sherwin-Williams, CM0571081 --- --- RT 24 mos
DOM
284 A-6741-284 Reducer, Acry Glo, Med, Tmp, Y Sherwin-Williams, CM0110701 --- --- RT 24 mos
gallon DOM
285 A-6741-285 Reducer, Acry Glo, Low, Tmp, Y Sherwin-Williams, CM0110755 --- --- RT 24 mos
gallon DOM
286 A-6741-286 Reducer, Acry Glo, Hi Tmp, Y Sherwin-Williams, CM0110821 --- --- RT 24 mos
gallon DOM
287 A-6741-287 Accelerator, Acry Glo, pint Y Sherwin-Williams, CM0571082 --- 1 hour, RT 24 mos
2-3 hrs DOM
VOLUME 7
gelled
288 A-6741-288 Obsolete n/a --- --- --- --- ---

Use A-6741-106
290 A-6741-290 Paint, Conventional Clear, Y Sherwin-Williams, Acry Glo, --- --- RT 36 mos
gallon CM0571080 DOM

61-01-02
Rev. 54 Nov/23
Page 1-54
Table 1-1
291 A-6741-291 Paint, Sterling Silver Met, Y Sherwin-Williams, Acry Glo, --- --- RT 36 mos
gallon CM0571186 DOM
292 A-6741-292 Stabilizer, Acry Glo, pint Y Sherwin-Williams, Acry Glo, --- --- RT 36 mos
CM0571085 DOM
293 A-6741-293 Tubing, Heat Shrink Y Alpha Wire Fit 105-1/8 --- --- RT ---
294 A-6741-294 Tubing, Heat Shrink Y Alpha Wire Fit-Clear-1/8 --- --- RT ---
301 A-6741-301 Oil, case (6 quart) Y Shell Rotella T4 10W-30 --- --- UC ---
A-6741-301-1 Oil, quart Y Shell Rotella T4 10W-30 --- --- UC ---
302 A-6741-302 Oil, case (6 quart) Y Shell Rotella T6 5W-40 --- --- UC ---
A-6741-302-1 Oil, quart Y Shell Rotella T6 5W-40 --- --- UC ---
303 A-6741-303 Paint, Sterling, Polane, Y Sherwin-Williams, --- --- UC 36 mos

VOLUME 7
314 n/a Structural Adhesive, 6 ounce N Scotch-Weld EC-3448 60 minutes --- F MD

Replaces CM95 at 250° F
(121° C)
316 n/a Thinner, gallon N MIL-T-81772B Type III Thinner --- --- UC ---
Chemsol/Sherwin Williams
1000-7406

61-01-02
Rev. 54 Nov/23
Page 1-55
Table 1-1
317 A-6741-317 Paint, Polane®, Ghost Gray, Y Sherwin-Williams, --- --- UC 24 mos
gallon F63TXA27973-4311, DOM
FED STD 36375
A-6741-317-1 Paint, Polane®, Ghost Gray, Y Sherwin-Williams, --- --- UC 24 mos

quart F63TXA27973-4311 DOM
FED STD 36375
318 n/a Primer Sealer, gallon N Sherwin-Williams, E65-A-4 --- --- UC 36 mos
Alternate - CM29 DOM
n/a Primer Sealer, quart N Sherwin-Williams, E65-A-4 --- --- UC 36 mos

Alternate - CM29 DOM
335 A-6741-335 Composite Blade Cosmetic Y Sherwin-Williams 1007-10490 1-2 --- UC 24 mos
Touch-up Kit hours DOM
341 A-6741-341 Corrosion Inhibitor Y Anticorit 307 “Winsor 307” --- --- UC ---
VOLUME 7
A-6741-341-2 Corrosion Inhibitor Y Anticorit SV 70386 HF --- --- UC ---
A-6741-341-3 Corrosion Inhibitor Y Anticorit DFW 7301 --- --- UC ---

61-01-02
Rev. 55 Apr/24
Page 1-56
Table 1-1
A-6741-341-2 Corrosion Inhibitor Y Anticorit SV 70386 HF --- --- UC ---
A-6741-341-3 Corrosion Inhibitor Y Anticorit DFW 7301 --- --- UC ---
342 A-6741-342 Solvent, Loctite SF 768 Y Loctite SF 768 Clean Up Solvent --- --- RT ---
Alternate - Loctite 768 X-NMS
Cleanup Solvent
343 A-6741-343 Tubing, Heat Shrink, Roll Y Alpha Wire Fit 105-3/32 --- --- UC 12 mos
AMS-DTL-23053/2 Class 1 DOS
exc Longitudinal Shrinkage
344 A-6741-344 Silicone Foam Sheet, 12” X 12” Y McMaster Carr 8785K86 --- --- UC ---
Extra Soft
345 A-6741-345 Compound, Anti-Corrosion, Y Lear Chemical --- --- RT 24 mos

13 ounce ACF-50 Anti-Corrosion DOM
Compound
346 A-6741-346 Polishing Cmpd, 200 Grit, N 200 Grit Formax Mfg. Corp --- --- UC ---
VOLUME 7

61-01-02
Rev. 54 Nov/23
Page 1-57
Table 1-1
Formax Satin-Glo Greaseless Polishing
Compound
A-6741-346-1 Polishing Cmpd 240 Grit, N 240 Grit Formax Mfg. Corp. --- --- UC ---
Formax Satin-Glo Greaseless Polishing
Compound
A-6741-346-2 Polishing Cmpd 200 Gr, N 200 Grit Jackson Lea --- --- UC ---
Jackson Greaseless Abrasive
Composition
A-6741-346-3 Polishing Cmpd 240 Gr, N 240 Grit Jackson Lea --- --- UC ---
Jackson Greaseless Abrasive
Composition
352 n/a Corrosion Inhibitor, N Chemetall Aerospace 3 hours --- RT 36 mos

13 ounce Aerosol Technologies/Ardrox AV30 at ambient DOS
n/a Corrosion Inhibitor, N Chemetall Aerospace 3 hours --- RT 36 mos

1 liter liquid Technologies/Ardrox AV30 at ambient DOS
VOLUME 7
360 A-6741-360 Shim Stock, Plastic Y Precision Brand/Grainger --- --- UC ---
Grainger P/N 3L881
Mfr. Model #44905
361 A-6741-361 Oil, quart Y Mobil Jet Oil II --- --- UC ---

61-01-02
Rev. 54 Nov/23
Page 1-58
Table 1-1
367 A-6741-367 Nozzle, Mixing Y 3M, #62-9154-9148-4 --- --- UC ---
368 A-6741-368 Torque Marker, Dykem, Y Dykem / 83314 --- --- RT ---
1 ounce tube
399 A-6741-399 Threadlocker, 1.69 fluid ounce Y Loctite, 243 --- --- RT MD
410 A-6741-410 Washer Primer, Gallon Y Sherwin Williams E90G16 --- --- UC MD
MIL-C-8514
411 A-6741-411 Catalyst, Wash Primer, Quart Y Sherwin Williams V93V17 --- --- UC MD
MIL-C-8514
412 A-6741-412 Alcohol, Isopropyl, Gallon N Alternate: --- --- UC ---

99% Minimum Sherwin Williams R6K20
VOLUME 7

61-01-02
Rev. 55 Apr/24
Page 1-59
Table 1-1
VOLUME 7

Rev. 55 Apr/24
VOLUME 7
VENDOR CROSS REFERENCE
The information that was in this chapter is now in Hartzell Propeller Standard Practices
Manual 202A (61-01-02), Volume 6.
VENDOR CROSS REFERENCE 61-01-02 Page 2-1

Rev. 55 Apr/24
VOLUME 7
VENDOR CROSS REFERENCE 61-01-02 Page 2-2

Rev. 55 Apr/24
VOLUME 7
PACKAGING AND STORAGE - CONTENTS
1. Packaging and Storage Guidelines.........................................................................3-3

A. General...............................................................................................................3-3
2. Packaging and Storage of Parts Shipped From Hartzell Propeller LLC..................3-5
3. Packaging and Storage of a Governor Assembly Shipped
From Hartzell Propeller LLC....................................................................................3-6
A. Overview............................................................................................................3-6
B. General ..............................................................................................................3-6
C. Inspecting a Governor That Has Been in Storage and Will Be
Returned to Storage...........................................................................................3-7
D. Activating a Governor Assembly That Has Been in Short Term Storage...........3-8
E. Activating a Governor Assembly That Has Been in Long Term Storage............3-8
4. Packaging and Storage of a Propeller Assembly Shipped From
Hartzell Propeller LLC ...........................................................................................3-10
A. Standard Packaging.........................................................................................3-10
B. Preservation Packaging for a Propeller Assembly........................................... 3-11
5. Inspecting a Propeller Assembly That Has Been in Storage and
Will Be Returned to Storage..................................................................................3-13
A. General.............................................................................................................3-13
B. Procedure.........................................................................................................3-13
6. Activating a Propeller Assembly After Storage......................................................3-14
A. General.............................................................................................................3-14
B. Activating a Propeller Assembly That Has Been in Short Term Storage..........3-14
C. Activating a Propeller Assembly That Has Been in Long Term Storage...........3-16
7. Packaging Guidelines When Sending a Propeller to a Repair Station..................3-18
A. General.............................................................................................................3-18
B. Guidelines........................................................................................................3-18
8. Preservation Packaging Instructions for Storage or Shipping of a Propeller.........3-19
A. General.............................................................................................................3-19
B. Materials And Tools..........................................................................................3-19
C. Procedure.........................................................................................................3-21
61-01-02
Page 3-1
PACKAGING AND STORAGE Rev. 55 Apr/24
VOLUME 7
PACKAGING AND STORAGE - CONTENTS, CONTINUED
9. Packaging of Propellers Shipping with Partially Disassembled

Aircraft/Intermodal Containers...............................................................................3-29
A. General.............................................................................................................3-29
B. Materials And Tools..........................................................................................3-30
C. Procedure.........................................................................................................3-30
LIST OF FIGURES
Wooden Shipping Box..............................................................Figure 3-1....................3-20
Putting the Propeller on the Foam Blocks................................Figure 3-2....................3-20
Conforming the Paper..............................................................Figure 3-3....................3-22
Forming a Wrap Around the Propeller......................................Figure 3-4....................3-22
Protecting the Blade Tips.........................................................Figure 3-5....................3-24
Securing the Box Containing the Beta Valve Assembly...........Figure 3-6....................3-24
Making a Cage for the Propeller...............................................Figure 3-7....................3-25
Attaching the Propeller Owner's Manual Logbook...................Figure 3-8....................3-25
Attaching the Lid.......................................................................Figure 3-9....................3-26
Shipping Information on the Wooden Shipping Box.................Figure 3-10..................3-26
PACKAGING AND STORAGE 61-01-02 Page 3-2

Rev. 54 Nov/23
VOLUME 7
1. Packaging and Storage Guidelines
CAUTION: INSTRUCTIONS AND PROCEDURES IN THIS CHAPTER

MAY INVOLVE PROPELLER CRITICAL PARTS. REFER TO
THE INTRODUCTION CHAPTER OF THIS MANUAL FOR
INFORMATION ABOUT PROPELLER CRITICAL PARTS. REFER
TO THE ILLUSTRATED PARTS LIST CHAPTER OF THE
APPLICABLE OVERHAUL MANUAL(S) FOR THE IDENTIFICATION
OF SPECIFIC PROPELLER CRITICAL PARTS.
NOTE: For criteria for preferred conditions, refer to the section "Environmental
Conditions" in this chapter.
A. General
(1) For packaging and storage requirements for parts, refer to the section,
"Packaging and Storage Parts Shipped from Hartzell Propeller LLC"
(2) For packaging and storage requirements for a governor assembly, refer to
the section, "Packaging and Storage of a Governor Assembly Shipped from
Hartzell Propeller LLC"
(3) For packaging and storage requirements for a Propeller Assembly, refer to
the section, "Packaging and Storage of a Propeller Assembly Shipped From
Hartzell Propeller LLC"
(4) Hartzell Propeller LLC does not warrant propellers against corrosion if they
are stored outside of the "Preferred Conditions" outlined below. The following
storage criteria is considered "Preferred Conditions":
(5) Environmental Conditions
(a) Annually evaluate the propeller storage conditions to confirm the
environment still meets the preferred conditions.
1 If the storage area evaluation indicates possible problems, inspect
the propeller in accordance with the section, "Inspecting a Propeller
Assembly That Has Been in Storage and Will Be Returned to
Storage".
(b) Criteria for "Preferred Conditions":
1 Low humidity environment
a Storage facility average humidity is maintained below 85%
2 Salt-free environment
a Storage facility salt levels are less than 0.8 NaCl/dm^2
NOTE: In general, NaCl air content drops to acceptable levels
at 400 meters from ocean/salt water.
61-01-02
Page 3-3
VOLUME 7
3 Non-corrosive environment
a The product is stored in a separate facility from corrosive
chemicals
4 Negligible air pollution exposure
a Average Air Quality Index (AQI) rating below 100
5 Stable storage temperatures
a Acceptable storage temperature conditions are dependent on
the humidity level, but wide temperature fluctuations of +/- 50° F
(+/- 10° C) should be avoided.
b Propeller storage container temperatures must be less than
150° F (66° C).
(6) Short Term Storage Definition
(a) Propeller stored for less than two years in standard packaging in preferred
conditions
(b) Propeller stored for less than four years in preservation packaging in
preferred conditions
(7) Long Term Storage Definition
(a) Propeller stored for more than two years in standard packaging in
(b) Propeller stored for more than four years in preservation packaging in

Rev. 54 Nov/23
VOLUME 7
2. Packaging and Storage of Parts Shipped From Hartzell Propeller LLC

A. Important Information
(1) This section provides information about the use of Hartzell Propeller standard
packaging for parts shipped from Hartzell Propeller LLC.
(a) Parts shipped from Hartzell Propeller LLC do not include propeller
assemblies or governor assemblies.
(b) The term "Standard Packaging" refers to the standard packaging used by
Hartzell Propeller for shipment of parts from Hartzell Propeller LLC.
1 This standard packaging is not designed for use as a container for
long-term storage.
2 The standard packaging is designed to preserve the part under
preferred conditions for six months.
3 Non-preferred conditions can reduce the storage time.
(c) Hartzell Propeller LLC is not responsible for a part stored in preferred
conditions for more than six months using standard packaging.
(d) Hartzell Propeller LLC is not responsible for a part stored in non-preferred
conditions for more than thirty days using standard packaging.
(e) Hartzell Propeller LLC is not responsible for a part repackaged and stored.
(f) Standard packaging is intended for protection during non-ocean
surface freight transit only and for storage that is dependent on certain
environmental conditions.
1 For information about standard packaging, refer to the section,
"Standard Packaging" in this chapter.
2 For information about environmental conditions, refer to the section,
"Environmental Conditions" in this chapter.
(g) Hartzell Propeller LLC does not provide "Preservation Packaging" for parts
shipped from Hartzell Propeller LLC.
(h) Inspection for Individual Parts That are Stored in Standard Packaging
1 Hartzell Propeller LLC requires that the stored parts be inspected
every six months to make sure that corrosion is not developing.
a When the parts are inspected, if applicable, replace the
desiccant bag or corrosion preventative.
61-01-02
Page 3-5
VOLUME 7
3. Packaging and Storage of a Governor Assembly Shipped from Hartzell Propeller LLC
A. Overview
(1) The governor is lubricated and stored in a sealed plastic bag when shipped
from Hartzell Propeller LLC.
(a) This standard packaging is not designed for use as a container for
long-term storage.
(b) The packaging is designed to preserve the governor under preferred
conditions for less than two years.
(c) Non-preferred conditions can reduce the storage time.
(2) Hartzell Propeller LLC will guarantee a governor stored for less than two years
when stored in the original Hartzell Propeller LLC packaging and the sealed
bag is still sealed.
(3) Hartzell Propeller LLC is not responsible for a governor stored for more than
two years when stored in the original Hartzell Propeller LLC packaging and the
sealed bag is still sealed.
(4) Hartzell Propeller LLC is not responsible for a governor stored for more
than thirty days in non-preferred conditions if the original Hartzell Propeller
packaging and the sealed bag has been opened.
(5) Hartzell Propeller LLC is not responsible for a governor repackaged
and stored.
B. General
(1) A flight hour/calendar limit between overhauls is specified by Hartzell
Propeller LLC. Refer to Hartzell Propeller Service Letter HC-SL-61-61Y.
(a) The start date for the flight hour/calendar limit is when the governor is first
installed on an engine.
(2) These procedures apply to new governors, governors with zero hours since
overhaul, and governors with time-in-service that have been in long-term
storage.
(3) The start date for long-term storage begins at the original ship date, the date
of overhaul, or the date the governor was removed from the aircraft, whichever
occurs last.

Rev. 55 Apr/24
VOLUME 7
C. Activating A Governor Assembly That Has Been in Short Term Storage

(1) For the procedures for activating a governor, refer to the section, "Activating
a Governor Assembly That Has Been in Short Term Storage" or the section,
"Activating a Governor Assembly That Has Been in Long Term Storage", as
applicable.
(2) General
(a) A governor that has been in short term storage is:
1 A governor that has been in storage for less than two years and is
stored in the original Hartzell Propeller packaging and the sealed bag
is still sealed
2 A governor that has been in storage for less than thirty days but the
original Hartzell Propeller packaging and the sealed bag have been
opened
(b) For a governor in storage, if the governor calendar limit is more than the
calendar limits specified in Hartzell Propeller Service Letter HC-SL-61-61Y,
overhaul the governor before further flight.
1 New governors, governors with zero hours, or governors with time in
service and the calendar limit has not been exceeded do not require
overhaul.
(3) Procedure
(a) Remove the governor from the sealed bag.
(b) Visually examine the governor for corrosion and damage.
1 If there is corrosion or damage, repairs must be performed by a
certified governor service facility in accordance with Hartzell
Propeller Mechanically Actuated Governors and Accessories
Maintenance Manual 130B (61-23-30).
2 If corrosion or damage is not found, lubricate the governor with oil
and seal in a plastic bag.
(c) Review current FAA Airworthiness Directives and Hartzell Propeller
Service Documentation.
1 There may be documents that have been issued since the date that
the governor was put into storage.
a Compliance with documents that have been issued since the
date that the governor was put into storage is required.
(d) Return the governor in the sealed bag to storage.
61-01-02
Page 3-7
VOLUME 7
D. Activating a Governor Assembly That Has Been in Short Term Storage

(1) General
(a) A governor that has been in short term storage is:
1 A governor that has been in storage for less than two years and is
is still sealed
2 A governor that has been in storage for less than thirty days but the
opened
(b) For a governor in storage, if the governor calendar limit is more than the
overhaul the governor before further flight.
1 New governors, governors with zero hours, or governors with time in
service and the calendar limit has not been exceeded do not require
overhaul.
(2) Procedure
(a) Remove the governor from the sealed bag.
(b) Visually examine the governor for corrosion and damage.
(c) Review current FAA Airworthiness Directives and Hartzell Propeller
(d) Return the governor to service.
E. Activating a Governor Assembly that has been in Long Term Storage
(1) General
(a) A governor that has been in long term storage is:
1 A governor that has been in storage for more than two years and is
is still sealed
2 A governor that has been in storage for more than thirty days but the
opened

Rev. 55 Apr/24
VOLUME 7
(2) Procedure
(a) The requirements in this section must be completed by a certified
governor service facility in accordance with Hartzell Propeller
Mechanically Actuated Governors and Accessories Maintenance
Manual 130B (61-23-30).
(b) Remove the governor from the sealed bag.
(c) Visually examine the governor internally and externally for damage or
corrosion.
1 Removal of paint and plating is not required.
3 Replace all seals (O-ring, seal washer, gaskets, etc.).
(d) The governor must be tested in compliance with the Assembly and Testing
chapter of Hartzell Propeller Mechanically Actuated Governors and
Accessories Maintenance Manual 130B (61-23-30).
1 If test results do not meet the requirements, a complete governor
overhaul must be performed.
(e) Governors stored longer than five years in standard packaging require an
internal seal replacement.
(1) The governor must be tested in accordance with the Assembly
and Testing chapter of Hartzell Propeller Mechanically Actuated
Governors and Accessories Maintenance Manual 130B (61-23-30).
(a) If the test results do not meet the requirements, a complete
governor overhaul must be performed.
(f) Review current FAA Airworthiness Directives and Hartzell Propeller
(g) Return the governor to service.
61-01-02
Page 3-9
VOLUME 7
4. Packaging and Storage of a Propeller Assembly Shipped From Hartzell Propeller LLC
A. Standard Packaging
CAUTION: STANDARD PACKAGING IS NOT RECOMMENDED WHEN

SHIPPING BY OCEAN SURFACE FREIGHT. PRESERVATION
PACKAGING IS HIGHLY RECOMMENDED FOR PROPELLER
PROTECTION DURING TRANSIT BY OCEAN SURFACE FREIGHT.
(1) The term "Standard Packaging" refers to the standard packaging used by
Hartzell Propeller for shipment of a propeller assembly from Hartzell
Propeller LLC.
(a) Standard packaging is intended for propeller protection during non-ocean
surface freight transit only and for storage that is dependent on certain
1 For information about environmental conditions, refer to the section
(2) Standard packaging is not intended for:
(a) Propeller storage that is more than 30 days in non-preferred conditions
(b) Propeller storage that is more than two years in preferred conditions
(3) Hartzell Propeller LLC will guarantee a propeller stored in the original standard
packaging in confirmed preferred conditions for up to six months from the date
that the propeller was originally shipped from Hartzell Propeller LLC.
(4) Hartzell Propeller LLC will guarantee a propeller stored in the original standard
packaging in non-preferred conditions for up to 30 days from the date that the
propeller was originally shipped from Hartzell Propeller LLC.
(5) Hartzell Propeller LLC is not responsible for corrosion on a propeller that is
stored in standard packaging for more than six months in preferred conditions
or more than 30 days in non-preferred conditions.
(6) Inspection for a Propeller that is Stored in Standard Packaging and will be
Returned to Storage
(a) When a propeller has been stored for two years, the propeller must
be removed from the standard packaging, inspected, and resealed in
accordance with the section, "Inspecting a Propeller Assembly That Has
Been in Storage and Will Be Returned to Storage" in this chapter.
1 After compliance with the section, "Inspecting a Propeller Assembly
That Has Been in Storage and Will Be Returned to Storage" in
this chapter, the propeller should be repackaged using appropriate
packaging.
(a) To determine the correct packaging to be used, refer to the
sections, "Environmental Conditions", "Standard Packaging", and
"Preservation Packaging for a Propeller Assembly" in this chapter.

Rev. 55 Apr/24
VOLUME 7
2 Without prior written agreement, Hartzell Propeller LLC is not

responsible for corrosion on propellers repackaged after leaving
Hartzell Propeller LLC.
(7) When activating a propeller that has been in storage, follow the applicable
steps in the section "Activating a Propeller After Storage" in this chapter.
B. Preservation Packaging for a Propeller Assembly
CAUTION: PRESERVATION PACKAGING IS HIGHLY RECOMMENDED

FOR PROTECTION OF THE PROPELLER DURING TRANSIT
BY OCEAN SURFACE FREIGHT.
(1) Preservation Packaging
(a) The term "Preservation Packaging" refers to the specific preservation
packaging used by Hartzell Propeller for shipment of a propeller assembly
from Hartzell Propeller LLC.
(b) Preservation packaging is intended for propeller protection during
ocean surface freight and for storage that is dependent on certain
1 For information about environmental conditions, refer to the section
(2) Preservation packaging is intended for:
(a) Propeller protection during transit by ocean surface freight
(b) Propeller storage up to two years in non-preferred conditions
(c) Propeller storage up to four years in preferred conditions.
(3) Hartzell Propeller LLC is not responsible for corrosion on propellers shipped by
ocean surface freight without preservation packaging.
(4) Hartzell Propeller LLC recommends preservation packaging for:
(a) A propeller that will be stored more than 30 days in non-preferred
conditions
(b) A propeller that will be stored for more than two years in preferred
conditions
(c) A propeller that will be shipped with a partially disassembled aircraft
(d) For preservation packaging instructions, refer to the section "Preservation
Packaging Instructions for Storage or Shipping of a Propeller" in this
chapter.
(5) A propeller should never be stored in preservation packaging for more than four
years, even under preferred conditions.
61-01-02
Page 3-11
VOLUME 7
(6) If the propeller is stored under confirmed preferred conditions, Hartzell

Propeller LLC will guarantee a propeller stored in the original Hartzell
Propeller preservation packaging for up to four years from the date the
propeller was originally shipped from Hartzell Propeller LLC.
(7) If the propeller is stored under non-preferred conditions, Hartzell
Propeller LLC will guarantee a propeller stored in the original Hartzell
Propeller preservation packaging for up to two years from the date the propeller
was originally shipped from Hartzell Propeller LLC.
(8) Hartzell Propeller LLC is not responsible for corrosion on a propeller
that is stored in the original Hartzell Propeller preservation packaging for more
than four years in preferred conditions or for more than two years in
non-preferred conditions.
(9) When a propeller has been stored for two years in non-preferred conditions, the
propeller must be removed from the preservation packaging, inspected, and
resealed in accordance with the section, "Inspecting a Propeller Assembly that
has Been in Storage" in this chapter.
(a) If the propeller is repackaged after the removal from the preservation
packaging, inspection, and reseal, appropriate packaging should be used.
1 To determine the correct packaging to be used, refer to the
sections "Environmental Conditions", "Standard Packaging", and
"Preservation Packaging for a Propeller Assembly" in this chapter.
(b) Without prior written agreement, Hartzell Propeller LLC is not responsible
for corrosion on propellers repackaged after leaving Hartzell Propeller LLC.
(10) When a propeller has been stored for four years in preferred conditions, the
propeller must be removed from the preservation packaging, inspected, and
resealed in accordance with the section, "Inspecting a Propeller Assembly That
Has Been in Storage" in this chapter.
(a) If the propeller is repackaged after the removal from the preservation
packaging, inspection, and reseal, appropriate packaging should
be used.
1 To determine the correct packaging to be used, refer to the
sections "Environmental Conditions", "Standard Packaging", and
"Preservation Packaging" in this chapter.
(b) Without prior written agreement, Hartzell Propeller LLC is not responsible
for corrosion on propellers repackaged after leaving Hartzell Propeller LLC.

Rev. 55 Apr/24
VOLUME 7
5. Inspecting a Propeller Assembly That Has Been in Storage and Will Be Returned
to Storage
A. General
(1) The requirements in this section must be completed by a certified propeller
repair station with the appropriate rating in accordance with the applicable
Hartzell Propeller LLC instruction or overhaul manual.
(2) This procedure applies to:
(a) A propeller that has been in storage for two years in standard packaging
(b) A propeller that has been in storage for two years in preservation
packaging in non-preferred conditions
(c) A propeller that has been in storage for four years in preservation
packaging in preferred conditions
(3) The inspections in this section are for a propeller that will be returned to storage.
(a) If the propeller will be activated instead of stored, follow the steps in the
section, "Activating a Propeller Assembly That Has Been in Storage" in
this chapter.
B. Procedure
(1) Using a clean cloth soaked with solvent CM109, remove the corrosion
preventative that may have been added at the time of storage.
(2) Visually examine the propeller externally for damage or corrosion.
(a) Removal of paint and plating is not required.
(b) Total disassembly of the propeller, such as removing the counterweights,
is not necessary unless there is corrosion or damage.
1 If there is corrosion or damage, refer to the Check chapter of the
applicable propeller overhaul manual.
(c) Make sure that the boots are still bonded with no signs of blistering or
peeling in accordance with Hartzell Propeller Ice Protection System
Manual 180 (30-61-80), as applicable.
(3) Repaint and/or replate components as required.
(4) When the propeller is repackaged after the removal from the standard
packaging or preservation packaging, inspected, and resealed, the appropriate
packaging should be used.
(a) To determine the correct packaging to be used, refer to the sections
"Environmental Conditions", "Standard Packaging", and "Preservation
Packaging" in this chapter.
(5) Without prior written agreement, Hartzell Propeller LLC is not responsible for
corrosion on propellers repackaged after leaving Hartzell Propeller LLC.
61-01-02
Page 3-13
VOLUME 7
6. Activating a Propeller Assembly After Storage

A. General
(1) A flight hour/calendar limit between overhauls is specified by Hartzell
Propeller LLC. Refer to Hartzell Propeller Service Letter HC-SL-61-61Y.
(a) The start date for the flight hour/calendar limit is when the propeller is first
installed on an engine.
(2) These procedures apply to new propellers, propellers with zero hours since
overhaul, and propellers with time-in-service that have been in storage.
(3) The start date for storage begins at the date of shipment from Hartzell
Propeller LLC, the date of last overhaul or the date the propeller was removed
from the aircraft and placed in storage, whichever occurred last.
(4) For the procedures for activating a propeller, refer to the section, "Activating
a Propeller Assembly That Has Been in Short Term Storage" or the section,
"Activating a Propeller Assembly That Has Been in Long Term Storage", as
applicable.
B. Activating a Propeller Assembly That Has Been in Short Term Storage
NOTE: For criteria for preferred conditions, refer to the section "Environmental
Conditions" in this chapter.
(1) General
(a) A propeller that has been in short term storage is:
1 A propeller that has been in storage for less than thirty days in
standard packaging in non-preferred conditions
2 A propeller that has been in storage for less than two years in
standard packaging in preferred conditions
3 A propeller that has been in storage for less than two years in
preservation packaging in non-preferred conditions
4 A propeller that has been in storage for less than four years in
preservation packaging in preferred conditions
(b) For a propeller in storage with time in service, if the propeller calendar limit
is more than the calendar limits specified in Hartzell Propeller Service
Letter HC-SL-61-61Y, overhaul the propeller before further flight.
1 New propellers, propellers with zero hours time since overhaul, or
propellers with time in service and the calendar limit has not been
exceeded do not require overhaul.

Rev. 55 Apr/24
VOLUME 7
WARNING: ADHESIVES AND SOLVENTS ARE FLAMMABLE AND TOXIC

TO THE SKIN, EYES, AND RESPIRATORY TRACT. SKIN AND
EYE PROTECTION ARE REQUIRED. AVOID PROLONGED
CONTACT AND BREATHING OF VAPORS. USE SOLVENT
RESISTANT GLOVES TO MINIMIZE SKIN CONTACT AND
WEAR SAFETY GLASSES FOR EYE PROTECTION. USE IN A
WELL VENTILATED AREA AWAY FROM SPARKS AND FLAME.
READ AND OBSERVE ALL WARNING LABELS.
(2) Procedure
(a) Using a clean cloth soaked with solvent CM109, remove the corrosion
(b) Make a general visual examination of the condition of the parts.
1 As necessary, rework and correct any questionable conditions. Refer
to the Check chapter of the applicable propeller overhaul manual.
(c) Test the ice protection system including the de-ice or anti-icing boots in
accordance with Hartzell Propeller Ice Protection System Manual 180
(30-61-80).
1 Make sure that the boots are still correctly bonded with no signs
of blistering or peeling in accordance with Hartzell Propeller Ice
Protection System Manual 180 (30-61-80), as applicable.
2 If the propeller is equipped with an ice protection system that
uses components supplied by Hartzell Propeller LLC, applicable
instructions and technical information for the components supplied
by Hartzell Propeller LLC can be found in Hartzell Propeller Ice
Protection System Manual 180 (30-61-80), available on the Hartzell
Propeller website at www.hartzellprop.com.
3 Propeller ice protection system components not supplied by Hartzell
Propeller LLC are controlled by the applicable TC or STC holder’s
Instructions for Continued Airworthiness (ICA).
(d) Review current FAA Airworthiness Directives and Hartzell Propeller
1 Compliance with documents that have been issued since the date
that the propeller was put into storage is required.
(e) After accomplishing the required procedures, the propeller may be
released for the remaining overhaul and flight and calendar time.
61-01-02
Page 3-15
VOLUME 7
C. Activating a Propeller Assembly That Has Been in Long Term Storage

(1) General
(a) A propeller that has been in long term storage is:
1 A propeller that has been in storage for more than two years in
standard packaging
2 A propeller that has been in storage for more than two years in
preservation packaging in non-preferred conditions
3 A propeller that has been in storage for more than four years in
preservation packaging in preferred conditions
(b) The requirements in this section must be completed by a certified propeller
repair station with the appropriate rating in accordance with the applicable
Hartzell Propeller instruction or overhaul manual.
(c) For a propeller in storage, if the propeller calendar limit is more than the
overhaul the propeller before further flight.
1 New propellers, propellers with zero hours in service since overhaul,
or propellers with time in service and the calendar limit has not been
exceeded do not require overhaul.
(d) A customer/end user may remove the propeller from long term storage
and overhaul it in accordance with this section.
1 The propeller can then be stored for up to two years, installed on an
aircraft, if needed, during that two year storage period.
(2) Procedure
(a) Using a clean cloth soaked with solvent CM109, remove the corrosion
(b) Visually examine the propeller internally and externally for damage or
corrosion.
1 Removal of paint and plating is not required.
2 Total disassembly of the propeller assembly, such as removing
counterweights, is not necessary unless there is corrosion
or damage.
a If there is corrosion or damage, refer to the Check chapter of the
applicable propeller overhaul manual.
(c) Replace all seals (O-rings, seal washers, gaskets, etc.).
(d) Replace the lubricant in accordance with the Propeller Lubrication chapter
of Hartzell Propeller Standard Practices Manual 202A (61-01-02).

Rev. 55 Apr/24
VOLUME 7
(e) Test the ice protection system including the de-ice or anti-icing boots in
accordance with Hartzell Propeller Ice Protection System Manual 180
(30-61-80).
1 Make sure that the boots are still correctly bonded with no signs
of blistering or peeling in accordance with Hartzell Propeller Ice
Protection System Manual 180 (30-61-80), as applicable.
2 If the propeller is equipped with an ice protection system that
uses components supplied by Hartzell Propeller LLC, applicable
instructions and technical information for the components supplied
by Hartzell Propeller LLC can be found in Hartzell Propeller Ice
Protection System Manual 180 (30-61-80), available on the Hartzell
Propeller website at www.hartzellprop.com.
3 Propeller ice protection system components not supplied by Hartzell
Propeller LLC are controlled by the applicable TC or STC holder’s
Instructions for Continued Airworthiness (ICA).
(f) Repaint and/or replate components as required.
(g) Review current FAA Airworthiness Directives and Hartzell Propeller
1 Compliance with documents that have been issued since the date
that the propeller was put into storage is required.
(h) After accomplishing the required procedures, the propeller may be
released for the remaining overhaul and flight and calendar time.
61-01-02
Page 3-17
VOLUME 7
7. Packaging Guidelines When Sending a Propeller to a Repair Station

A. General
(1) This section provides guidelines for packaging a propeller to send it to a repair
station.
B. Guidelines
(1) The container must support the propeller using the hub, not the bulkhead, the
slip ring, or the beta ring.
(2) Parts must not be loose in the container.
(3) A stand-alone aluminum hub must have both halves attached to each other to
prevent damage.
(a) Optionally, ship each half of the hub in a separate container.
(4) The container must be longer than the blade to permit space for padding
between the container and blade tip.

Rev. 54 Nov/23
VOLUME 7
8. Preservation Packaging Instructions for Storage or Shipping of a Propeller
CAUTION 1: A PROPELLER THAT HAS A DESTINATION THAT WILL REQUIRE

LONG TERM STORAGE OR OCEAN SURFACE FREIGHT SHOULD
BE PACKAGED IN ACCORDANCE WITH THE INSTRUCTIONS
GIVEN IN THIS SECTION.
CAUTION 2: HARTZELL PROPELLER LLC IS NOT RESPONSIBLE FOR

CORROSION THAT MAY DEVELOP ON PROPELLERS THAT
ARE PRESERVATION PACKAGED IN ACCORDANCE WITH THE
INSTRUCTIONS IN THIS SECTION.
CAUTION 3: STANDARD PACKAGING IS NOT RECOMMENDED WHEN

A. General
(1) This section provides instructions for preservation packaging of a propeller
assembly.
(2) This section provides for the procedure used by Hartzell Propeller LLC for
Preservation Packaging of a three blade steel hub propeller.
(3) This section provides instructions for building a wooden shipping box that is
suitable for long term storage or for shipping a propeller.
(a) The wood used to build the wooden shipping box should comply
with international shipping container standard ISPM 15.
B. Materials And Tools
(1) When using the wooden shipping box for storage:
(a) 1/2 inch or 3/8 inch plywood
(b) 1 inch x 4 inch (wood external bracing that is in compliance with ISPM 15)
(c) 4-mil thick Cortec VCI impregnated shrink wrap or equivalent
(d) Closed cell foam padding material
(e) Duct tape or packaging tape
(f) MIL-D-3464, Type I, 16 Units
(g) Nails, screws, and if desired, a latching system
(h) Nox-Rust Vapor Wrapper or equivalent
(i) Black permanent marker
61-01-02
Page 3-19
VOLUME 7
1 inch x 4 inch
1/2 inch or 3/8 inch plywood wood external bracing
Wooden Shipping Box

Figure 3-1
In this Figure
the propeller
is shown in a
box. Put the
propeller in a
similar postion
when using
a shipping
pallet.
Putting the Propeller on the Foam Blocks

Figure 3-2

Rev. 54 Nov/23
VOLUME 7
(2) Additionally, when using the wooden shipping box for shipping:
(a) Method to stamp ISPM 15 compliance symbol
(b) Banding materials - Steel banding, nylon banding or equivalent and the
applicable banding equipment
(c) Liquid adhesive or self-adhering see-through bags and staples
(d) Appropriate shipping label
(e) Stickers with the word "Fragile"
(f) Copy of the applicable forms
C. Procedure
(1) Using materials compliant with international shipping container standard
ISPM 15, build a wooden shipping box of minimum 1/2 inch or 3/8 inch plywood
and 1 x 4 inch (25.4 x 101.6 mm) minimum wood external bracing. Refer to
Figure 3-1.
(a) The internal dimensions of the wooden shipping box with padding
allowance must be of a sufficient size to permit the propeller to rest
securely and permit padding between the blade tips and the sides of the
box.
1 The padding allowance is 2 inches (50.8 mm) minimum on the
top, bottom, and all sides of the wooden shipping box that adds
approximately 4 inches (101.6 mm) in each direction.
2 Extra depth is permitted.
(b) Construct the wooden shipping box with skids on the bottom near both
edges and in the center so that the wooden shipping box can be handled
with a forklift.
(c) Stamp the international shipping container standard ISPM 15 compliance
symbol on at least two opposite sides of the wooden shipping box. Refer
to the ISPM 15 specifications.
(2) Put a layer of 4-mil thick Cortec VCI impregnated shrink wrap across the bottom
of the inside of the wooden shipping box, with the edges of the shrink wrap
lapping over the sides as necessary to have enough material to completely
encase the propeller.
61-01-02
Page 3-21
PACKAGING AND STORAGE Rev. 54 Nov/23
VOLUME 7
In this Figure
the propeller
is shown in a
box. Put the
propeller in a
similar postion
when using
a shipping
pallet.
Conforming the Paper

Figure 3-3
In this Figure
the propeller
is shown in a
box. Put the
propeller in a
similar postion
when using
a shipping
pallet.
Forming a Wrap Around the Propeller

Figure 3-4

Rev. 54 Nov/23
VOLUME 7
(3) Put 2 inches (50.8 mm) of closed cell foam padding materials on the Cortec
VCI impregnated shrink wrap in the bottom of the wooden shipping box.
CAUTION: THE PROPELLER MUST BE SUPPORTED BY THE HUB,

NOT THE BULKHEAD, THE BETA RING, OR THE SLIP RING.
(a) Put one piece of foam padding material that is approximately
15 x 15 inches (381 x 381 mm) on the centerline across the shorter
dimension of the wooden shipping box and center the foam padding
material approximately 1/3 of the way between the opposite sides, so that
the propeller hub flange will be approximately centered on the pad when
put in the box.
1 If necessary, cut material to make a center hole cut-out.
(b) Put pieces of foam padding material, approximately 8 x 8 inches
(203 x 203 mm), under where the blade trail edges will be, positioned from
the hub center so that the foam will contact the blade trail edges, but the
weight of the propeller is still supported by the hub flange.

(4) Put the propeller on the foam padding material with the blade tips equal
distance from the walls of the wooden shipping box.
(5) Wrap the propeller blades in 1/8 inch closed cell foam sheets, covering the
blade tips completely. Refer to Figure 3-2.
(6) Wrap the bag of propeller mounting hardware with foam padding or bubble
wrap.
(7) Attach the wrapped bag to the bottom pad inside of the wooden shipping box.
(8) Put the appropriate amount of desiccant bags in accordance with MIL-D-3464,
Type I, inside the Cortec VCI impregnated shrink wrap.
(9) Put a sheet of Nox-Rust Vapor Wrapper over the hub and piston area of the
propeller, conforming the paper to the general shape of the hub and piston
area. Refer to Figure 3-3.
(10) Fold the Cortec VCI impregnated shrink wrap over the propeller.
(a) Trim the Cortec VCI impregnated shrink wrap as necessary to form a wrap
that will completely cover the propeller assembly. Refer to Figure 3-4.
CAUTION: DO NOT PERMIT TOO MUCH DWELL TIME WITH THE SEALING
TORCH OVER THE ALUMINUM PROPELLER COMPONENTS.
(11) Using a gas sealing torch, seal and shrink the Cortec VCI impregnated shrink
wrap. Refer to Figure 3-4.
61-01-02
Page 3-23
VOLUME 7
Protecting the Blade Tips

Figure 3-5
Securing the Box Containing the Beta Valve Assembly

Figure 3-6

Rev. 54 Nov/23
VOLUME 7
Four-sided
Cage
Making a Cage for the Propeller

Figure 3-7
Owner’s
Manual
& Logbook
box
Attaching the Propeller Owner's Manual Logbook

Figure 3-8
61-01-02
Page 3-25
VOLUME 7
Attaching the Lid

Figure 3-9
Shipping Information on the Wooden Shipping Box

Figure 3-10

Rev. 54 Nov/23
VOLUME 7
(12) Install pieces of 2 inch ( 50.8 mm) closed cell foam to protect the blade tips.
(a) Bend the closed cell foam at the corners to protect the tip of each blade.
(b) Put one piece of closed cell foam between any blade tip and the side wall.
Refer to Figure 3-5.
(c) If the corners of the wooden shipping box are too tight to use the 2 inch
(50.8 mm) foam thickness, it is permitted to neatly cut down the foam
thickness.
1 If the foam thickness is cut, the smooth side of the foam should be
the side contacting the blade tips.
(13) Put a piece of 1/8 inch (3.18 mm) foam sheeting over the top of the Cortec VCI
impregnated shrink wrap covering the piston.
(14) Cut two 2 inch x 4 inch (50.8 mm x 101.6 mm) planks to span the inside of the
wooden shipping box.
(15) Put the 2 inch x 4 inch (50.8 mm x 101.6 mm) planks on opposite sides of the
piston or spinner to hold it with gentle contact against the foam sheet.
(16) Using nails or screws, attach the 2 inch x 4 inch (50.8 mm x 101.6 mm) planks
to the side wall of the wooden shipping box.
(17) Cut two short 2 inch x 4 inch (50.8 mm x 101.6 mm) pieces to hold the piston or
spinner perpendicular to the 2 inch x 4 inch (50.8 mm x 101.6 mm) planks.
(18) Using nails, attach the 2 x 4 inch (25.4 x 101.6 mm) pieces, with light contact
against the foam sheet to form a four-sided “cage” for the piston or spinner.
Refer to Figure 3-7.
NOTE: Figure 3-7 shows a propeller that has a spinner.
(19) Using duct tape or packaging tape, attach the Owner’s Manual & Logbook box
to two of the horizontal 2 x 4 inch (25.4 x 101.6 mm) pieces.
NOTE: Double banding is recommended over the single banding shown in
Figure 3-8.
(20) Cut a 2 x 4 inch (25.4 x 101.6 mm) plank to span the inside of the box.
(21) Cut two plywood pieces of the appropriate size to make a box cover.
(a) To prevent interference with the “cage” structure, the seam of the lid
pieces must not be on the propeller centerline.
(22) Using nails or screws, attach the plank to the side walls in position to support
the two lid pieces below the seam between them.
(23) Using nails, screws, or a latching system, attach the lid pieces in place along all
the outer edges and along the supporting plank. Refer to Figure 3-9.
(a) To prevent interference with the “cage” structure, the seam of the lid
pieces must not be on the propeller centerline.
61-01-02
Page 3-27
VOLUME 7
(24) When shipping the propeller, use the following steps:

(a) Using banding material, band the box in two places on opposite sides of
the box.
(b) Using a black permanent marker, identify the contents of the box, as
appropriate.
(c) Using a black permanent marker, write the following instructions on at
least two sides of the wooden shipping box: Refer to Figure 3-10.
1 Box orientation (“Up” with an arrow )
2 “Handle With Care”
(d) Using liquid adhesive or self-adhering transparent bags attached with
staples as appropriate, attach the following documents to the side of the
wooden shipping box:
1 Appropriate shipping label
2 “Fragile” stickers

Rev. 54 Nov/23
VOLUME 7
9. Packaging of Propellers Shipping with Partially Disassembled Aircraft/Intermodal

Containers
CAUTION 1: IF THE PROPELLER WILL BE PUT IN LONG TERM STORAGE

AFTER THE ARRIVAL TO THE FINAL DESTINATION OF
THE PROPELLER, USE THE PRESERVATION PACKAGING
INSTRUCTIONS IN SECTION 8 OF THIS MANUAL. THIS
INSTRUCTION IS INTENDED FOR PREVENTION OF CORROSION
ON PROPELLERS DURING SHIPMENT WITH A PARTIALLY
DISASSEMBLED AIRCRAFT/INTERMODAL CONTAINERS.
HARTZELL PROPELLER LLC INTENDS FOR THE PROPELLER(S)
THAT WAS PACKAGED IN ACCORDANCE WITH THIS SECTION
TO BE REMOVED AND INSTALLED ONTO THE ASSEMBLED
AIRCRAFT UPON ITS ARRIVAL AT THE FINAL DESTINATION.
CAUTION 2: A PROPELLER THAT HAS A DESTINATION THAT WILL REQUIRE

OCEAN SURFACE FREIGHT SHOULD BE PACKAGED IN
ACCORDANCE WITH THE INSTRUCTIONS GIVEN IN THIS
SECTION.
CAUTION 3: HARTZELL PROPELLER LLC IS NOT RESPONSIBLE FOR

CORROSION THAT MAY DEVELOP ON PROPELLERS THAT
ARE PRESERVATION PACKAGED IN ACCORDANCE WITH THE
INSTRUCTIONS IN THIS SECTION.
CAUTION 4: STANDARD PACKAGING IS NOT RECOMMENDED WHEN

A. General
(1) This section requires removal of the propeller from the aircraft before
preservation packaging of a propeller assembly.
(2) This section provides procedures recommended by Hartzell Propeller LLC for
Preservation Packaging of a propeller that has been removed from the aircraft
and that will be shipped on a shipping pallet in a shipping container.
(3) This section provides instructions for attaching a propeller assembly to a
shipping pallet that is suitable for use in a shipping container.
61-01-02
Page 3-29
VOLUME 7
B. Materials And Tools

(1) When shipping a propeller assembly in a shipping container:
(a) 4-mil thick Cortec VCI impregnated shrink wrap or equivalent
(b) Closed cell foam padding material
(c) Duct tape or packaging tape
(d) MIL-D-3464, Type I, 16 Units
(e) Plastic tie straps
(f) Nox-Rust Vapor Wrapper or equivalent
(g) Black permanent marker
C. Procedure
(1) The dimensions of the shipping pallet with padding allowance must be of a
sufficient size to permit the propeller to rest safely and permit padding between
the blade tips and the sides of the shipping container.
(a) The padding allowance between the blade tips and the sides of the
shipping container should be approximately 4 inches (101.6 mm) in each
direction.
(b) The shipping pallet should have skids on the bottom near both edges and
in the center so that the shipping pallet can be handled with a forklift.
(2) Put a layer of 4-mil thick Cortec VCI impregnated shrink wrap across the
shipping pallet, with enough of the shrink wrap lapping over the sides as
necessary to have enough material to completely encase the propeller.
(3) Put 2 inches (50.8 mm) of closed cell foam padding materials on the Cortec
VCI impregnated shrink wrap in the center of the shipping pallet.

(a) Put one piece of foam padding material that is approximately
15 x 15 inches (381 x 381 mm) on the centerline across the shorter
dimension of the shipping pallet and center the foam padding material
approximately 1/3 of the way between the opposite sides, so that the
propeller hub flange will be approximately centered on the pad when put
on the pallet. Refer to Figure 3-2.
1 If necessary, cut material to make a center hole cut-out.
(b) Put pieces of foam padding material, approximately 8 x 8 inches
(203 x 203 mm), where the blade trail edges will be, positioned from the
hub center so that the foam will contact the blade trail edges, but the
weight of the propeller is still supported by the hub flange Refer to
Figure 3-2.

Rev. 54 Nov/23
VOLUME 7

(4) Put the propeller on the foam padding material with the blade tips equal
distance from the edges of the shipping pallet. Refer to Figure 3-2.
(5) Wrap the propeller blades in 1/8 inch (3.18 mm) closed cell foam sheets,
covering the blade tips completely. Refer to Figure 3-2.
(6) Wrap the bag of propeller mounting hardware with foam padding or bubble
wrap.
(7) Attach the wrapped bag to the bottom of the shipping pallet.
(8) Put the appropriate amount of desiccant bags in accordance with MIL-D-3464,
Type I, inside the Cortec VCI impregnated shrink wrap.
(9) Put a sheet of Nox-Rust Vapor Wrapper over the hub and piston area of the
propeller, conforming the paper to the general shape of the hub and piston
area. Refer to Figure 3-3.
(10) Fold the Cortec VCI impregnated shrink wrap over the propeller.
(a) Trim the Cortec VCI impregnated shrink wrap as necessary to form a wrap
that will completely cover the propeller assembly. Refer to Figure 3-4.
CAUTION: DO NOT PERMIT TOO MUCH DWELL TIME WITH THE SEALING
TORCH OVER THE ALUMINUM PROPELLER COMPONENTS.
(11) Using a gas sealing torch, seal and shrink the Cortec VCI impregnated shrink
wrap. Refer to Figure 3-4.
(12) Install pieces of 2 inch (50.8 mm) closed cell foam to protect the blade tips.
(a) Bend the closed cell foam at the corners to protect the tip of each blade.
(b) Using duct tape or packaging tape, attach one piece of closed cell foam
around any blade tip.
1 If the foam thickness is cut, the smooth side of the foam should be
the side contacting the blade tips.
(13) Put a piece of 1/8 inch (3.18 mm) foam sheeting over the top of the Cortec VCI
impregnated shrink wrap covering the piston.
(14) Using duct tape or packaging tape, attach the Owner’s Manual & Logbook box
to the shipping pallet.
(15) Using plastic tie straps, attach the packaged propeller to the shipping pallet.
(a) Under each plastic tie strap, put a piece of cardboard or other material to
prevent the plastic tie straps from damaging the blades.
(b) Put the plastic tie straps inboard near the propeller hub. This is the
thickest part of the blade.
61-01-02
Page 3-31
VOLUME 7
(16) Secure the shipping pallet in the shipping container to prevent movement of the
shipping pallet.
(a) Make sure that there is a minimum of 4 inches (101.6 mm) clearance
between the tips of the propeller blades and the side of the shipping
container.

Rev. 54 Nov/23

Hartzell Propeller LLC: One Propeller Place Piqua, Ohio 45356-2634 U.S.A. Telephone: 937.778.4200 Fax: 937.778.4215

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HARTZELL PROPELLER LLC

One Propeller Place

MANUAL REVISION TRANSMITTAL

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Standard Practices Manual

Hartzell Propeller LLC

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202A, VOLUME 7 - REVISION 55 HIGHLIGHTS

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INTRODUCTION 61-01-02 Page 1

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INTRODUCTION 61-01-02 Page 2

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A. Hartzell Propeller Publications

INTRODUCTION 61-01-02 Page 4

Manual No. Available at

INTRODUCTION 61-01-02 Page 5

3. Personnel Requirements (Rev. 2)

A. Service and Maintenance Procedures in this Manual

4. Special Tooling and Consumable Materials (Rev. 2)

INTRODUCTION 61-01-02 Page 6