Mmel LJ60

U.S.
Department of Transportation
Federal Aviation Administration
Washington, DC
Master Minimum Equipment List (MMEL)

Revision: 6
Date: 01/21/2022
Learjet Inc.
Model 60
James B. Adams, Chair

Flight Operations Evaluation Board (FOEB)
Federal Aviation Administration (FAA)

Small Aircraft Evaluation Group (MKC-AEG)
DOT Building, Room 332
901 Locust Street
Kansas City, MO 64106-2641
Telephone: (816) 329-3233

Fax: (816) 329-3241
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
REVISION NO. 6 PAGE NO. I
DATE: 01/21/2022
AIRCRAFT:
TABLE OF CONTENTS AND CONTROL PAGE
Learjet Model 60
SYSTEM NO. SYSTEM PAGE NO. REV NO. DATE
-- Cover Page -- 6 01/21/2022
-- Table of Contents and Control Page I 6 01/21/2022
-- Log of Revisions II 6 01/21/2022
-- Highlights of Change III thru XIII 6 01/21/2022
-- Definitions and Preamble XIV 6 01/21/2022
-- Guidelines for (M) and (O) Procedures XV 6 01/21/2022
21 Air Conditioning 21-1 thru 6 6 01/21/2022
22 Autoflight 22-1 6 01/21/2022
23 Communications 23-1 thru 6 6 01/21/2022
24 Electrical Power 24-1 6 01/21/2022
25 Equipment/Furnishings 25-1 thru 8 6 01/21/2022
26 Fire Protection 26-1 6 01/21/2022
27 Flight Controls 27-1 thru 3 6 01/21/2022
28 Fuel 28-1 thru 3 6 01/21/2022
29 Hydraulic Power 29-1 6 01/21/2022
30 Ice and Rain Protection 30-1 thru 3 6 01/21/2022
31 Indicating/Recording Systems 31-1 thru 2 6 01/21/2022
32 Landing Gear 32-1 6 01/21/2022
33 Lights 33-1 thru 11 6 01/21/2022
34 Navigation 34-1 thru 18 6 01/21/2022
35 Oxygen 35-1 thru 2 6 01/21/2022
38 Water/Waste 38-1 thru 2 6 01/21/2022
45 Central Maintenance System 45-1 4 08/15/2011
46 Information Systems 46-1 thru 2 6 01/21/2022
49 Airborne Auxiliary Power 49-1 6 01/21/2022
52 Doors 52-1 thru 2 6 01/21/2022
74 Ignition 74-1 6 01/21/2022
76 Engine Control 76-1 4 08/15/2011
77 Engine Indicating 77-1 6 01/21/2022
78 Engine Exhaust 78-1 4 08/15/2011
REVISION NO. 6 PAGE NO. II
DATE: 01/21/2022
AIRCRAFT:
LOG OF REVISIONS
Learjet Model 60
REV NO. DATE
0a 01/30/1996
0b 06/12/1996
0c 06/09/1997
0d 09/15/1998
0e Undated
1 10/13/1999
1a 08/14/2001
1b 12/10/2001
2 02/28/2005
2a 12/07/2005
3 07/12/2007
4 08/15/2011
5 09/16/2016
6 01/21/2022
REVISION NO. 6 PAGE NO. III
DATE: 01/21/2022
AIRCRAFT:
HIGHLIGHTS OF CHANGE
Learjet Model 60
The following changes are the Highlights of Changes for Revision 6. The changes in this revision were
made to align with FAA policy letters (PL) and updated to the new Master Minimum Equipment List
(MMEL) format. All changes are reflected in the table below and are indicated by revision bars in the
associated ATA section.
PAGE NO. EXPLANATION OF CHANGE

General Minor editorial corrections and formatting changes were made throughout the
document, indicated with change bars. These editorial corrections may be
adopted in minimum equipment lists (MEL) at the operator’s discretion.
Throughout: Item sequence numbers formatted to be consistent with policy

letter format.
ATA 21 AIR CONDITIONING
21-1 Sub-items 21-1A) thru C): Changed all instances of “feet” to “ft” and changed
“one flight day” to “1 flight-day” for consistency. Spelled out first instance of
MSL for clarity.
Item 21-2: Changed “feet” to “ft” in list item b) for consistency.
21-2 Item 21-3 thru 8: Changed all instances of “feet” to “ft” for consistency.
21-3 21-9 and changed “feet” to “ft” in list item b).
21-11 and changed “feet” to “ft” in list item b).
21-4 Sub-item 21-12C): Changed “feet” to “ft” in list item b), changed “one flight day”
to “1 flight-day” in list item d), and fixed spelling of “flightcrew” in list item e).
21-5 Sub-item 21-14C): Changed “feet” to “ft” in list item b).
21-6 Item 21-19: Changed “feet” to “ft” in list item a).
Item 21-20: Changed “feet” to “ft” in list item b).
ATA 22 AUTOFLIGHT
22-1 Item 22-3: Changed “feet” to “ft” and spelled out “AGL,” “ILS,” and “MDA” for
first instances in list item a).
Item 22-4: Changed “feet” to “ft” in list item a).

REVISION NO. 6 PAGE NO. IV
DATE: 01/21/2022
AIRCRAFT:
Learjet Model 60
ATA 23 COMMUNICATIONS
23-1 Item 23-1: Lowercased “and” in Item Title and added comma after
“DC Transfer Bus” in column 4.
Sub-item 23-2A): changed “three flight days” to “3 flight-days” in list item b).
23-2 Sub-item 23-5A): Added “is” in list item a).
Item 23-6: Lowercased “and” in Item Title.
23-4 Sub-item 23-11A): Added hyphen between “flight” and “days” in list item b).
Sub-item 23-11B): Added hyphen between “flight” and “days.”
Sub-item 23-11C): Lowercased “or” in Sub-Item Title.
23-6 Sub-item 23-18B : Revised per PL-120.
ATA 25 EQUIPMENT/FURNISHINGS
25-1 Item 25-1: Pluralized “Seats” in Item Title. Added comma after “placarded” and
fixed punctuation in list item c).
Sub-item 25-1 pluralized Item Title.
Sub-item 25-1C): Added comma after “takeoff” in column 4.
25-2 Sub-item 25-3: Corrected spelling of Item Title. Corrected spelling of

“flightcrew” in column 4.
25-3 Item 25-5, A, Automatic External Defibrillator (AED) and/or Associated

Equipment, updated per PL 132.
Sub-item 25-5B): Lowercased “and/or” in Item Title..
Sub-item 25-5B: added comma after “missing” in column 4.
25-4 Item 25-5, C First Aid Kit (FSK) and or Associated Equipment updated per PL-
132
Item 25-7: Lowercased "and" in Item Title.
Item 25-9: Capitalized "Visor" in Item Title.
Item 25-10: Added hyphen between "calendar" and "days" in column 4.
(Continued)
REVISION NO. 6 PAGE NO. V
DATE: 01/21/2022
AIRCRAFT:
Learjet Model 60
ATA 25 EQUIPMENT/FURNISHINGS (Cont’d)
25-5 Item 25-11: Portable Flashlights/Flashlight Holders replaced with updated

information per PL-132.
Item 25-12: Corrected spelling of "Flightcrew" in Item Title.
Sub-item 25-12A): Corrected spelling of "flightcrew" in list item c).
Sub-item 25-12D): Corrected spelling of "flightcrew" in column 4.
Sub-item 25-12E): Corrected spelling of "flightcrew" in column 4.
25-6 Item 25-14: Lowercased "and" in Item Title.
Item 25-15: Lowercased "and" in Item Title.
Item 25-17: Corrected spelling of “Underseat” in Item Title.
ATA 26 FIRE PROTECTION
Item 26-2 Portable Fire Extinguisher updated per PL-132.
Item 26-4: Changed "feet" to "ft" in list item b).
Item 26-5: Added "APU" in column 4.
ATA 27 FLIGHT CONTROLS
27-1 Item 27-1: Changed "feet" to "ft" in list item a).
Item 27-3: Changed "feet" to "ft" in list items b) and e). Corrected spelling of
"V1" with subscript in list item 1 in the NOTE. Changed "feet" to "ft" to list item
2. Changed "pounds" to "lb" in list items 3 and 5.
27-3 Item 27-7: Lowercased "of" in Item Title.
Item 27-8: Lowercased "of" in column 4.

REVISION NO. 6 PAGE NO. VI
DATE: 01/21/2022
AIRCRAFT:
Learjet Model 60
ATA 28 FUEL
28-1 Item 28-1: Changed "pounds" to "lb" in list item b) and "feet" to "ft" in list
item c).
Sub-item 28-2 changed "pounds" to "lb."
28-3 Item 28-7: Changed "pounds" to "lb" in list item d).
ATA 30 ICE AND RAIN PROTECTION
30-1 Sub-item 30-1B): Changed "degrees" to its symbol in list item a).
Sub-item 30-1D): Changed "degrees" to its symbol in list item a).
30-2 Sub-item 30-3 Changed "degrees" to its symbol in list item.
Item 30-4: Changed "degrees" to its symbol in list item.
30-3 Item 30-5): Corrected spelling of "Co-Pilot."
Item 30-8): Changed "degrees" to its symbol in list item b).
Item 30-11) Corrected spelling of “flightcrew” in column 4.
ATA 31 INDICATING/RECORDING SYSTEMS
31-1 Sub-item 31-3): Changed "three flight days" to "3 flight-days" in list item d).
31-2 Sub-item 31-3): Added hyphen between "calendar" and "days" in list item b).
Sub-item 31-3E): Lowercased "of" and "or" in Item Title.
ATA 32 LANDING GEAR
32-1 Item 32-2: Deleted Revision 6.

REVISION NO. 6 PAGE NO. VII
DATE: 01/21/2022
AIRCRAFT:
Learjet Model 60
ATA 33 LIGHTS
33-1, 2, 3, 5, 10 Item 33-1, 2, 3, 6, 11, 15. Changed all instances of “night” with “between
sunset and sunrise.”
33-2 Deleted per 14 CFR part 91, § 91.209(b) and PL-31, item 6.
33-4 Item 33-8: Corrected spelling of "flightcrew" in list items b) and c). Put "NOTE"
in ALL CAPS for both NOTES.
Item 33-9: Corrected spelling of "flightcrew" in column 4.
33-5 Sub-item 33-10A): Added "Part" between "14 CFR" and "91" in Item Title.
Lowercased "and" and "of" in Item Title.
Item 33-13: Updated sequence number.
33-6 Item 33-14: Updated sequence number.
Sub-item 33-14A): Removed spaces on each side of slash in Item Title.
Sub-item 33-14A)1): Removed spaces on each side of slash in Item Title.
Sub-item 33-14B): Removed spaces on each side of slash in Item Title.
Sub-item 33-14B)1): Removed spaces on each side of slash in Item Title.
Sub-item 33-14C): Removed spaces on each side of slash in Item Title.
Sub-item 33-14C)1): Removed spaces on each side of slash in Item Title.
33-7 Sub-item 33-14D): Removed spaces on each side of slash in Item Title.
Sub-item 33-14D)1): Removed spaces on each side of slash in Item Title.
Sub-item 33-14E): Removed spaces on each side of slash in Item Title.
Sub-item 33-14F): Removed spaces on each side of slash in Item Title.
Sub-item 33-14G): Removed spaces on each side of slash in Item Title.
(Continued)
REVISION NO. 6 PAGE NO. VIII
DATE: 01/21/2022
AIRCRAFT:
Learjet Model 60
ATA 33 LIGHTS (Cont’d)
33-8 Sub-item 33-14H): Removed spaces on each side of slash in Item Title.
Updated sub-item number.
Sub-item 33-14H)1): Removed spaces on each side of slash in Item Title.
Sub-item 33-14I): Removed spaces on each side of slash in Item Title.

Sub-item 33-14J): Removed spaces on each side of slash in Item Title.

Sub-item 33-14K): Removed spaces on each side of slash in Item Title.

Sub-item 33-14L): Removed spaces on each side of slash in Item Title.

Sub-item 33-14M): Removed spaces on each side of slash in Item Title.

33-9 Sub-item 33-14N): Removed spaces on each side of slash in Item Title.
Sub-item 33-14O): Removed spaces on each side of slash in Item Title.

Sub-item 33-14P): Removed spaces on each side of slash in Item Title.

Sub-item 33-14Q): Removed spaces on each side of slash in Item Title.

Sub-item 33-14R): Removed spaces on each side of slash in Item Title.

Sub-item 33-14S): Removed spaces on each side of slash in Item Title.

Sub-item 33-14T): Removed spaces on each side of slash in Item Title.

(Continued)
REVISION NO. 6 PAGE NO. IX
DATE: 01/21/2022
AIRCRAFT:
Learjet Model 60
ATA 33 LIGHTS (Cont’d)
33-10 Sub-item 33-14U): Removed spaces on each side of slash in Item Title.
Sub-item 33-14U)1): Removed spaces on each side of slash in Item Title.
Item 33-15: Lowercased "and/or" and added hyphen between "Light" and
"Dimming" in Item Title.
Item 33-16A): Removed spaces on each side of slash in Item Title.
Item 33-16B): Removed spaces on each side of slash in Item Title.
Item 33-16C): Removed spaces on each side of slash in Item Title.
Item 33-16D): Removed spaces on each side of slash in Item Title.
Item 33-16E): Removed spaces on each side of slash in Item Title.
Item 33-16F): Removed spaces on each side of slash in Item Title.
ATA 34 NAVIGATION
34-2 Item 34-6: Updated per PL-039. "i.e. RVSM" and added comma after "i.e." in
list item b. Added hyphen between "flight" and "days" in list item d).
Item 34-6: Changed item in column 3 from "0” to “1” per PL-39 and CFR
91.219.
Item 34-6B:. Added parentheses around "i.e. RVSM" and added comma after
"i.e." in column 4.
(Continued)
REVISION NO. 6 PAGE NO. X
DATE: 01/21/2022
AIRCRAFT:
Learjet Model 60
ATA 34 NAVIGATION (Cont’d)
34-4 Item 34-12: Updated sequence number. Lowercased "and" in Item Title.
Item 34-12, 2 ADS-B Out Extended Squitter updated per PL-105.
Item 34-14: Updated sequence number. Changed "two flight days" to "2 flight-
days" in list item d).
Item 34-17: Updated sequence number. Corrected spelling of "flightcrew" and

added "(PFD)" in column 4.
Item 34-18: Updated sequence number. Title Cased Item Title, corrected
spelling of "Windshear," and added comma after "Guidance."
Item 34-18: Title Cased Item Title.
Item 34-18A)1): Lowercased "and" in Item Title.
34-6 item 34-18A)2): Lowercased "and" in Item Title
item 34-18B): Title Cased Item Title.
item 34-18B)1): Lowercased "and" in Item Title.
item 34-18B)2): Lowercased "and" in Item Title.
(Continued)
REVISION NO. 6 PAGE NO. XI
DATE: 01/21/2022
AIRCRAFT:
Learjet Model 60
Sub-item 34-20A): Replaced period with open parentheses after sub-item

number.
Sub-item 34-20A)1): Changed from "two flight days" to "2 flight-days" in list
item b).
Sub-item 34-20A)1)a): Changed from "two flight days" to "2 flight-days" in list
item b).
Sub-item 34-20A)1)b): Changed "1" to "4" in column 2. Changed from "two

flight days" to "2 flight-days" in list item b).
34-8 Sub-item 34-20A)2): Lowercased "and" in Item Title.
34-9 Sub-item 34-20A)4): Lowercased "and" in Item Title.
Sub-item 34-20B): Replaced period with open parentheses after sub-item

number.
Sub-item 34-20B)1): Changed "two flight days" to "2 flight-days" in list item b).
Sub-item 34-20B)1)a): Changed "two flight days" to "2 flight-days" in list item
b).
Sub-item 34-20B)1)b): Changed "two flight days" to "2 flight-days" in list item
b).
34-10 Sub-item 34-20B)2): Lowercased "and" in Item Title.
Sub-item 34-20B)4): Lowercased "and" in Item Title.
Sub-item 34-20C): Replaced period with open parentheses after sub-item

number.
34-11 Item 34-22: Updated sequence number and lowercased "and" in Item Title.
Moved Repair Category B information down one line to be consistent with
Repair Category C information and added sub-item number.
Item 34-23: Updated sequence number and lowercased "and" in Item Title.
(Continued)
REVISION NO. 6 PAGE NO. XII
DATE: 01/21/2022
AIRCRAFT:
Learjet Model 60
34-12 Sub-item 34-23C): Updated sub-item number and lowercased "and" in Item
Title.
34-13 Sub-item 34-26,A: Revised per PL-98. Changed “ten (10) flight days” to
“10 flight-days” in list item e) and made "NOTE" all caps.
34-14 Item 34-26: Added “FMS” acronym.
Item 34-27: Revised per PL-105.
Sub-item 34-27B): Lowercased "and" in Item Title.
Sub-item 34-27B): Updated sub-item number. Corrected "flightcrew" in list item

b).
34-15 Item 34-29: Added hyphen between "FMS" and "computed" in NOTE.
Item 34-30: Added hyphen between "FMS" and "computed" in NOTE.
34-16 Item 34-29: Added “and” and ”(TAWS)” acronym in “Terrain Awareness and
Warning System (TAWS).”
Item 34-31: Updated sequence number. Corrected "flightcrew" in column 4.

Added hyphen between "FMS" and "computed."
ATA 35 OXYGEN
35-1 Item 35-1, 2 Portable Oxygen Bottles or Unites (Including Masks and Hoses)
updated per PL-132 update.
Item 35-1, 4 Protective Breathing equipment (PBE) updated per PL-132

update.
REVISION NO. 6 PAGE NO. XIII
DATE: 01/21/2022
AIRCRAFT:
Learjet Model 60
ATA 46 INFORMATION SYSTEMS
46-1 Replace entire section per PL-121.
ATA 49 AIRBORNE AUXILIARY POWER
49-1 Item 49-1: Added "No." between "STC" and "ST00265NY."
Item 49-2: Added "No." between "STC" and "ST00280WI."
ATA 52 DOORS
52-1 Item 52-1: Removed spaces on each side of slash in Item Title.
Sub-item 52-1A): Title Cased "Does Not Illuminate" in Item Title.
Sub-item 52-1B): Title Cased "Does Not Illuminate" in Item Title.
Sub-item 52-1C): Title Cased "Does Not Illuminate" in Item Title. Removed
"two" from "2 locking pins..." list item a).
ATA 73 ENGINE FUEL & CONTROL
73-1 Removed Chapter 73, Engine Fuel & Control, in Revision 6.
ATA 74 IGNITION
74-1 Item 74-1: Pluralized "Lights" in Item Title.
ATA 77 ENGINE INDICATING
77-1 Item 77-4: Added comma after "displays" in list item a). Corrected spelling of
"flightcrew" in list item c).
REVISION NO. 6 PAGE NO. XIV
DATE: 01/21/2022
AIRCRAFT:
DEFINITIONS AND PREAMBLE
Learjet Model 60
Definitions
Refer to the current FAA MMEL PL-25, MMEL/MEL Definitions, found on the FAA Flight Standards
Information Management System (FSIMS) website.
Preamble
For operations under Title 14 of Code of Federal Regulations (14 CFR) parts 91 subpart K (part 91K),
121, 125, 125 Letter of Deviation Authority (LODA), 129, and 135, refer to the current FAA MMEL
PL-34, MMEL and MEL Preamble. For operations under 14 CFR part 91, refer to current FAA MMEL
PL-36, 14 CFR Part 91 MEL Approval and Preamble. Both PLs are found on the FSIMS website.
REVISION NO. 6 PAGE NO. XV
DATE: 01/21/2022
AIRCRAFT:
GUIDELINES FOR (M) AND (O) PROCEDURES
Learjet Model 60
The Flight Operations Evaluation Board (FOEB) has identified a need for certain procedures to provide
an adequate level of safety while providing relief for some items. These procedures must be
established by the operator and may be based on the aircraft manufacturer’s recommended
procedures, Supplemental Type Certificate (STC) modifier’s recommended procedures, or equivalent
operator procedures. When recommended procedures are published, the operator should comply with
these procedures. If recommended procedures are not published, the following guidelines delineate the
aspects to be considered by the operator in the development of required procedures:
Guidelines for (M) and (O) Procedures should be based on the Maintenance and Operational
Procedures for the MEL Learjet Model 60 (M) and (O) Procedures, published by Learjet, Inc. in the
Learjet 60/60XR Dispatch Deviation Guide.
REVISION NO. 6 PAGE NO. 21-1
DATE: 01/21/2022
TABLE KEY
AIRCRAFT: 1. REPAIR CATEGORY
2. NO. INSTALLED
Learjet Model 60 3. NO. REQUIRED FOR DISPATCH
4. REMARKS OR EXCEPTIONS
21. Air Conditioning
Change
Sequence No. Item 1 2 3 4 Bar
1. Cabin Pressurization
Control System
A. Automatic Mode C 1 0 May be inoperative provided: |

a) Cabin Pressurization Manual
Mode is operative, and
b) Aircraft is operated at
41,000 ft mean sea level |
(MSL) or below. |
B. Manual Mode C 1 0 May be inoperative provided: |

a) Cabin Pressurization
Automatic Mode is operative,
and
41,000 ft MSL or below. |
C. Both Modes A 2 0 Both the Automatic and Manual |

Modes may be inoperative provided:
a) Aircraft is operated
unpressurized,
b) Aircraft is operated at 9,000 ft |
MSL or below, and
c) Repairs are made within
1 flight-day. |
2. Cabin Air Primary C 1 0 May be inoperative provided:

Outflow Valve a) Aircraft is operated
unpressurized,
MSL or below,
c) Cabin Air Secondary Outflow
Valve is operative,
d) EMER DEPRESS is selected,
and
e) CAB AIR is ON for flight.
DATE: 01/21/2022
TABLE KEY
2. NO. INSTALLED
Change
3. Cabin Air Secondary C 1 0 May be inoperative provided:

Outflow Valve a) Aircraft is operated
unpressurized,
MSL or below,
c) Cabin Air Primary Outflow
Valve is operative,
and
4. Cabin Differential Relief separated into ATA 21-2,

Pressure Relief Valves Cabin Air Primary Outflow Valve, and
ATA 21-3, Cabin Air Secondary
Outflow Valve, Revision 4.
5. Cabin Altitude Limiter C 2 1 One may be inoperative provided

aircraft is operated at 25,000 ft MSL |
or below.
6. Emergency C 2 1 (M) One may be inoperative

Pressurization Bleed provided:
Air Shutoff Valve a) Inoperative Valve must be
secured in CLOSED position,
41,000 ft MSL or below, and |
c) BLEED AIR and CAB AIR are
operative and ON.
7. Emergency C 1 0 (O) May be inoperative provided both

Pressurization Lights Emergency Pressurization Systems
are verified operative before each
flight.
8. Cabin Altitude Warning C 1 0 May be inoperative provided aircraft

System is operated at 9,000 ft MSL or below. |
DATE: 01/21/2022
TABLE KEY
2. NO. INSTALLED
Change
9. Cabin Altimeter C 1 0 (O) May be inoperative provided:

a) Cabin Differential Pressure
Display is operative, and
b) A chart to convert Cabin
Differential Pressure to Cabin
Altitude is provided and used.
C 1 0 May be inoperative provided:

unpressurized,
MSL or below,
c) Cabin Air Primary and
Secondary Outflow Valves are
operative,
and
e) CAB AIR is ON for the flight.
10. CABIN RATE Display C 1 0 May be inoperative provided:

a) Cabin Altimeter is operative,
b) Cabin Differential Pressure
Display is operative, and
c) Cabin Pressurization System
Automatic Mode is operative.
11. Cabin Differential C 1 0 (O) May be inoperative provided:

Pressure Display a) Cabin Altimeter is operative,
and
b) A chart to convert Cabin
Altitude to Cabin Differential
Pressure is provided and
used.

unpressurized,
b) Aircraft is operated at 9,000 ft
MSL or below,
operative,
and
e) CAB AIR is ON for the flight.
DATE: 01/21/2022
TABLE KEY
2. NO. INSTALLED
Change
12. Temperature Control

System
A. Automatic Mode |
1) Crew C 1 0 May be inoperative provided

Manual Temperature Control System
is operative.
2) Cabin C 1 0 May be inoperative provided

Manual Temperature Control System
is operative.
B. Manual Mode |
1) Crew C 1 0 May be inoperative provided

Automatic Temperature Control
System is operative.
2) Cabin C 1 0 May be inoperative provided

C. Both Modes A 2 0 Both Automatic and Manual Modes |

may be inoperative provided:
a) BLEED AIR and CAB AIR are
selected OFF,
MSL or below,
c) Aircraft is not operated in
known or forecast icing
conditions,
d) Repairs are made within
1 flight-day, and
e) Cockpit temperature is
acceptable to flightcrew.
DATE: 01/21/2022
TABLE KEY
2. NO. INSTALLED
Change
13. Temperature Control

Valve Indicator (LR-60)
A. Crew C 1 0 May be inoperative provided |

C 1 0 May be inoperative provided Manual

Temperature Control System is
operative.
B. Cabin C 1 0 May be inoperative provided |

C 1 0 May be inoperative provided Manual

Temperature Control System is
operative.
14. Air Conditioning System
A. Air Conditioning System C 1 0 (M) |

(Freon)
B. Auxiliary Air Conditioning C 1 0 (M) |

System (Freon)
(FAA Flight Inspection
Aircraft Only)
C. Air Cycle Machine B 1 0 May be inoperative provided: |

(ACM) (FAA Flight a) Aircraft is operated
Inspection Aircraft Only) unpressurized,
MSL or below,
operative,
and
DATE: 01/21/2022
TABLE KEY
2. NO. INSTALLED
Change
15. Cabin Temperature C 1 0

Indicator (LR-60)
16. Crew Fan C 1 0
17. Cabin Fan C 1 0
18. Auxiliary Heaters
A. Crew C 1 0 |
B. Cabin C 1 0 |
19. Engine Bleed Air Mixing C 2 1 One may be inoperative provided:

Valve a) Aircraft is operated at
25,000 ft MSL or below, and
b) Aircraft is not operated in
conditions.
20. Flow Control Valve C - 0 (M) May be inoperative provided:

unpressurized,
MSL or below,
operative,
and
21. Variable Opening Air

Vent/Gasper (WEMAC)
A. Flight Deck C - 0 |
B. Cabin D - 0 |
22. Baggage Compartment C 1 0 (M)(O)

Heater
DATE: 01/21/2022
TABLE KEY
2. NO. INSTALLED
22. Autoflight
Change
1. Autopilot System B 1 0 (M) Except where enroute operations

require its use, may be inoperative
provided Autopilot is deactivated.
NOTE: For RVSM operations, the

Autopilot must be operative.
2. Yaw Dampers C 1 0 NOTE: Rudder Boost will be

inoperative.
3. GO-AROUND (GA) C 1 0 (O) May be inoperative provided:

Button a) Autopilot and Flight Director
are not used below 500 ft |
above ground level (AGL) for |
an instrument landing system |
(ILS) or the minimum descent |
altitude (MDA) for a |
nonprecision approach, and
b) Alternate procedures are
established and used.
4. Control Wheel Master C 2 1 One may be inoperative on the

Switch (MSW) non-flying pilot side provided:
a) Autopilot is not used below
1,500 ft AGL, and |
b) Approach minimums do not
require use of Autopilot.
NOTE: Control Wheel Master Switch

(MSW) is required for
functions other than the
Autopilot System.
5. Flight Control Panel/ C - 0 (O) Annunciation Light may be

Flight Director Green inoperative provided associated
Selection Light annunciation on the PFD can be
displayed.
DATE: 01/21/2022
TABLE KEY
2. NO. INSTALLED
23. Communications
Change
1. Communication Systems D - - Any in excess of those required by

(VHF and UHF) CFR may be inoperative provided it is |
not powered by the Emergency AC
Bus, Emergency DC Bus, Battery
Bus, Battery Direct Bus, or the DC
Transfer Bus, and not required for |
emergency procedures.
2. Flight Deck Headsets D - - Any in excess of those required by

Earphones/Headphones regulation may be inoperative.
and Boom Microphones
A. Headset Boom A - 0 May be inoperative provided: |

Microphones a) Associated hand microphone
is installed and operates
normally, and
b) Repairs are made within
3 flight-days. |
A - 0 May be inoperative provided:

c) Associated hand microphone
is installed and operates
normally, and
d) Repairs are made in
accordance with applicable
regulations.
D - - Any in excess of those required by

regulation may be inoperative.
B. Headset C - 1 May be inoperative provided |

Earphones/Headphones associated flight deck speaker
operates normally.

(Continued)
U.S. DEPARTMENT OF
TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
DATE: 01/21/2022
TABLE KEY
2. NO. INSTALLED
23. Communications
Change
2. Flight Deck Headsets

Earphones/Headphones
and Boom Microphones
(Cont’d)
C. Active Noise D - 0 May be inoperative provided normal |

Canceling/Reduction audio function of headset is
Function operative.
3. Flight Deck Hand C - 0 May be inoperative provided |

Microphones associated boom microphone |
operates normally. |
D - 0 Any in excess of those required by

4. Flight Deck Speaker C 2 0 May be inoperative provided an

operative Headset is used by each
Flight Deck crewmember.
5. Passenger Address
System (PA)
A. Passenger Configuration C 1 0 (O) May be inoperative provided: |

a) PA is not required by 14 CFR, |
and
b) Alternate, normal, and
emergency procedures,
and/or operating restrictions
are established and used.
NOTE: Any function that operates

normally may be used.
B. Cargo Configuration D 1 0 May be inoperative provided |

procedures do not require its use.
U.S. DEPARTMENT OF
TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
DATE: 01/21/2022
TABLE KEY
2. NO. INSTALLED
23. Communications
Change
6. ACARS C - 0 (O) May be inoperative provided:

*** Communications/ a) Affected equipment is
Addressing and properly secured or |
Reporting System deactivated, and
b) Alternate procedures are used
for Air/Ground
Communications.
7. Flight Phone D - 0
***
8. Maintenance Interphone D - 0
*** System
9. Selective Call System C - 0 (O) May be inoperative provided

*** (SELCAL) alternate procedures are established
and used.
D - 0 May be inoperative provided

A. Channels C - 0 (O) May be inoperative provided |

alternate procedures are established
and used.

10. Pre-Recorded C 1 0 (O) May be inoperative provided

*** Passenger alternate procedures are established
Announcement System and used.
DATE: 01/21/2022
TABLE KEY
2. NO. INSTALLED
23. Communications
Change
11. Cockpit Voice Recorder

(CVR)
A. With Flight Data A 1 0 May be inoperative provided:

Recorder (FDR) Installed a) Flight Data Recorder (FDR)
operates normally, and
3 flight-days. |
1) Independent Power C 1 0
Source
B. Without Flight Data A 1 0 May be inoperative provided repairs |

Recorder (FDR) Installed are made within 3 flight-days. |
Source
C. For Operators Other A 1 0 May be inoperative provided repairs |

Than Air Carriers or are made in accordance with
Commercial Operators applicable 14 CFRs.
Source
12. Satellite C - 0
*** Communications System
13. Static Discharge Wick C 19 14 Five or less Discharge Wicks may be

missing or broken in any of the
following locations:
a) One on each Winglet,
b) Most inboard position on
each Elevator, and
c) Directly above
White Navigation Light.
14. Cabin Chime C - 0 May be inoperative provided

Passenger Address System operates
normally.
C - 0 (O) Alternate procedures are

DATE: 01/21/2022
TABLE KEY
2. NO. INSTALLED
23. Communications
Change
15. Passenger C - 0 (O) May be inoperative provided

Cabin/Lavatory Speaker alternate normal and emergency
procedures and/or operating
restrictions are established and used.
16. High Frequency (HF) D - - Any in excess of those required by |

Communication System 14 CFR may be inoperative. |
C - 1 (O) May be inoperative while

conducting operations that require
two LRCS provided:
a) Aircraft SATVOICE system
operates normally,
b) SATVOICE services are
available as a LRCS over the
intended route of flight,
c) The ICAO Flight Plan is
updated (as required) to notify
ATC of the communications
equipment status of the
aircraft, and
d) Alternate procedures are
A. High Frequency (HF) C - 0 (M) May be inoperative or missing |

Externally Mounted Wire provided:
Antenna a) Antenna and associated
mounting hardware are
removed, and
b) High Frequency (HF)
Communication System is
considered inoperative.
17. Radio Tuning Unit (RTU) C 2 1 RTU 1 must be operative. |

DATE: 01/21/2022
TABLE KEY
2. NO. INSTALLED
23. Communications
Change
18. Emergency Locator |

*** Transmitter (ELT)
A. Survival Type ELT D - - Any in excess of those required by |

14 CFR may be inoperative or
missing.
B. Fixed ELT A - 0 (M) May be inoperative provided: |

a) System is deactivated, and
90 days.
A - 0 (M) May be missing provided: |

a) Placard stating, “ELT not |
installed,” is placed in view of |
the pilot, and |
b) Repairs are made within |
90 days. |
D - - (M) Any in excess of those required

by 14 CFR may be inoperative
provided System is deactivated.
D - - Any in excess of those required by |

14 CFR may be missing. |
19. Communication C 1 0 (O) May be inoperative provided |

*** Management Unit (CMU) alternate procedures are established
and used for Datalink and Universal
Weather.
20. Datalink VHF C 1 0 (O) May be inoperative provided |

*** Communication Radio alternate procedures are established
and used for Datalink and Universal
Weather.
DATE: 01/21/2022
TABLE KEY
6. NO. INSTALLED
24. Electrical Power
Change
1. AC Voltmeter Display C 2 1 (O) One may be inoperative provided

(LR-60 Electric Power both Inverters are verified operative.
Monitor)
2. External Power D 1 0 |
3. Electrical Power Monitor C - - May be inoperative provided: |

LED Segment (LR-60) a) No more than one LED
Segment per numeral is
inoperative, and
b) Crew is able to determine the
intended value.
DATE: 01/21/2022
TABLE KEY
2. NO. INSTALLED
25. Equipment/Furnishings
Change
1. Passenger Seats D - - May be inoperative provided: |

a) Seat does not block an
Emergency Exit,
b) Seat does not restrict any
passenger from access to the
main aircraft aisle, and
c) The affected Seat(s) are
blocked and placarded, |
“DO NOT OCCUPY.” |
NOTE 1: A Seat with an inoperative

Seat Belt is considered
inoperative.
NOTE 2: Affected Seat(s) may

include the Seat(s) behind
and/or adjacent outboard
Seats.
A. Recline Mechanism D - - (O) May be inoperative and Seat |

occupied provided Seat Back is
verified immovable in FULL
UPRIGHT position.
D - - (M) May be inoperative and Seat

occupied provided Seat is secured in
the FULL UPRIGHT position.
B. Armrests D - - (M) May be inoperative or missing |

and Seat occupied provided:
a) Armrest does not block an
Emergency Exit, and
b) Armrest does not restrict any
passenger from access to the
main aircraft aisle.
C. Swivel Mechanism D - - May be inoperative and Seat |

occupied provided Seat is immovable
in placarded taxi, takeoff, and landing |
position.
DATE: 01/21/2022
TABLE KEY
2. NO. INSTALLED
Change
2. “FASTEN SEAT BELT C - - One or more Signs or Placards may

WHILE SEATED” Sign be illegible or missing provided a
or Placard legible Sign or Placard is visible from
each occupied Passenger Seat. |
3. Nonessential Equipment - 0 May be inoperative, damaged, or |

*** and Furnishings (NEF) missing provided that the item(s) is |
deferred in accordance with the
operator’s NEF deferral program.
The NEF program, procedures, and
processes are outlined in the
operators (insert name) Manual.
(M) and (O) procedures, if required,
must be available to the flightcrew |
and included in the operator’s
appropriate document.
NOTE: Exterior Lavatory Door Ash

Trays are not considered
NEF items.
4. Aft Cabin Baggage C - - May be inoperative or missing

Compartment Restraint provided Baggage Compartment
System remains EMPTY.
DATE: 01/21/2022
TABLE KEY
2. NO. INSTALLED
Change
5. Emergency Medical |
Equipment
A. Automatic External A - 0 (O) May be incomplete, inoperative, |

Defibrillator (AED) or removed provided: |
and/or Associated a) AED is labeled or placarded in |
Equipment a manner that will identify it as
a unit that cannot be mistaken |
for a fully serviceable unit, |
b) Location placarding is removed |
or obscured, and |
c) Repairs or replacements are |
made within one flight. |
D - - Any in excess of those required by |

14 CFR may be incomplete, missing,
or inoperative.
B. Emergency Medical Kit A - 0 (O) May be incomplete or removed |

(EMK) and/or provided: |
Associated Equipment a) EMK is labeled or placarded in |
a manner that will identify it as
a unit that cannot be mistaken |
for a fully serviceable unit, |
b) Location placarding is removed |
or obscured, and |
c) Repairs or replacements are
NOTE: Medical equipment installed in |

the aircraft as part of an EMS |
operation is not considered part |
of the normal complement of |
equipment. No MMEL relief |
applies to that equipment and |
14 CFR maintenance and |
inspection requirements do not |
apply. |
(Continued)
DATE: 01/21/2022
TABLE KEY
2. NO. INSTALLED
Change
5. Emergency Medical Any in excess of those required by |

Equipment 14 CFR may be incomplete or |
(Cont’d) removed. |
C. First Aid Kit (FAK) A - - (O) If more than one is required by |

and/or Associated 14 CFR, only one of the required |
Equipment FAKs may be incomplete or removed |
provided:
a) The FAK is labeled or |
placarded in a manner that |
will identify it as a unit that |
cannot be mistaken for a fully |
serviceable unit, |
b) Location placarding is |
removed or obscured, and |
c) Repairs or replacements are |
NOTE: Medical equipment installed in |

the aircraft as part of an EMS |
operation is not considered |
part of the normal |
complement of equipment. |
No MMEL relief applies to that |
equipment and 14 CFR |
maintenance and inspection |
requirements do not apply. |

14 CFR may be incomplete, missing, |
or inoperative.
6. Flight Inspection Panel D - 0 May be inoperative provided |

*** System procedures are not dependent on its
(FAA LR-60 Only) use.
7. Life Preserver D - - Any in excess of those required by |

(Crew and Passenger) 14 CFR may be inoperative or |
missing provided required distribution
is maintained.
DATE: 01/21/2022
TABLE KEY
2. NO. INSTALLED
Change
8. Chart Holder C - 0 |
9. Flight Deck Sun Visor D - 0 May be missing or inoperative |

System provided pilot’s field of vision is not
obstructed.
10. Exterior Lavatory Door A 1 0 May be missing provided it is |

Ashtray replaced within 3 calendar-days. |
11. Portable Flashlights/ C 2 0 May be inoperative or removed |

Flashlight Holders provided: |
a) Crewmember assigned to the |
affected position has an |
equivalent operative flashlight |
readily available, |
b) Inoperative flashlight remains |
in a certified location or is |
removed from the aircraft, and |
c) Location placarding is |
removed or obscured. |
D 2 0 Any in excess of those required by |

14 CFR may be inoperative or |
removed provided: |
a) Inoperative flashlight remains |
in a certified location until |
removed from the aircraft at |
the next suitable maintenance |
facility, and |
removed or obscured. |
12. Flightcrew Seat |
A. Manual Vertical B 2 0 (M) May be inoperative provided: |

Adjustment a) Seat(s) are LOCKED in a
position that permits normal
visibility,
b) Full Flight Control movement
is available, and
c) Position of Seat is acceptable
to flightcrew. |
B. Lumbar Support C 2 0 |
(Continued)
DATE: 01/21/2022
TABLE KEY
2. NO. INSTALLED
Change
12. Flightcrew Seat

(Cont’d)
C. Armrest C 4 0 |
D. Recline Function C 2 0 May be inoperative provided Seat is |

acceptable to flightcrew. |
E. Headrest C 2 0 May be inoperative provided Seat is |

acceptable to the flightcrew. |
13. Galley Waste C - - (M)(O) May be inoperative provided: |

Receptacle Access a) Container is EMPTY,
Door/Cover b) Access is SECURED to
prevent waste introduction
into the Compartment, and
c) Procedures are established to
ensure sufficient Galley
Waste Receptacles are
available to accommodate all
waste that may be generated
on a flight.
14. Flight Deck Decorative D - - (M) May be damaged, broken, |
Trim Panel and Molding cracked, or missing provided: |
a) All missing or loose parts are
SECURED in place, and
b) There is no possible head
impact or interference with
crew duties.
DATE: 01/21/2022
TABLE KEY
2. NO. INSTALLED
Change
15. Cabin and Galley C - - (M)May be inoperative in closed |

Storage Compartment/ position provided: |
Closet a) Affected bin, compartment, or |
closet is prominently |
placarded “DO NOT USE,” |
b) Any emergency equipment |
located in affected bin, |
compartment, or closet is |
considered inoperative, and |
c) Location placarding for any |
emergency equipment stored |
in affected bin, compartment, |
or closet is removed or |
obscured. |
NOTE: Use of this proviso may be |

dependent upon an operator’s |
aircraft security program, as |
appropriate. |
16. Cabin Power Outlet D - 0 (M) May be inoperative provided the |

System System is deactivated.
17. Cabin Underseat D - 0 (M) May be missing or inoperative |

Storage Door/Drawer provided:
a) If missing, contents must be
relocated,
b) If inoperative, Door must be
closed and SECURED and
contents relocated,
c) If contents contain Emergency
Equipment, the equipment
must be relocated and
accessible for the passenger
or the Seat must be
considered inoperative, and
d) If Emergency Equipment is
relocated, passengers must
be briefed as to its location.
DATE: 01/21/2022
TABLE KEY
2. NO. INSTALLED
Change
18. Passenger Audio Control D - 0 |

Panel
19. Windshield Terminal B - 0 (M) May be missing or inoperative |

Block Cover provided the Terminal is covered with
electrically insulated material.
DATE: 01/21/2022
TABLE KEY
2. NO. INSTALLED
26. Fire Protection
Change
1. Fire Extinguisher Bottle C 2 0 May be missing provided Bottle

Thermal and Discharge Pressure is adequate. |
Indicator Disk
2. Portable Fire D - - Any in excess of those required by

Extinguisher 14 CFR may be inoperative or
removed provided: |
a) Inoperative fire extinguisher |
remains in a certified location |
until removed from the aircraft |
at the next suitable |
maintenance facility, |
c) Required distribution is
maintained.
NOTE: Inoperative fire extinguishers, |

removed from a certified |
location or removed from the |
aircraft, are subject to 49 CFR |
dangerous goods regulations. |
3. Cabin Fire Detection C 1 0 May be inoperative provided

System Cabin Baggage Compartment
remains EMPTY.
4. Bleed Air Overheat C 1 0 May be inoperative provided:

Warning System a) Aircraft is operated
unpressurized,
MSL or below,
c) Bleed Air Switches are OFF,
and
d) Aircraft is not operated in
conditions.
5. Auxiliary Power Unit C 1 0 May be inoperative provided Auxiliary

*** (APU) Fire Detection Power Unit (APU) is considered |
System inoperative.
DATE: 01/21/2022
TABLE KEY
2. NO. INSTALLED
27. Flight Controls
Change
1. Spoileron System C 1 0 (M) May be inoperative provided:

a) Aircraft is operated at
38,000 ft MSL or below, and |
b) Emergency Pressurization
System is operative, and
c) Aircraft is operated in
accordance with AFM
Limitations.
2. Autospoiler System C 1 0 May be inoperative provided aircraft

is operated in accordance with AFM
Limitations.
3. Spoiler System C 1 0 May be inoperative provided:

a) ANTI-SKID System is
operative and ON,
b) Airport elevation is less than
8,000 ft MSL, |
c) Rudder Boost System is
operative and ON,
d) There is no tail wind
component,
e) Aircraft is operated at
38,000 ft MSL or below, |
f) Emergency Pressurization is
operative, and
g) Performance factors are
applied.
NOTE: The following performance

factors must be applied:
1. Lower V1 speed by |
2 knots but not less
than 100 knots,
2. Increase takeoff
distance by 400 ft, |
3. Lower takeoff weight
limit by 700 lb, |
4. Increase landing
distance by a factor of
1.25, and
5. Lower landing weight
limit by 800 lb. |
DATE: 01/21/2022
TABLE KEY
2. NO. INSTALLED
27. Flight Controls
Change
4. Mach Trim System C 1 0 May be inoperative provided aircraft

Limitations.
5. Rudder Boost System C 1 0 May be inoperative provided aircraft

Limitations.
6. Spoiler Position Indicator C 1 0 May be inoperative provided:

(LR-60) a) The Autospoiler System is
operative,
b) SPOILER ARM Light is
operative,
c) Spoiler System is operative,
and
d) SPOILER EXT Light is
operative.
C 1 0 May be inoperative provided: |

a) Spoiler System is not used for
flight, and
b) AFM Limitations are complied
with.
DATE: 01/21/2022
TABLE KEY
2. NO. INSTALLED
27. Flight Controls
Change
7. Angle of Attack Indicator C 2 1 One may be inoperative provided |

Low Speed Cues are operative on
both sides.
8. PFD Low Speed Cue C 2 0 May be inoperative provided both

Angle of Attack Indicators are |
operative.
9. Rudder Pedal B 2 1 One may be inoperative provided full

Adjustment Mechanism range of motion is available and
acceptable to the crewmember in the
SEATED position.
DATE: 01/21/2022
TABLE KEY
2. NO. INSTALLED
28. Fuel
Change
1. Jet Pump System C 2 1 One side may be inoperative

provided:
a) Both Standby Electric Pumps
are operative and ON
(except when transferring
Fuselage fuel or balancing
fuel),
b) Takeoffs and intentional
go-arounds are not conducted
with less than 600 lb fuel |
quantity in the associated
Wing Tank, and
c) Aircraft is operated at
25,000 ft MSL or below. |
2. Fuselage Tank C 2 1 One may be inoperative provided

Transfer Pump Fuselage Tank Transfer Valve
(NORM/AUX XFR) associated with remaining Pump is
operative.

a) Both Fuselage Tank Transfer
Valves are operative,
b) Operations do not require use
of approximately 350 lb of |
unusable Fuselage Tank fuel,
and
c) Aircraft is operated in
accordance with AFM
Limitations and procedures.
3. Fuselage Tank C 2 1 (O) One may be inoperative provided:

Transfer Valve a) Fuselage Tank Transfer
(NORM/AUX XFR) Pump associated with
remaining Valve is operative,
and
b) Failed Transfer Valve is in the
CLOSED position.
(Continued)
DATE: 01/21/2022
TABLE KEY
2. NO. INSTALLED
28. Fuel
Change
3. Fuselage Tank
Transfer Valve
(NORM/AUX XFR)
(Cont’d)
C 2 0 (O) May be inoperative provided:

a) Operations do not require use
of any Fuselage Tank fuel,
b) Both Fuselage Tank Transfer
Valves are in the CLOSED
position, and
c) Both Fuselage Tank Transfer
Pumps are operative.
4. Fuselage Tank C 1 0 May be inoperative provided

Refueling System operations do not require use of
(Includes Two Standby Fuselage Tank fuel.
Pumps, Two Fuselage
Tank Transfer Valves,
and Full Float Switch) |
a) Single Point Pressure Refuel
(SPPR) System is used, and
b) Inoperative component(s) will
not prevent transfer of
Fuselage Tank fuel to Wing
Tanks.
5. Single Point Pressure C 1 0

Refuel (SPPR) System
DATE: 01/21/2022
TABLE KEY
2. NO. INSTALLED
28. Fuel
Change
6. Fuel Quantity Indicator C - - One illuminated Segment of a

Light Segment numeral may be inoperative provided:
a) Crew can clearly distinguish
which Segment is inoperative,
b) The Indicator in which the
Light Segment is inoperative
must be disregarded, and
c) Crew can compute the
missing number by using the
other three Indicators.
7. LOW FUEL Caution C 1 0 May be inoperative provided:

Annunciator a) All Fuel Quantity Indicating
Systems are operative,
b) All Fuel Flow Indicators are
operative,
c) All Motive Flow Switches are
in the ON position, and
d) Flight is planned so that the
aircraft will have not less than
700 lb of fuel quantity per |
Wing when landing.
8. Fuel Cap Retention C 1 0

Cable (SPPR System)
DATE: 01/21/2022
TABLE KEY
2. NO. INSTALLED
29. Hydraulic Power
Change
1. Auxiliary Electrical C 1 0 (M)(O) May be inoperative provided:

Hydraulic Pump System a) Pump is DEACTIVATED, and
(HYD PUMP) b) Alternate means of setting the
Brakes are used.
C 1 0 (O) May be inoperative provided

aircraft is Chocked prior to Engine
start.
2. Hydraulic Accumulator C 1 0 (M) May be inoperative provided an

Gauge alternate means is established and
used to check Accumulator
Precharge Pressure prior to each
flight.
3. Low Hydraulic C 2 1 (O) One may be inoperative provided:

Pressure Annunciator a) Auxiliary Hydraulic Pump is
(L/R HYDR PRESS) operative, and
b) Engine-Driven Hydraulic
Pumps are verified to be
operative prior to taxi.
DATE: 01/21/2022
TABLE KEY
2. NO. INSTALLED
30. Ice and Rain Protection
Change
1. Airframe Anti-Ice System
A. Wing C 1 0 May be inoperative provided aircraft |

is not flown in known or forecast icing
conditions.
B. Stabilizer C 1 0 May be inoperative provided: |

a) Aircraft is not flown in visible
moisture with Static Air
Temperature (SAT) below
+10°C, and |
b) Aircraft is not flown in known
or forecast icing conditions.
C. Windshield C 1 0 May be inoperative provided aircraft |

conditions.
D. Engine Inlet Anti-Ice C 2 1 One may be inoperative provided: |

System (Nacelle Heat) a) Aircraft is not flown in visible
+10°C, and |
2. Alcohol Anti-Ice System C 1 0 May be inoperative provided aircraft

conditions.
DATE: 01/21/2022
TABLE KEY
2. NO. INSTALLED
Change
3. Pitot Static System B 3 2 One may be inoperative provided: |

Heater a) Aircraft is not operated in
visible moisture with Static Air
+10°C, and |
NOTE: Both left and right Pitot Static

Mast Heaters must be
operative for RVSM
operations.
B 3 1 Two may be inoperative provided:

a) Aircraft is not operated in
visible moisture with Static Air
+10°C, |
or forecast icing conditions,
and
c) Aircraft is flown in
VMC ONLY.
NOTE: RVSM not authorized.
4. Stall Vane Heater C 2 1 One may be inoperative provided: |

System a) Aircraft is not flown in visible
+10°C, and |
DATE: 01/21/2022
TABLE KEY
2. NO. INSTALLED
Change
5. Windshield Ice Detect B 2 1 Right side (Co-Pilot) Light must be |

Light operative and monitored.
B 2 0 May be inoperative provided aircraft

is not operated at night.
6. Ice Detector C - 0 May be inoperative provided the |

*** Ice Detect Lights are operative.
7. Wing Temperature C 1 0 May be inoperative provided: |

Gauge a) Airframe Anti-Ice System for
Wings remains OFF, and
8. STAB HT Caution C 1 0 May be inoperative provided: |

Annunciator a) Airframe Anti-Ice System for
Stabilizer remains OFF,
b) Aircraft is not flown in visible
+10°C, and |
c) Aircraft is not flown in known
9. WING HT Warning C 1 0 May be inoperative provided the |

System aircraft is not flown in known or
forecast icing conditions.
10. PITOT HT Annunciator B 1 0 May be inoperative provided: |

a) All other elements of
Pitot Heat System are
operative, and
11. Windshield Defog C 2 1 One may be inoperative provided it is |

System acceptable to the flightcrew. |
NOTE: Meteorological conditions in

which the aircraft is to be
operated should be
considered.
DATE: 01/21/2022
TABLE KEY
2. NO. INSTALLED
31. Indicating/Recording Systems
Change
1. Clock C 2 1
2. Flight Hour Meter C 1 0 (O)

***
3. Flight Data Recorder C - - Any in excess of those required by

(FDR) System 14 CFR may be inoperative.
A - 0 May be inoperative provided:

a) Cockpit Voice Recorder
(CVR) operates normally,
b) Airplane is not dispatched
from a designated airport as
listed in the operator’s MEL
unless:
1. The FDR failure occurs
after pushback but prior to
takeoff, or
2. The FDR repair was
attempted but was not
successful.
c) In those cases where repair is
attempted but not successful,
the aircraft may be dispatched
on a flight or series of flights
until the next designated
airport where repair must be
accomplished prior to
dispatch, and
3 flight-days. |
(Continued)
DATE: 01/21/2022
TABLE KEY
2. NO. INSTALLED
31. Indicating/Recording Systems
Change
3. Flight Data Recorder

(FDR) System
(Cont’d)
A. FDR Recording A - - Up to three (3) recording parameters |

Parameters Required By may be inoperative provided:
14 CFR a) Cockpit Voice Recorder
(CVR) operates normally, and
20 calendar-days. |
B. FDR Recording A - - May be inoperative provided repairs |

Parameters Not are made prior to completion of the
Required By 14 CFR next scheduled inspection.
C. Operators Other Than C - 1 Any in excess of those required by |

Holders of Air Carrier or 14 CFR may be inoperative. |
Commercial Operator
Certificates
A - 0 May be inoperative provided repairs

are made in accordance with
applicable 14 CFRs.
4. Hydraulic Reservoir/Fire C 1 0 May be inoperative provided alternate

Bottle Remote Indicator means of verifying system indications
Panel (FAA Flight are used.
Inspection Aircraft Only)
DATE: 01/21/2022
TABLE KEY
2. NO. INSTALLED
32. Landing Gear
Change
1. Anti-Skid System C 1 0 (M)(O) May be inoperative provided:

a) System is DEACTIVATED,
and
b) Aircraft is operated in
accordance with AFM
Limitations and performance
data.
2. Parking Brake Caution Deleted Revision 6. |

Light
3. Tire Pressure D 5 0 (M) May be inoperative provided the |

Measuring System, tire pressure on the affected Wheel is
Tire Pressure Sensor manually checked within 96 hours
prior to takeoff.
DATE: 01/21/2022
TABLE KEY
2. NO. INSTALLED
33. Lights
Change
1. Position (NAV) Light

System
A. Aircraft Equipped With |

Incandescent Lamp
Navigation Light System
(LR-60)
1) Wing-Left Position C 1 0 May be inoperative provided aircraft

(NAV) Light is not operated between sunset and
sunrise.
2) Wing-Right Position C 1 0 May be inoperative provided aircraft

(NAV) Light is not operated between sunset and
sunrise.
3) Tail Position (NAV) Light B 2 1 One Lamp may be inoperative.
C 2 0 May be inoperative provided aircraft

is not operated between sunset and
sunrise.
B. Aircraft Equipped With |

LED Navigation Light
System (LR-60XR)
1) Wing-Left Position (NAV) C 1 0 May be inoperative provided aircraft

LED Light Assembly is not operated between sunset and
sunrise.
NOTE: If a single LED is inoperative,

the entire assembly is
(Continued)
DATE: 01/21/2022
TABLE KEY
2. NO. INSTALLED
33. Lights
Change
B. Aircraft Equipped With

LED Navigation Light
System (LR-60XR)
(Cont’d)
2) Wing-Right Position C 1 0 May be inoperative provided aircraft

(NAV) LED Light is not operated between sunset and
Assembly sunrise.

3) Tail Position (NAV) C 1 0 May be inoperative provided aircraft

LED Light Assembly is not operated between sunset and
sunrise.

2. Anti-Collision Light Deleted Rev 6 |

System
DATE: 01/21/2022
TABLE KEY
2. NO. INSTALLED
33. Lights
Change
3. Landing-Taxi Light
A. Landing Light B 2 1 |
B 2 0 May be inoperative provided aircraft

is not operated between sunset and
sunrise.
B. Taxi Light C 2 1 |
C 2 0 May be inoperative provided one

Landing or Recognition Light is
operative.
4. Recognition Light C 1 0
5. Recognition Light Pulse C 1 0

*** System
6. Wing Icing Detection C 1 0 May be inoperative provided:

Light (Wing Inspection a) Aircraft is not operated in
Light) known or forecast icing
conditions between sunset |
and sunrise, and |
b) Ground deicing procedures do
not require their use.

a) Primary Ice Detection system
is operative, and
b) Ground deicing procedures do
not require their use.
7. Entry Light C 1 0 May be inoperative provided

sufficient ambient lighting illuminates
the Steps.
DATE: 01/21/2022
TABLE KEY
2. NO. INSTALLED
33. Lights
Change
8. Cockpit/Flight C - - Individual lights may be inoperative

Compartment and provided:
Instrument Lighting a) Remaining Lighting System
System (Including lights are sufficient to clearly
Back Lighting) illuminate all required
instruments, controls, and
other devices for which they
are provided,
b) Remaining Lighting System
lights are positioned so that
direct rays are shielded from
flightcrew members’ eyes, |
and
c) Lighting configuration and
intensity is acceptable to the
flightcrew. |
NOTE 1: Individual button/switch |

lights and/or
annunciations/indications
are excluded from this relief.
NOTE 2: Unaided operation |

(without NVGs) may be
permitted with inoperative
NVG supplemental lights; |
cracked or missing filters.
9. Cabin Interior Lighting C - 0 May be inoperative provided lighting

System (Excludes configuration is acceptable to the
Cabin Emergency flightcrew. |
Lighting System)
DATE: 01/21/2022
TABLE KEY
2. NO. INSTALLED
33. Lights
Change
10. Passenger Lighted C - - (O) May be inoperative and

Information Sign associated Passenger Seat or
Lavatory may be occupied provided:
a) PA System operates normally,
and
b) PA System is used to notify
passengers and Cabin crew
when associated Sign(s) are
placed ON or OFF.
A. For 14 CFR Part 91 C - - (O) May be inoperative provided |

Operations and alternate procedures are established |
Operations Not and used to notify Cabin occupants.
Requiring Use of |
PA System
11. Exterior Emergency C 1 0 May be inoperative provided aircraft

*** Lighting System is not operated between sunset and
sunrise.
12. Logo Light System C 1 0

***
13. Baggage Door/Pylon C 2 0 |

External Light
DATE: 01/21/2022
TABLE KEY
2. NO. INSTALLED
33. Lights
Change
14. EFIS Control Panel |

Assembly Light
A. AHS/Amber Lamp C 2 0 (O) Switch Backlight and |

(LR-60) Annunciation Bulbs may be
inoperative provided associated
annunciation on the PFD can be
displayed.
1) AHS/Amber Lamp C 8 0 Switch Backlight and Annunciation |

(LR-60XR) LEDs may be inoperative provided
associated annunciation on the PFD
can be displayed.
B. AHS/Green Lamp C 2 0 (O) Switch Backlight and |

displayed.
1) AHS/Green Lamp C 8 0 Switch Backlight and Annunciation |

can be displayed.
C. ADC/Amber Lamp C 2 0 (O) Switch Backlight and |

displayed.
1) ADC/Amber Lamp C 8 0 Switch Backlight and Annunciation |

can be displayed.
(Continued)
DATE: 01/21/2022
TABLE KEY
2. NO. INSTALLED
33. Lights
Change
14. EFIS Control Panel

Assembly Light
(Cont’d)
D. ADC/Green Lamp C 2 0 (O) Switch Backlight and |

displayed.
1) ADC/Green Lamp C 8 0 Switch Backlight and Annunciation |

can be displayed.
E. CDU/Amber Lamp C 2 0 (O) Switch Backlight and |

displayed.
F. CDU/Green Lamp C 2 0 (O) Switch Backlight and |

displayed.
G. REV/(PFD) Amber Lamp C 2 0 (O) Switch Backlight and |

annunciation of the PFD can be
displayed.
1) REV/(PFD) White Lamp C 8 0 (O) Switch backlight and |

(LR-60XR) annunciation LEDs may be
displayed.
DATE: 01/21/2022
TABLE KEY
2. NO. INSTALLED
33. Lights
Change

Assembly Light
(Cont’d)
H. PFD/White Lamp C 2 0 (O) Switch Backlight and |

displayed.
1) PFD/White Lamp C 8 0 Switch Backlight and Annunciation |

can be displayed.
I. RTU/White Lamp C 2 0 (O) Switch Backlight and |

inoperative provided the Switch
operates normally by verifying the
On-Side RTU is ON.
J. OFF (RTU)/Amber Lamp C 2 0 (O) Switch Backlight and |

(LR-60) Annunciation Bulb may be
operates normally.
K. RMT Tune/White Lamp C 2 0 (O) Switch Backlight and |

operates normally.
L. ATC/White Lamp C 2 0 (O) Switch Backlight and |

operates normally.
M. CAT II/White Lamp C 2 0 (O) Switch Backlight and |

operates normally and the respective
CAT II amber and green portion of
the Annunciator are still operational.
(Continued)
DATE: 01/21/2022
TABLE KEY
2. NO. INSTALLED
33. Lights
Change

Assembly Light
(Continued)
N. MFD/White Lamp C 8 0 (O) Switch Backlight and |

(LR-60XR) Annunciation LEDs may be
annunciation on the MFD can be
displayed.
O. REV (MFD)/White Lamp C 8 0 (O) Switch Backlight and |

displayed.
P. ENG/White Lamp C 8 0 (O) Switch Backlight and |

annunciation on the MFD can be
displayed.
Q. ON/White Lamp C 8 0 (O) Switch Backlight and |

displayed.
R. OFF (RMT Tune)/Amber C 2 0 (O) Switch Backlight and |

Lamp (LR-60) Annunciation Bulb may be
operates normally.
S. 1 (ATC)/Amber Lamp C 1 0 (O) Switch Backlight and |

operates normally.
T. 2 (ATC)/Amber Lamp C 1 0 (O) Switch Backlight and |

operates normally.
(Continued)
DATE: 01/21/2022
TABLE KEY
2. NO. INSTALLED
33. Lights
Change

Assembly Light
(Cont’d)
U. SPARE/White Lamp C 2 0 |
(LR-60)
1) SPARE/White Lamp C 8 0 |
(LR-60XR)
15. Flight Deck Annunciator C 1 0 May be inoperative provided aircraft |

and/or Instrument Panel is not operated between sunset and |
Light-Dimming Function sunrise. |
16. Landing Gear Control |

Panel Light
A. Nose UNSAFE/Red C 2 1 |
Lamp (LR-60)
B. Nose DOWN/Green C 2 1 |
Lamp (LR-60)
C. Left UNSAFE/Red Lamp C 2 1 |

(LR-60)
D. Left DOWN/Green Lamp C 2 1 |

(LR-60)
E. Right UNSAFE/Red C 2 1 |
Lamp (LR-60)
F. Right DOWN/Green C 2 1 |
Lamp (LR-60)
G. Mute Lamp C 1 0 |
17. Service Light |
A. Baggage C - 0 |
B. Tailcone C - 0 |
C. Maintenance C - 0 |
DATE: 01/21/2022
TABLE KEY
2. NO. INSTALLED
33. Lights
Change
18. Lavatory Vanity Light C 2 0 |
19. Engine Fire T-Handle B 4 2 One Lamp may be inoperative in |

Light each T-Handle provided the
nomenclature remains legible.
20. Push Button Light B - - One Lamp may be inoperative in |

each independent module provided
the nomenclature remains legible.
DATE: 01/21/2022
TABLE KEY
2. NO. INSTALLED
34. Navigation
Change
1. Sensor Display Unit C 1 0 May be inoperative provided:

(SDU) (LR-60) a) Both Multifunction Displays
are operative, and
b) Magnetic Compass is
operative.

a) Multifunction Display is
operative,
b) Navigation Display is
operative, and
c) Magnetic Compass is
operative.
2. Multifunction Display C 2 1 One may be inoperative provided the

(MFD) (Navigation Sensor Display Unit (SDU) is
Display) (LR-60) operative.
3. FMS Control Display C 2 1 One may be inoperative provided:

Unit (CDU) (LR-60) a) CDU reversion is selected,
b) Approved Flight Manual
procedure for CDU failure is
followed, and
c) SDU is operative.
4. Air Data Reference C 2 1 One may be inoperative provided:

Panel (ARP) (LR-60) a) Standby Airspeed Indicator
and Standby Altimeter are
operative,
b) Air Data Reversion (ADC) is
used,
c) Aircraft is operated in day
VMC conditions,
d) If Autopilot is engaged, it must
be transferred to the operative
ARP side, and
e) Enroute operations do not
require its use.
NOTE: For RVSM operations, both

ARPs must be operative.
5. Altitude Awareness C 2 1 (O) One may be inoperative.

Panel (AAP) (LR-60)
DATE: 01/21/2022
TABLE KEY
2. NO. INSTALLED
34. Navigation
Change
6. Altitude Alerting System A - 0 (O) May be inoperative provided:

a) Autopilot with Altitude Hold,
and Altitude Capture operates
normally,
b) Enroute operations
(i.e., RVSM) do not require |
its use,
c) Airplane does not depart from
a designated airport (as listed
in the operator’s MEL) where
repair or replacement can be
made, and
3 flight-days. |
C - 1
1) Aural Alert C - 0 May be inoperative provided: |

a) Visual Alert operates
normally, and
b) Autopilot with Altitude Hold
normally.
2) Visual Alert C - 0 May be inoperative provided: |

a) Aural Alert operates normally,
and
b) Autopilot with Altitude Hold
normally.
C - 0 May be inoperative provided Enroute

operations (i.e., RVSM) do not |
require its use.
DATE: 01/21/2022
TABLE KEY
2. NO. INSTALLED
34. Navigation
Change
7. Course Heading Panel C 1 0 May be inoperative provided:

(CHP) (LR-60) a) Sensor Display Unit (SDU) is
operative,
b) FMS is operative and used for
course navigation, and
c) FMS Navigation and FMS
Heading (if installed) Modes
are used for Autopilot and
Flight Director Operation.
8. Course Heading Panel C 1 0

(CHP) Joy Stick (LR-60)
9. Navigation Equipment C - - May be inoperative provided: |

(VOR/ILS, LORAN, a) NAV 1 must be operative, and
RNAV, INS, b) System is not required by
VLF/Omega, Doppler, 14 CFR.
FMS, GPS, MLS,
TACAN)
10. Distance Measuring D - - Any in excess of those required by |

Equipment (DME) 14 CFR may be inoperative provided
System approach procedures do not require
its use.
11. Marker Beacon System C - - Any in excess of those required by |

14 CFR may be inoperative provided
approach procedures do not require
its use.
DATE: 01/21/2022
TABLE KEY
2. NO. INSTALLED
34. Navigation
Change
12. ATC Transponder and B - 0 May be inoperative provided: |

Automatic Altitude a) Operations do not require its
Reporting System use, and
b) Prior to flight, approval is
obtained from ATC facilities
having jurisdiction over the
planned route of flight.
NOTE: For RVSM operations, at least

one ATC Transponder and
Automatic Altitude Reporting
System must be operative.
D - 1 Any in excess of those required by

14 CFR may be inoperative.
1) Elementary and A - 0 May be inoperative provided: |

Enhanced Downlink a) Operations do not require its
Aircraft Reportable use, and
Parameters Not b) Repairs are made prior to
Required By 14 CFR completion of the next
scheduled maintenance visit.
2) ADS-B Out Extended B - 0 (O) May be inoperative provided |

Squitter prior to flight, authorization is |
obtained from ATC facilities |
having jurisdiction over the |
|
planned route of flight using an
approved authorization process. |
|
NOTE: Any ADS-B Out function that
|
operates normally may be
used.
C - 1 One may be inoperative |
D - 0 May be inoperative provided: |

a) Enroute operations do not |
require its use, and |
b) It is not required by 14 CFR. |
NOTE: Any ADS-B Out function that |

operates normally may be |
used. |
DATE: 01/21/2022
TABLE KEY
2. NO. INSTALLED
34. Navigation
Change
13. Automatic Direction C - - Any in excess of those required by |

Finding (ADF) 14 CFR may be inoperative.
Equipment
14. Radio Altimeter A 1 0 May be inoperative provided: |

a) Approach minimums or
operating procedures do not
require its use,
b) GPWS is considered
inoperative,
c) TCAS is considered
inoperative, and
2 flight-days. |
15. Weather Radar C - - Any in excess of those required by |

14 CFR may be inoperative.
16. Flight Management C 1 0 |

System (FMS) Data
Transfer Unit (DTU)
(LR-60)
17. Flight Director System C 2 0 May be inoperative provided: |

a) Command Bars are not
displayed,
b) Approach minimums do not
require use of Flight Director,
and
c) Autopilot is considered
inoperative.
Mode Button Light C 1 0 May be inoperative provided

flightcrew verifies that the Flight |
Director Mode will be annunciated in
the Primary Flight Display (PFD).
DATE: 01/21/2022
TABLE KEY
2. NO. INSTALLED
34. Navigation
Change
18. Windshear Detection, |

Guidance, and |
Avoidance System |
A. Installation Required |
By 14 CFR |
1) Windshear Warning and B - 0 (O) May be inoperative provided |

*** Flight Guidance System alternate procedures are established
(Reactive) and used.
NOTE: Operator’s alternate

procedures should include
reviewing windshear
avoidance and windshear
recovery procedure.
C - 0 (O) May be inoperative provided:

a) Alternate procedures are
established and used, and
b) Windshear Detection and
Avoidance System
(Predictive) operates
normally.
2) Windshear Detection B - 0 (O) May be inoperative provided

*** and Avoidance System alternate procedures are established |
(Predictive) and used.

reviewing windshear
recovery procedures.

b) Windshear Warning and Flight
Guidance System (Reactive)
operates normally.
(Continued)
DATE: 01/21/2022
TABLE KEY
2. NO. INSTALLED
34. Navigation
Change
18. Windshear Detection,

Guidance, and
Avoidance System
(Cont’d)
B. Installation Not Required |

By 14 CFR |
1) Windshear Warning and C - 0 (O) May be inoperative provided |

*** Flight Guidance System alternate procedures are established
(Reactive) and used.
2) Windshear Detection C - 0 (O) May be inoperative provided

*** and Avoidance System alternate procedures are established |
(Predictive) and used.
19. Weather Storm Scope C - 0 |

***
DATE: 01/21/2022
TABLE KEY
2. NO. INSTALLED
34. Navigation
Change
20. Terrain Awareness and |

Warning System (TAWS)
A. Class A TAWS |
Equipment Required
1) Ground Proximity A 1 0 (O) May be inoperative provided:

Warning System a) Alternate procedures are
(GPWS) established and used, and
2 flight-days. |
a) Modes 1-4 A 4 0 (O) May be inoperative provided:

2 flight-days. |
b) Test Mode A 4 0 May be inoperative provided: |

a) GPWS is considered
inoperative, and
2 flight-days. |
c) Glideslope Deviation(s) C - 1
(Mode 5)
d) Advisory Callouts B - 0 (O) May be inoperative provided

and used.
C - 0 (O) May be inoperative provided: |

a) Advisory Callout not required
by 14 CFR, and
(Continued)
DATE: 01/21/2022
TABLE KEY
2. NO. INSTALLED
34. Navigation
Change
20. Terrain Awareness and

(Cont’d)
A. Class A TAWS
Equipment
(Cont’d)
1) GPWS
(Cont’d)
e) Windshear Mode B 1 0 (O) May be inoperative provided

*** (Reactive) alternate procedures are established
and used.

reviewing windshear
recovery procedures.
C 1 0 (O) May be inoperative provided:

b) Windshear Detection and
Avoidance System
(Predictive) operates
normally.
2) Terrain System-Forward B 1 0 (O) May be inoperative provided

Looking Terrain alternate procedures are established
Avoidance (FLTA) and and used. |
Premature Descent Alert
(PDA) Function
3) Terrain Display C - 1
B - 0
4) Runway Awareness and C 1 0 |

*** Advisory System (RAAS)
(Continued)
DATE: 01/21/2022
TABLE KEY
2. NO. INSTALLED
34. Navigation
Change

(Cont’d)
B. Class B TAWS
Equipment Required
1) Ground Proximity A 1 0 (O) May be inoperative provided:
Warning System a) Alternate procedures are
(GPWS) established and used, and
2 flight-days. |
a) Modes 1 & 3 A 2 0 (O) May be inoperative provided:

2 flight-days. |
b) Test Mode A 1 0 May be inoperative provided:

a) GPWS is considered
inoperative, and
2 flight-days. |
c) Modes 2, 4, & 5 C 3 0 |
***
d) Advisory Callouts B - 0 (O) May be inoperative provided
and used.

a) Advisory Callouts not required
by 14 CFR, and
e) Windshear Mode C 1 0 (O) May be inoperative provided

*** (Reactive) alternate procedures are established
and used.
(Continued)
DATE: 01/21/2022
TABLE KEY
2. NO. INSTALLED
34. Navigation
Change

(Cont’d)
B. Class B TAWS
Equipment Required
(Cont’d)
2) Terrain System-Forward B 1 0
Looking Terrain
Avoidance (FLTA) and |
Premature Descent Alert
(PDA) Function
3) Terrain Display C - 0
***
4) Runway Awareness and C 1 0 |

*** Advisory System (RAAS)
C. Class C TAWS
Equipment
1) TAWS/GPWS C 1 0 (O) May be inoperative provided

*** alternate procedures are established
and used.
NOTE: Any Mode that operates

normally may be used.
21. Airborne Flight C - 0 |

*** Information System
(AFIS)
DATE: 01/21/2022
TABLE KEY
2. NO. INSTALLED
34. Navigation
Change
22. Traffic Alert and Collision B - 0 (M) May be inoperative provided: |

Avoidance System a) System is deactivated and
(TCAS I) secured, and
b) Enroute or approach
procedures do not require its
use.
C - 0 (M) May be inoperative provided:

a) Not required by 14 CFR,
b) System is deactivated and
secured, and
c) Enroute or approach
use.
23. Traffic Alert and Collision B - 0 (M) May be inoperative provided: |

Avoidance System a) System is deactivated and
(TCAS II) secured, and
use.
C - 0 (M) May be inoperative provided:

a) Not required by 14 CFR,
b) System is deactivated and
secured, and
use.
A. Combined Traffic Alert C 2 1 May be inoperative on the non-flying |

(TA) and Resolution pilot side provided: |
Advisory (RA) Dual a) TA and RA visual display is
Display System operative on the flying pilot
side, and
b) TA and RA audio function is
operative on the flying pilot
side.
(Continued)
DATE: 01/21/2022
TABLE KEY
2. NO. INSTALLED
34. Navigation
Change
23. Traffic Alert and Collision

Avoidance System
(TCAS II)
(Cont’d)
B. Resolution Advisory (RA) C 2 1 May be inoperative on non-flying pilot |

Display System side.
C - 0 (O) May be inoperative provided: |

a) Traffic Alert (TA) visual
display and audio functions
are operative,
b) TA ONLY Mode is selected by
the crew, and
use.
C. Traffic Alert (TA) Display C - 0 (O) May be inoperative provided: |

System a) RA visual display and audio
functions are operative, and
use.
D. Audio Function B 1 0 May be inoperative provided enroute |

or approach procedures do not
require use of TCAS.
E. Airspace Selection C - 0 |
*** Function
24. Traffic Alert Collision C - 0 |

Avoidance Device
(TCAD)
DATE: 01/21/2022
TABLE KEY
2. NO. INSTALLED
34. Navigation
Change
25. Non-Stabilized Magnetic B 1 0 (O) May be inoperative provided: |

Compass a) Any combination of two
Gyro or INS (IRU) Stabilized
Compass Systems operate
normally, and
b) Airplane is operated with
Dual Independent Navigation
Capability and under Positive
Radar Control by ATC on the
enroute portion of the flight.
B 1 0 (O) May be inoperative for flights that |

are entirely within areas of magnetic
unreliability provided at least two
Stabilized Directional Gyro Systems
are installed, operate normally, and
used in conjunction with approved
Free Gyro Navigation Techniques.
26. Flight Management |

System (FMS) |
A. Navigation Database A - 0 May be inoperative provided: |

a) Operations do not require its |
use, |
b) It is not used in a primary |
navigation system required by |
14 CFR, |
c) Alternate procedures are |
developed and used, |
d) The ICAO Flight Plan is |
updated (as required) to notify |
ATC of the navigation |
equipment status of the |
aircraft, and |
e) Is repaired within |
10 flight-days. |
NOTE: An out-of-currency or |
out-of-date navigation |
database is not authorized |
MMEL relief per 14 CFR. |
DATE: 01/21/2022
TABLE KEY
2. NO. INSTALLED
34. Navigation
Change
27. Automatic Dependent C - 0 (O) May be inoperative provided: |

Surveillance-Broadcast a) Alternate procedures are |
(ADS-B) System established and used, and |
NOTE: Any ADS-B function that |

used. |
D - 0 May be inoperative provided: |

a) Enroute operations do not |
require its use, and |

used. |
C - 1 One must be operative as required by |

14 CFR. |

used. |
A. Link and Display D - 0 NOTE: Cockpit Display Traffic |

Processor Unit (LDPU) Information (CDTI) display of
data from other Aircraft
Systems may be used.
B. Cockpit Display and D - 0 NOTE: ADS-B data transmissions |

Traffic Information may continue.
(CDTI)
C. CDTI Control Panel D - 0 May be inoperative provided: |

a) Flight ID can be set, and
b) Screen display is acceptable
to the flightcrew. |
D. Data Link Transmitter D - 0 |
E. Data Link Receiver D - 0 |

DATE: 01/21/2022
TABLE KEY
2. NO. INSTALLED
34. Navigation
Change
28. In-Flight Weather D - 0 |

*** Briefing System
29. Global Positioning C 2 0 (O) Except where enroute operations |

System (GPS) or approach procedures require its
(LR-60XR) use, may be inoperative provided:
a) Terrain/Obstacle Awareness
Functions of Terrain
Awareness and Warning |
System (TAWS) are |
considered not available for
use, and
NOTE: When operating with one

FMS inoperative,
FMS-computed takeoff and |
approach performance must
be verified using applicable
AFM data.
30. Flight Management C 2 0 (O) Except as required by 14 CFR |

Computer (LR-60XR) may be inoperative provided:
a) Fuel Used Readout is
considered not available for
use, and

FMS inoperative,
AFM data.
DATE: 01/21/2022
TABLE KEY
2. NO. INSTALLED
34. Navigation
Change
31. FMS Control Display C 2 1 (O) Except as required by 14 CFR, |

Units (LR-60XR) may be inoperative provided alternate
procedures are established and used
by the flightcrew. |

FMS inoperative,
AFM data.
32. Dataload Panel Portable C 1 0 |

Access Software
(LR-60XR)
33. Course Select Panel C 1 0 (O) May be inoperative provided |

(LR-60XR) alternate procedures are established
and used.
34. Integrated Flight C - 0 (O) May be inoperative provided |

*** Information System alternate procedures are established
(IFIS) File Server Unit and used for charts and NAV
(LR-60XR) database information.
35. Adaptive Flight Display A 2 1 (O) One Adaptive Flight Display |

With Ethernet (MFD) (MFD) may be inoperative provided:
(LR-60XR) a) The flight is made to a
location where repairs can be
made,
b) MFD reversionary is selected,
and
c) Approved Flight Manual
procedure for MFD failure is
followed.
DATE: 01/21/2022
TABLE KEY
2. NO. INSTALLED
34. Navigation
Change
36. Cursor Control Panel C 2 0 (O) May be inoperative provided |

(LR-60XR) Alternate Procedures are established
and used for charts and NAV
database information.
37. XM Satellite Weather C 1 0 (O) |

(LR-60XR)
DATE: 01/21/2022
TABLE KEY
2. NO. INSTALLED
35. Oxygen
Change
1. Oxygen System
(Cabin Only)
A. Passenger Configuration B 1 - As required by 14 CFR. |
B. Cargo Configuration C 1 0 |
C. Passenger Mask and C - 0 May be inoperative provided affected |

Stowage Position Seats are not useable and placarded, |
“DO NOT OCCUPY.” |
2. Portable Oxygen Bottles D - - Any in excess of those required by |

*** or Units (including Masks 14 CFR may be inoperative or |
and Hoses) removed provided: |
a) An inoperative or not properly |
serviced portable oxygen |
bottle/unit remains in a |
certified location until |
removed or serviced at the |
next suitable maintenance |
facility, |
c) Required distribution is |
maintained. |
NOTE 1: Inoperative portable oxygen |

bottles or units, removed |
from a certified location or |
removed from the aircraft, |
are subject to 49 CFR |
dangerous goods |
regulations. |
NOTE 2: Medical equipment installed |

in the aircraft as part of an |
EMS operation is not |
considered part of the |
normal complement of |
equipment. No MMEL relief |
applies to that equipment |
and 14 CFR maintenance |
and inspection |
requirements do not apply. |
DATE: 01/21/2022
TABLE KEY
2. NO. INSTALLED
35. Oxygen
Change
3. Crew Mask Storage Box B 2 0 (M) May be inoperative provided:

Door a) Associated Mask is secured in
the Stowage Box, and
b) Quick donning capability is
not affected.
4. Protective Breathing D - - Any in excess of those required by

Equipment (PBE) 14 CFR may be inoperative or |
removed provided: |
a) Inoperative PBE remains in a |
certified location until |
removed from the aircraft at |
the next suitable maintenance |
facility, |
c) Required distribution is |
maintained. |
NOTE: Inoperative PBEs, removed |

from a certified location or |
removed from the aircraft, are |
subject to 49 CFR dangerous |
goods regulations. |
5. Oxygen System C - 0 (O) May be missing provided there is

Discharge Indicator an adequate supply of oxygen for
(Oxygen Blowout Disc) passengers and crew for the intended
flight.
DATE: 01/21/2022
TABLE KEY
2. NO. INSTALLED
38. Water/Waste
Change
1. Potable Water System C - - (M) Individual Components may be

inoperative provided:
a) Associated Components are
deactivated or isolated, and
b) Associated System
Components are verified not
to have leaks.
NOTE: Any portion of System which

used.
C - - (M) May be inoperative provided:

a) System is drained, and
b) Procedures are established to
ensure that System is not
serviced.
2. Lavatory Toilet System C - - (M) Individual Components may be

inoperative provided:
deactivated or isolated, and
b) Associated System
Components are verified not
to have leaks.
NOTE: Any portion of System which

used.
(Continued)
DATE: 01/21/2022
TABLE KEY
2. NO. INSTALLED
38. Water/Waste
Change
2. Lavatory Toilet System

(Cont’d)
C - - (M) Associated Lavatory System(s)

may be inoperative provided:
deactivated or isolated to
prevent leaks,
b) The Pilot-in-Command will
determine if flight duration is
acceptable with Lavatory
unusable, and
c) Associated Toilet Lid is
secured DOWN and
placarded, “INOPERATIVE –
DO NOT USE.” |
NOTE: These provisions are not

intended to prohibit
inspections by crewmembers.
DATE: 08/15/2011
TABLE KEY
2. NO. INSTALLED
45. Central Maintenance System
Change
1. Maintenance Diagnostic D 1 0
Computer (MDC)
(LR-60XR)
DATE: 01/21/2022
TABLE KEY
2. NO. INSTALLED
46. Information Systems
Change
1. Electronic Flight Bag

*** (EFB) System |
A. EFB System C - - (O) May be inoperative provided |

*** (Installed EFB System) alternate procedures are established |
and used.
NOTE: Any function, program, or |

document which operates
normally may be used

B. Data Connectivity C - - (O) May be inoperative provided |

*** alternate procedures are established |
and used. |
D - 0 May be inoperative provided |

procedures do not require its use. |
C. Power Supply/Power C - 0 (M)(O) May be inoperative provided |

*** Connection alternate procedures are established |
and used.
NOTE: Depending upon |

configuration, power |
supply/power connection may |
require deactivation by (M) |
procedure. If not required, M |
symbol and this NOTE should |
not appear in the MMEL. |

DATE: 01/21/2022
TABLE KEY
2. NO. INSTALLED
46. Information Systems
Change
D. Mounting Device C - 0 (M)(O) May be inoperative provided: |

*** a) The associated EFB and |
hardware is secured by an
alternate means or removed
from the aircraft, and
D - 0 (M) May be inoperative provided: |

a) Associated EFB and |
hardware is stowed, |
secured by an alternate |
means, or removed from |
|
the aircraft, and
|
b) Procedures do not require its
|
use.
DATE: 01/21/2022
TABLE KEY
2. NO. INSTALLED
49. Airborne Auxiliary Power
Change
1. Auxiliary Power Unit D 1 0 (M)

*** (APU)
(STC No. ST00265NY) |
A. Generator System D 1 0 (M) |
2. Auxiliary Power Unit D 1 0 (M)

*** (APU)
(STC No. ST00280WI) |
A. Generator System D 1 0 (M) |
B. Bleed Air System D 1 0 (M) |

DATE: 01/21/2022
TABLE KEY
2. NO. INSTALLED
52. Doors
Change
1. Cabin/External Door |
WARNING System
A. ENTRY DOOR C 1 0 May be inoperative provided: |

Annunciator a) Crewmember verifies by
(Annunciator Does Not visual inspection before each |
Illuminate) departure that the Entry Door |
is CLOSED and LATCHED,
and
b) FASTEN SEAT BELT Sign
remains ON for the entire
flight.
B. AFT CAB DOOR C 1 0 May be inoperative provided: |

Annunciator a) Crewmember verifies by
(Annunciator Does Not visual inspection before each |
Illuminate) departure that the Aft Cabin |
Door is CLOSED and
LATCHED, and
b) FASTEN SEAT BELT Sign
remains ON during the entire
flight.
C. EXT DOORS C 1 0 May be inoperative provided: |

Annunciator a) Crewmember visually verifies
(Annunciator Does Not prior to every flight 2 locking |
Illuminate) pins extend and retract on |
both Tailcone Baggage and
Tailcone Servicing Door with
door latch handle operation
while door is in the open
position, and
b) Both doors are CLOSED and
LATCHED prior to engine
start.
DATE: 01/21/2022
TABLE KEY
2. NO. INSTALLED
52. Doors
Change
2. Tailcone Baggage Door C 1 0 May be inoperative provided the

Retaining Cable Cable does not interfere with Door
operation.
3. Keyable Door Lock D - 0 May be inoperative provided the Door

opens and closes normally and can
be secured CLOSED.
4. Cabin Door Lower C 1 0 May be inoperative provided a

Dampener crewmember opens and closes the |
Door.
5. Tailcone Access Door C 1 0 May be inoperative provided the Strut

Support Strut does not interfere with Door
operation.
DATE: 01/21/2022
TABLE KEY
2. NO. INSTALLED
74. Ignition
Change
1. Ignition Lights B 2 1 May be inoperative provided: |

a) All other indications during the
start are normal,
b) Generator functions normally
after Engine start, and
c) No FADEC faults occur on
affected Engine.
DATE: 08/15/2011
TABLE KEY
2. NO. INSTALLED
76. Engine Control
Change
1. Engine Synchronizer C 1 0 (M) May be inoperative provided:

System a) System is selected OFF, and
b) ENG SYNC System is
deactivated.
DATE: 01/21/2022
TABLE KEY
2. NO. INSTALLED
77. Engine Indicating
Change
1. N1 (Digital Display Only) C 2 0 May be inoperative provided

(LR-60) associated Pointer is operative.
2. N2 (Digital Display Only) C 2 0 May be inoperative provided

3. ITT (Digital Display Only) C 2 0 May be inoperative provided

4. Fuel Flow C 2 1 (O) One may be inoperative provided:

a) All other Engine Indicating
Systems, displays, and |
parameters are operative and
monitored,
b) Fuel Quantity Indicators are
operative, and
c) Weight and performance
calculations based on FMS
numbers are not relied on by
the flightcrew. |
A. Digital Display (LR-60) C 2 0 May be inoperative provided |

associated Pointer is operative.
5. Engine Vibration Monitor B 2 0
6. Engine Diagnostic D 1 0
System
7. Engine Chip Detector C 2 0

Light
DATE: 08/15/2011
TABLE KEY
2. NO. INSTALLED
78. Engine Exhaust
Change
1. Thrust Reverser System C 2 0 (M) May be inoperative provided:

a) Both Thrust Reversers are
DEACTIVATED,
b) AFM Operational Limitations
are observed, and
c) AFM Wet/Contaminated
Runway Data Addendum
Limitations are observed.

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U.S.

Master Minimum Equipment List (MMEL)

James B. Adams, Chair

Federal Aviation Administration (FAA)

Telephone: (816) 329-3233

PAGE NO. EXPLANATION OF CHANGE

Throughout: Item sequence numbers formatted to be consistent with policy

ATA 21 AIR CONDITIONING

Item 21-2: Changed “feet” to “ft” in list item b) for consistency.

21-3 21-9 and changed “feet” to “ft” in list item b).

21-11 and changed “feet” to “ft” in list item b).

21-5 Sub-item 21-14C): Changed “feet” to “ft” in list item b).

21-6 Item 21-19: Changed “feet” to “ft” in list item a).

Item 21-20: Changed “feet” to “ft” in list item b).

Item 22-4: Changed “feet” to “ft” in list item a).

23-2 Sub-item 23-5A): Added “is” in list item a).

Item 23-6: Lowercased “and” in Item Title.

Sub-item 23-11B): Added hyphen between “flight” and “days.”

Sub-item 23-11C): Lowercased “or” in Sub-Item Title.

23-6 Sub-item 23-18B : Revised per PL-120.

Sub-item 25-1 pluralized Item Title.

Sub-item 25-1C): Added comma after “takeoff” in column 4.

25-2 Sub-item 25-3: Corrected spelling of Item Title. Corrected spelling of

25-3 Item 25-5, A, Automatic External Defibrillator (AED) and/or Associated

Sub-item 25-5B): Lowercased “and/or” in Item Title..

Sub-item 25-5B: added comma after “missing” in column 4.

Item 25-7: Lowercased "and" in Item Title.

Item 25-9: Capitalized "Visor" in Item Title.

Item 25-10: Added hyphen between "calendar" and "days" in column 4.

25-5 Item 25-11: Portable Flashlights/Flashlight Holders replaced with updated

Item 25-12: Corrected spelling of "Flightcrew" in Item Title.

Sub-item 25-12A): Corrected spelling of "flightcrew" in list item c).

Sub-item 25-12D): Corrected spelling of "flightcrew" in column 4.

Sub-item 25-12E): Corrected spelling of "flightcrew" in column 4.

25-6 Item 25-14: Lowercased "and" in Item Title.

Item 25-15: Lowercased "and" in Item Title.

Item 25-17: Corrected spelling of “Underseat” in Item Title.

ATA 26 FIRE PROTECTION

26-1 Item 26-1: Lowercased "and" in Item Title.

Item 26-2 Portable Fire Extinguisher updated per PL-132.

Item 26-4: Changed "feet" to "ft" in list item b).

Item 26-5: Added "APU" in column 4.

ATA 27 FLIGHT CONTROLS

27-1 Item 27-1: Changed "feet" to "ft" in list item a).

27-3 Item 27-7: Lowercased "of" in Item Title.

Item 27-8: Lowercased "of" in column 4.

Sub-item 28-2 changed "pounds" to "lb."

28-2 Item 28-4: Lowercased "and" in Item Title.

28-3 Item 28-7: Changed "pounds" to "lb" in list item d).

ATA 30 ICE AND RAIN PROTECTION

Sub-item 30-1D): Changed "degrees" to its symbol in list item a).

30-2 Sub-item 30-3 Changed "degrees" to its symbol in list item.

Item 30-4: Changed "degrees" to its symbol in list item.

30-3 Item 30-5): Corrected spelling of "Co-Pilot."

Item 30-8): Changed "degrees" to its symbol in list item b).

Item 30-11) Corrected spelling of “flightcrew” in column 4.

ATA 31 INDICATING/RECORDING SYSTEMS

Sub-item 31-3E): Lowercased "of" and "or" in Item Title.

ATA 32 LANDING GEAR