U.S.

Department of Transportation
Federal Aviation Administration
Washington, D.C.

Master Minimum Equipment List

Revision: 13
Date: 07/23/2015

Beechcraft Corporation
Model 90 Series
65-90 / 65-A90 / B90 / C90 / E90 / C90A / C90GT / C90GTi

James B. Adams
Chair, Flight Operations Evaluation Board

Federal Aviation Administration

Kansas City Aircraft Evaluation Group
901 Locust Street, Department of Transportation Building
Kansas City, MO 64106

Telephone: (816) 329-3233

FAX: (816) 329-3241
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: BEECHCRAFT REVISION NO: 13 PAGE NO.
Model 90 Series DATE: 07/23/2015 I
CONTROL PAGE - TABLE OF CONTENTS
SYSTEM PAGES REVISION DATE

Cover Page - 13 07/23/2015

Control Page / Table of Contents I 13 07/23/2015
Highlights of Change II 13 07/23/2015
Definitions and Preamble III 12 01/15/2015
Guidelines for (O) & (M) Procedures IV THRU VIII 13 07/23/2015
11 Placards and Markings 11-1 13 07/23/2015
21 Air Conditioning 21-1 12 01/15/2015
21-2 11 06/16/2008
22 Auto Flight 22-1 12 01/15/2015
23 Communications 23-1, 2, 3, 4 13 07/23/2015
24 Electrical Power 24-1 11 06/16/2008
25 Equipment/Furnishings 25-1, 2, 4 13 07/23/2015
25-3, 5 12 01/15/2015
26 Fire Protection 26-1 12 01/15/2015
27 Flight Controls 27-1 13 07/23/2015
28 Fuel 28-1, 2 12 01/15/2015
30 Ice and Rain Protection 30-1 12 01/15/2015
31 Indicating/Recording Systems 31-1, 2 12 01/15/2015
32 Landing Gear 32-1 12 01/15/2015
33 Lights 33-1, 2 12 01/15/2015
34 Navigation 34-1 thru 34-14 12 01/15/2015
35 Oxygen 35-1 12 01/15/2015
46 Information Systems 46-1 11 06/16/2008
46-2 11b 07/30/2010
52 Doors 52-1 11 06/16/2008
61 Propellers 61-1 11 06/16/2008
73 Engine Fuel & Control 73-1 12 01/15/2015
77 Engine Indicating 77-1 11 06/16/2008
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: BEECHCRAFT REVISION NO: 13 PAGE NO.
Model 90 Series DATE: 07/23/2015 II
HIGHLIGHTS OF CHANGE

Revision 13 is issued with the following changes.

Various editing errors throughout including Item numbering that may have
been out of order.

Guidelines Renumbered 21-00-01 to 21-50-01 and moved to page V.

for (O) and Renumbered 23-00-05 to 23-00-02 for correct Item.
(M) Renumbered 23-00-04 to 23-50-04 for correct Item.
Procedures Added (M) procedure for 11-00-02
Added (M) procedure for 23-62-00-02
Added (M) procedure for 25-20-01-01 and -02.
Added (M) procedure for 25-20-01-05.
Added (O) procedure for 25-40-01.
Added (M) procedure for 25-50-03
Added (O) procedure for 34-61-01.

11-00-02 Added relief for a missing placard.

23-50-03 New Item number for correct JASC code.

23-50-04 New Item number for correct JASC code. Added Remarks and Exceptions.
Added relief for optional third audio panel.

23-62-00-02 Added (M) procedures per Policy Letter 120. Updated Remarks or
Exceptions per Policy Letter 120.
23-62-00- Right-indented item number for clearer identification.
02-01

25-20-01 Changed per PL-79, Passenger Seat Relief.

25-20-01-01 Changed per PL-79, Passenger Seat Relief. Added (M) procedure.
25-20-01-02 Changed per PL-79, Passenger Seat Relief.
25-20-01-03 Added per PL-79, Passenger Seat Relief.
25-20-01-04 Added per PL-79, Passenger Seat Relief.
25-20-01-05 Added per PL-79, Passenger Seat Relief. Added (O) procedure.
25-50-03 Add relief for Raisbeck Engineering Nacelle Overwing Storage Locker Door
Gas Spring. Added (M) procedure.

27-11-01 Changed Number Installed to 1.

27-21-01 Changed Number Installed to 1. Corrected bullet errors in Remarks and
Exceptions.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: BEECHCRAFT REVISION NO: 12 PAGE:
Model 90 Series DATE: 01/15/2015 III
DEFINITIONS AND PREAMBLE

DEFINITIONS

The required definitions listed are listed in Appendix B of MMEL Policy Letter 25.
Additional definitions may be included in an operator’s MEL as desired. Revision of PL-
025 does not require revision to the operator’s MEL.

PREAMBLE

The applicable preamble must be inserted in the operator’s MEL from current FAA
Policy Letter PL-34 or Policy Letter PL-36.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: BEECHCRAFT REVISION NO: 13 PAGE NO.
Model 90 Series DATE: 07/23/2015 IV
Guidelines for (O) & (M) Procedures

The 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 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, excluding Non-Essential Equipment & Furnishings
(NEF) (M) and (O) procedures:

11-00-02 (M) Maintenance procedure to replace illegible or missing Raisbeck |

Engineering wing locker loading limitation placard with a |
temporary placard.

21-10-01 (M) Requires operator to develop a maintenance procedure to

determine failure mode will have no adverse effect on aircraft
operation.

(O) Requires operator to develop an operational procedure to ensure

compliance with regulations, operational requirements and
passenger briefing information for unpressurized flight.

21-30-01-01 (M) Requires operator to develop a maintenance procedure to

ensure bleed air shutoff valve is secured in closed position.

21-30-01-02 (M) Requires operator to develop a maintenance procedure to

ensure bleed air shutoff valve(s) are secured in closed position.

(O) Requires operator to develop an operational procedure to ensure

compliance with regulations, operational requirements and
passenger briefing information for unpressurized flight.

21-30-01-03 (M) Requires the operator to develop a maintenance procedure to

ensure the effected valve(s) is secured in the closed position.

21-30-02 (M) Requires the operator to develop a maintenance procedure to

ensure safety valve is secured open.

(O) Requires operator to develop an operational procedure to ensure

compliance with regulations, operational requirements and
passenger briefing information for unpressurized flight.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: BEECHCRAFT REVISION NO: 13 PAGE NO.
Model 90 Series DATE: 07/23/2015 V
Guidelines for (O) & (M) Procedures
21-30-03 (O) Requires operator to develop an operational procedure to ensure
21-31-01 compliance with regulations, operational requirements and
21-32-02 passenger briefing information for unpressurized flight.
21-34-01

21-40-02 (M) Requires the operator to develop a maintenance procedure to

ensure no fuel leak or mechanical/electrical fault will cause a fire
or additional damage.

21-40-04 (O) Requires an operations procedure to record heater time.

21-50-01 (M) Requires the operator to develop a maintenance procedure to |

inspect the air conditioning system to ensure there is no |
interference with aircraft operation and system is deactivated. |

22-10-02 (M) Requires the operator to develop a maintenance procedure to

ensure no electrical or mechanical fault exists that will have an
adverse effect on any flight control function.

22-10-03 (M) Requires the operator to develop a maintenance procedure to

ensure no electrical or mechanical fault exists that will have an
adverse effect on any flight control function.

23-00-02 (M) Requires the operator to develop a procedure to deactivate the |

23-00-02-01 affected Flight Phone or Automatic Position Reporting System. |

23-10-01 (O) Requires the operator to develop an operations procedure to

ensure the SATCOM System operates normally.

23-40-01-01 (O) Requires the operator to develop an operations procedure to

specify how passengers will be briefed.

23-50-04 (M) Requires the operator to develop a procedure to deactivate the |

inoperative Audio Panel. |

23-60-00-02 (M) Requires the operator to deactivate Fixed ELT. |

23-62-00- (M) Requires the operator to develop a procedure to disconnect the

02-01 remote switch from the ELT and manually arm the ELT per the
manufacturer instructions.

25-20-01-01 (M) Requires operator to develop a procedure to secure seat back in |

25-20-01-02 the upright position. |

25-20-01-05 (M) Requires operator to develop procedure to alert crew of |

inoperative baggage restraining bar. |
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
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AIRCRAFT: BEECHCRAFT REVISION NO: 13 PAGE NO.
Model 90 Series DATE: 07/23/2015 VI
Guidelines for (O) & (M) Procedures
25-40-01 (O) Requires the operator to develop an operations procedure to |
ensure all in-flight waste is stored appropriately. |

25-50-01 (O) Requires the operator to develop an operations procedure to

ensure affected compartment remains closed and empty.
25-50-02 (M) Requires the operator to develop a maintenance procedure to
ensure available cargo restraint is acceptable for use.

25-50-03 (M) Maintenance procedure to ensure Raisbeck Engineering wing |

lockers with an inoperative door gas spring close flush with |
nacelle. |

25-60-02 (M) Requires the operator to develop a maintenance procedure to

deactivate and secure affected equipment.

27-31-01 (M) Requires the operator to develop a maintenance procedure to

deactivate Electric Trim and ensure there is no interference with
operation of manual trim.

28-41-01 (O) Requires the operator to develop an operations procedure to

ensure fuel balance and quantity on board meets the
requirements for the intended flight.

28-41-02 (O) Requires the operator to develop an operations procedure to

ensure fuel balance and quantity on board meets the
requirements for the intended flight. Flight must be planned using
main wing fuel quantity only.

28-41-03 (M) Requires the operator to develop a maintenance procedure to

ensure no fuel or electrical fault adversely affects aircraft
operation.

28-41-04 (O) Requires the operator to develop an operations procedure to

ensure fuel balance and quantity on board meets the
requirements for the intended flight.

28-41-05 (O) Requires the operator to develop an operations procedure to

ensure fuel balance and quantity on board meets the
requirements for the intended flight. Flight must be planned
considering 28 gallons unusable fuel on associated side.

30-00-03 (M) Requires the operator to develop a maintenance procedure to

deactivate system & ensure no adverse effect on aircraft
operation.

31-20-02 (O) Requires an operations procedure to record flight time.

U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: BEECHCRAFT REVISION NO: 13 PAGE NO.
Model 90 Series DATE: 07/23/2015 VII
Guidelines for (O) & (M) Procedures
32-42-01 (O) Requires the operator to develop an operations procedure to
prevent movement of the aircraft when parked or stopped.

33-20-02 (O) Requires the operator to develop an operations procedure to

appropriately brief the passengers.

34-00-02 (O) Operations procedure must identify all systems and functions
affected by the inoperative MFD specific to each installation and
provide for MEL deferral of those affected systems.

34-00-03 (O) Operations procedure to verify the MPU is operative.

34-44-01 (O) Operations procedure to ensure pilot planning and awareness of

terrain clearance.

34-44-01-01 (O) Operations procedure to ensure alternate procedures are

established and used for inoperative GPWS.

34-44-01- (O) Operations procedure to ensure alternate procedures are

01-01 established and used for inoperative mode(s).

34-44-01- (O) Operations procedure to ensure alternate procedures are

01-02 established and used for inoperative GPWS.

34-44-01-02 (O) Operations procedure to ensure alternate procedures are

established and used for inoperative advisory callout(s).

34-44-01-03 (O) Operations procedure to ensure alternate procedures are

established and used for inoperative windshear mode.

34-44-01-04 (O) Operations procedure to ensure alternate procedures are

established and used for inoperative FLTA/PDA mode.

34-44-02 (M) Procedure to deactivate and secure the Radar Altimeter System.
(O) Alternate procedures for terrain clearance awareness and
approach minimums with the radar altimeter inoperative.

34-45-01 (M) Maintenance procedure to deactivate and secure the system.

(O) Operations procedures to ensure enroute and approach
procedures do not require its use.

34-45-02 (M) Maintenance procedure to deactivate and secure the system.

34-45-02-01 (O) Operations procedure to ensure TA and RA display and audio

functions are operative.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: BEECHCRAFT REVISION NO: 13 PAGE NO.
Model 90 Series DATE: 07/23/2015 VIII
Guidelines for (O) & (M) Procedures
34-45-02-02 (O) Operations procedure to ensure TA ONLY mode is selected and
all TA functions/elements are operative.

34-45-02-03 (O) Operations procedure to ensure RA display/functions are

operative.

34-52-01-02 (O) Alternate procedure for operation with inoperative ADS-B

Squitter Transmissions.

34-61-01 (O) Operations procedure to verify status and suitability of Navigation |

Facilities used for route of flight. |

46-00-01 (O) Procedure for alternate means to provide flight operating

information in current and appropriate form accessible for each
flight at the pilot station.

46-00-01-01 (O) Procedure to ensure adequate backup or Battery Power Supply

is available to operate the EFB for the entire flight duration.

46-00-01-02 (M) Procedure to secure Mounting Device in an acceptable location

or remove it from the aircraft.
(O) Procedure for alternate means to provide flight operating
information in current and appropriate form accessible for each
flight at the pilot station if the normal use of the EFB is not
available.

46-00-01-03 (O) Procedures for alternate means to operate the EFB without
automatic data input.

46-00-02-01 (O) Operations procedure to ensure alternate procedures are

established and used for aeronautical information.

46-00-02-02 (O) Operations procedure to ensure alternate procedures are

established and used for aeronautical information.

46-00-02-03 (O) Operations procedure to ensure alternate procedures are

established and used for information from inoperative data link.

46-00-02-04 (O) Operations procedure to ensure alternate procedures are

established and used for information from inoperative data link.

52-70-01 (O) Requires operator to develop an operational procedure to ensure

compliance with regulations, operational requirements and
passenger briefing information for unpressurized flight.

73-31-01 (M) Maintenance procedure to ensure no fuel or electrical fault

adversely affects aircraft operation.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT: BEECHCRAFT REVISION NO: 13 PAGE NO:
Model 90 Series DATE: 07/23/2015 11-1
SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & NUMBER INSTALLED
ITEM NUMBER REQUIRED FOR DISPATCH
REMARKS OR EXCEPTIONS
11 PLACARDS AND
MARKINGS

00-01 “Fasten Seat Belt C - - One or more placards may be illegible

While Seated” or missing provided a legible sign or
Placard placard is visible from each occupied
passenger seat.

00-02 Raisbeck C 2 0 (M) May be illegible or missing |

Engineering Nacelle provided no cargo is stored within |
Overwing Storage affected locker. A locker may become |
Lockers Loading eligible for cargo with a temporary |
Limitation Placard placard. |
U.S. DEPARTMENT OF TRANSPORTATION
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AIRCRAFT: BEECHCRAFT REVISION NO: 12 PAGE NO:
Model 90 Series DATE: 01/15/2015 21-1
SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & NUMBER INSTALLED
ITEM NUMBER REQUIRED FOR DISPATCH
REMARKS OR EXCEPTIONS
21 AIR
CONDITIONING

10-01 Cabin Supercharger C 1 0 (M)(O) May be inoperative for

(65-90, 65-A90, unpressurized flight.
B90)

30-01 Bleed Air Shutoff

Valve(s)

-01 Model B90 C 1 0 (M) May be inoperative in the closed

position.

-02 Models C90, C90A, C 2 1 (M) One may be inoperative in the

C90GT, E90, closed position for pressurized flight.
C90GTi

C 2 0 (M)(O) May be inoperative in the

closed position for unpressurized flight.

-03 Model 65-A90-1 C 2 0 (M) May be inoperative provided:

When Modified By a) Affected valve(s) is/are verified
MRI Number 02-21- in the closed position, and
01, b) Windshield heat is operative.
dated 06/01/02

30-02 Safety Valve C 1 0 (M)(O) May be inoperative provided:

a) Airplane remains
unpressurized, and
b) The dump valve is secured
open.

30-03 Outflow Valve C 1 0 (O) May be inoperative provided:

a) Airplane remains
unpressurized, and
b) The dump valve is open.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
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AIRCRAFT: BEECHCRAFT REVISION NO: 11 PAGE NO:
Model 90 Series DATE: 06/16/2008 21-2
SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & NUMBER INSTALLED
ITEM NUMBER REQUIRED FOR DISPATCH
REMARKS OR EXCEPTIONS
21 AIR
CONDITIONING

31-01 Pressurization C 1 0 (O) May be inoperative for

Controller unpressurized flight.

32-01 Cabin Rate Of Climb C 1 0 May be inoperative for pressurized

Indicator flight provided Differential
Pressure/Cabin Altitude Indicator is
operative.

32-02 Differential C 1 0 (O) May be inoperative for

Pressure/Cabin unpressurized flight.
Altitude Indicator

34-01 Cabin Altitude C 1 0 (O) May be inoperative for

Warning System unpressurized flight.

40-01 Electric Heater C 1 0

40-02 Combustion Heater C 1 0 (M)

40-03 Combustion Air C 1 0 May be inoperative provided

Blower combustion heater is not operated.

40-04 Heater Hourmeter C 1 0 (O)

50-01 Air Conditioner C 1 0 (M)

60-01 Automatic C 1 0 May be inoperative provided manual

Temperature control is operative.
Controller
U.S. DEPARTMENT OF TRANSPORTATION
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Model 90 Series DATE: 01/15/2015 22-1
SYSTEM, REPAIR CATEGORY
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ITEM NUMBER REQUIRED FOR DISPATCH
REMARKS OR EXCEPTIONS
22 AUTO FLIGHT

10-01 Autopilot System C - 0 (M) May be inoperative provided

operations do not require its use.

NOTE: RVSM is not authorized.

10-02 Yaw Damper C 1 0 (M)

(Except Winglet
STC #SA02054SE)

(Winglet STC C 1 0 (M) May be inoperative provided

#SA02054SE only) airplane is operated at or below FL 240

10-03 Autopilot Disconnect C 2 1 One may be inoperative on the non-

(AP/YD/DISC Trim flying pilot side provided:
Switches) a) Autopilot is not used below
1,500 feet AGL, and
b) Approach minimums do not
require the use of the autopilot.

(Except GFC-700) B 2 0 May be inoperative provided:

a) Autopilot is not used, and
b) Second level switch trim
interrupt function remains
operative.

NOTE: RVSM is not authorized.

(Except GFC-700) B 2 0 (M) May be inoperative provided:

a) Autopilot is considered
inoperative,
b) Electric Elevator Trim is
considered inoperative, and
c) Yaw Damper is considered
inoperative.

NOTE: RVSM is not authorized.

U.S. DEPARTMENT OF TRANSPORTATION
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AIRCRAFT: BEECHCRAFT REVISION NO: 13 PAGE NO:
Model 90 Series DATE: 07/23/2015 23-1
SYSTEM, REPAIR CATEGORY
SEQUENCE NUMBERS & NUMBER INSTALLED
ITEM NUMBER REQUIRED FOR DISPATCH
REMARKS OR EXCEPTIONS
23 COMMUNICATIONS

00-01 Ground D - 0
*** Communications
Power

00-02 Flight Phone System D - 0 (M) |

***

-01 Automatic Position D - 0 (M) |

*** Reporting Functions

10-01 High Frequency (HF) D - - Any in excess of those required by 14

Communication CFR may be inoperative.
System

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
established and used.

12-01 VHF and/or UHF D - - Any in excess of those required by 14

Communication CFR may be inoperative provided it is
System not powered by an emergency power
source and not required for emergency
procedures.

12-02 FM Communications D - 0 May be inoperative provided affected

*** System (TDFM-136) FM Radio remains OFF.
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23 COMMUNICATIONS

40-01 Passenger Address

System

-01 Passenger D 1 0 (O) May be inoperative provided

Configuration alternate normal and emergency
procedures and/or operating
restrictions are established and used.

-02 Cargo Configuration D 1 0

40-02 Voice Activated C - 0

Interphone

50-01 Flight Deck

Headsets
Earphones/
Headphones and
Boom Microphones

-01 Headset Boom A - 0 May be inoperative provided:

Microphones a) Associated hand microphone is
installed and operates normally,
and
b) Repairs are made within three
flight days.

D - - Any in excess of those required by

regulation may be inoperative.

-02 Headset Earphone/ C - 1 May be inoperative provided

Headphones associated flight deck speaker
operates normally.

D - - Any in excess of those required by

regulation may be inoperative.

-03 Active Noise D - 0 May be inoperative provided normal

Canceling/Reduction audio function of headset is operative.
Function
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23 COMMUNICATIONS

50-02 Flight Deck Hand C - 0 May be inoperative provided

Microphones associated boom microphone operates
normally.

D - 0 Any in excess of those required by

regulation may be inoperative.

50-03 Radio Tuning Unit C 1 0 May be inoperative provided:

(RTU) a) CDU TUNE page is selected
(Proline 21 Only) and used to tune radios, and
b) EMER TUNE switch is installed
and operative.

50-04 Audio Panel C 2 1 (M) Right side panel may be |

(Proline 21 Only) inoperative provided aircraft is |
operated single-pilot. |

*** (Third Panel Only) D 3 0 (M) |

50-05 Cockpit Speaker C 2 0 May be inoperative provided an

System operative headset is provided for each
(Includes Audio crewmember.
Amp.)

60-01 Static Discharge C - - One wick may be missing or broken

Wicks from:
a) Each wing (includes aileron)
b) Each side of horizontal
stabilizer, and
c) Vertical Stabilizer (includes tail
cone and ventral fin(s).

NOTE: A maximum of three (3) Static

Wicks may be broken or missing.
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23 COMMUNICATIONS

62-00 Emergency Locator

Transmitter (ELT)

-01 Survival Type ELTs D - - Any in excess of those required by 14

CFR may be inoperative or missing.

-02 Fixed ELTs A - 0 (M) May be inoperative provided: |

a) System is deactivated, and |
b) Repairs are made within 90 |
days. |

A - 0 May be missing provided 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. |

-01 Remote Switch D 1 0 (M) May be inoperative provided: |

*** a) Remote switch is disconnected
from the ELT, and
b) ELT switch is placed in the
ARM position.

70-01 Cockpit Voice A 1 0 May be inoperative provided:

Recorder (CVR) a) Flight Data Recorder (FDR)
(With Flight Data operates normally, and
Recorder (FDR) b) Repairs are made within three
Installed (3) flight days.

(Without Flight Data A 1 0 May be inoperative provided repairs

Recorder (FDR) are made within three flight days.
Installed)

(For other than Air A 1 0 May be inoperative provided repairs

Carrier or are made in accordance with 14 CFR.
Commercial
Operator Certificate
Holder)
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24 ELECTRICAL
POWER

22-01 Inverters B 2 1 One may be inoperative for day VFR.

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REMARKS OR EXCEPTIONS
25 EQUIPMENT/
FURNISHINGS

00-00 “Fasten Seat Belt MOVED to chapter 11.

While Seated” Sign
Or Placard

10-01 Cockpit Shoulder B - 1 May be inoperative on right side

Harness provided the seat is not occupied.

20-01 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) 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.

-01 Recline Mechanism D - - (M) May be inoperative and seat |

occupied provided seat back is |
secured in the full upright position. |

-02 Armrest with Recline D - - (M) May be inoperative or missing |

Mechanism and seat occupied provided: |
a) Armrest does not block an |
Emergency Exit, |
b) Armrest does not restrict any |
passenger from access to the |
main aircraft aisle, and |
c) If armrest is missing, seat is |
secured in the full upright |
position. |
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25 EQUIPMENT/
FURNISHINGS

20-01 Passenger Seats

(Continued)

-03 Armrest without D - - May be inoperative or missing and seat |

Recline Mechanism 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. |

-04 Seat Belt Air Bag |

Restraint Systems |

-01 Seat Belt Air Bags D - - May be inoperative provided affected |

Required by CFR seat is blocked and placarded DO NOT |
OCCUPY. |

-02 Seat Belt Air Bags D - - May be inoperative or disconnected |

Not Required By provided seat belt operates normally. |
CFR |

-05 Under seat Baggage C - - (O) May be inoperative provided: |

Restraining Bars a) Baggage is not stowed under |
seat with inoperative restraining |
bar, |
b) Associated seat is placarded |
DO NOT STOW BAGGAGE |
UNDER THIS SEAT, and |
c) Procedures are established to |
alert Crew of inoperative |
restraining bar. |
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25 EQUIPMENT/
FURNISHINGS

20-02 Non-Essential - 0 May be inoperative, damaged, or

*** Equipment & missing provided the item(s) is
Furnishings (NEF) deferred in accordance with the
operator’s NEF deferral program. The
NEF program, and procedures, are
outlined in the (insert name) Manual.
(M) & (O) procedures, if required, must
be available to flight crew.

NOTE: Exterior Lavatory Door Ash

Trays are not considered NEF
items.

40-01 Waste Receptacles C - - (O) May be inoperative provided:

Access a) The Container is EMPTY and
Doors/Covers the access is SECURED to
prevent waste introduction into
the Compartment, and
b) Procedures are established to
ensure that sufficient Galley
Waste Receptacles are
available to accommodate all
waste that may be generated
on a flight.

40-02 Exterior Lavatory A 1 0 May be missing provided it is replaced

Door Ashtrays within three calendar days.

50-01 Storage C - - (O) May be inoperative provided:

Compartments / a) Procedures are established to
Closets secure Compartment closed,
b) Any Emergency Equipment
located in affected compartment
is considered inoperative, and
c) Affected Compartment is not
used for storage of any item(s)
except for those permanently
affixed.
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25 EQUIPMENT/
FURNISHINGS

50-02 Cargo Restraint C - - (M) May be inoperative or missing

Systems provided acceptable cargo loading
limits from an approved source, i.e., an
Approved Cargo Loading Manual,
Cargo Handling Manual, or Weight and
Balance Document are observed.

C - - May be inoperative or missing provided

Cargo Compartment remains EMPTY.

50-03 Raisbeck D 2 0 (M) May be inoperative provided gas |

Engineering Nacelle spring shaft moves freely and does not |
Overwing Storage hinder the opening and closing of the |
Lockers Door Gas locker door. |
Spring |

60-01 Emergency Medical

Equipment

-01 Automatic External D - 0 May be incomplete, missing, or

Defibrillator (AED) inoperative.
And/Or Associated
Equipment

-02 Emergency Medical D - 0 May be incomplete, missing, or

Kit (EMK) And/Or inoperative.
Associated
Equipment

-03 First Aid Kit (FAK) D - - Any in excess of those required by 14

And/Or Associated CFR may be incomplete or missing
Equipment provided required distribution is
maintained.

60-02 EMS Equipment C - 0 (M) May be inoperative provided the

*** inoperative system/component is
deactivated and secured.

60-03 Pyrotechnic D - 0 Any in excess of those required by 14

Signaling Devices CFR may be inoperative or missing.
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61-01 Flotation Equipment D - - Any in excess of those required by 14
*** (Life Vest, Life Raft) CFR may be inoperative or missing.
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26 FIRE PROTECTION

20-01 Engine Fire C 2 0

*** Extinguisher
Systems

22-01 Portable Fire D - - Any in excess of those required by 14

Extinguisher CFR may be inoperative or missing
provided:
a) Inoperative fire extinguisher is
tagged inoperative, removed
from the installed location and
placed out of sight so it cannot
be mistaken for a functional
unit, and
b) Required distribution is
maintained.
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27 FLIGHT
CONTROLS

11-01 Aileron Trim Tab C 1 0 May be inoperative provided: |

Indicator a) Tab is visually checked for full
range of operation,
b) Tab operation is not restricted,
and
c) Tab is positioned to neutral
prior to each departure and
neutral position is verified by
visual inspection.

20-01 Rudder Boost C 1 0

System (C90A,
C90GT & C90GTi
Only)

21-01 Rudder Trim Tab C 1 0 May be inoperative provided: |

Indicator a) Tab is visually checked for full |
range of operation,
b) Tab operation is not restricted, |
and
c) Tab is positioned to neutral |
prior to each departure and
neutral position is verified by
visual inspection.

31-01 Electric Elevator C 1 0 (M) May be inoperative provided:

Trim a) Manual trim is operative and
unaffected, and
b) Autopilot is not used.

51-01 Flap Position C 1 0 May be inoperative provided:

Indicator a) Flaps are visually checked for
full travel and flap operation is
not restricted, and
b) Flaps are visually checked for
proper setting prior to each
departure.
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28 FUEL

22-01 Standby Fuel Boost C 2 1 One may be inoperative.

Pumps (65-90, E90)
NOTE: AFM limitations must be
observed.

24-01 Fuel Transfer C 2 0 May be inoperative provided:

Pumps (65-90, 65- a) Usable fuel is reduced by 28
A90, B90, C90, gallons on the side(s) with
C90A, C90GT, inoperative pump, and
C90GTi) b) Fuel Quantity Indicators are
operative.

24-02 Auxiliary Fuel C 2 0 May be inoperative provided:

Transfer Systems a) All fuel contained in the auxiliary
(E90) tank(s) on the inoperative
side(s) is considered unusable,
and
b) Fuel quantity indicating system
is operative.

40-01 NO FUEL XFR C 2 1 One may be inoperative provided both

Annunciators Fuel Quantity Indicators are operative.
(65-90, 65-A90,
B90, C90, C90A,
C90GT, C90GTi)

40-02 AUX EMPTY C 2 1 One may be inoperative provided both

Annunciators (E90) Fuel Quantity Indicators are operative.

41-01 Main Fuel Quantity C 2 1 (O) One may be inoperative provided:

Indicators a) A reliable means is established
(65-90, 65-A90, to determine that fuel quantity
B90) on board meets the regulatory
requirements for the flight,
b) Both Fuel Flow Indicators are
operative,
c) Both Auxiliary Fuel Quantity
Indicators are operative, and
d) Both NO FUEL XFR
Annunciators are operative.
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28 FUEL

41-02 Fuel Quantity C 2 1 (O) One may be inoperative provided:

Indicators (E90) a) A reliable means is established
to determine that fuel quantity
on board meets the regulatory
requirements for the flight,
b) Both AUX EMPTY Lights are
operative, and
c) Both Fuel Flow Indicators are
operative.

41-03 Fuel Totalizer C 1 0 (M)

(Foxboro System
Only)

41-04 Auxiliary Fuel C 2 1 (O) One may be inoperative provided:

Quantity Indicators a) Both Main Fuel Quantity
(65-90, 65-A90, Indicators are operative, and
B90) b) A reliable means is established
to determine that fuel quantity
on board meets the regulatory
requirements for the flight.

41-05 Fuel Quantity C 2 1 (O) One may be inoperative provided:

Indicators (C90, a) A reliable means is established
C90A, C90GT, to determine that fuel quantity
C90GTi) on board meets the regulatory
requirements for the flight,
b) Both NO FUEL XFR
Annunciators are operative, and
c) Both Fuel Flow Indicators are
operative.

41-06 Shadin Fuel Flow MOVED to chapter 73.

*** Indicator
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30 ICE & RAIN
PROTECTION

00-01 Stall Warning C 1 0 May be inoperative provided aircraft is

Heater not operated in known or forecast icing
conditions.

00-02 Heated Fuel Vents C 2 0 May be inoperative provided aircraft is

not operated in known or forecast icing
conditions.

00-03 Brake Deice System C 1 0 (M)

***

10-01 Surface Deice C 1 0 May be inoperative provided aircraft is

System (Wing, not operated in known or forecast icing
Vertical And conditions.
Horizontal
Stabilizer)

30-01 Pitot Heaters B 2 0 May be inoperative provided:

a) Aircraft is not operated in
Instrument Meteorological
Conditions (IMC),
b) Aircraft is not operated in
known, forecast, or AFM-
defined icing conditions, and
c) Not required by 14 CFR.

40-01 Windshield Heat C 2 0 May be inoperative provided aircraft is

not operated in known or forecast icing
conditions.

40-02 Windshield Wipers C 2 0 May be inoperative provided flight is

not conducted in precipitation within 5
nautical miles of the airport of takeoff
or intended landing.

60-01 Propeller Deice C 2 0 May be inoperative provided aircraft is

Systems not operated in known or forecast icing
conditions.
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31 INDICATING/
RECORDING
SYSTEMS

20-01 Clock With Sweep C - 0 May be inoperative for VFR.

Second Hand, Or
Electric Digital Clock
C - 1

20-02 Flight Hour C 1 0 (O)

Recorder

30-01 Flight Data Recorder C 1 0 Any in excess of those required by 14

*** (FDR) System CFR may be inoperative.
(Holder of an Air A - 0 May be inoperative provided:
Carrier or a) Cockpit Voice Recorder (CVR)
Commercial operates normally,
Operator Certificate) b) Airplane is not dispatched from
a designated airport as listed in
the operator’s MEL unless:
1. The FDR failure occurs
after taxi 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
d) Repairs are made within three
flight days.

(Continued)
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31 INDICATING/
RECORDING
SYSTEMS

30-01 Flight Data Recorder

*** (FDR) System
(Continued)

-01 FDR Recording A - - Up to three (3) recording parameters

Parameters may be inoperative provided:
Required By 14 CFR a) Cockpit Voice Recorder (CVR)
operates normally, and
b) Repairs are made within 20
calendar days.

-02 FDR Recording A - - May be inoperative provided repairs

Parameters Not are made prior to completion of the
Required By 14 CFR next heavy maintenance check.

(Operators Other C - 1 Any in excess of those required by 14

Than Holders Of Air CFR may be inoperative.
Carrier Or
Commercial
Operator
Certificates)

A - 0 May be inoperative provided repairs

are made in accordance with 14 CFR.
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32 LANDING GEAR

42-01 Parking Brake C 1 0 (O)

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33 LIGHTS

10-01 Cockpit/ Flight Deck C - - Individual lights may be inoperative

Flight Compartment provided:
And Instrument a) Remaining Lighting System
Lighting System lights are sufficient to clearly
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
flight crewmembers eyes, and
c) Lighting configuration and
intensity is acceptable to the
flight crew.

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

20-01 Cabin Light System C - - (O) Individual lights may be inoperative

provided:
a) Emergency Exit Lighting
System is operative, if installed,
b) Sufficient Lighting is available
for crew to perform required
duties, and
c) Sufficient Lighting is operative
for passenger carrying
operations at night.

20-02 Passenger Notice C 1 0 (O) May be inoperative provided

System (Fasten appropriate verbal briefings are given
Seat Belt-No to the passengers.
Smoking)
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33 LIGHTS

30-01 Baggage C - 0
Compartment Lights

40-01 Landing Lights C 2 0 May be inoperative for day operations.

C 2 1 One may be inoperative for night

operations provided Taxi Light is
operative.

40-02 Taxi Light C 1 0

40-03 Wing Icing Detection C - 0 May be inoperative provided:

Lights a) Aircraft is not operated in
known or forecast icing
conditions at night, and
b) Ground deicing procedures do
not require their use.

C 2 1 One may be inoperative provided:

a) The left light is operative for
single pilot operations, and
b) Ground deicing procedures do
not require their use.

40-04 Position Lights C 3 0 May be inoperative for day operations.

40-05 Anti-Collision B 1 0 May be inoperative for day operations.

Beacon Light
System

40-06 Strobe Light System C 1 0

40-07 Recognition Lights C 2 0

40-08 Pulse Light System D 1 0

***
40-09 Logo Lights D - 0
***
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34 NAVIGATION

00-01 Flight Profile D - -

*** Advisory System

00-02 Independent Multi- C 1 0 (O) May be inoperative provided:

*** Function Display a) MFD system does not provide
(Excludes EFIS any primary flight or engine
Equipped Aircraft) instrument display, and
b) MFD integrated systems are
considered inoperative.
• Weather Radar
• TCAS Display
• Navigation Map Display
• TAWS Display
• Thunderstorm Detection

00-03 Multifunction Display C 1 0 (O) May be inoperative provided the

(Collins EFIS-84 Multifunction Processing Unit (MPU) is
Only) operative
(3 tube or 5 tube)
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34 NAVIGATION

13-01 Mechanical Vertical B - - Any in excess of those required by 14

Speed Indicators CFR may be inoperative.
(Except Proline 21
equipped) NOTE: Any required indicator must be
visible from pilot flying side.

14-01 Mechanical Airspeed B - 1 May be inoperative provided an

Indicators (Except operative pneumatic or independent
Proline 21 equipped) standby airspeed indicator is visible
from pilot flying side.

NOTE: Independent standby airspeed

indicator may be an electronic display
provided display is powered
independent of primary electrical
system.

16-01 Mechanical B - 1 May be inoperative provided an

Altimeter, operative pneumatic or independent
Barometric Pressure standby altimeter is visible from pilot
Adjustable (Except flying side.
Proline 21 equipped)
NOTE: Independent standby
altimeter may be an electronic
display provided display is powered
independent of primary electrical
system.

16-02 Altitude Alerting C - 0 May be inoperative provided

System (Except operations do not require its use.
Proline 21 equipped)
NOTE: RVSM is not authorized.
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34 NAVIGATION

21-01 Mechanical B - 1 May be inoperative provided an

Gyroscopic Pitch operative gyroscopic or independent
And Bank Indicators standby attitude indicator is visible
(Except Proline 21 from pilot flying side.
equipped)
NOTE: Independent standby attitude
indicator may be an electronic display
provided display is powered
independent of primary electrical
system.

22-01 Mechanical B - - Any in excess of those required by 14

Gyroscopic CFR may be inoperative provided non-
Directional Indicator stabilized magnetic compass is
Systems (Except operative.
Proline 21 equipped)
NOTE: Any required indicator must be
visible from pilot flying side.

22-02 Radio Magnetic C - - May be inoperative provided:

Indicator (RMI) a) Magnetic Compass is operative,
(Except Proline 21 and,
equipped) b) Any navigation source not
displayed on another indicator
is considered inoperative.
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34 NAVIGATION

23-01 Non-Stabilized B 1 0 May be inoperative provided any

Magnetic Compass combination of three Gyro or
IRU/AHRS stabilized compass
systems are operative

B 1 0 May be inoperative provided:

a) Any combination of two gyro or
IRU/AHRS stabilized compass
systems are operative, and
b) Aircraft is operated with dual
independent navigation
capability and under positive
radar control by ATC on the
enroute portion of the flight.

B 1 0 May be inoperative for flights that are

entirely within areas of magnetic
unreliability provided at least two
stabilized directional gyro systems are
installed, operative, and used in
conjunction with approved free gyro
navigation techniques.

24-01 Mechanical B - - Any in excess of those required by 14

Gyroscopic Rate Of CFR may be inoperative.
Turn/Slip Skid
Indicators (Except NOTE: Any required indicator must be
Proline 21 visible from pilot flying side.
equipped)

25-01 Flight Director C 1 0 May be inoperative provided approach

(Except Proline 21 minimums are not based on its use.
equipped)
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34 NAVIGATION

31-01 VOR/ILS System D 2 1 One may be inoperative provided:

a) Not required by 14 CFR, and
b) Operations do not require its use

C - 0 May be inoperative provided:

a) Not required by 14 CFR, and
b) Operations do not require its use

32-01 Glide Slope System C - - May be inoperative provided:

a) Not required by 14 CFR, and
b) Operations do not require its use

34-01 Marker Beacon C - 0 May be inoperative provided:

System a) Not required by 14 CFR, and
b) Operations do not require its use

42-01 Weather C 1 0 As required by 14 CFR.

Radar/Thunderstorm
Detection
Equipment
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34 NAVIAGTION

44-01 Terrain Awareness A - 0 (O) May be inoperative provided:

Warning System a) Alternate procedures are
(TAWS)/Ground established and used, and
Proximity Warning b) Repairs are made within two (2)
System (GPWS) flight days.
(Class A Or B
Required)

(Class C TAWS Or C - 0 (O) May be inoperative provided

GPWS Not required alternate procedures are established
By 14 CFR) and used.

NOTE: Any mode that operates

normally may be used.

-01 GPWS (Class A Or A - 0 (O) May be inoperative provided:

B Required) a) Alternate procedures are
established and used, and
b) Repairs are made within two (2)
flight days.

-01 Modes 1-4 (Class A A 4 0 (O) May be inoperative provided:

TAWS Required) a) Alternate procedures are
established and used, and
b) Repairs are made within two (2)
flight days.

Modes 1 & 3 (Class A 2 0 (O) May be inoperative provided:

B TAWS Required) a) Alternate procedures are
established and used, and
b) Repairs are made within two (2)
flight days.

-02 Test Mode (Class A A 1 0 (O) May be inoperative provided:

Or B Required) a) GPWS is considered
inoperative, and
b) Repairs are made within two (2)
flight days.

(Continued)
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34 NAVIGATION

44-01 Terrain Awareness

Warning System
(TAWS)/Ground
Proximity Warning
System (GPWS)
(Class A or B
Required)
(Continued)

-03 Glideslope (Mod C - 1

Deviation(Mode 5)
(Class A TAWS
Required) B - 0

Modes 2, 4, & 5 C 3 0
*** (Class B TAWS
Required)

-02 Advisory Callouts B - 0 (O) May be inoperative provided

(Class A or B alternate procedures are established
Required) and used.

C - 0 (O) May be inoperative provided:

a) Advisory callout not required by
14 CFR, and
b) Alternate procedures are
established and used.

(Continued)
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34 NAVIGATION

44-01 Terrain Awareness

Warning System
(TAWS)/Ground
Proximity Warning
System (GPWS)
(Class A or B
Required)
(Continued)

-03 Windshear Mode B 1 0 (O) May be inoperative provided

*** (Reactive) (Class A alternate procedures are established
TAWS Required) and used.

NOTE: Alternate procedures should

include reviewing windshear
avoidance and windshear
recovery procedures.

C 1 0 (O) May be inoperative provided:

a) Alternate procedures are
established and used, and
b) Windshear Detection and
Avoidance System (Predictive)
operates normally.

Windshear Mode C 1 0 (O) May be inoperative provided

*** (Reactive) (Class B alternate procedures are established
TAWS Required) and used.

-04 Terrain System B 1 0 (O) May be inoperative provided

Forward Looking alternate procedures are established
Terrain Avoidance and used.
(FLTA) And
Premature Descent
Alert (PDA)
Functions (Class A
Or B Required)

(Continued)
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34 NAVIGATION

44-01 Terrain Awareness

Warning System
(TAWS)/Ground
Proximity Warning
System (GPWS)
(Class A or B
Required)
(Continued)

-05 Terrain Display C - 1

(Class A TAWS
Required)
B - 0

Terrain Display C - 0
*** (Class B TAWS
Required)

-06 Runway C 1 0
*** Awareness &
Advisory System
(Class A Or B
Required)

44-02 Radar Altimeter C - 0 (M)(O) May be inoperative provided:

a) Approach procedures do not
require its use, and
b) Alternate procedures are
established and used.

NOTE: TAWS, GPWS and/or TCAS

may be inoperative.

44-03 Ground Proximity D - -

*** Alert Advisory
System (GPAAS)
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34 NAVIGATION

45-01 Traffic Alert And B - 0 (M)(O) May be inoperative provided:

*** Collision Avoidance a) System is deactivated and
System (TCAS I) secured, and
b) Enroute or approach
procedures do not require its
use.

C - 0 (M)(O) May be inoperative provided:

a) Not required by 14 CFR,
b) System is deactivated and
secured, and
c) Enroute or approach
procedures do not require its
use.

45-02 Traffic Alert And B - 0 (M) May be inoperative provided:

*** Collision Avoidance a) System is deactivated and
System (TCAS II) 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
procedures do not require its
use.

-01 Combined Traffic C 2 1 (O) One may be inoperative on the

*** Alert (TA) And non-flying pilot side provided:
Resolution Advisory a) TA and RA visual display is
(RA) Dual Display operative on the flying pilot
side, and
b) TA and RA audio function is
operative on flying pilot side.

(Continued)
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34 NAVIGATION

45-02 Traffic Alert And

*** Collision Avoidance
System (TCAS II)
(Continued)

-02 Resolution Advisory C 2 1 One may be inoperative on non-flying

(RA) Display pilot side.
System(s)

C - 0 (O) May be inoperative provided:

a) Traffic Alert (TA) display
elements and voice command
audio functions are operative,
b) TA ONLY Mode is selected by
the crew, and
c) Enroute or approach
procedures do not require its
use.

-03 TA Display C - 0 (O) May be inoperative provided:

System(s) a) RA visual display and audio
functions are operative, and
b) Enroute or approach
procedures do not require its
use.

-04 Audio Functions B 1 0 May be inoperative provided enroute or

approach procedures do not require
use of TCAS.

-05 Airspace Selection C - 0

*** Function

45-03 Traffic Collision D - -

*** Avoidance Device
(TCAD)
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34 NAVIGATION

45-04 Automatic D - 0 May be inoperative provided it is not

Dependent required by 14 CFR.
Surveillance
Broadcast (ADS-B) NOTE: If ADS-B is installed in lieu of
System or as replacement for 14 CFR
required equipment, the repair
category in the operator’s MEL
will be the same as that of the
14 CFR required equipment.

-01 Link And Display D - 0

Processor Unit NOTE: Cockpit Display Traffic
(LDPU) Information (CDTI) display of
data from other aircraft
systems may be used.

-02 Cockpit Display D - 0

And Traffic NOTE: ADS-B data transmissions
Information (CDTI) may continue.

-03 CDTI Control Panel D - 0 May be inoperative provided:

a) Flight ID can be set, and
b) Screen display is acceptable to
the flight crew.

-04 Data Link D - 0

Transmitter(s)

-05 Data Link D - 0

Receiver(s)

45-05 Skywatch Traffic D - 0

*** Advisory System
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34 NAVIGATION

51-01 Distance Measuring C - 0 May be inoperative provided a suitable

Equipment (DME) operative RNAV system is available.

C - 0 May be inoperative provided

operations do not require its use.
D 2 1

52-01 ATC Transponders B - 0 May be inoperative provided:

And Automatic a) Enroute operations do not
Altitude Reporting require its use, and
Systems b) Prior to flight, approval is
obtained from ATC facilities
having jurisdiction over the
planned route of flight.

D - 1 Any in excess of those required by 14

CFR may be inoperative.

-01 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 completion of next heavy
CFR maintenance visit.

-02 ADS-B Squitter D - 0 May be inoperative provided

*** Transmissions operations do not require its use.

C - 0 (O) May be inoperative provided

alternate procedures are established
and used.

NOTE: Any ADS-B Out function that

operates normally may be used.
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34 NAVIGATION

55-01 Automatic Direction C - - May be inoperative provided

Finder (ADF) operations do not require its use

57-01 Area Navigation C - - May be inoperative provided:

(RNAV) (Multi- a) Not required by 14 CFR, and
Sensor, LORAN, b) Operations do not require its use.
and/or GPS)

61-01 Navigation C - - (O) May be out of currency provided:

Databases a) Current Aeronautical Charts are
used to verify Navigation Fixes
prior to each departure,
b) Procedures are established and
used to verify status and
suitability of Navigation
Facilities used to define route of
flight,
c) Approach Navigation Radios
are manually tuned and
identified.
.
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35 OXYGEN

20-01 Passenger Oxygen C - 0 Individual oxygen masks or dispensers

Masks may be inoperative or missing provided
the affected seat is placarded “DO
NOT OCCUPY”.

30-01 Protective Breathing D - - Any in excess of those required by 14

*** Equipment CFR may be inoperative or removed
provided location placarding is
removed or obscured.
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46 INFORMATION
SYSTEMS

00-01 Electronic Flight Bag C - 0 (O) May be inoperative provided

*** System (EFB) alternate procedures are established
and used to ensure all information
associated with the flight is available at
the pilot station in current and
appropriate form.

NOTE 1: If alternate source is

electronic, dual redundancy is
required for operation.

NOTE 2: Any function, program or

document which operates
normally may be used.

-01 Power Connection C - 0 (O) May be inoperative provided

*** (Class 1 & 2) alternate procedures are established
and used.

-02 Mounting Device C - 0 (M)(O) May be inoperative provided:

*** (Class 2) a) The associated EFB and
hardware is secured by an
alternate means or removed
from the aircraft, and
b) Alternate procedures are
established and used.

-03 Data Connectivity C - 0 (O) May be inoperative provided

*** (Class 2) alternate procedures are established
and used.

-04 EFB Printer C - 0 May be inoperative provided all

*** affected pertinent flight information is
printed and available prior to
departure.
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46 INFORMATION
SYSTEMS

00-02 Integrated Flight

Information System
(Pro Line 21 IFIS-
5000 only)

-01 File Server Unit C 1 0 (O) May be inoperative provided all

(FSU) information associated with the flight is
(FSU INOP available at the pilot station in current
message) and appropriate form.

*** C 2 0 (O) One or both may be inoperative

provided alternate procedures are
established and used to ensure all
information associated with the flight is
available at the pilot station in current
and appropriate form.

NOTE: If alternate source is electronic,

dual redundancy is required for
operation.

-02 Cursor Control C - 0 (O) May be inoperative provided

Panel (CCP) alternate procedures are established
and used to ensure all information
associated with the flight is available at
the pilot station in current and
appropriate form.

-03 Communications C 1 0 (O) May be inoperative provided

*** Management Unit alternate procedures are established
(CMU) and used for ACARS and Universal
WX inoperative.

-04 Third VHF Comm C 1 0 (O) May be inoperative provided

*** Radio alternate procedures are established
and used for ACARS and Universal
WX inoperative.

00-03 XM Satellite D 1 0
*** Weather System
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52 DOORS

70-01 Cabin Door Warning C 1 0 (O) May be inoperative provided:

Light a) A flight crewmember confirms
by visual inspection that the
door is latched prior to each
departure,
b) Fasten seat belt sign remains
on, or passengers are orally
briefed to remain seated with
their seat belts fastened, and
c) Aircraft must be operated
unpressurized
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61 PROPELLERS

21-01 Propeller C 1 0
Synchrophaser

21-02 Propeller C 1 0
Synchroscope

23-01 Autofeathering C 1 0
System (Except
C90GT & C90GTi)

23-02 Reverse Not Ready C 1 0 May be inoperative provided propeller

Light levers are in high rpm position for
reversing.
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73 ENGINE FUEL &
CONTROL

31-01 Shadin Fuel Flow D - 0 (M)

*** Indicator
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77 ENGINE
INDICATING

00-01 Engine Trend D 1 0

*** Monitoring System