Revision:

1

 

Date: 01/09/2009

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

DEPARTMENT OF TRANSPORTATION

 

 

 

 

 

FEDERAL AVIATION ADMINISTRATION

 

 

 

 

 

WASHINGTON , D.C.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

MASTER MINIMUM EQUIPMENT LIST

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

LET-420

 

 

 

 

 

Douglas L. Edwards

 

 

Chairman, Flight Operations Evaluation Board

(FOEB)

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Federal Aviation Administration

 

 

Kansas City Aircraft Evaluation Group

 

 

DOT Building

 

 

901 Locust Street , Room 332

 

 

Kansas City , MO  64106-2641

 

 

 

 

 

 

 

 

Telephone:

(816)-329-3233

 

FAX:

(816)-329-3241

 

 

 

 

 

 


 

 

 

--

Cover Page

--

--

Table of Contents

I

--

Log of Revisions

II

--

Control Page

III, IV

--

Highlights of Change

V, VI, VII

--

Definitions

VIII

--

Preamble

IX

--

Guidelines for (O) & (M) Procedures

X, XI, XII

--

Guidelines for (O) & (M) Procedures

XIII, XIV, XV

21

Air Conditioning

21-1

22

Autopilot

22-1

23

Communications

23-1 THRU 5

24

Electrical

24-1

25

Equipment/Furnishings

25-1 THRU 7

26

Fire Protection

26-1, 2

27

Flight Controls

27-1, 2

28

Fuel

28-1, 2

29

Hydraulic Power

29-1

30

Ice & Rain Protection

30-1, 2

31

Indicating/Recording Systems

31-1, 2

32

Landing Gear

32-1

33

Lights

33-1, 2

34

Navigation

34-1 THRU 14

35

Oxygen

35-1

38

Water/Waste

38-1, 2

46

Information Systems

46-1, 2

49

Airborne Auxiliary Power

49-1

52

Doors

52-1

61

Propellers

61-1

76

Engine Controls

76-1

79

Engine Oil

79-1

80

Starting

80-1

 

 

 


 

 

 

 

ORIGINAL

03/03/2000

ALL PAGES

 

1

01/09/2009

COVER PAGE, TABLE OF CONTENTS

 

1

01/09/2009

LOG OF REVISIONS, CONTROL PAGES

 

1

01/09/2009

HIGHLIGHTS OF CHANGE, DEFINITIONS

 

1

01/09/2009

PREAMBLE, GUIDELINES (O & M)

 

1

01/09/2009

22-1, 23-1, 23-2, 23-3, 23-4

 

1

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23-5, 24-1, 25-1, 25-2, 25-3

 

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25-4, 25-5, 25-6, 25-7, 26-1

 

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26-2, 28-1, 30-1, 30-2, 31-1

 

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34-13, 34-14, 35-1, 38-1

 

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38-2, 46-1, 46-2, 79-1

 

 

 

 

 


 

 

 

 

Cover Page

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Table of Contents

I

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01/09/2009

Log of Revisions

II

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Control Page

III

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IV

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Highlights of Change

V

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VI

1

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VII

1

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Definitions

VIII

1

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Preamble

IX

1

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Guidelines for (O) & (M) Procedures

X

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XI

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XII

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XIII

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XIV

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XV

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28-2

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29

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34-6

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34-8

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34-9

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34-10

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34-11

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34-12

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34-13

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34-14

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38-2

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ORIGINAL

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76

76-1

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79

79-1

1

01/09/2009

80

80-1

ORIGINAL

03/03/2000

 

 

 

 

 


 

 

Cover Page

Updated to Revision 1 and FOEB Chairman’s name added.

 

Table Of Contents

 

Updated to reflect changes to Revision 1.

Log Of Revisions

 

Updated to reflect changes to Revision 1.

Control Pages

 

Updated to reflect changes to Revision 1.

Highlights Of Change

 

Updated to reflect changes to Revision 1.

Definitions

 

Updated to reference current Policy Letter 25 revision for applicable portions to include in operator’s MEL.

 

Preamble

Updated to reference current Policy Letter 34 (or 36 for Pt 91 only operations) revision to include in operator’s MEL.

 

Guidelines (O & M)

 

Updated to reflect changes to Revision 1.

ATA 22-1

Autopilot System relief updated IAW PL-101.

 

ATA 22-2

Autopilot Disconnect relief updated IAW PL-93.

 

ATA 23-1

Communications System relief updated IAW PL-95 (VHF and UHF).  HF relief separated from Item 23-1 and relocated to Item 23-8 IAW PL-106.

 

ATA 23-2

Passenger Address System relief updated IAW PL-9.

 

ATA 23-5

ELT relief updated IAW PL-120.

 

ATA 23-6

Cockpit Voice Recorder relief updated IAW PL-29.

 

ATA 23-7

Boom Microphone relief updated IAW PL-58.

 

ATA 23-8

HF Communications relief relocated from Item 23-1 and updated IAW PL-106.

 

 

 


 

 

ATA 23-9

SELCAL relief added IAW PL-117.

 

ATA 24

Chapter title changed to coincide with title in opspecs.com.

 

ATA 25-1

Passenger Seat relief updated IAW PL-79.

 

ATA 25-2

First Aid Kits relief updated to Emergency Medical Equipment relief IAW PL-73.

 

ATA 25-4

Passenger Convenience Item relief updated to PCI/NEF relief IAW PL-116.

 

ATA 25-5

“Fasten Seat Belt While Seated” Sign or Placard relief added IAW PL-89.

 

ATA 25-6

Exterior Lavatory Door Ashtrays relief added IAW PL-85.

 

ATA 25-7

Galley Waste Receptacles Access Doors/Covers relief added IAW PL-96.

 

ATA 25-8

Cargo Restraint Systems relief added IAW PL-100.

 

ATA 25-9

Overhead /Cabin/Galley Storage relief added IAW PL-104.

 

ATA 25-10

Observer Seats relief added IAW PL-56.

 

ATA 26-1

Minor change to Item title to coincide with PL-75.

 

ATA 26-3

Lavatory Fire Extinguisher System relief added IAW PL-24.

 

ATA 26-4

Lavatory Smoke Detection System relief added IAW PL-24.

 

ATA 26-5

Cargo Compartment Fire Detection/Suppression Systems relief added IAW PL-102.

 

ATA 28-4

“OR” removed between provisos IAW PL-31.

 

ATA 30

Minor change to Chapter title to coincide with opspecs.com.

 

ATA 30-13

Pitot Heat Indicating System relief added IAW PL-90.

 

ATA 31-2

Flight Data Recorder relief updated IAW PL87.

 

 

 


 

 

ATA 33-10

Leading Edge Lighting relief updated and renamed Wing Ice Lights.

 

ATA 34-1

Standby Attitude Indicator relief updated IAW PL-111.

 

ATA 34-6

Transponder relief updated IAW PL-76.

 

ATA 34-9

Non-Stabilized Magnetic Compass System relief updated IAW PL-10.

 

ATA 34-11

Minor change to DME relief title IAW PL-3.

 

ATA 34-13

TCAS I relief updated IAW PL-32

 

ATA 34-14

TCAS II relief updated IAW PL-32.

 

ATA 34-15

Ground Proximity Warning System relief incorporated into and replaced by TAWS relief IAW PL-54.

 

ATA 34-16

Flight Management System Navigation Database relief added IAW PL-98.

 

ATA 34-17

Navigation Management System Navigation Database relief added IAW PL-98.

 

ATA 34-18

Windshear Detection, Guidance, and Avoidance System relief added

IAW PL-67.

 

ATA 34-19

ADS-B System relief added IAW PL-105.

 

ATA 34-20

Altitude Alerting System relief added IAW PL-39.

 

ATA 34-2

Protective Breathing Equipment relief added IAW PL-43.

 

ATA 38

Chapter added for Water/Waste relief items.

 

ATA 38-1

Potable Water Systems relief added IAW PL-83.

 

ATA 38-2

Lavatory Waste System relief added IAW PL-83.

 

ATA 46

Chapter added for Information Systems relief items.

 

ATA 46-1

Electronic Flight Bag relief added IAW PL-121.

 

ATA-79-2

“appropriate” inserted before “Engine” in the proviso to coincide with AFM.

 

 

 


 

 

 

 

The definitions must be inserted here in each Minimum Equipment List (MEL) from current FAA MMEL Policy Letter PL-25, MMEL DEFINITIONS in accordance with current FAA MMEL Policy Letter PL-70, DEFINITIONS REQUIRED IN MELs.

 

 

 

 


 

 

 

 

The applicable preamble must be inserted here in each Minimum Equipment List (MEL) from current FAA MMEL Policy Letter PL-34, MMEL AND MEL PREAMBLE or FAA MMEL Policy Letter PL-36, FAR PART 91 MEL APPROVAL.

 

 

 


 

The FOEB has identified a need for certain procedures to provide an adequate level of safety while providing relief for the following items. These procedures must be established by the operator. The following guidelines are to help establish these required procedures:

 

 

22-1

 

(M)       Maintenance procedure to disable the Autopilot and determine that       the Servos do not cause binding of the Control Cables.

 

23-2-A

(O)       Operations procedure to ensure passengers are adequately briefed.

23-8

(O)       Operations procedure to ensure SATCOM Voice or Data Link                     operates normally, alternate procedures are established and used,             SATCOM coverage is available over the intended route of flight,                  and if INMARSAT Codes are not available while using SATCOM                  Voice prior coordination with the appropriate ATS facility is required.

 

23-9

(O)       Operations procedure to ensure alternate procedures are                            established and used.

 

23-9-A

(O)       Operations procedure to ensure alternate procedures are                            established and used.

 

25-1-A

(M)       Maintenance procedure to ensure Seat is secured in the UPRIGHT             position.

 

(M)       Maintenance procedure to ensure SEAT BACK is immovable in full             UPRIGHT position.

 

25-1-B

(O)       Operations procedure to ensure baggage is not stowed under Seat             with inoperative Restraining Bar, Seat is properly placarded, and                 Cabin Crew is alerted.

 

25-2-A

(O)       Operations procedure to ensure AED is resealed in a manner that             will identify it as a Unit that cannot be mistaken for a fully                              serviceable Unit.

 

25-2-B

(O)       Operations procedure to ensure EMK is resealed in a manner that       will identify it as a Unit that cannot be mistaken for a fully                              serviceable Unit.

 

 

 


 

25-2-C

 

(O)       Operations procedure to ensure FAK is resealed in a manner that             will identify it as a Unit that cannot be mistaken for a fully                              serviceable Unit.

 

25-7

(M)       Maintenance procedure to ensure Container is EMPTY and access             is SECURED to prevent waste in the Compartment.

 

(O)       Operations procedure to ensure enough Waste Receptacles are                available for the flight.

 

25-8

(M)       Maintenance procedure to ensure cargo loading limits from and                  approved source are observed.

 

25-9

(M)       Maintenance procedure to ensure Compartment is not used for                  storage and is secured CLOSED.

 

26-3

(M)       Maintenance procedure to ensure Lavatory Waste Receptacle is                EMPTY and Door is locked CLOSED and properly placarded.

 

(O)       Operations procedure to ensure Lavatory is used only by                             crewmembers.

 

26-4

(M)       Maintenance procedure to ensure Lavatory Waste Receptacle is                EMPTY and Door is locked CLOSED and properly placarded.

 

(O)       Operations procedure to ensure Lavatory is used only by                             crewmembers.

 

27-4

(O)       Operations procedure to ensure Spoiler System operates normally.

28-1

(O)       Operations procedure to ensure FUEL PRESSURE Signal Light is             operative.  An acceptable procedure is to turn off the Fuel Pump on             the associated operating engine.

 

28-3

(M)       Maintenance procedure to check the Fuel Filter Insert for purity.

 

 


 

34-9

 

(O)       Operations procedure to ensure any combination of three Gyro or               INS (IRU) Stabilized Compass Systems are operative.

 

(O)       Operations procedure to ensure any combination of two Gyro or                 INS (IRU) Stabilized Compass Systems operate normally, the                     Airplane is operated with   Dual Independent Navigation Capability,       and is under Positive Radar Control by ATC on the enroute portion             of the flight.

 

(O)       Operations procedure to ensure the flight is entirely within areas of             magnetic unreliability provided at least two Stabilized Directional                 Gyro Systems are installed, operate normally, and are used in                    conjunction with approved Free Gyro Navigation Techniques.

 

34-13

(M)       Maintenance procedure to ensure System is deactivated and                      SECURED.  Applies to both provisos.

 

34-14

(M)       Maintenance procedure to ensure System is deactivated and                      SECURED.  Applies to both provisos.

 

34-14-B

(O)       Operations procedure to ensure TA visual display and audio                        functions are operative, TA ONLY Mode is selected by the crew,                 and enroute or approach procedures do not require use of the RA               Display System.

 

34-14-C

(O)       Operations procedure to ensure RA visual display and audio                       functions are operative, and enroute or approach procedures do not             require use of the TA Display System.

 

34-15-A-1

(O)       Operations procedure to ensure alternate procedures are                            established and used.

 

34-15-A-1-a

(O)       Operations procedure to ensure alternate procedures are                            established and used.

 

34-15-A-1-d

(O)       Operations procedure to ensure alternate procedures are                            established and used.

 

(O)       Operations procedure to ensure alternate procedures are                            established and used and Advisory Callouts are not required by                  FAR.

 

 

 


 

34-15-A-1-e

 

(O)       Operations procedure to ensure alternate procedures are                            established and used.

 

(O)       Operations procedure to ensure alternate procedures are                            established and used and Windshear Detection and Avoidance                   System (Predictive) operates normally.

 

34-15-A-2

(O)       Operations procedure to ensure alternate procedures are                            established and used.

 

34-15-B-1

(O)       Operations procedure to ensure alternate procedures are                            established and used.

 

34-15-B-1-a

(O)       Operations procedure to ensure alternate procedures are                            established and used.

 

34-15-B-1-d

(O)       Operations procedure to ensure alternate procedures are                            established and used.

 

(O)       Operations procedure to ensure alternate procedures are                            established and used and Advisory Callouts are not required by                  FAR.

 

34-15-B-1-e

(O)       Operations procedure to ensure alternate procedures are                            established and used.

 

34-15-C-1

(O)       Operations procedure to ensure alternate procedures are                            established and used.

 

34-16-A

(O)       Operations procedure to ensure current Aeronautical Charts are                 used, status and suitability of Navigation Facilities to be used are                verified, and Approach Navigation Radios are manually tuned and               identified.

 

34-17-A

(O)       Operations procedure to ensure current Aeronautical Charts are                 used, status and suitability of Navigation Facilities to be used are                verified, and Approach Navigation Radios are manually tuned and               identified.

 

 

 


 

34-18-A-1

 

(O)       Operations procedure to ensure alternate procedures are                            established and used.

 

(O)       Operations procedure to ensure alternate procedures are                            established and used and Windshear Detection and Avoidance                   System (Predictive) operates normally.

 

34-18-A-2

(O)       Operations procedure to ensure alternate procedures are                            established and used.

 

(O)       Operations procedure to ensure alternate procedures are                            established and used and Windshear Warning and Flight Guidance             System (Reactive) operates normally.

 

34-18-B-1

(O)       Operations procedure to ensure alternate procedures are                            established and used.

 

34-18-B-2

(O)       Operations procedure to ensure alternate procedures are                            established and used.

 

34-20

(O)       Operations procedure to ensure the Autopilot with Altitude Hold is               operative, and enroute operations do not require use of the Altitude             Alerting System.

 

34-38-1

(M)       Maintenance procedure to ensure associated Components are                   deactivated or isolated and System Components do not have                      leaks.

 

(M)       Maintenance procedure to ensure System is drained and                             procedures are established to ensure the System is not serviced.

 

38-2

(M)       Maintenance procedure to ensure associated Components are                   deactivated or isolated and System Components do not have                      leaks.

 

(M)       Maintenance procedure to ensure associated Components are                   deactivated or isolated, System Components do not have                            leaks, and the Lavatory Door is secured CLOSED and properly                  placarded.

 

 

 


 

46-1-A

 

(O)       Operations procedure to establish and use alternate procedures.

 

46-1-B

(O)       Operations procedure to establish and use alternate procedures.

 

46-1-C

(O)       Operations procedure to establish and use alternate procedures.

 

46-1-D

(M)       Maintenance procedure to ensure associated EFB and hardware is             secured by an alternate means or removed from the aircraft. 

 

(O)       Operations procedure to ensure alternate procedures are                            established and used.

 

(M)       Maintenance procedure to ensure associated EFB and hardware is             secured by an alternate means or removed from the aircraft. 

 

52-1

(O)       Operations procedure to ensure a flight crewmember confirms the                   Door is LATCHED prior to Engine start, and the FASTEN SEAT                   BELT Sign remains on during the entire flight.

 

79-2

(M)       Maintenance procedure to ensure the Oil Filter Insert of appropriate             Engine is checked for purity before dispatch.

 

80-1

(O)       Operations procedure to ensure Electric Hydraulic Converter is                  monitored during the start sequence.  The 20 Second Timer should             be checked before Engine starting by dry motoring the Engine.

 

 

 


21

AIR CONDITIONING

 

 

 

 

 

 

 

 

 

 

 

 

1.

***

Air Conditioning System (Freon)

C

1

0

 

 

 

 

 

 

 

 

 

2.

Flight Compartment Fan

C

1

0

 

 

 

 

 

 

 

 

 

3.

Individual Cabin Air Showers

C

-

0

 

 

 

 

 

 

 

 

 


22

AUTOPILOT

 

 

 

 

 

 

 

 

 

 

 

 

1.

Autopilot System

C

-

0

(M) May be inoperative provided operations do not require its use.

|

|

 

 

 

 

 

 

 

2.

Autopilot Disconnect Functions

(Quick Release Controls)

C

 

 

 

 

 

B

 

2

 

 

 

 

 

2

 

1

 

 

 

 

 

0

 

One may be inoperative provided:

a)          Autopilot is not used below 1,500 feet AGL, and

b)          Approach minimums do not require the use of the Autopilot.

 

May be inoperative provided Autopilot is not used.

|

|

|

|

|

 

|

|

 

 

 

 

 

 

 


23

COMMUNICATIONS

 

 

 

 

 

 

 

 

 

 

 

 

1.

Communications System (VHF And UHF)

D

-

-

Any in excess of those required by FAR may be inoperative provided it is not powered by any Emergency Power Source and not required for emergency procedures.

|

|

|

|

|

 

 

 

 

 

 

 

 

 

 

 

 

NOTE:  VHF 1 must be operative.

 

 

 

 

 

 

 

 

2.

Passenger Address System (PA)

 

 

 

 

 

|

 

 

 

 

 

 

 

A)

Passenger Configuration

C

 

 

1

0

(O) May be inoperative provided:

a)          PA not required by FAR, and

b)          Alternate, normal and emergency procedures, and/or operating restrictions are established and used.

 

NOTE:  Any station function(s) that

             operate normally may be used.

|

|

|

|

|

|

 

|

|

 

 

 

 

 

 

 

B)

Cargo Configuration

D

 

1

 

0

 

May be inoperative provided procedures do not require its use.

|

|

 

 

 

 

 

 

 

3.

Cockpit Speakers

C

2

0

May be inoperative provided an operative Headset is provided for each crewmember.

 

 

 

 

 

 

 

 

4.

Static Discharge Wicks

C

13

10

Three or less Discharge Wicks may be missing or broken in any of the following locations:

a)          One on each Wing, and

b)          One on the Elevator.

 

 

 

 

 

 

 

 


23

COMMUNICATIONS

 

 

 

 

 

 

 

 

 

 

 

 

5.

***

Emergency Locator Transmitter (ELT)

 

 

 

 

|

|

 

 

 

 

 

 

 

A)

Survival Type ELTs

D

-

-

Any in excess of those required by FAR may be inoperative or missing.

|

|

 

 

 

 

 

 

 

B)

Fixed ELTs

A

-

0

May be inoperative or missing provided repairs are made within 90 days.

|

|

 

 

 

 

 

 

 

 

 

D

-

-

Any in excess of those required by FAR may be inoperative or missing.

|

|

 

 

 

 

 

 

 

6.

Cockpit Voice Recorder (CVR)

 

 

 

 

|

|

 

 

 

 

 

 

 

A)

For Air Carrier And Commercial Operators

 

 

 

 

|

|

 

 

 

 

 

 

 

1)

With Flight Data Recorder (FDR) Installed

A

1

0

May be inoperative provided:

a)          Flight Data Recorder (FDR) operates normally, and

b)          Repairs are made within three flight days.

|

|

|

|

|

 

 

 

 

 

 

 

2)

Without Flight Data Recorder (FDR) Installed

A

1

0

May be inoperative provided repairs are made within three flight days.

|

|

|

 

 

 

 

 

 

 

B)

For Operators Other Than Air Carriers And Commercial Operators

A

1

0

May be inoperative provided repairs are made in accordance with applicable FARs.

|

|

|

 

 

 

 

 

 

 


23

COMMUNICATIONS

 

 

 

 

 

 

 

 

 

 

 

 

7.

Boom Microphones

 

 

 

 

|

 

 

 

 

 

 

 

A)

Cockpit Voice Recorder With Flight Data Recorder Installed

 

 

 

 

|

|

|

|

 

 

 

 

 

 

 

1)

Cockpit Voice Recorder Equipped To Record Boom Microphone Per FAR 135.151(d).

A

-

0

May be inoperative provided:

a)          Flight Data Recorder (FDR) operates normally, and

b)          Repairs are made within three flight days.

|

|

|

|

|

 

 

 

 

 

 

 

2) ***

Cockpit Voice Recorder Not Equipped To Record Boom Microphone

D

-

0

Any in excess of those required by FAR may be inoperative.

|

|

|

|

 

 

 

 

 

 

 

B)

Cockpit Voice Recorder Without Flight Data Recorder Installed

 

 

 

 

|

|

|

|

 

 

 

 

 

 

 

1)

Cockpit Voice Recorder Equipped To Record Boom Microphone per FAR 135.151(d)

A

-

0

May be inoperative provided repairs are made within three flight days.

|

|

|

|

|

 

 

 

 

 

 

 

2) ***

Cockpit Voice Recorder Not Equipped To Record Boom Microphones

D

-

0

Any in excess of those required by FAR may be inoperative.

|

|

|

|

 

 

 

 

 

 

 


23

COMMMUNICATIONS

 

 

 

 

 

 

 

 

 

 

 

 

8.

High Frequency  (HF)

Communication System

 

D

 

 

 

C

-

 

 

 

-

-

 

 

 

1

Any in excess of those required by FAR may be inoperative.

 

 

(O) May be inoperative while conducting operations that require two LRCS provided:

a)          SATCOM Voice or Data Link operates normally,

b)          Alternate procedures are established and used,

c)          SATCOM coverage is available over the intended route of flight, and

d)          If INMARSAT Codes are not available while using SATCOM Voice prior coordination with the appropriate ATS facility is required.

 

NOTE:  SATCOM is to be used only as

             a backup to normal HF

             communications unless

             otherwise authorized by the

             appropriate ATS facilities.

|

|

|

 

|

|

|

|

|

|

|

|
|
|
|

|

|

|

|

|

 

|

|

|

|

|

 

 

 

 

 

 

 


23

COMMUNICATIONS

 

 

 

 

 

 

 

 

 

 

 

 

9.

Selective Call Systems (SELCAL)

C

-

0

(O) May be inoperative provided alternate procedures are established and used.

|

|

|

 

 

 

 

 

 

 

 

 

D

-

0

May be inoperative provided procedures do not require its use.

|

|

 

 

 

 

 

 

 

A)

Channels

C

-

0

(O) May be inoperative provided alternate procedures are established and used.

|

|

|

 

 

 

 

 

 

 

 

 

D

-

0

May be inoperative provided procedures do not require its use.

|

|

 

 

 

 

 

 

 


24

ELECTRICAL

 

 

 

 

|

 

 

 

 

 

 

 

1.

AC Generators

C

2

1

One may be inoperative provided aircraft is not operated in known or forecast icing conditions.

 

 

 

 

 

 

 

 

2.

AC GENERATOR Signal Lights (Left, Right)

C

2

0

May be inoperative provided:

a)          Windshield Heating is checked for operation prior to takeoff,

b)          Windshield Heating Signal is operative, and

c)          Propeller Deicing Signal is operative.

 

 

 

 

 

 

 

 

3.

Inverters 115V

B

2

1

One may be inoperative for day VMC operations.

 

 

 

 

 

 

 

 

4.

INVERTER I 115 V AC Signal Light

C

1

0

May be inoperative provided:

a)          Both Inverters are operative, and

b)          Voltage 115V is monitored during flight.

 

 

 

 

 

 

 

 

5.

INVERTER I Or II 36 V AC Signal Light

C

2

1

One may be inoperative provided:

a)          Both 36V AC Inverters are operative, and

b)          Voltage 36V is monitored during flight.

 

 

 

 

 

 

 

 


25

EQUIPMENT/ FURNISHINGS

 

 

 

 

 

 

 

 

 

 

 

 

1.

Passenger Seat(s)

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.

 

 

 

 

 

 

 

 

A)

Recline Mechanism

D

-

-

(M) May be inoperative and Seat occupied provided Seat is secured in the UPRIGHT position.

 

 

 

 

 

 

 

 

 

 

C

-

-

(M) May be inoperative and Seat occupied provided Seat Back is immovable in full UPRIGHT position.

|

|

|

 

 

 

 

 

 

 

B)

Underseat Baggage Restraining Bars

C

-

-

(O) May be inoperative provided:

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 Cabin Crew of inoperative Restraining Bar.

|

|

|

|

|

|

|

|

|

|

 

 

 

 

 

 

 

 

 

 

 

 

(Continued)

|

 

 

 

 

 

 

 


25

EQUIPMENT/ FURNISHINGS

 

 

 

 

 

 

 

 

 

 

 

 

1.

Passenger Seat(s) (Continued)

 

 

 

 

 

 

 

 

 

 

 

 

C)

Armrest

C

-

-

May be inoperative or missing 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)          For an Armrest with a Recline Mechanism, Seat is secured in the UPRIGHT position.

|

|

|

|

|

|

|

|

|

|

 

 

 

 

 

 

 

2.

Emergency Medical Equipment

 

 

 

 

|

|

 

 

 

 

 

 

 

A)

Automatic External Defibrillator (AED) And/Or Associated Equipment

A

-

0

(O) May be incomplete, missing or inoperative provided:

a)          AED is resealed in a manner that will identify it as a Unit that cannot be mistaken for a fully serviceable Unit, and

b)          Repairs or replacements are made within three flight cycles.

|

|

|

|

|

|

|

|

 

 

 

 

 

 

 

 

 

D

-

-

Any in excess of those required by FAR may be incomplete, missing, or inoperative.

|

|

|

 

 

 

 

 

 

 

 

 

 

 

 

(Continued)

|

 

 

 

 

 

 

 


25

EQUIPMENT/ FURNISHINGS

 

 

 

 

 

 

 

 

 

 

 

 

2.

Emergency Medical Equipment (Continued)

 

 

 

 

|

|

 

 

 

 

 

 

 

B)

Emergency Medical Kit (EMK) And/Or Associated Equipment

A

-

0

(O) May be incomplete, missing or inoperative provided:

a)          EMK is resealed in a manner that will identify it as a Unit that cannot be mistaken for a fully serviceable Unit, and

b)          Repairs or replacements are made within three flight cycles.

|

|

|

|

|

|

|

|

 

 

 

 

 

 

 

 

 

D

-

-

Any in excess of those required by FAR may be incomplete, missing, or inoperative.

|

|

|

 

 

 

 

 

 

 

C)

First Aid Kit (FAK) And/Or Associated Equipment

A

-

-

(O) If more than one is required by FAR, only one of the required First Aid Kits may be incomplete, missing or inoperative provided:

a)          FAK is resealed in a manner that will identify it as a Unit that can not be mistaken for a fully serviceable Unit, and

b)          Repairs or replacements are made within three flight cycles.

|

|

|

|

|

|

|

|

|

|

 

 

 

 

 

 

 

 

 

D

-

-

Any in excess of those required by FAR may be incomplete, missing, or inoperative.

|

|

|

 

 

 

 

 

 

 

3.

Flotation Devices

D

-

-

Any in excess of those required by FAR may be inoperative.

 

 

 

 

 

 

 

 


25

EQUIPMENT/ FURNISHINGS

 

 

 

 

 

 

 

 

 

 

 

 

4.

Passenger Convenience/ NEF Items

 

 

 

 

 

|

 

 

 

 

 

 

 

 

A)

***

Passenger Convenience Items (Expires on April 30, 2008)

 

 

 

DELETED

|

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

B)

***

Non-Essential Equipment & Furnishings (NEF)

 

-

0

May be inoperative, damaged, or 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 flight crew and included in the operator’s appropriate document.

|

|

|

|

|

|

|

|

|

|

 

 

 

 

 

 

 

 

 

 

 

 

NOTE:  Exterior Lavatory Door Ash

             Trays are not considered NEF

             Items.

|

|

|

 

 

 

 

 

 

 


25

EQUIPMENT/ FURNISHINGS

 

 

 

 

 

 

 

 

 

 

 

 

5.

“Fasten Seat Belt While Seated” Sign Or Placard

C

-

-

One or more Signs or Placards may be illegible or missing provided a legible Sign or Placard is visible from each occupied Passenger Seat.

|

|

|

|

 

 

 

 

 

 

 

6. ***

Exterior Lavatory Door Ashtrays

 

 

 

 

|

|

 

 

 

 

 

 

 

A)

Airplanes With More Than One Exterior Lavatory Door Ashtray Installed

A

-

-

One may be missing provided it is replaced within 10 calendar days.

|

|

|

|

 

 

 

 

 

 

 

B)

 Airplanes With Only One Exterior Lavatory Door Ashtray Installed

A

1

0

May be inoperative provided it is replaced within 3 calendar days.

|

|

|

 

 

 

 

 

 

 

7. ***

Galley Waste Receptacles Access Doors/Covers

C

-

-

(M)(O) May be inoperative provided:

a)          The Container is EMPTY and 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.

|

|

|

|

|

|

|

|

|

|

|

 

 

 

 

 

 

 

8. ***

Cargo Restraint Systems

C

-

-

(M) May be inoperative or missing 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.

|

|

 

 

 

 

 

 

 


25

EQUIPMENT/ FURNISHINGS

 

 

 

 

 

 

 

 

 

 

 

 

9.

Overhead Storage Bin(s)/Cabin And Galley Storage Compartments/  Closets

C

-

-

(M) May be inoperative provided:

a)          Procedures are established to 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.

|

|

|

|

|

|

|

|

|

|

|

 

 

 

 

 

 

 

 

 

 

 

 

NOTE:  If no Partitions are installed,

             the entire Overhead Storage

             Compartment is considered

             one Bin.

|

|

|

|

 

 

 

 

 

 

 

10.

Observer Seat(s)

 

 

 

 

|

 

 

 

 

 

 

 

A)

Primary Observer Seat (Including Associated Equipment)

A

-

-

May be inoperative provided:

a)          A Passenger Seat in the Passenger Cabin is made available to an FAA Inspector for the performance of official duties, and

b)          Repairs are made within two flight days.

|

|

|

|

|

|

|

|

 

 

 

 

 

 

 

 

 

A

-

-

May be inoperative provided:

a)          Required minimum safety equipment (Safety Belt and Oxygen) is available,

b)          Seat is acceptable to the FAA Inspector for performance of official duties, and

c)          Repairs are made within two flight days.

|

|

|

|

|

|

|

|

|

 

 

 

 

 

 

 

 

 

 

 

 

(Continued)

|

 

 

 

 

 

 

 


25

EQUIPMENT/ FURNISHINGS

 

 

 

 

 

 

 

 

 

 

 

 

10.

Observer Seat(s) (Continued)

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

NOTE 1:  These provisos are intended

                 to provide for occupancy of

                 the above Seat by an FAA    

                 Inspector when the

                 minimum safety equipment

                 (Oxygen and Safety Belt) is

                 functional and the inspector

                 determines the conditions to

                 be acceptable.

 

NOTE 2:  The Pilot-in-Command will

                determine if the minimum

                safety equipment is

                functional for other persons

                authorized to occupy any

                Observer Seat(s).

|

|

|

|

|

|

|

|

|

 

|

|

|

|

|

|

 

 

 

 

 

 

 


26

FIRE PROTECTION

 

 

 

 

 

 

 

 

 

 

 

 

1.

Portable Fire Extinguisher(s)

D

-

-

Any in excess of those required by FAR may be inoperative or missing provided:

a)          The 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.

 

|

 

 

 

 

 

 

 

2.

Engine Fire Warning Bell

B

1

0

May be inoperative provided both Fire Warning Lights are operative.

 

 

 

 

 

 

 

 

3. ***

Lavatory Fire Extinguisher System

C

-

-

Lavatory Fire Extinguisher System may be inoperative provided Lavatory Smoke Detector System operates normally.

|

|

|

|

 

 

 

 

 

 

 

 

 

C

-

-

(M)(O) Lavatory Fire Extinguisher may be inoperative provided:

a)          Lavatory Waste Receptacle is EMPTY,

b)          Lavatory Door is locked CLOSED and placarded, “INOPERATIVE-DO NOT ENTER”, and

c)          Lavatory is used only by crewmembers.

|

|

|

|

|

|

|

|

|

|

 

 

 

 

 

 

 

 

 

 

 

 

NOTE 1:  These provisos are not

                intended to prohibit Lavatory

                use or inspections by

                crewmembers.

|

|

|

|

 

 

 

 

 

 

 

 

 

 

 

 

NOTE 2:  Lavatory Fire Extinguisher

                System is not required for all-

                cargo operations.

|

|

|

 

 

 

 

 

 

 


26

FIRE PROTECTION

 

 

 

 

 

 

 

 

 

 

 

 

4. ***

Lavatory Smoke Detection System

C

-

-

(M)(O) Lavatory Smoke Detection System may be inoperative provided:

a)          Lavatory Waste Receptacle is EMPTY,

b)          Lavatory Door is locked CLOSED and placarded, “INOPERATIVE-DO NOT ENTER”, and

c)          Lavatory is used only by crewmembers.

|

|

|

|

|

|

|

|

|

|

 

 

 

 

 

 

 

 

 

 

 

 

NOTE 1:  These provisos are not

                intended to prohibit Lavatory

                use or inspections by

                crewmembers.

|

|

|

|

 

 

 

 

 

 

 

 

 

 

 

 

NOTE 2:  Lavatory Smoke Detection

                System is not required for all-

                cargo operations.

|

|

|

 

 

 

 

 

 

 

5. ***

Cargo Compartment Fire Detection/ Suppression Systems

C

-

0

May be inoperative provided Cargo Compartment remains EMPTY.

|

|

|

 

 

 

 

 

 

 

 

 

 

 

 

NOTE:  Does not preclude the carriage

             of empty cargo containers,

             pallets, ballast, etc.

|

|

|

 

 

 

 

 

 

 


27

FLIGHT CONTROLS

 

 

 

 

 

 

 

 

 

 

 

 

1.

Rudder Trim Tab Indicator

B

1

0

May be inoperative provided:

a)          Tab operation is visually checked for full range of operation,

b)          Tab is positioned to NEUTRAL prior to each takeoff, and

c)          Neutral Position is verified by visual inspection.

 

 

 

 

 

 

 

 

2.

Aileron Trim

B

1

0

May be inoperative provided:

a)          Aileron operation is not affected,

b)          Tab is positioned to NEUTRAL prior to each takeoff, and

c)          Neutral Position is verified by visual inspection.

 

 

 

 

 

 

 

 

3.

Aileron Trim Tab Indicator

B

1

0

May be inoperative provided:

a)          Tab operation is visually checked for full range of operation,

b)          Tab is positioned to NEUTRAL prior to each takeoff, and

c)          Neutral Position is verified by visual inspection.

 

 

 

 

 

 

 

 

4.

Spoiler Control System Signal

C

1

0

(O) May be inoperative provided Spoiler Tab operation is visually checked for proper operation before each takeoff.

 

 

 

 

 

 

 

 


27

FLIGHT CONTROLS

 

 

 

 

 

 

 

 

 

 

 

 

5.

Flap Position Indicator

B

1

0

May be inoperative provided:

a)          Flaps are retracted for landing,

b)          Flap Angle is visually checked according to Control Lever Position before each takeoff, and

c)          FLAPS 18 Degree Signal is operative.

 

 

 

 

 

 

 

 

6.

FLAPS 18 Degrees Signal (Green, Yellow)

C

1

0

May be inoperative provided Flap Position Indicator is operative.

 

 

 

 

 

 

 

 

7.

AUTOMATIC BANK CONTROL Signal (Green, Yellow)

C

2

0

May be inoperative provided ABC Tab operation is verified prior to takeoff.

 

 

 

 

 

 

 

 

8.

AUTOMATIC BANK CONTROL System

C

2

0

May be inoperative provided AUTOMATIC BANK CONTROL System is turned OFF.

 

 

 

 

 

 

 

 

9.

Nose Wheel Pedal STEERING Signal

C

1

0

May be inoperative provided Pedal Steering operates normally.

 

 

 

 

 

 

 

 


28

FUEL

 

 

 

 

 

 

 

 

 

 

 

 

1.

Fuel Pressure Gauge

B

2

1

(O) One may be inoperative provided:

a)          Associated Minimum FUEL PRESSURE Signal Light is operative, and

b)          Associated FUEL TEMPERATURE Signal Light is operative.

 

 

 

 

 

 

 

 

2.

FUEL PRESSURE Signal Lights

B

2

1

One may be inoperative provided associated Fuel Pressure Gauge is operative.

 

 

 

 

 

 

 

 

3.

FUEL BY-PASS Signal Lights

B

2

1

(M) May be inoperative provided:

a)          Fuel Filter Insert of associated Engine is checked for purity before dispatch, and

b)          Associated Fuel Temperature Signal Light is operative.

 

 

 

 

 

 

 

 

4.

FUEL TRANSFER Signal Lights

C

2

0

May be inoperative provided Wing Tip Fuel Tanks are EMPTY.

 

 

 

 

 

 

 

|

 

 

C

2

0

May be inoperative provided Fuel Transfer System is operative.

 

 

 

 

 

 

 

 

5.

Fuel Transfer System

C

1

0

May be inoperative provided Wing Tip Fuel Tanks are EMPTY.

 

 

 

 

 

 

 

 

6.

ACTUATE TRANSFER Signal Lights

C

2

0

May be inoperative provided Wing Tip Fuel Tanks are EMPTY.

 

 

 

 

 

 

 

 


28

FUEL

 

 

 

 

 

 

 

 

 

 

 

 

7.

FUEL TEMPERATURE Signal Lights

C

2

0

May be inoperative provided:

a)          Associated Fuel Pressure Gauge is operative, and

b)          Associated FUEL BYPASS Signal Light is operative.

 

 

 

 

 

 

 

 

8.

Wing Tip Fuel Tank Gauges

C

2

0

May be inoperative provided Wing Tip Fuel Tanks are EMPTY.

 

 

 

 

 

 

 

 


29

HYDRAULIC POWER

 

 

 

 

 

 

 

 

 

 

 

 

1.

Brake Accumulator Pressure Indicator

B

1

0

May be inoperative provided Dual Brake Pressure Indicator is operative.

 

 

 

 

 

 

 

 

2.

Hydraulic Light

C

1

0

 

 

 

 

 

 

 

 

 


30

ICE & RAIN PROTECTION

 

 

 

 

|

 

 

 

 

 

 

 

1.

Surface Deicing System (Wing And Tail)

C

1

0

May be inoperative provided aircraft is not operated in known or forecast icing conditions.

 

 

 

 

 

 

 

 

2.

Automatic Airframe Pneumatic Deicing Timer

C

1

0

May be inoperative provided Manual Airframe Pneumatic Deicing Timer is operative.

 

 

 

 

 

 

 

 

3.

Rotary Ice Detector

C

1

0

May be inoperative provided Static Ice detector Heating is operative.

 

 

 

 

 

 

 

 

 

 

 

 

 

NOTE:  Increase attention in icing

             conditions.

 

 

 

 

 

 

 

 

4.

Static Ice Detector Heating

C

2

1

May be inoperative provided Rotary Ice Detector is operative.

 

 

 

 

 

 

 

 

5.

Windshield Wipers (Set)

C

1

0

May be inoperative provided flight is not conducted in precipitation within 5 nautical miles of the airport of takeoff or intended landing.

 

 

 

 

 

 

 

 

6.

Propeller Deicing

C

2

0

May be inoperative provided aircraft is not operated in known or forecast icing conditions.

 

 

 

 

 

 

 

 

7.

Windshield Heating

B

2

0

May be inoperative provided aircraft is not operated in known or forecast icing conditions.

 

 

 

 

 

 

 

 

8.

WINDSHIELD HEATING Signal

C

2

0

May be inoperative provided Windshield Heating is operative.

 

 

 

 

 

 

 

 


30

ICE & RAIN PROTECTION

 

 

 

 

|

 

 

 

 

 

 

 

9.

SEPARATOR VANE Signal

C

2

0

May be inoperative provided Separator Vanes are operative.

 

 

 

 

 

 

 

 

10.

Pitot Heater

B

2

1

One may be inoperative provided aircraft is operated in VMC conditions.

 

 

 

 

 

 

 

 

11.

Static Pressure Head Heater

B

2

1

One may be inoperative provided aircraft is not operated in known or forecast icing conditions.

 

 

 

 

 

 

 

 

12.

Stall Probe Heater

B

1

0

May be inoperative provided aircraft is not operated in known or forecast icing conditions.

 

 

 

 

 

 

 

 

13.

Pitot Heat Indicating System

 

 

 

 

|

|

 

 

 

 

 

 

 

A)

System Required By The Certification Or Operating Rules

B

-

0

May be inoperative provided:

a)          All other Elements of the Pitot Heat System operate normally, and

b)          The airplane is not operated into known or forecast icing conditions.

|

|

|

|

|

|

|

 

 

 

 

 

 

 

B)

System Not Required By The Certification Or Operating Rules

C

-

0

May be inoperative provided:

a)          All other Elements of the Pitot Heat System operate normally, and

b)          The airplane is not operated into known or forecast icing conditions.

|

|

|

|

|

|

|

 

 

 

 

 

 

 


31

INDICATING/ RECORDING SYSTEMS

 

 

 

 

 

 

 

 

 

 

 

 

1.

Clock

C

-

0

May be inoperative for VFR.

 

 

 

 

 

 

 

 

2.

Flight Data Recorder (FDR) System

C

-

-

Any in excess of those required by FAR 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

d)          Repairs are made within three flight days.

|

|

|

|

|

|

|

|

|

|

|

|

|

|

|

|

|

|

|

|

|

|

 

 

 

 

 

 

 

 

 

 

 

 

(Continued)

|

 

 

 

 

 

 

 


31

INDICATING/ RECORDING SYSTEMS

 

 

 

 

 

 

 

 

 

 

 

 

2.

Flight Data Recorder (FDR) System (Continued)

 

 

 

 

|

|

|

 

 

 

 

 

 

 

A)

For Air Carrier And Commercial Operators

 

 

 

 

|

|

 

 

 

 

 

 

 

1)

FDR Recording Parameters Required By FAR

A

-

-

May be inoperative provided:

a)          Cockpit Voice Recorder (CVR) operates normally, and

b)          Repairs are made within 20 calendar days.

|

|

|

|

|

 

 

 

 

 

 

 

2)

FDR Recording Parameters Not Required By FAR

A

-

-

May be inoperative provided repairs are made prior to completion of the next heavy maintenance check.

|

|

|

 

 

 

 

 

 

 

B)

Operators Other Than Holders Of Air Carrier Or Commercial Operator Certificates

C

-

1

Any in excess of those required by FAR may be inoperative.

|

|

|

|

 

 

 

 

 

 

 

 

 

A

-

0

May be inoperative provided repairs are made in accordance with applicable FARs.

|

|

|

 

 

 

 

 

 

 


32

LANDING GEAR

 

 

 

 

 

 

 

 

 

 

 

 

1.

Landing Gear Position Mechanical Indicators

C

3

0

 

 

 

 

 

 

 

 

 

2.

EXTEND LANDING GEAR Signal Light

C

1

0

May be inoperative provided EXTEND LANDING GEAR Signal Horn is operative.

 

 

 

 

 

 

 

 

3.

EXTEND LANDING GEAR Signal Horn

C

1

0

May be inoperative provided EXTEND LANDING GEAR Signal Light is operative.

 

 

 

 

 

 

 

 

4.

Dual Brake Pressure Indicator

C

1

0

May be inoperative provided:

a)          Hydraulic System Pressure Indicator is operative, and

b)          Brake System operates normally.

 

 

 

 

 

 

 

 

5.

LH (RH) BRAKE RELEASED Signals

C

2

0

 

 

 

 

 

 

 

 

 

6.

Parking Brake Pressure Indicator

C

1

0

May be inoperative provided Parking Brake System is operative.

 

 

 

 

 

 

 

 


33

LIGHTS

 

 

 

 

 

 

 

 

 

 

 

 

1.

Anti-Collision Beacon Lights

B

2

1

One may be inoperative for day operations.

 

 

 

 

 

 

 

 

2.

Position Lights

C

1

0

May be inoperative for day operations.

 

 

 

 

 

 

 

 

3.

Landing Lights

C

3

2

One may be inoperative for night operations.

 

 

 

 

 

 

 

 

 

 

C

3

0

May be inoperative for day operations.

 

 

 

 

 

 

 

 

4.

SEARCH LIGHTS Signal

C

1

0

 

 

 

 

 

 

 

 

 

5.

Cabin Interior Lights

C

-

-

May be inoperative provided lighting configuration is acceptable to the flight crew.

 

 

 

 

 

 

 

 

6.

Front Baggage Compartment Light

C

1

0

 

 

 

 

 

 

 

 

 

7.

Toilet Lighting

C

1

0

 

 

 

 

 

 

 

 

 

8.

Orientation Lights

C

2

0

 

 

 

 

 

 

 

 

 

9.

Passenger Notice FASTEN SEAT BELTS

D

1

0

May be inoperative for cargo operations only.

 

 

 

 

 

 

 

 


33

LIGHTS

 

 

 

 

 

 

 

 

 

 

 

 

10.

Wing Ice Lights

C

-

0

May be inoperative provided aircraft is not operated at night.

|

|

 

 

 

 

 

 

 

 

 

C

-

0

May be inoperative provided:

a)          Aircraft is equipped with an approved Ice Detection System, and

b)          Ground deicing procedures do not require use of Wing Ice Lights.

|

|

|

|

|

|

|

 

 

 

 

 

 

 

 

 

C

2

1

One may be inoperative provided:

a)          Left Light is operative for single pilot operations, and

b)          Ground deicing procedures do not require use of Wing Ice Lights.

|

|

|

|

|

|

 

 

 

 

 

 

 

11.

Rear Baggage Compartment Light

C

1

0

 

 

 

 

 

 

 

 

 

12.

Cockpit/ Flight Deck/ Flight Compartment And Instrument Lighting System

C

-

-

Individual Lights may be inoperative provided remaining Lights are:

a)          Sufficient to clearly illuminate all required instruments, controls, and other devices for which it is provided,

b)          Positioned so that direct rays are shielded from flight crewmembers eyes, and

c)          Lighting configuration and intensity is acceptable to the flight crew.

 

 

 

 

 

 

 

 


34

NAVIGATION

 

 

 

 

 

 

 

 

 

 

 

 

1.

Standby Attitude Indicator

C

 

 

B

-

 

 

-

0

 

 

0

May be inoperative provided not required by FAR.

 

May be inoperative provided:

a)          Operations are conducted in day VMC only, and

b)          Operations are not conducted into known or forecast over-the-top conditions.

|

|

 

|

|

|

|

|

|

 

 

 

 

 

 

 

2.

Vertical Speed Indicators

B

2

1

One may be inoperative for day VMC operations.

 

 

 

 

 

 

 

 

3.

Radio Altimeter

C

-

0

 

 

 

 

 

 

 

 

 

4.

Turn And Bank Indicators

B

2

0

May be inoperative provided all three Artificial Horizons are operative.

 

 

 

 

 

 

 

 

5.

Weather Radar

C

-

0

As required by FAR.