Revision:

5

 

Date: 01/09/2009

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

DEPARTMENT OF TRANSPORTATION

 

 

 

 

 

FEDERAL AVIATION ADMINISTRATION

 

 

 

 

 

WASHINGTON , D.C.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

MASTER MINIMUM EQUIPMENT LIST

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

GRUMMAN G-44 AND G-44A WIDGEON (PISTON)

 

 

 

 

 

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

21

Air Conditioning

21-1

22

Autopilot

22-1

23

Communications

23-1, 2, 3, 4

25

Equipment/Furnishings

25-1, 2, 3, 4, 5

26

Fire Protection

26-1

30

Ice & Rain Protection

30-1

31

Indicating/Recording Systems

31-1, 2

33

Lights

33-1, 2

34

Navigation

34-1 THRU 15

35

Oxygen

35-1

37

Vacuum

37-1

46

Information Systems

46-1, 2

61

Propellers

61-1

 

 

 


 

 

 

 

ORIGINAL

12/09/1984

 

 

1

09/15/1986

ALL

 

2

05/19/1989

ALL PAGES

 

3

06/22/1989

HIGHLIGHTS OF REV., DEFINITIONS

 

3

06/22/1989

PREAMBLE

 

4

03/30/1992

HIGHLIGHTS OF REV., DEFINITIONS

 

4

03/30/1992

21-1, 23-1, 23-2, 25-1, 25-2

 

4

03/30/1992

26-1, 31-1, 33-1, 33-2, 34-1

 

4

03/30/1992

34-2, 61-1

 

4a

01/19/1996

HIGHLIGHTS OF REV., DEFINITIONS

 

4a

01/19/1996

GUIDELINES

 

4a

01/19/1996

21-1, 22-1, 23-1, 23-2, 25-1

 

4a

01/19/1996

25-2, 26-1, 30-1, 31-1, 33-1

 

4a

01/19/1996

33-2, 34-1, 34-2, 34-3, 34-4

 

4a

01/19/1996

34-5, 35-1, 37-1, 61-1

 

5

01/09/2009

COVER PAGE, TABLE OF CONTENTS

 

5

01/09/2009

LOG OF REVISIONS, CONTROL PAGES

 

5

01/09/2009

HIGHLIGHTS OF CHANGE, DEFINITIONS

 

5

01/09/2009

PREAMBLE, GUIDELINES

 

5

01/09/2009

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

 

5

01/09/2009

25-1, 25-2, 25-3, 25-4, 25-5

 

5

01/09/2009

26-1, 30-1, 31-1, 31-2, 33-2

 

5

01/09/2009

34-1, 34-2, 34-3, 34-4, 34-5

 

5

01/09/2009

34-6, 34-7, 34-8, 34-9

 

5

01/09/2009

34-12, 34-13, 34-14, 34-15

 

5

01/09/2009

35-1, 46-1, 46-2

 

 

 

 

 


 

 

 

 

Cover Page

-

5

01/09/2009

Table of Contents

I

5

01/09/2009

Log of Revisions

II

5

01/09/2009

Control Page

III

5

01/09/2009

 

IV

5

01/09/2009

Highlights of Change

V

5

01/09/2009

 

VI

5

01/09/2009

 

VII

5

01/09/2009

Definitions

VIII

5

01/09/2009

Preamble

IX

5

01/09/2009

Guidelines for (O) & (M) Procedures

X

5

01/09/2009

 

XI

5

01/09/2009

 

XII

5

01/09/2009

 

XIII

5

01/09/2009

 

XIV

5

01/09/2009

21

21-1

4a

01/19/1996

22

22-1

5

01/09/2009

23

23-1

5

01/09/2009

 

23-2

5

01/09/2009

 

23-3

5

01/09/2009

 

23-4

5

01/09/2009

25

25-1

5

01/09/2009

 

25-2

5

01/09/2009

 

25-3

5

01/09/2009

 

25-4

5

01/09/2009

 

25-5

5

01/09/2009

 

 

 

 


 

 

 

 

26

26-1

5

01/09/2009

30

30-1

5

01/09/2009

31

31-1

5

01/09/2009

 

31-2

5

01/09/2009

33

33-1

4a

01/19/1996

 

33-2

5

01/09/2009

34

34-1

5

01/09/2009

 

34-2

5

01/09/2009

 

34-3

5

01/09/2009

 

34-4

5

01/09/2009

 

34-5

5

01/09/2009

 

34-6

5

01/09/2009

 

34-7

5

01/09/2009

 

34-8

5

01/09/2009

 

34-9

5

01/09/2009

 

34-10

4a

01/19/1996

 

34-11

4a

01/19/1996

 

34-12

5

01/09/2009

 

34-13

5

01/09/2009

 

34-14

5

01/09/2009

 

34-15

5

01/09/2009

35

35-1

5

01/09/2009

37

37-1

4a

01/19/1996

46

46-1

5

01/09/2009

 

46-2

5

01/09/2009

61

61-1

4a

01/19/1996

 

 

 

 


 

Cover Page

 

 

Updated to Revision 5 and incorporate MKC AEG Cover Page format.

Table Of Contents

 

Updated to incorporate Revision 5 changes.

Log Of Revisions

 

Updated to incorporate Revision 5 changes.

Control Pages

 

Updated to incorporate Revision 5 changes.

Highlights Of Change

 

Updated to incorporate Revision 5 changes.

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 incorporate Revision 5 changes.

ATA 22

ATA chapter title changed to coincide with chapter title 22 in opspecs.com.

 

ATA 22-1

Autopilot relief updated IAW PL-101.

 

ATA 22-2

Autopilot Disconnect Functions relief added in accordance with PL-93.

 

ATA 23-1

Communications Systems relief updated IAW PL-95.  HF relief separated and relocated to ATA 23-7 IAW PL-106.

 

ATA 23-3

Public Address System relief updated IAW PL-9.

 

ATA 23-4

Cockpit Voice Recorder relief updated IAW PL-29.

 

ATA 23-5

Boom Microphone relief updated IAW PL-58.

 

ATA 23-6

ELT relief relocated from ATA 25-4 and updated IAW PL-120.

 

 

 


 

ATA 23-7

 

HF Communications relief relocated from ATA 23-1 and updated IAW

PL-106.

 

ATA 23-8

SELCAL relief added IAW PL-117.

 

ATA 25-2

Passenger Seat relief updated IAW PL-79.

 

ATA 25-4

ELT relief relocated to ATA 23-6 IAW PL-120.

 

ATA 25-5

Passenger Convenience Items relief updated to Non-Essential Equipment and Furnishings relief IAW PL-116.

 

ATA 25-6

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

 

ATA 25-7

Fasten Seat Belt Sign relief added IAW PL-89.

 

ATA 25-8

Cargo Restraint Systems relief added IAW PL-100.

 

ATA 26-2

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

 

ATA 30-5

Pitot Heat Indicating Systems relief added IAW PL-90.

 

ATA 31-3

Flight Data Recorder relief updated IAW PL-87.

 

ATA 33-9

Ice Detection Lights relief updated to Wing Ice Light relief.

 

ATA 34-5

DME relief updated IAW PL-3.

 

ATA 34-7

Transponder relief updated IAW PL-76.

 

ATA 34-13

 TCAS relief updated to TCAS I relief IAW PL-32.

 

ATA 34-14

TCAS I relief updated to TCAS II relief IAW PL-32.

 

ATA 34-15

GPWS relief combined with TAWS and updated IAW PL-54.

 

ATA 34-17

Non-Stabilized Magnetic Compass relief added IAW PL-10.

 

ATA 34-18

Altitude Alerting System relief added IAW PL-39.

 

 

 


 

ATA 34-19

 

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

 

ATA 34-20

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

 

ATA 34-21

Windshear Detection System relief added IAW PL-67.

 

ATA 34-22

Standby Attitude Indicator relief added IAW PL-111.

 

ATA 34-23

ADS-B relief added IAW PL-105.

 

ATA 35-2

Protective Breathing Equipment relief added IAW PL-43.

 

ATA 46

ATA chapter added for Information Systems relief.

 

ATA 46-1

Electronic Flight Bag relief added IAW PL-121.

 

 

 


 

 

 

 

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:

 

 

21-1

 

(M)       Maintenance procedure to ensure no fuel leak or                                          mechanical/electrical fault will cause a fire or additional damage.

 

22-1

(M)       Maintenance procedure to ensure no electrical or mechanical fault       will have any adverse effect on any flight control System.

 

23-3

(O)       Operations procedure to ensure PA is not required by FAR and                   alternate procedures are established and used to brief passengers.

 

23-7

(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.

     

23-8

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

23-8A

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

 

25-2-A

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

 

(M)       Maintenance procedure to ensure Seat Back is IMMOVABLE in the             full UPRIGHT position.

 

25-2-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.

 

25-6-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.

 

25-6-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.

 

 

 


 

25-6-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.

 

25-8

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

 

31-2

(O)       Operations procedure to ensure aircraft time is recorded for                        maintenance purposes.

 

33-6

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

 

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 alternate procedures are                            established and used.

 

34-16-B

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

 

34-16-C

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

 

34-16-D

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

 

34-16-F

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

 

 

 


 

34-17

 

(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.

 

34-18

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

 

34-19-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.

 

34-20-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.

 

34-21-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.

 

34-21-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.

 

 

 


 

34-21-B-1

 

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

 

34-21-B-2

 

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

 

37-1

(M)       Maintenance procedure to ensure no unsafe conditions exist which             could affect the engine operation or Systems function.

 

46-1-A

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

 

46-1-B

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

 

46-1-C

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

 

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. 

 

 

 


21

AIR CONDITIONING

 

 

 

 

 

 

 

 

 

 

 

 

1.

Combustion Heater

C

1

0

(M) May be inoperative unless required for defrost.

 

 

 

 

 

 

 

 

2.

Cabin Heat Valves

C

2

0

May be inoperative provided failed Valve is in the CLOSED/OFF position.

 

 

 

 

 

 

 

 

3.

Air Conditioner

C

1

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.

|

|

|

|

|

 

 

 

 

 

 

 

2.

Cockpit Speaker

C

1

0

May be inoperative provided two operative Headsets are available to the flight crew.

 

 

 

 

 

 

 

 

3.

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.

|

|

 

 

 

 

 

 

 

4.

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.

|

|

|

|

|

 

 

 

 

 

 

 

 

 

 

 

 

(Continued)

|

 

 

 

 

 

 

 


23

COMMUNICATIONS

 

 

 

 

 

 

 

 

 

 

 

 

A)

For Air Carrier And Commercial Operators (Continued)

 

 

 

 

|

|

|

 

 

 

 

 

 

 

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.

|

|

|

 

 

 

 

 

 

 

5.

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.

|

|

|

|

 

 

 

 

 

 

 

 

 

 

 

 

(Continued)

|

 

 

 

 

 

 

 


23

COMMUNICATIONS

 

 

 

 

 

 

 

 

 

 

 

 

5.

Boom Microphones (Continued)

 

 

 

 

|

|

 

 

 

 

 

 

 

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.

|

|

|

|

 

 

 

 

 

 

 

6.

***

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.

|

|

 

 

 

 

 

 

 


23

COMMUNICATIONS

 

 

 

 

 

 

 

 

 

 

 

 

7.

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.

|

|

|

 

|

|

|

|

|

|

|

|

|
|
|
|

|

|

|

 

|

|

|

|

|

 

 

 

 

 

 

 

8.

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.

|

|

 

 

 

 

 

 

 


25

EQUIPMENT/ FURNISHINGS

 

 

 

 

 

 

 

 

 

 

 

 

1.

Cockpit Shoulder Harness

B

2

1

Right side may be inoperative for single pilot operations, however Right Seat must remain unoccupied.

 

 

 

 

 

 

 

 

2.

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.

|

|

|

 

 

 

 

 

 

 

 

 

 

 

 

(Continued)

|

 

 

 

 

 

 

 


25

EQUIPMENT/ FURNISHINGS

 

 

 

 

 

 

 

 

 

 

 

 

2.

Passenger Seat(s) (Continued)

 

 

 

 

|

|

 

 

 

 

 

 

 

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.

|

|

|

|

|

|

|

|

|

|

 

 

 

 

 

 

 

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.

|

|

|

|

|

|

|

|

|

|

 

 

 

 

 

 

 

3.

Approved Flotation Equipment

C

-

-

As required by FAR.

 

 

 

 

 

 

 

 

4.

ELT

 

 

 

RELOCATED TO ATA 23-6, REVISION 5.

|

|

 

 

 

 

 

 

 


25

EQUIPMENT/ FURNISHINGS

 

 

 

 

 

 

 

 

 

 

 

 

5.

***

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.

|

|

|

|

|

|

|

|

|

|

 

|

|

|

 

 

 

 

 

 

 

6.

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

 

 

 

 

 

 

 

 

 

 

 

 

6.

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.

|

|

|

 

 

 

 

 

 

 

7.

“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.

|

|

|

|

 

 

 

 

 

 

 


25

EQUIPMENT/ FURNISHINGS

 

 

 

 

 

 

 

 

 

 

 

 

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.

|

|

 

 

 

 

 

 

 


26

FIRE PROTECTION

 

 

 

 

 

 

 

 

 

 

 

 

1.

Portable Fire Extinguisher

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.

Cargo Compartment Fire Detection/ Suppression Systems

C

-

0

May be inoperative provided associated Cargo Compartment remains EMPTY.

 

NOTE 1:  Does not preclude the                        carriage of empty Cargo                     Containers, Pallets, Ballast,                 etc.

 

NOTE 2:  Class E Cargo                                    Compartments require only                 the installation of Smoke or                 Fire Detection Systems (not                 Suppression).

|

|

|

 

|

|

|

|

 

|

|

|

|

|

 

 

 

 

 

 

 


30

ICE & RAIN PROTECTION

 

 

 

 

 

 

 

 

 

 

 

 

1.

Pitot Heater

B

1

0

Left Unit must be operative for IFR passenger carrying and for flight in known or forecast icing conditions.  Two heated Pitot Tubes are required for these conditions if a second Airspeed Indicator is installed and operative.

 

 

 

 

 

 

 

 

2.

Surface Deicing System (Wing, Vertical and Horizontal Stabilizer)

C

1

0

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

 

 

 

 

 

 

 

 

3.

Windshield Deice System

C

1

0

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

 

 

 

 

 

 

 

 

4.

Propeller Anti-Icing/ Deicing System

C

1

0

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

 

 

 

 

 

 

 

 

5.

Pitot Heat Indicating Systems (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 With Sweep Second Hand Or Electric Digital Clock

C

1

0

May be inoperative for VFR flight.

 

 

 

 

 

 

 

 

2.

Flight Hour Recorder

C

1

0

(O)

 

 

 

 

 

 

 

 

3.

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

 

 

 

 

 

 

 

 

 

 

 

 

3.

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.

|

|

|

 

 

 

 

 

 

 


33

LIGHTS

 

 

 

 

 

 

 

 

 

 

 

 

1.

Anti-Collision Beacon Light System

B

1

0

May be inoperative for day operations.

 

 

 

 

 

 

 

 

2.

Position Lights

C

3

0

May be inoperative for day operations.

 

 

 

 

 

 

 

 

3.

Landing Lights

C

2

0

May be inoperative for day operations.

 

 

 

 

 

 

 

 

4.

Cabin Lights

C

-

-

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

 

 

 

 

 

 

 

 

5.

Strobe Light System

C

1

0

 

 

 

 

 

 

 

 

 

6.

Passenger Notice System(Fasten Seat Belt/No Smoking)

C

1

0

(O) May be inoperative provided appropriate verbal briefings are given to the passengers.

 

 

 

 

 

 

 

 

7.

Anchor Light

C

-

-

As required by FAR.

 

 

 

 

 

 

 

 

8.

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.

 

 

 

 

 

 

 

 


33

LIGHTS

 

 

 

 

 

 

 

 

 

 

 

 

9.

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.

|

|

|

|

|

|

 

 

 

 

 

 

 


34

NAVIGATION

 

 

 

 

 

 

 

 

 

 

 

 

1.

Vertical Speed Indicator

B

1

0

Must be operative on left side for IFR passenger carrying.

 

 

 

 

 

 

 

 

2.

Gyroscopic Rate Of Turn/Slip Skid Indicator

B

1

0

Must be operative on left side for IFR, passenger carrying VFR over the top, and passenger carrying VFR night flights.

 

 

 

 

 

 

 

 

3.

Navigation Equipment (VOR/ILS, LORAN, VLF/OMEGA, INS, DOPPLER, GPS, RNAV)

C

-

-

As required by FAR.

 

 

 

 

 

 

 

 

4.

Weather Radar/ Thunderstorm Detection Equipment

C

1

0

As required by FAR.

 

 

 

 

 

 

 

 

5.

Distance Measuring Equipment (DME) Systems

D

-

-

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

|

|

|

 

 

 

 

 

 

 

6.

Marker Beacon

C

1

0

May be inoperative provided approach does not require its use.

 

 

 

 

 

 

 

 

7.

ATC Transponders And Automatic Altitude Reporting Systems

B

 

 

 

 

 

 

 

D

-

 

 

 

 

 

 

 

-

0

 

 

 

 

 

 

 

1

May be inoperative provided:

a)          Operations do not require its use, and

b)          Prior to flight, approval is obtained from ATC facilities having jurisdiction over the planned route of flight.

 

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

|

|

|

|

|

|

|

 

|

|

 

 

 

 

 

 

 

 

 

 

 

 

(Continued)

|

 

 

 

 

 

 

 


34

NAVIGATION

 

 

 

 

 

 

 

 

 

 

 

 

7.

ATC Transponders And Automatic Altitude Reporting Systems (Continued)

 

 

 

 

|

|

|

|

 

 

 

 

 

 

 

A)

Elementary And Enhanced Downlink Aircraft Reportable Parameters Not Required By FAR

A

-

0

May be inoperative provided:

a)          Operations do not require its use, and

b)          Repairs are made prior to completion of the next heavy maintenance visit.

|

|

|

|

|

|

 

 

 

 

 

 

 

B)

ADS-B Squitter Transmissions

A

-

0

May be inoperative provided:

a)          Operations do not require its use, and

b)          Repairs are made prior to completion of the next heavy maintenance visit.

|

|

|

|

|

|

 

 

 

 

 

 

 

8.

Radar Altimeter

C

1

0

 

 

 

 

 

 

 

 

 

9.

Flight Director

C

1

0

 

 

 

 

 

 

 

 

 

10.

RMI

C

1

0

 

 

 

 

 

 

 

 

 

11.

ADF

C

1

0

 

 

 

 

 

 

 

 

 

12.

Altitude Encoder

 

 

 

COMBINED WITH ATC TRANSPONDERS, REVISION 4a.

 

 

 

 

 

 

 

 


34

NAVIGATION

 

 

 

 

 

 

 

 

 

 

 

 

13.

Traffic Alert Collision Avoidance System (TCAS I)

B

-

0

(M) May be inoperative provided:

a)          System is deactivated and SECURED, and

b)          Enroute or approach procedures do not require its use.

|

|

|

|

|

|

 

 

 

 

 

 

 

 

 

C

-

0

(M) May be inoperative provided:

a)          Not required by FAR,

b)          System is deactivated and SECURED, and

c)          Enroute or approach procedures do not require its use.

|

|

|

|

|

|

|

 

 

 

 

 

 

 

14. ***

Traffic Alert Collision Avoidance System (TCAS II)

B

-

0

(M) May be inoperative provided:

a)          System is deactivated and secured, and

b)          Enroute or approach procedures do not require its use.

|

|

|

|

|

|

 

 

 

 

 

 

 

 

 

C

-

0

(M) May be inoperative provided:

a)          System is not required by FAR,

b)          System is deactivated and secured, and

c)          Enroute or approach procedures do not require its use.

|

|

|

|

|

|

|

 

 

 

 

 

 

 

A)

Combined Traffic Alert (TA) And Resolution Advisory (RA) Dual Display 

C

2

1

One may be inoperative on the non-flying pilot side provided:

a)          TA and RA Visual Display is operative on flying pilot side, and

b)          TA and RA Audio Function is operative on flying pilot side.

|

|

|

|

|

|

|

 

 

 

 

 

 

 

 

 

 

 

 

(Continued)

|

 

 

 

 

 

 

 


34

NAVIGATION

 

 

 

 

 

 

 

 

 

 

 

 

14. ***

Traffic Alert Collision Avoidance System (TCAS II)  (Continued)

 

 

 

 

|

|

|

 

 

 

 

 

 

 

B)

Resolution Advisory (RA) Display System(s)

C

2

1

May be inoperative on non-flying pilot side.

|

|

 

 

 

 

 

 

 

 

 

C

-

0

(O) May be inoperative provided:

a)          Traffic Alert (TA) Visual Display and Audio Functions are operative,

b)          TA ONLY Mode is selected by the crew, and

c)          Enroute or approach procedures do not require its use.

|

|

|

|

|

|

|

|

|

 

 

 

 

 

 

 

C)

Traffic Alert Display System(s)

C

-

0

(O) May be inoperative provided:

a)          RA Visual Display and Audio Functions are operative, and

b)          Enroute or approach procedures do not require its use.

|

|

|

|

|

|

 

 

 

 

 

 

 

D)

Audio Functions

B

1

0

May be inoperative provided enroute or approach procedures do not require use of TCAS.

|

|

|

 

 

 

 

 

 

 

E)

***

Airspace Selection Function

C

-

0

 

|

|

 

 

 

 

 

 

 


34

NAVIGATION

 

 

 

 

 

 

 

 

 

 

 

 

15.

Terrain Awareness And Warning System (TAWS)

 

 

 

 

|

|

|

 

 

 

 

 

 

 

A)

Class A TAWS Equipment Required

 

 

 

 

|

|

 

 

 

 

 

 

 

1)

Ground Proximity Warning System (GPWS)

A

1

0

(O) May be inoperative provided:

a)          Alternate procedures are established and used, and

b)          Repairs are made within two flight days.

|

|

|

|

|

 

 

 

 

 

 

 

a)

Modes 1-4

A

4

0

(O) May be inoperative provided:

a)          Alternate procedures are established and used, and

b)          Repairs are made within two flight days.

|

|

|

|

|

 

 

 

 

 

 

 

b)

Test Mode

A

1

0

May be inoperative provided:

a)          GPWS is considered inoperative, and

b)          Repairs are made within two flight days.

|

|

|

|

|

 

 

 

 

 

 

 

c)

Glideslope Deviation(s)

(Mode 5)

C

-

1

 

|

|

 

 

 

 

 

 

 

 

 

B

-

0

 

|

 

 

 

 

 

 

 

 

 

 

 

 

(Continued)

|

 

 

 

 

 

 

 


34

NAVIGATION

 

 

 

 

 

 

 

 

 

 

 

 

A)

Class A TAWS Equipment  (Continued)

 

 

 

 

|

|

|

 

 

 

 

 

 

 

1)

Ground Proximity Warning System (GPWS) (Continued)

 

 

 

 

|

|

|

 

 

 

 

 

 

 

d)

Advisory Callouts

B

-

0

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

|

|

|

 

 

 

 

 

 

 

 

 

C

-

0

(O) May be inoperative provided:

a)          Advisory Callouts not required by FAR, and

b)          Alternate procedures are established and used.

|

|

|

|

|

 

 

 

 

 

 

 

e)

***

Windshear Mode (Reactive)

 

B

1

0

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

 

NOTE:  Operator’s 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.

|

|

|

|

|

|

 

 

 

 

 

 

 

 

 

 

 

 

(Continued)

|

 

 

 

 

 

 

 


34

NAVIGATION

 

 

 

 

 

 

 

 

 

 

 

 

A)

Class A TAWS Equipment Required (Continued)

 

 

 

 

|

|

|

 

 

 

 

 

 

 

2)

Terrain System-Forward Looking Terrain Avoidance (FLTA) And Premature Descent Alert (PDA) Functions

B

1

0

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

|

|

|

|

|

|

 

 

 

 

 

 

 

3)

Terrain Displays

C

-

1

 

|

 

 

 

 

 

 

 

 

 

B

-

0

 

|

 

 

 

 

 

 

 

4)

***

Runway Awareness And Advisory System (RAAS)

C

1

0

 

|

|

|

 

 

 

 

 

 

 

B)

Class B TAWS Equipment Required

 

 

 

 

|

|

 

 

 

 

 

 

 

1)

Ground Proximity Warning System (GPWS)

 

A

1

0

(O) May be inoperative provided:

a)          Alternate procedures are established and used, and

b)          Repairs are made within two flight days.

|

|

|

|

|

 

 

 

 

 

 

 

a)

Modes 1 & 3

A

2

0

(O) May be inoperative provided:

a)          Alternate procedures are established and used, and

b)          Repairs are made within two flight days.

|

|

|

|

|

 

 

 

 

 

 

 

 

 

 

 

 

(Continued)

|

 

 

 

 

 

 

 


34

NAVIGATION

 

 

 

 

 

 

 

 

 

 

 

 

B)

Class B TAWS Equipment Required (Continued)

 

 

 

 

|

|

|

 

 

 

 

 

 

 

1)

Ground Proximity Warning System (GPWS) (Continued)

 

 

 

 

|

|

|

 

 

 

 

 

 

 

b)

Test Mode

A

1

0

May be inoperative provided:

a)          GPWS is considered inoperative, and

b)          Repairs are made within two flight days.

|

|

|

|

|

 

 

 

 

 

 

 

c)

***

Modes 2, 4 & 5

 

C

3

0

 

|

|

 

 

 

 

 

 

 

d)

Advisory Callouts

B

-

0

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

|

|

|

 

 

 

 

 

 

 

 

 

C

-

0

(O) May be inoperative provided:

a)          Advisory Callouts not required by FAR, and

b)          Alternate procedures are established and used.

|

|

|

|

|

 

 

 

 

 

 

 

e)

***

Windshear Mode (Reactive)

C

1

0

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

|

|

|

 

 

 

 

 

 

 

 

 

 

 

 

(Continued)

|

 

 

 

 

 

 

 


34

NAVIGATION

 

 

 

 

 

 

 

 

 

 

 

 

B)

Class B TAWS Equipment Required (Continued)

 

 

 

 

|

|

|

 

 

 

 

 

 

 

2)

Terrain System-Forward Looking Terrain Avoidance (FLTA) And Premature Descent Alert (PDA) Functions

B

1

0

 

|

|

|

|

|

|

 

 

 

 

 

 

 

3)

***

Terrain Displays

 

C

-

0

 

|

|

 

 

 

 

 

 

 

4)

***

Runway Awareness & Advisory System (RAAS)

C

1

0

 

|

|

|

 

 

 

 

 

 

 

C)

Class C TAWS Equipment

 

 

 

 

|

|

 

 

 

 

 

 

 

1)

***

 

TAWS/GPWS

 

C

1

0

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

 

NOTE:  Any Mode that operates

             normally may be used.

|

|

|

 

|

|

 

 

 

 

 

 

 


34

NAVIGATION

 

 

 

 

 

 

 

 

 

 

 

 

16.

***

Flight Profile Advisory System (FPAS)

 

 

 

 

 

 

 

 

 

 

 

 

A)

Gear Mode

A

1

0

(O) May be inoperative provided:

a)          Alternate procedures are established and used,  and

b)          Repairs are made within two flight days.

 

 

 

 

 

 

 

 

B)

Minimums Mode

A

1

0

(O) May be inoperative provided:

a)          Alternate procedures are established and used,  and

b)          Repairs are made within two flight days.

c)   

 

 

 

 

 

 

 

C)

Radio Altitude Mode

A

1

0

(O) May be inoperative provided:

a)          Alternate procedures are established and used,  and

b)          Repairs are made within two flight days.

 

 

 

 

 

 

 

 

D)

Test Mode

A

1

0

(O) May be inoperative provided:

a)          Alternate procedures are established and used,  and

b)          Repairs are made within two flight days.

 

 

 

 

 

 

 

 

E)

Glideslope Deviation Mode

B

1

0

 

 

 

 

 

 

 

 

 

F)

Advisory Callouts

C

-

0

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

 

 

 

 

 

 

 

 


34

NAVIGATION

 

 

 

 

 

 

 

 

 

 

 

 

17.

Non-Stabilized Magnetic Compass System

B

1

0

(O) May be inoperative provided any combination of three Gyro or INS (IRU) Stabilized Compass Systems are operative.

 

 

 

 

 

 

 

 

 

 

B

1

0

(O) May be inoperative provided:

a)          Any combination of two Gyro or INS (IRU) Stabilized Compass Systems operate normally, and

b)          Airplane is operated with Dual Independent Navigation Capability and under Positive Radar Control by ATC on the enroute portion of the flight.

 

 

 

 

 

 

 

 

 

 

B

1

0

(O) May be inoperative for flights that are entirely within areas of magnetic unreliability provided at least two Stabilized Directional Gyro Systems are installed, operate normally, and used in conjunction with approved Free Gyro Navigation Techniques.

 

 

 

 

 

 

 

 

18.

Altitude Alerting System

A

-

0

(O) May be inoperative provided:

a)          Autopilot with Altitude Hold is operative,

b)          Enroute operations do not require its use, and

c)          Repairs are made within three flight days.