Revision:

4

 

Date: 01/09/2009

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

DEPARTMENT OF TRANSPORTATION

 

 

 

 

 

FEDERAL AVIATION ADMINISTRATION

 

 

 

 

 

WASHINGTON , D.C.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

MASTER MINIMUM EQUIPMENT LIST

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

HANSA 320

 

 

 

 

 

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, VIII

--

Definitions

IX

--

Preamble

X

--

Guidelines for (O) & (M) Procedures

XI, XII, XIII, XIV

--

Guidelines for (O) & (M) Procedures

XV, XVI, XVII

21

Air Conditioning

21-1, 2

22

Autopilot

22-1

23

Communications

23-1, 2, 3, 4

24

Electrical

24-1

25

Equipment/Furnishings

25-1 THRU 7

26

Fire Protection

26-1, 2

27

Flight Controls

27-1

28

Fuel

28-1, 2

29

Hydraulic Power

29-1

30

Ice & Rain Protection

30-1

31

Indicating/Recording Systems

31-1, 2

32

Landing Gear

32-1

33

Lights

33-1, 2, 3

34

Navigation

34-1 THRU 15

35

Oxygen

35-1

46

Information Systems

46-1, 2

49

Airborne Auxiliary Power

49-1

77

Engine Indicating

77-1

79

Engine Oil

79-1

 

 

 


 

 

 

 

2

02/03/1992

ALL PAGES

 

3

03/29/1995

HIGHLIGHTS OF REV., DEFINITIONS

 

3

03/29/1995

GUIDELINES

 

3

03/29/1995

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

 

3

03/29/1995

24-1, 25-1, 25-2, 26-1, 26-2

 

3

03/29/1995

27-1, 27-2, 28-1, 28-2, 29-1

 

3

03/29/1995

30-1, 31-1, 32-1, 33-1, 33-2

 

3

03/29/1995

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

 

3

03/29/1995

34-5, 35-1, 49-1, 77-1, 79-1

 

4

01/09/2009

COVER PAGE, TABLE OF CONTENTS

 

4

01/09/2009

LOG OF REV., CONTROL PAGES

 

4

01/09/2009

HIGHLIGHTS OF CHANGE, DEFINITIONS

 

4

01/09/2009

PREAMBLE, GUIDELINES

 

4

01/09/2009

21-1, 22-1, 23-1, 23-2, 23-3

 

4

01/09/2009

23-4, 25-1, 25-2, 25-3, 25-4

 

4

01/09/2009

25-5, 25-6, 25-7, 26-1, 26-2

 

4

01/09/2009

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

 

4

01/09/2009

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

 

4

01/09/2009

34-5, 34-6, 34-7, 34-8, 34-9

 

4

01/09/2009

34-10, 34-11, 34-12, 34-13

 

4

01/09/2009

34-14, 34-15, 35-1, 46-1

 

4

01/09/2009

46-2

 

 

 

 

 


 

 

 

 

Cover Page

-

4

01/09/2009

Table of Contents

I

4

01/09/2009

Log of Revisions

II

4

01/09/2009

Control Page

III

4

01/09/2009

 

IV

4

01/09/2009

Highlights of Change

V

4

01/09/2009

 

VI

4

01/09/2009

 

VII

4

01/09/2009

 

VIII

4

01/09/2009

Definitions

IX

4

01/09/2009

Preamble

X

4

01/09/2009

Guidelines for (O) & (M) Procedures

XI

4

01/09/2009

 

XII

4

01/09/2009

 

XIII

4

01/09/2009

 

XIV

4

01/09/2009

 

XV

4

01/09/2009

 

XVI

4

01/09/2009

 

XVII

4

01/09/2009

21

21-1

4

01/09/2009

 

21-2

3

03/29/1995

22

22-1

4

01/09/2009

23

23-1

4

01/09/2009

 

23-2

4

01/09/2009

 

23-3

4

01/09/2009

 

23-4

4

01/09/2009

24

24-1

3

03/29/1995

25

25-1

4

01/09/2009

 

25-2

4

01/09/2009

 

25-3

4

01/09/2009

 

25-4

4

01/09/2009

 

25-5

4

01/09/2009

 

25-6

4

01/09/2009

 

25-7

4

01/09/2009

26

26-1

4

01/09/2009

 

26-2

4

01/09/2009

27

27-1

3

03/29/1995

28

28-1

3

03/29/1995

 

28-2

3

03/29/1995

 

 

 

 


 

 

 

 

29

29-1

3

03/29/1995

30

30-1

4

01/09/2009

31

31-1

4

01/09/2009

 

31-2

4

01/09/2009

32

32-1

3

03/29/1995

33

33-1

4

01/09/2009

 

33-2

4

01/09/2009

 

33-3

4

01/09/2009

34

34-1

4

01/09/2009

 

34-2

4

01/09/2009

 

34-3

4

01/09/2009

 

34-4

4

01/09/2009

 

34-5

4

01/09/2009

 

34-6

4

01/09/2009

 

34-7

4

01/09/2009

 

34-8

4

01/09/2009

 

34-9

4

01/09/2009

 

34-10

4

01/09/2009

 

34-11

4

01/09/2009

 

34-12

4

01/09/2009

 

34-13

4

01/09/2009

 

34-14

4

01/09/2009

 

34-15

4

01/09/2009

35

35-1

4

01/09/2009

46

46-1

4

01/09/2009

49

49-1

3

03/29/1995

77

77-1

3

03/29/1995

79

79-1

3

03/29/1995

 

 

 

 


 

Cover Page

 

 

Updated to Revision 4 and incorporate MKC AEG Cover Page format.

Table Of Contents

 

Updated to incorporate Revision 4 changes.

Log Of Revisions

 

Updated to incorporate Revision 4 changes.

Control Pages

 

Updated to incorporate Revision 4 changes.

Highlights Of Change

 

Updated to incorporate Revision 4 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 4 changes.

ATA 21-1

“OR” removed between provisos in accordance with Policy Letter 31.

 

ATA 21-2

“OR” removed between provisos IAW PL-31.

 

ATA 22

ATA chapter title updated to coincide with chapter title in opspecs.com.

 

ATA 22-1

Autopilot relief updated IAW PL-101.

 

ATA 22-2

Control Wheel Autopilot Disengage Button relief updated to Autopilot Disconnect Functions relief IAW PL-93.

 

ATA 23-1

VHF and UHF Communications Systems relief updated IAW PL-95.  HF relief relocated to ATA 23-8 to comply with PL-106.

 

ATA 23-2

“OR” removed between provisos IAW PL-31.

 

ATA 23-3

Cockpit Voice Recorder updated IAW PL-29.

 

 

 


 

ATA 23-5

 

Passenger Address System relief updated IAW PL-9.

 

ATA 23-6

Boom Microphone relief updated IAW PL-58.

 

ATA 23-7

SELCAL relief added IAW PL-117.

 

ATA 23-8

High Frequency (HF) Communications relief relocated from ATA 23-1 and updated IAW PL-106.

 

ATA 23-9

ELT relief relocated from ATA 25-3 and updated IAW PL-120.

 

ATA 25-2

Passenger Seat relief updated IAW PL-79.

 

ATA 25-3

ELT relief relocated to ATA 23-9 IAW PL-120.

 

ATA 25-4

Passenger Convenience Items relief replaced by Non-Essential Equipment and Furnishings relief IAW PL-116.

 

ATA 25-5

Emergency Medical Equipment relief added IAW PL-73.

 

ATA 25-6

Fasten Seat Belt Sign relief added IAW PL-89.

 

ATA 25-7

Lavatory Ash Tray relief added IAW PL-85.

 

ATA 25-8

Galley Waste Receptacle relief added IAW PL-96.

 

ATA 25-9

Cargo Restraint System relief added IAW PL-100.

 

ATA 25-10

Overhead Storage Bins/Cabin and Galley Storage Compartments/Closets relief added IAW PL104.

 

ATA 26-1

Lavatory Smoke Detector System updated IAW PL-24.

 

ATA 26-2

Hand Fire Extinguisher relief updated to Portable Fire Extinguisher relief IAW PL-75.

 

ATA 26-3

Lavatory Fire Extinguisher System relief updated IAW PL-24.

 

 

 


 

ATA 26-4

 

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

 

ATA 30-7

Pitot Heat Indicating Systems relief added IAW PL-90.

 

ATA 31-1

Repair category, number installed and number required items in relocated system removed to comply with current standards.

 

ATA 31-3

Flight Data Recorder relief updated IAW PL-87.

 

ATA 33-1

Wing Ice Light relief updated.

 

ATA 33-6

Cockpit and Instrument Lighting System relief updated IAW PL-77.

 

ATA 33-8

Anti-Collision Light System relief proviso restructured to comply with standard practice.

 

ATA 33-9

“OR” added at the end of item “c)” in the proviso for proper sentence structure and to clarify meaning.

 

ATA 34-1

Standby Attitude Indicator relief updated IAW PL-111.

 

ATA 34-3

DME relief updated IAW PL-3.

 

ATA 34-9

Transponder relief updated IAW PL-76.

 

ATA 34-10

Altitude Alerting System updated IAW PL-39.

 

ATA 34-14

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

 

ATA 34-15

TCAS relief updated IAW PL-32.

 

ATA 34-16

GPWS relief incorporated into and updated to the current TAWS relief IAW PL-54.

 

ATA 34-17

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

 

ATA 34-18

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

 

 

 


 

ATA 34-19

 

Windshear Detection and Avoidance Systems relief added IAW PL-67.

 

ATA 34-20

ADS-B relief added IAW PL-105.

 

ATA 35-2

Protective Breathing Equipment relief added IAW PL-43.

 

ATA 46

Chapter added for Information Systems relief items.

 

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 the inoperative Valve is secured       CLOSED.

 

(O)       Operations procedure to address conducting flight operations at

            FL 250 or below.

 

21-2

(M)       Maintenance procedure to ensure the Dump Valve remains in the               OPEN position.

 

22-1

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

 

22-3

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

 

23-5

(O)       Operations procedure to ensure passengers receive all appropriate             briefings.

 

23-7

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

     

23-7-A

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

 

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.

 

24-1

(M)       Maintenance procedure to ensure the Battery is disconnected and       all electrical components are properly stowed.

 

 

 


 

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.

 

25-5-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.

 

25-5-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.

 

25-5-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 Container is EMPTY and access             to the Compartment is SECURED.

 

(O)       Operations procedure to ensure sufficient Waste Receptacles are                   available to accommodate all waste that may be generated on the                   flight.

 

25-9

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

 

25-10

(M)       Maintenance procedure to ensure procedures are established to                 secure Compartment CLOSED and properly PLACARD.

 

(M)      Maintenance procedure to ensure Door(s) is properly removed,                        Compartment is appropriately placarded, and crew is alerted.

 

(O)       Operations procedure to ensure Bin or Compartment is not used for            storage and crew and passengers are alerted and briefed.

 

 

 


 

25-10-A

 

(M)      Maintenance procedure to secure Doors by an alternate means.

 

26-1

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

 

(O)       Operations procedure to ensure only crewmembers use the                       Lavatory.

 

26-3

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

 

(O)       Operations procedure to ensure only crewmembers use the                       Lavatory.

 

28-4

(O)       Operations procedure to ensure the Fuel Pumps and Fuel Low                   Pressure Warning Systems are both operative.

 

28-5

(O)       Operations procedure to ensure all required Fuel Pumps and the                Fuel Low Pressure Warning Systems are operative.

 

28-7

(O)       Operations procedure to ensure all Fuel Tank Pumps, Quantity                   Indicating Systems and the Pump Malfunction Indicator are                         operative.

 

28-9

(O)       Operations procedure to ensure the Emergency Tip Tank Fuel                    Pump is operative if the flight is predicated on use of Tip Tank fuel.

 

28-10

(O)       Operations procedure to ensure both Automatic Sequence Systems             and the associated Normal Tip Tank Fuel Pump are operative if the             flight is predicated on use of Tip Tank fuel.

 

30-4

(O)       Operations procedure to ensure the entire flight can be conducted             as a VFR operation in non-icing conditions.

 

31-4

(O)       Operations procedure to ensure an alternate method of recording               flight time is established and used.

 

 

 


 

32-1

 

(O)       Operations procedure to ensure the Locks are REMOVED or fixed             in the OPEN position.

 

33-5

(O)       Operations procedure to ensure all appropriate briefings are given       to the passengers.

 

33-7

(O)       Operations procedure to ensure the crew evaluates the Lighting                 Configuration at dispatch.

 

33-8

(O)       Operations procedure for the crew to ensure the Strobes are                      properly certificated if night operations are planned.

 

34-10

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

 

34-14

(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.

 

34-15-A

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

 

34-15-B

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

     

34-15-B-2

(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.

 

 

 


 

34-15-B-3

 

(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.

 

34-16-A-1

 

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

 

34-16-A-1-a

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

 

34-16-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.

 

34-16-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.

 

34-16-A-2

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

 

34-16-B-1

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

 

34-16-B-1-a

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

 

34-16-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.

 

 

 


 

34-16-B-1-e

 

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

 

34-16-C-1

 

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

 

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

(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.

 

34-19-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.

 

34-19-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.

 

34-19-B-1

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

 

34-19-B-2

 

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

 

 

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. 

 

77-2

(O)       Operations procedure to ensure the Fuel Pressure Warning System             is operative.

 

79-1

(O)       Operations procedure to ensure Oil Pressure Gauges are                           monitored.

 

 

 


21

AIR CONDITIONING

 

 

 

 

 

 

 

 

 

 

 

 

1.

Air Supply

C

2

1

(M) Right Engine Shutoff Valve may be inoperative provided:

a)          Left Engine Shutoff Valve is operative,

b)          Emergency Shutoff Valve is operative, and

c)          The inoperative Valve is secured CLOSED.

 

 

 

 

 

 

 

 

 

 

C

2

1

(O) Left Engine Shutoff Valve may be inoperative provided:

a)          Right Engine Shutoff Valve is operative,

b)          Emergency Shutoff Valve is operative, and

c)          Flight operations are restricted to 25,000 feet MSL or below.

 

 

 

 

 

 

 

|

 

 

C

2

0

May be inoperative provided the aircraft is operated unpressurized.

 

 

 

 

 

 

 

 

2.

Outflow Valves

C

2

1

One may be inoperative provided flight operations are restricted to 25,000 feet MSL or below.

 

 

 

 

 

 

 

|

 

 

C

2

0

(M) Both may be inoperative provided the aircraft is operated unpressurized with the Dump Valve in the OPEN position.

 

 

 

 

 

 

 

 

3.

Cabin Altitude Selector

C

1

0

May be inoperative provided the aircraft is operated unpressurized.

 

 

 

 

 

 

 

 

4.

Cabin Altitude Indicator

C

1

0

May be inoperative provided Cabin Differential Pressure Gauge is operative.

 

 

 

 

 

 

 

 


21

AIR CONDITIONING

 

 

 

 

 

 

 

 

 

 

 

 

5.

Cabin Differential Pressure Gauge

C

1

0

May be inoperative provided Cabin Altimeter is operative.

 

 

 

 

 

 

 

 

6.

Automatic Temperature Control

C

1

0

May be inoperative provided Manual Control is operative.

 

 

 

 

 

 

 

 

7.

Cabin Rate Of Climb

C

1

0

May be inoperative provided all other instruments and functions of Pressurization System operate normally.

 

 

 

 

 

 

 

 

8.

Manual Temperature Control

C

1

0

May be inoperative provided the aircraft is operated unpressurized.

 

 

 

 

 

 

 

 

9.

Cabin Altitude Warning Light

C

1

0

May be inoperative provided:

a)          Cabin Altimeter is operative, and

b)          Cabin Pressure Warning Horn is operative.

 

 

 

 

 

 

 

 

10.

Cabin Altitude Warning Horn

C

1

0

May be inoperative provided:

a)          Cabin Altimeter is operative, and

b)          Cabin Altitude Warning Light is operative.

 

 

 

 

 

 

 

 

11.

Cockpit Mixing Valve

C

1

0

May be inoperative provided the Mixing Valve is fixed in the COLD position.

 

 

 

 

 

 

 

 


22

AUTOPILOT

 

 

 

 

|

 

 

 

 

 

 

 

1.

Autopilot System

C

-

0

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

|

|

 

 

 

 

 

 

 

 

 

 

 

 

NOTE:  For RVSM operations, the

             Altitude Hold Function must be

             operative.

|

|

|

 

 

 

 

 

 

 

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.

|

|

|

|

|

 

|

|

 

 

 

 

 

 

 

3.

Yaw Damper

C

1

0

(M)

 

 

 

 

 

 

 

 


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(s)

C

-

0

One may be inoperative.

 

 

 

 

 

 

 

|

 

 

C

-

0

May be inoperative provided an operative Headset is used by the flight crew.

 

 

 

 

 

 

 

 

3.

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.

|

|

|

 

 

 

 

 

 

 

4.

Static Dischargers

C

-

-

All but one per installation location may be missing.

 

 

 

 

 

 

 

 


23

COMMUNICATIONS

 

 

 

 

 

 

 

 

 

 

 

 

5.

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.

|

|

 

 

 

 

 

 

 

6.

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

 

 

 

 

 

 

 

 

 

 

 

 

6.

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.

|

|

|

|

 

 

 

 

 

 

 

7.

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.

|

|

 

 

 

 

 

 

 


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.

|

|

 

 

|

|

|

|

|

|

|

|
|
|
|

|

|

|

|

|

 

|

|

|

|

 

 

 

 

 

 

 

9.

***

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.

|

|

 

 

 

 

 

 

 


24

ELECTRICAL

 

 

 

 

 

 

 

 

 

 

 

 

1.

Batteries

B

2

1

(M) Number 1 Battery may be inoperative provided:

a)          It is disconnected, and

b)          Either GPU or APU is used for engine starts.

 

 

 

 

 

 

 

 

2.

Generator Failure Warning System

B

2

1

One may be inoperative provided the associated Generator is monitored.

 

 

 

 

 

 

 

 

3.

Alternator Systems

 

 

 

DELETED, REVISION 2.

 

 

 

 

 

 

 

 

4.

Alternator Failure Warning Systems

B

2

1

One may be inoperative provided the associated Alternator is monitored.

 

 

 

 

 

 

 

 

5.

Inverter Failure Warning Systems

B

2

1

One may be inoperative provided the associated Inverter is monitored.

 

 

 

 

 

 

 

 

6.

Generators

 

 

 

DELETED, REVISION 2.

 

 

 

 

 

 

 

 

7.

Main Inverter

B

1

0

May be inoperative for VFR operations.

 

 

 

 

 

 

 

 

8.

Bus Tie Indicators

B

-

0

 

 

 

 

 

 

 

 

 


25

EQUIPMENT/ FURNISHINGS

 

 

 

 

 

 

 

 

 

 

 

 

1.

Crew Member Shoulder Harness

 

 

 

DELETED, REVISION 2.

 

 

 

 

 

 

 

 

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.

ELT

 

 

 

RELOCATED TO ATA 23-9, REVISION 4.

|

|

 

 

 

 

 

 

 


25

EQUIPMENT/ FURNISHINGS

 

 

 

 

 

 

 

 

 

 

 

 

4.

***

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.

|

|

|

|

|

|

|

|

|

|

 

|

|

|

 

 

 

 

 

 

 

5.

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

 

 

 

 

 

 

 

 

 

 

 

 

5.

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.

|

|

|

 

 

 

 

 

 

 

6.

“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

 

 

 

 

 

 

 

 

 

 

 

 

7. ***

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.

|

|

|

 

 

 

 

 

 

 

8. ***

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.

|

|

|

|

|

|

|

|

|

|

|

 

 

 

 

 

 

 

9. ***

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

 

 

 

 

 

 

 

 

 

 

 

 

10.

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)          Associated Bin or Compartment is prominently placarded DO NOT USE,

c)          Any Emergency Equipment located in affected Compartment is considered inoperative, and

d)          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.

|

|

|

|

 

 

 

 

 

 

 

 

 

 

 

 

(Continued)

|

 

 

 

 

 

 

 


25

EQUIPMENT/ FURNISHINGS

 

 

 

 

 

 

 

 

 

 

 

 

10.

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

 

 

 

 

|

|

|

|

|

 

 

 

 

 

 

 

 

 

C

-

-

(M)(O) May be inoperative provided:

a)          Affected Door(s) is removed,

b)          Associated Bin or Compartment is not used for storage of any items, except those permanently affixed,

c)          Associated Bin or Compartment is properly placarded DO NOT USE,

d)          Procedures are established and used to alert crewmembers and passengers of inoperative Bins, and

e)          Passengers are briefed that associated Bin or Compartment is not used.

|

|

|

|

|

|

|

|

|

|

|

|

|

|

|

|

 

 

 

 

 

 

 

 

 

 

 

 

NOTE 1:  If no partitions are installed, 

                the entire Overhead Storage

                Compartment is considered

                one Bin or Compartment.

|

|

|

|

 

 

 

 

 

 

 

 

 

 

 

 

NOTE 2:  Any Emergency Equipment

                located in the associated

                Compartment (permanently

                affixed) is available for use.

|

|

|

|

 

 

 

 

 

 

 

A)

***

Storage Compartment Key Locks

D

-

0

(M) May be inoperative in the UNLOCKED position provided Doors can be secured by other means.

|

|

|

 

 

 

 

 

 

 


26

FIRE PROTECTION

 

 

 

 

 

 

 

 

 

 

 

 

1. ***

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.

 

 

 

 

 

 

 

 

2.

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.

|

|

 

 

 

 

 

 

 

 


26

FIRE PROTECTION

 

 

 

 

 

 

 

 

 

 

 

 

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.

 

 

 

 

 

 

 

 

4. ***

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.

Slat Annunciator Lights

C

2

0

Both may be inoperative provided Slat Warning Lights are operative.

 

 

 

 

 

 

 

 

2.

Slat Warning Lights

C

2

0

Both may be inoperative provided Slat Annunciator Lights are operative.

 

 

 

 

 

 

 

 

3.

Rudder Trim Warning Light

C

1

0

 

 

 

 

 

 

 

 

 

4.

Aileron Trim Warning Light

C

1

0

 

 

 

 

 

 

 

 

 

5.

Elevator Trim Warning Light

C

1

0

 

 

 

 

 

 

 

 

 

6.

Stall Warning Systems

 

 

 

 

 

 

 

 

 

 

 

 

1)

Stall Margin Indicator(s)

C

2

0

 

 

 

 

 

 

 

 

 

7.

Rudder Trim Position Indicator

C

1

0

May be inoperative provided:

a)    Aileron Trim Position Indicator is operative, and

b)    A visual check of the Rudder Trim operation is made before each flight.

 

 

 

 

 

 

 

 

8.

Aileron Trim

C

1

0

May be inoperative provided:

a)          Rudder Trim Position Indicator is operative, and

b)          A visual check of the Aileron Trim operation is made before each flight.

 

 

 

 

 

 

 

 

9.

Elevator Hydraulic Trim Control System

C

1

0

 

 

 

 

 

 

 

 

 


28

FUEL

 

 

 

 

 

 

 

 

 

 

 

 

1.

Wing Tank Fuel Quantity Indicating System

 

 

 

DELETED, REVISION 2.

 

 

 

 

 

 

 

 

2.

Tip Tank And Fuselage Tank Fuel Quantity Indicating Systems

C

3

2

One may be inoperative provided:

a)          Associated Fuel Tank is fueled to capacity or defueled and refueled using delivery meter for positive quantity check,

b)          Fuel Consumed Indicator is operative, and

c)          Automatic Sequence Control is operative.

 

 

 

 

 

 

 

 

3.

Auto Sequence Control

C

1

0

 

 

 

 

 

 

 

 

 

4.

Wing Tank Fuel Pumps

C

4

3

(O) One may be inoperative provided:

a)          Fuel Low Pressure Warning System is operative, and

b)          Fuel Quantity Indicating System is operative.

 

 

 

 

 

 

 

 

5.

Pump Malfunction Indicator

C

1

0

(O) May be inoperative provided:

a)          All required Fuel Pumps are operative, and

b)          Fuel Low Pressure Warning System is operative.

 

 

 

 

 

 

 

 

6.

Fuel Consumed Indicator

C

1

0

May be inoperative provided all Fuel Tank Quantity Indicating Systems are operative.

 

 

 

 

 

 

 

 

7.

Pump Test Switch

C

1

0

(O) May be inoperative provided:

a)          All Fuel Tank Pumps are operative,

b)          Quantity Indicating Systems are operative, and

c)          Pump Malfunction Indicator is operative.

 

 

 

 

 

 

 

 


28

FUEL

 

 

 

 

 

 

 

 

 

 

 

 

8.

Fuel Filter De-Icing Indicators

C

2

1

One may be inoperative.

 

 

 

 

 

 

 

 

9.

Normal Tip Tank Fuel Pumps

C

2

1

(O) One may be inoperative provided the associated Emergency Tip Tank Fuel Pump is operative if dispatch is predicated on use of Tip Tank Fuel.

 

 

 

 

 

 

 

 

10.

Emergency Tip Tank Fuel Pumps

C

2

1

(O) One may be inoperative provided:

a)          Dispatch is predicated on use of Tip Tank Fuel.

b)          Both Automatic Sequence Systems are operative, and

c)          Associated Normal Tip Tank Fuel Pump is operative.

 

 

 

 

 

 

 

 

11.

Fuselage Fuel Pump

C

1

0

May be inoperative provided dispatch is not predicated on Fuselage Fuel.

 

 

 

 

 

 

 

 


29

HYDRAULIC POWER

 

 

 

 

 

 

 

 

 

 

 

 

1.

Hydraulic Temperature Gauge

C

1

0

 

 

 

 

 

 

 

 

 

2.

Low Level Warning Light

C

1

0

May be inoperative provided the Hydraulic Fluid is verified to be adequate before departure.

 

 

 

 

 

 

 

 

3.

Low Pressure Warning Light

 

 

 

DELETED, REVISION 2.

 

 

 

 

 

 

 

 

4.

Brake Pressure Low Warning Light

C

1

0

 

 

 

 

 

 

 

 

 


30

ICE & RAIN PROTECTION

 

 

 

 

 

 

 

 

 

 

 

 

1.

Wing And Empennage Anti- and De-Icing System

C

1

0

May be inoperative provided the airplane is not operated into known or forecast icing conditions.

 

 

 

 

 

 

 

 

2.

Side Window Heat

C

1

0

 

 

 

 

 

 

 

 

 

3.

Windshield Heat

C

2

1

One may be inoperative provided both Side Windows are HEATED.

 

 

 

 

 

 

 

 

 

 

 

 

 

NOTE:  Aircraft is to be controlled from the Seat behind the Heated Windshield.

 

 

 

 

 

 

 

 

4.

Pitot Tube Heat

B

3

0

(O) All may be inoperative for VFR operations in non-icing conditions.

 

 

 

 

 

 

 

 

5.

Windshield Wipers

C

2

0

Both may be inoperative provided aircraft is not operated in precipitation within 5 nautical miles of the airport of takeoff or intended landing.

 

 

 

 

 

 

 

 

6.

Rain Repellent System

C

1

0

May be inoperative provided both Windshield Wipers are operative.

 

 

 

 

 

 

 

 

7.

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.

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31

INDICATING/ RECORDING SYSTEMS

 

 

 

 

 

 

 

 

 

 

 

 

1.

Standby Bank-And-Pitch Indicator

 

 

 

MOVED TO ATA CHAPTER 34.

|

 

 

 

 

 

 

 

2.

Clock

C

-

-

May be inoperative for VFR operations.

 

 

 

 

 

 

 

 

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.

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|

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(Continued)

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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.

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|

|

|

|

 

 

 

 

 

 

 

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.

|

|

|

 

 

 

 

 

 

 

4.

***

Flight Hour Recorder

C

1

0

(O)

 

 

 

 

 

 

 

 


32

LANDING GEAR

 

 

 

 

 

 

 

 

 

 

 

 

1.

Main Gear Door Front Locks

C

2

0

(M) Both may be inoperative provided the Locks are removed or fixed in the OPEN position.

 

 

 

 

 

 

 

 


33

LIGHTS

 

 

 

 

 

 

 

 

 

 

 

 

1.

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.

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|

|

|

|

|

 

 

 

 

 

 

 

2.

Taxi Lights

C

-

0

 

 

 

 

 

 

 

 

 

3.

Landing Lights

C

2

0

Both may be inoperative for day operations.

 

 

 

 

 

 

 

 

4.

Navigation Lights

C

3

0

All may be inoperative for day operations.

 

 

 

 

 

 

 

 

5.

Passenger Notice System (Fasten Seat Belt-No Smoking)

C

1

0

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

 

 

 

 

 

 

 

 


33

LIGHTS

 

 

 

 

 

 

 

 

 

 

 

 

6.

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.

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|

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|

 

 

 

 

 

 

 

 

7.

Cabin Lighting Systems

C

-

-

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

 

 

 

 

 

 

 

 

8.

Anti-Collision Light System

B

1

0

(O) May be inoperative provided:

a)          Airplane is operated day only, or

b)          Strobes are installed and operate normally.

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NOTE:  The Strobe Light System must              be approved and certificated              as an Anti-Collision Light 

             System if used in place of a              Rotating Beacon.

 

 

 

 

 

 

 

 


33

LIGHTS

 

 

 

 

 

 

 

 

 

 

 

 

9.

Floor Proximity Emergency Escape Path Marking System Lights

C

-

-

In