Revision:

16

 

Date: 01/15/2009

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

DEPARTMENT OF TRANSPORTATION

 

 

 

 

 

FEDERAL AVIATION ADMINISTRATION

 

 

 

 

 

WASHINGTON , D.C.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

MASTER MINIMUM EQUIPMENT LIST

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

FAIRCHILD/SWEARINGEN MODELS SA226/SA227

 

 

SERIES

 

 

 

 

 

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

 

 

 

 

 

 


 

 

 

--

Table of Contents

I

--

Log of Revisions

II, III, IV

--

Control Page

V, VI, VII

--

Highlights of Change

VIII, IX, X, XI

--

Definitions

XII

--

Preamble

XIII

--

Guidelines for (O) & (M) Procedures

XIV, XV, XVI

--

Guidelines for (O) & (M) Procedures

XVII, XVIII, XIX

--

Guidelines for (O) & (M) Procedures

XX, XXI, XXII

21

Air Conditioning

21-1, 2, 3

22

Autopilot

22-1

23

Communications

23-1 THRU 6

24

Electrical

24-1, 2, 3

25

Equipment/Furnishings

25-1 THRU 12

26

Fire Protection

26-1, 2, 3

27

Flight Controls

27-1

28

Fuel

28-1, 2

29

Hydraulic Power

29-1

30

Ice & Rain Protection

30-1, 2, 3

31

Indicating/Recording Systems

31-1, 2

32

Landing Gear

32-1, 2

33

Lights

33-1, 2, 3

34

Navigation

34-1 THRU 17

35

Oxygen

35-1

37

Vacuum

37-1

46

Information Systems

46-1, 2

52

Doors

52-1, 2, 3

61

Propellers

61-1

71

Powerplant

71-1

73

Engine Fuel & Control

73-1

74

Ignition

74-1

77

Engine Indicating

77-1, 2

80

Starting

80-1

82

Water Injection

82-1

 

 

 


 

 

 

 

2

01/15/1982

Complete Reissue

 

3

11/08/1982

77-1

 

4

02/14/1984

Complete Reissue

 

5

01/10/1986

Pages 33-1 and 33-2

 

6

05/29/1986

Pages I, III, 23-1, 24-2

 

 

 

24-3, & 37-1

 

7

08/13/1986

Pages III, 77-1 and 77-2

 

8

04/17/1987

Complete Reissue

 

9

11/17/1987

Page 21-3

 

10

02/19/1989

All Pages

 

11

06/22/1989

HIGHLIGHTS OF REV., DEFINITIONS

 

11

06/22/1989

PREAMBLE

 

11a

10/22/1990

HIGHLIGHTS OF REV., DEFINITIONS

 

11a

10/22/1990

GUIDELINES

 

11a

10/22/1990

52-1, 52-3

 

12

04/11/1991

HIGHLIGHTS OF REV., GUIDELINES

 

12

04/11/1991

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

 

12

04/11/1991

24-1, 24-2, 24-3, 25-1, 25-2

 

12

04/11/1991

26-1, 27-1, 28-1, 28-2, 29-1

 

12

04/11/1991

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

 

12

04/11/1991

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

 

12

04/11/1991

34-4, 34-5, 35-1, 37-1, 52-1

 

12

04/11/1991

52-2, 52-3, 61-1, 73-1, 74-1

 

12

04/11/1991

77-1, 77-2, 82-1

 

12a

04/18/1991

HIGHLIGHTS OF REV.

 

12a

04/18/1991

28-1, 74-1

 

12b

08/08/1991

HIGHLIGHTS OF REV., GUIDELINES

 

12b

08/08/1991

28-1, 28-2, 29-1

 

12c

08/27/1991

HIGHLIGHTS OF REV.

 

12c

08/27/1991

34-5

 

12d

10/15/1991

HIGHLIGHTS OF REV.

 

12d

10/15/1991

33-2

 

12e

12/04/1991

HIGHLIGHTS OF REV., GUIDELINES

 

12e

12/04/1991

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

 

12e

12/04/1991

25-1, 25-2, 30-2, 30-3

 

12f

03/08/1993

HIGHLIGHTS OF REV., GUIDELINES

 

12f

03/08/1993

23-1, 23-2

 

12g

05/26/1993

HIGHLIGHTS OF REV., DEFINITIONS

 

12g

05/26/1993

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

 

12g

05/26/1993

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

 

12g

05/26/1993

25-2, 26-1, 27-1, 28-1, 28-2

 

12g

05/26/1993

29-1, 30-1, 30-2, 30-3, 31-1

 

12g

05/26/1993

32-1, 33-1, 33-2, 34-1, 34-2

 

 

 

 

 


 

 

 

 

12g

05/26/1993

34-3, 34-4, 34-5, 35-1, 37-1

 

12g

05/26/1993

52-1, 52-2, 52-3, 61-1, 73-1

 

12g

05/26/1993

74-1, 77-1, 77-2, 82-1

 

13

05/05/1994

HIGHLIGHTS OF REV., DEFINITIONS

 

13

05/05/1994

GUIDELINES

 

13

05/05/1994

21-1, 21-2, 21-3, 21-4, 22-1

 

13

05/05/1994

23-1, 23-2, 23-3, 23-4, 24-1

 

13

05/05/1994

24-2, 24-3, 24-4, 25-1, 25-2

 

13

05/05/1994

25-3, 26-1, 27-1, 28-1, 28-2

 

13

05/05/1994

29-1, 30-1, 30-2, 30-3, 31-1

 

13

05/05/1994

32-1, 32-2, 33-1, 33-2, 34-1

 

13

05/05/1994

34-2, 34-3, 34-4, 34-5, 34-6

 

13

05/05/1994

34-7, 35-1, 37-1, 52-1, 52-2

 

13

05/05/1994

52-3, 61-1, 71-1, 73-1, 74-1

 

13

05/05/1994

77-1, 77-2, 80-1, 82-1

 

13a

08/18/1994

HIGHLIGHTS OF REV., DEFINITIONS

 

13a

08/18/1994

GUIDELINES

 

13a

08/18/1994

23-1, 23-2, 23-3, 23-4, 24-3

 

13a

08/18/1994

25-2

 

13b

01/31/1995

HIGHLIGHTS OF REV., DEFINITIONS

 

13b

01/31/1995

71-1

 

13c

08/30/1995

HIGHLIGHTS OF REV., DEFINITIONS

 

13c

08/30/1995

24-1, 24-2, 24-3, 24-4, 24-5

 

13d

10/30/1995

HIGHLIGHTS OF REV., DEFINITIOONS

 

13d

10/30/1995

77-2

 

14

07/18/1996

HIGHLIGHTS OF REV., DEFINITIONS

 

14

07/18/1996

GUIDELINES

 

14

07/18/1996

21-1, 21-2, 21-3, 21-4, 22-1

 

14

07/18/1996

23-1, 23-2, 23-3, 23-4, 24-1

 

14

07/18/1996

24-2, 24-3, 24-4, 24-5, 25-1

 

14

07/18/1996

25-2, 25-3, 26-1, 27-1, 28-1

 

14

07/18/1996

28-2, 29-1, 30-1, 30-2, 30-3

 

14

07/18/1996

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

 

14

07/18/1996

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

 

14

07/18/1996

34-5, 34-6, 34-7, 35-1, 37-1

 

14

07/18/1996

52-1, 52-2, 52-3, 61-1, 71-1

 

14

07/18/1996

73-1, 74-1, 77-1, 77-2, 80-1

 

14

07/18/1996

82-1

 

14a

07/02/1997

HIGHLIGHTS OF REV., DEFINITIONS

 

14a

07/02/1997

23-2, 23-3

 

14b

 

HIGHLIGHTS OF REV., DEFINITIONS

 

14b

 

26-1, 26-2

 

 

 

 

 


 

 

 

 

15

08/13/2001

HIGHLIGHTS OF REV., DEFINITIONS

 

15

08/13/2001

GUIDELINES

 

15

08/13/2001

21-1, 21-2, 21-3, 21-4, 22-1

 

15

08/13/2001

23-1, 23-2, 23-3, 23-4, 23-5

 

15

08/13/2001

24-1, 24-2, 24-3, 24-4, 24-5

 

15

08/13/2001

25-1, 25-2, 25-3, 26-1, 26-2

 

15

08/13/2001

27-1, 28-1, 28-2, 29-1, 30-1

 

15

08/13/2001

30-2, 30-3, 31-1, 32-1, 32-2

 

15

08/13/2001

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

 

15

08/13/2001

34-3, 34-4, 34-5, 34-6, 34-7

 

15

08/13/2001

34-8, 34-9, 35-1, 37-1, 52-1

 

15

08/13/2001

52-2, 52-3, 61-1, 71-1, 73-1

 

15

08/13/2001

74-1, 77-1, 77-2, 80-1, 82-1

 

15a

01/07/2002

HIGHLIGHTS OF REV., DEFINITIONS

 

15a

01/07/2002

GUIDELINES

 

15a

01/07/2002

24-2, 24-3, 24-4, 34-1, 34-2

 

15a

01/07/2002

34-3, 34-4, 34-5, 34-6, 34-7

 

16

01/15/2009

COVER PAGE, TABLE OF CONTENTS

 

16

01/15/2009

LOG OF REVISIONS, CONTROL PAGES

 

16

01/15/2009

HIGHLIGHTS OF REV., DEFINITIONS

 

16

01/15/2009

PREAMBLE, GUIDELINES

 

16

01/15/2009

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

 

16

01/15/2009

23-3, 23-4, 23-5, 23-6, 24-1

 

16

01/15/2009

24-2, 24-3, 25-1, 25-2, 25-3

 

16

01/15/2009

25-4, 25-5, 25-6, 25-7, 25-8

 

16

01/15/2009

25-9, 25-10, 25-11, 25-12

 

16

01/15/2009

26-1, 26-2, 26-3, 27-1, 30-3

 

16

01/15/2009

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

 

16

01/15/2009

34-2, 34-3, 34-4, 34-5, 34-6

 

16

01/15/2009

34-7, 34-8, 34-9, 34-10

 

16

01/15/2009

34-11, 34-12, 34-13, 34-14

 

16

01/15/2009

34-15, 35-1, 46-1, 46-2

 

16

01/15/2009

52-2, 52-3

 

 

 

 

 


 

 

 

 

Cover Page

-

16

01/15/2009

Table of Contents

I

16

01/15/2009

Log of Revisions

II

16

01/15/2009

 

III

16

01/15/2009

 

IV

16

01/15/2009

Control Page

V

16

01/15/2009

 

VI

16

01/15/2009

 

VII

16

01/15/2009

Highlights of Change

VIII

16

01/15/2009

 

IX

16

01/15/2009

 

X

16

01/15/2009

 

XI

16

01/15/2009

Definitions

XII

16

01/15/2009

Preamble

XIII

16

01/15/2009

Guidelines for (O) & (M) Procedures

XIV

16

01/15/2009

 

XV

16

01/15/2009

 

XVI

16

01/15/2009

 

XVII

16

01/15/2009

 

XVIII

16

01/15/2009

 

XIX

16

01/15/2009

 

XX

16

01/15/2009

 

XXI

16

01/15/2009

 

XXII

16

01/15/2009

21

21-1

16

01/15/2009

 

21-2

16

01/15/2009

 

21-3

15

08/13/2001

22

22-1

16

01/15/2009

23

23-1

16

01/15/2009

 

23-2

16

01/15/2009

 

23-3

16

01/15/2009

 

23-4

16

01/15/2009

 

23-5

16

01/15/2009

 

23-6

16

01/15/2009

24

24-1

16

01/15/2009

 

24-2

16

01/15/2009

 

24-3

16

01/15/2009

 

 

 

 


 

 

 

 

25

25-1

16

01/15/2009

 

25-2

16

01/15/2009

 

25-3

16

01/15/2009

 

25-4

16

01/15/2009

 

25-5

16

01/15/2009

 

25-6

16

01/15/2009

 

25-7

16

01/15/2009

 

25-8

16

01/15/2009

 

25-9

16

01/15/2009

 

25-10

16

01/15/2009

 

25-11

16

01/15/2009

 

25-12

16

01/15/2009

26

26-1

16

01/15/2009

 

26-2

16

01/15/2009

 

26-3

16

01/15/2009

27

27-1

16

01/15/2009

28

28-1

15

08/13/2001

 

28-2

15

08/13/2001

 

29-1

15

08/13/2001

30

30-1

15

08/13/2001

 

30-2

15

08/13/2001

 

30-3

16

01/15/2009

31

31-1

16

01/15/2009

 

31-2

16

01/15/2009

32

32-1

15

08/13/2001

 

32-2

15

08/13/2001

33

33-1

16

01/15/2009

 

33-2

16

01/15/2009

 

33-3

15

08/13/2001

34

34-1

16

01/15/2009

 

34-2

16

01/15/2009

 

34-3

16

01/15/2009

 

34-4

16

01/15/2009

 

34-5

16

01/15/2009

 

 

 

 

(Continued)

 

 

 

 

 

 

 


 

 

 

 

34 (Continued)

34-6

16

01/15/2009

 

34-7

16

01/15/2009

 

34-8

16

01/15/2009

 

34-9

16

01/15/2009

 

34-10

16

01/15/2009

 

34-11

16

01/15/2009

 

34-12

16

01/15/2009

 

34-13

16

01/15/2009

 

34-14

16

01/15/2009

 

34-15

16

01/15/2009

 

34-16

15

08/13/2001

 

34-17

15

08/13/2001

35

35-1

16

01/15/2009

37

37-1

15

08/13/2001

46

46-1

16

01/15/2009

 

46-2

16

01/15/2009

52

52-1

15

08/13/2001

 

52-2

16

01/15/2009

 

52-3

16

01/15/2009

61

61-1

15

08/13/2001

71

71-1

15

08/13/2001

73

73-1

15

08/13/2001

74

74-1

15

08/13/2001

77

77-1

15

08/13/2001

 

77-2

15

08/13/2001

80

80-1

15

08/13/2001

82

82-1

15

08/13/2001

 

 

 

 


 

Cover Page

 

Updated to Revision 16 and FOEB Chairman’s name added.

 

Table of Contents

 

Updated to incorporate Revision 16 changes.

Log of Revisions

 

Updated to incorporate Revision 16 changes.

Control Pages

 

Updated to incorporate Revision 16 changes.

Highlights of Changes

 

Updated to reflect changes to Revision 16.

Definitions

 

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

 

Preamble

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

 

Guidelines (O & M)

 

Updated to reflect changes to Revision 16.

ATA 21-1

“OR” removed between provisos IAW PL-31.

 

ATA 21-2

“OR” removed between provisos IAW PL-31.

 

ATA 21-4

“The” in the proviso removed IAW PL-31.

 

ATA 21-5

“The” in the proviso removed IAW PL-31.

 

ATA 21-6

“OR” removed between provisos IAW PL-31.

 

ATA 21-7

“The” in the proviso removed IAW PL-31.

 

ATA 21-8

“The” in the proviso removed IAW PL-31.

 

ATA 22

Chapter title “AUTO FLIGHT” changed to “AUTOPILOT”.

 

ATA 22-1

Autopilot relief updated IAW PL-101 and PL-84 for RVSM NOTE.

 

ATA 22-3

Autopilot Disconnect relief updated IAW PL-93.

 

 

 


 

ATA 23-1

 

HF relief removed from Communications Equipment relief and relocated to Item 23-16 IAW PL-106.  “The” removed in the proviso.

 

ATA 23-4

Passenger Address System relief updated IAW PL-9.

 

ATA 23-6

CVR relief updated IAW PL-29.

 

ATA 23-8

Boom Microphone relief updated IAW PL-58.

 

ATA 23-9

Boom Microphone relief combined with updated Boom Microphone relief in Item 23-8 IAW PL-58.

 

ATA 23-10

“The(s)” removed IAW PL-31.

 

ATA 23-16

HF Communications relief added IAW PL-106.

 

ATA 23-17

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

 

ATA 23-18

SELCAL relief added IAW PL-117.

 

ATA 24

Chapter title “ELECTRICAL POWER” changed to “ELECTRICAL” to coincide with title in opspecs.com.

 

ATA 24-1

“Batteries” relief reformatted for clarity and to comply with MKC AEG internal guidance.

 

ATA 25-2

Passenger Seat relief updated IAW PL-79.

 

ATA 25-4

ELT relief relocated to ATA 23-17.

 

ATA 25-5

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

 

ATA 25-14

First Aid Kit relief replaced by Emergency Medical Equipment relief IAW PL-73.

 

ATA 25-15

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

 

 

 


 

ATA 25-16

 

Exterior Lavatory Door Ashtray relief added IAW PL-85.

 

ATA 25-17

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

 

ATA 25-18

Cargo Restraint Systems relief added IAW PL-100.

 

ATA 25-19

Overhead Storage relief added IAW PL-104.

 

ATA 25-20

Observer Seat relief added IAW PL-56.

 

ATA 25-21

Flight Attendant Seat relief added IAW PL-97.

 

ATA 26-4

Lavatory Smoke Detection System relief updated IAW PL-24.

 

ATA 26-5

Lavatory Fire Extinguishing System relief added IAW PL-24.

 

ATA 26-6

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

 

ATA 27-2

“The(s)” removed in the proviso IAW PL-31.

 

ATA 27-4

“The(s)” removed in the proviso IAW PL-31.

 

ATA 30-17

Pitot Heat Indicating System relief (required by the certification or operating rules) added IAW PL-90.

 

ATA 30-18

Pitot Heat Indicating System relief (not required by the certification or operating rules) added IAW PL-90.

 

ATA 31-3

Flight Data Recorder System relief updated IAW PL-87.

 

ATA 33-4

“OR” removed between provisos.

 

ATA 33-11

Wing Ice Light relief updated.

 

ATA 34-3

Transponder relief updated IAW PL-76.

 

ATA 34-4-A

Navigation Databases relief relocated IAW PL-98.

 

ATA 34-10

DME relief updated IAW PL-3.

 

 

 


 

ATA 34-11

 

Standby Attitude Indicator relief updated IAW PL-111.

 

ATA 34-12

Altitude Alerter System relief updated IAW PL-39.

 

ATA 34-13

ADF relief updated (title spelled out).

 

ATA 34-14

RMI relief updated (title spelled out).

 

ATA 34-15

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

 

ATA 34-16

TCAS (I & II) updated IAW PL-32.

 

ATA 34-17

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

 

ATA 34-22

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

 

ATA 34-23

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

 

ATA 34-24

Windshear System relief added IAW PL-67.

 

ATA 34-25

ADS-B relief added IAW PL-105.

 

ATA 35-3

Protective Breathing Equipment relief added IAW PL-43.

 

ATA 46

Chapter added for New Technology items.

 

ATA 46-1

Electronic Flight Bag relief added IAW PL-121.

 

ATA 52-3

“OR” removed between provisos.

 

ATA 52-6

“OR” removed between provisos.

 

 

 


 

 

 

 

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

 

(O)       Operations procedure to develop how to operate during                               unpressurized flight.

 

21-2

(O)       Operations procedure to develop how to operate during                               unpressurized flight or how to utilize the conversion chart if                         operating pressurized.  Applies to all provisos.

 

21-4

(M)       Maintenance procedure to ensure procedures are established and       used to determine the Flow Control Valves are in the CLOSED                   position.

 

21-5

(O)       Operations procedure to operate unpressurized or, if pressurized,             how to operate with the Automatic Pressurization Controller                        inoperative.

 

21-6

(O)       Operations procedure to operate unpressurized or, if pressurized,             how to operate with the Manual Pressurization Controller                             inoperative.

 

21-9

(O)       Operations procedure to identify, isolate, and operate with one              System inoperative and to determine Cockpit Fan is operative.

 

21-10

(O)       Operations procedure to operate the aircraft in unpressurized flight.

 

(M)       Maintenance procedure to ensure the Cabin Dump Valve is secured             in the OPEN position.

 

21-12

(M)       Maintenance procedure to assure that no electrical or mechanical             fault exists that will have an adverse effect on any other system.

 

21-13

(M)       Maintenance procedure to assure that no electrical or mechanical             fault exists that will have an adverse effect on any other system.

 

22-1

(M)       Maintenance procedure to assure that no electrical or mechanical             fault exists that will have an adverse effect on any flight control              function.

 

 

 


 

22-2

 

(M)       Maintenance procedure to assure that no electrical or mechanical             fault exists that will have an adverse effect on any flight control              function.

 

23-4-A

(O)       Operations procedure to ensure PA not required by 14 CFR and                 alternate, normal and emergency procedures, and/or operating                   restrictions are established and used.

 

23-5

 

(O)       Operations procedure to specify how passengers will be briefed.

 

23-12

(O)       Operations procedure to specify how passengers will be briefed.

 

23-14

(O)       Operations procedure to operate aircraft without use of the various             functions of the Service Interphone system.

 

23-16

(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 prior coordination with ATS facilities is completed if, necessary.

 

23-18

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

 

24-1

(M)       Maintenance procedure to disconnect and SECURE the Battery                 Cable.  Applies to all four provisos.

 

24-2

(O)       Operations procedure to determine the opposite Battery and DC                 Voltmeter are operative and monitored.

 

24-3

(O)       Operations procedure to determine the inoperative position and                  how to configure the Electrical System to determine the applicable             Voltmeter readings of the failed position.

 

24-8

(M)       Maintenance procedure to disconnect and SECURE the Battery                 Cable and ensure that no unsafe condition exists.

 

24-9

(M)       Maintenance procedure to disconnect and SECURE the Battery                 Cable and ensure that no unsafe condition exists.

     

24-10

(M)       Maintenance procedure to disconnect and SECURE the Battery                 Cable and ensure that no unsafe condition exists.

 

 

 


 

25-2-A

 

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

 

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

 

25-2-B

(O)       Operations procedure to ensure Cabin Crew is aware of inoperative             Restraining Bar.

 

25-13

(M)       Maintenance procedure to ensure other Aircraft Systems are not                affected.

 

25-14-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.

 

25-14-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.

 

25-14-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.

 

25-17

(M)       Maintenance procedure to ensure Container is EMPTY and access             is SECURED.

 

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

 

25-18

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

 

25-19

(M)       Maintenance procedure to ensure Compartment is secured                        CLOSED and properly placarded.

 

(M)       Maintenance procedure to ensure Door is removed and properly                 placarded.

 

(O)       Operations procedure to ensure Compartment is not used except             for permanently affixed items and passengers and crewmembers             are appropriately briefed.

 

 

 


 

25-19-A

 

(M)       Maintenance procedure to ensure Doors are properly SECURED.

 

25-21-A

(M)       Maintenance procedure to ensure Seat is stowed or secured in the             RETRACTED position and is properly placarded.  Applies to both               provisos.

 

(O)       Operations procedure to ensure Seat is not occupied, Flight                        Attendant occupies Seat most accessible to the inoperative Seat,               and alternate procedures are established and used in accordance             with crewmembers manuals.

 

25-21-B

(M)       Maintenance procedure to ensure Seat is stowed or secured in the             RETRACTED position and is properly placarded.

 

26-3

(O)       Operations procedure to ensure the System is properly charged                 prior to each departure.

 

26-4

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

 

(O)       Operations procedure to ensure Lavatory Waste Receptacle is                   EMPTY and Lavatory is used only by crewmembers.

 

26-5

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

 

(O)       Operations procedure to ensure Lavatory Waste Receptacle is                   EMPTY and Lavatory is used only by crewmembers.

 

27-4

(M)       Maintenance procedure to ensure Flight Control Locking Pins are               secured in the UNLOCKED position.

 

(O)       Operations procedure to ensure the Controls are SECURED.

 

28-1

(O)       Operations procedure to ensure fuel on board meets regulatory                  requirements.

 

30-10

(O)       Operations procedure to ensure the Deice Boots are visually                      monitored during the inflation cycle for proper operation.

 

30-13

(O)       Operations procedure to ensure the Windshield Wipers are                        manually PARKED in a satisfactory position.

 

31-2

(O)       Operations procedure to record elapsed flight time.

 

 

 


 

32-1

 

(M)       Maintenance procedure to deactivate the Nose Wheel Steering and             ensure no unwanted hydraulic commands will occur.

 

(O)       Operations procedure to operate the aircraft with the Nose Wheel               Steering deactivated.

 

32-1-A

(M)       Maintenance procedure to deactivate the Nose Wheel Steering and             ensure no unwanted hydraulic commands will occur.

 

(O)       Operations procedure to operate the aircraft with the Nose Wheel               Steering deactivated.

 

32-2

(O)       Procedure to advise flying pilot to depress the Power Lever                         Microswitch to activate Steering.  Takeoff and landings must be                  performed without NWS System.

 

32-5

(O)       Operations procedure to prevent movement of aircraft when                       stopped or parked.

 

32-7

(O)       Operations procedure to advise the flight crew of need to manually             override the Locking Mechanism.

 

33-3

(O)       Operations procedure to appropriately brief the passengers.

34-12

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

 

34-15

(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.

 

 

 


 

34-16

 

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

 

34-16-A

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

 

34-16-A-2

(O)       Operations procedure to ensure TA visual display and audio                        functions are operative and TA ONLY Mode is selected by the crew.

 

34-16-A-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 System.

 

34-17-A-1

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

 

34-17-A-1-a

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

 

34-17-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

            14 CFR.

 

34-17-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 Windshear Detection and Avoidance                   System (Predictive) operates normally.

 

34-17-A-2

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

 

34-17-B-1

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

 

34-17-B-1-a

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

 

 

 


 

34-17-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

            14 CFR.

 

34-17-B-1-e

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

 

34-17-C-1

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

 

34-18

(O)       Operations procedure to ensure DG Mode is operative.

 

34-22-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.

 

34-23-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.

 

34-24-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.

 

34-24-A-2

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

 

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

 

34-24-B-1

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

 

 

 


 

34-24-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. 

 

52-1

(O)       Operations procedure to advise flight crew how to operate aircraft             unpressurized.

 

52-2

(O)       Operations procedure to advise flight crew how to operate aircraft             unpressurized.

 

52-3

(O)       Operations procedure to determine the “AFT CARGO DOOR                     CLOSED Warning Light System” is operative.

 

(O)       Operations procedure to advise flight crew how to operate the                     aircraft unpressurized.

 

52-5

(O)       Operations procedure to ensure the “Click Clack Latches” are in                 the LATCHED position and a procedure is established to operate                the aircraft unpressurized.

 

(M)       Maintenance procedure to remove the Latch and restore the                       “CABIN DOOR OPEN” Warning Light function.

 

 

 


 

52-6

 

(O)       Operations procedure to ensure a procedure is established to                     operate the aircraft unpressurized.

 

(M)       Maintenance procedure to ensure the “Click Clack Latches” are in             the LATCHED position.

 

(O)       Operations procedure to ensure a procedure is established to                     operate the aircraft unpressurized.

 

(M)       Maintenance procedure to remove the Latch and restore the                       “AFT CARGO DOOR” Warning Light function.

 

52-7

(M)       Maintenance procedure to isolate and cap the Pneumatic Line of                the defective Door Seal to prevent loss of Pneumatic                                   Pressure/Vacuum to other Instruments/Systems.

 

73-1

(O)       Operations procedure to ensure the crew is aware of the inaccuracy             of the Fuel Totalizer when the Fuel Flow Meter is malfunctioning.

 

77-5

(M)       Maintenance procedure to obtain temperature compensation value             from maintenance data and how to mark Gauge.

 

77-6

(O)       Operations procedure to ensure the crew is aware of the                             requirement to observe the uncompensated temperature limits.

 

(M)       Maintenance procedure to obtain temperature compensation value             from maintenance data and how to mark Gauge.

 

80-1

(O)       AFM Manual Start procedure.

 

 

 


21

AIR CONDITIONING

 

 

 

 

 

 

 

 

 

 

 

 

1.

Cabin Altitude Warning System

C

1

0

(O) May be inoperative for unpressurized flight.

 

 

 

 

 

 

 

|

 

 

C

1

0

May be inoperative for pressurized flight below 10,000 feet MSL.

 

 

 

 

 

 

 

 

2.

Cabin Altitude And Differential Pressure Indicator

C

1

0

(O) May be inoperative for unpressurized flight.

 

 

 

 

 

 

 

|

A)

ALTITUDE Indication

C

1

0

(O) May be inoperative provided:

a)          Cabin DIFFERENTIAL PRESSURE portion of the Indicator is operative, and

b)          A chart is provided to the crew to convert Cabin Differential Pressure to Cabin Altitude.

 

 

 

 

 

 

 

 

B)

DIFFERENTIAL PRESSURE Indication

C

1

0

(O) May be inoperative provided:

a)          Cabin ALTITUDE portion of the Indicator is operative, and

b)          A chart is provided to the crew to convert Cabin Altitude to Cabin Differential Pressure.

 

 

 

 

 

 

 

 

3.

Cabin Rate Of Climb Indicator

C

1

0

 

 

 

 

 

 

 

 

 


21

AIR CONDITIONING

 

 

 

 

 

 

 

 

 

 

 

 

4.

Flow Control Valves

C

2

1

(M) May be inoperative in the CLOSED position provided:

a)          Cockpit Fresh Air Fan is operable with Gear retracted,

b)          Oxygen and Masks are provided for all occupants as required by 14 CFR, and

c)          Other Air Conditioning System is operative.

 

 

 

 

 

 

 

|

 

 

 

 

 

 

 

5.

Automatic Pressurization Controller

C

1

0

(O) May be inoperative for unpressurized flight.

 

 

 

 

 

 

 

|

 

 

C

1

0

(O) May be inoperative for pressurized flight provided Manual Pressurization Controller is operative.

 

 

 

 

 

 

 

 

6.

Manual Pressurization Controller

C

1

0

(O) May be inoperative for unpressurized flight.

 

 

 

 

 

 

 

|

 

 

C

1

0

(O) May be inoperative for pressurized flight provided Automatic Pressurization Controller is operative.

 

 

 

 

 

 

 

 

7.

Automatic Temperature Control System

C

1

0

Automatic System may be inoperative provided Manual System is operative.

|

|

 

 

 

 

 

 

 

8.

Manual Temperature Control System

C

1

0

Manual System may be inoperative provided Automatic System is operative.

|

|

 

 

 

 

 

 

 


21

AIR CONDITIONING

 

 

 

 

 

 

 

 

 

 

 

 

9.

Air Conditioning System

C

2

1

(O) One may be inoperative provided:

a)          Cockpit Fresh Air Fan is operable with Landing Gear retracted,

b)          Oxygen and Masks are provided for all occupants, as required by 14 CFR, and

c)          The other Flow Control Valve and Air Conditioning System are operative.

 

 

 

 

 

 

 

 

10.

Cabin Dump Valve

C

1

0

(O) May be inoperative provided the Cabin Dump Valve is secured in OPEN position and aircraft remains VMC.

 

 

 

 

 

 

 

 

 

 

 

 

 

NOTE:  Alternate Static System will be              unusable.

 

 

 

 

 

 

 

 

11.

***

Windshield De-Fog Fan

C

1

0

 

 

 

 

 

 

 

 

 

12.

***

Supplemental Air Conditioning System

C

1

0

(M)

 

 

 

 

 

 

 

 

13.

***

Cabin Supplemental (Auxiliary) Heater

C

1

0

(M)

 

 

 

 

 

 

 

 

14.

Cabin Temperature Indicator

C

1

0

 

 

 

 

 

 

 

 

 


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.

Yaw Damper

C

1

0

(M) (Exception:  The SA226-T,

SA226-T(B), and SA227-TT)

 

 

 

 

 

 

 

 

 

3.

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 the Emergency AC Bus, Emergency DC Bus, Battery Bus, Battery Direct Bus, or DC Transfer Bus (as appropriate to aircraft configuration) and not required for emergency procedures.

 

 

|

 

|

 

 

 

 

 

 

 

2.

Cockpit Speaker

C

2

0

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

 

 

 

 

 

 

 

 

3.

Audio Amplifier

C

2

0

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

 

 

 

 

 

 

 

 

4.

Passenger Address System (PA)

 

 

 

 

 

|

 

 

 

 

 

 

 

A)

Passenger Configuration

C

 

 

1

0

(O) May be inoperative provided:

a)          PA not required by 14 CFR, 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.

|

|

 

 

 

 

 

 

 

5.

Auxiliary Public Address System

C

1

0

(O)

 

 

 

 

 

 

 

 


23

COMMUNICATIONS

 

 

 

 

 

 

 

 

 

 

 

 

6.

Cockpit Voice Recorder (CVR)

 

 

 

 

 

 

 

 

 

 

 

 

 

A)

For Air Carrier And Commercial Operators

 

 

 

 

|

|

 

 

 

 

 

 

 

1)

With Flight Data Recorder (FDR) Installed

A

1

0

May be inoperative provided:

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

b)          Repairs are made within three flight days.

|

 

 

 

 

 

 

 

 

2)

Without Flight Data Recorder (FDR) Installed

A

1

0

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

|

 

 

 

 

 

 

 

 

B)

For Operators Other Than Air Carriers And Commercial Operators

A

1

0

May be inoperative provided repairs are made in accordance with applicable 14 CFRs.

|

|

|

 

 

 

 

 

 

 

7.

Cockpit Voice Recorder (CVR) Underwater Locating Device (ULD)

 

 

 

 

 

 

 

 

 

 

 

 

A)

Flight Data Recorder (FDR) Not Required By FAR

A

1

0

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

 

 

 

 

 

 

 

 

B)

Flight Data Recorder (FDR) Required By FAR

A

1

0

May be inoperative provided Flight Data Recorder is operative and repairs are made within three flight days.

 

 

 

 

 

 

 

 


23

COMMUNICATIONS

 

 

 

 

 

 

 

 

 

 

 

 

8.

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

14 CFR may be inoperative.

|

|

|

|

 

 

 

 

 

 

 

B)

Cockpit Voice Recorder Without Flight Data Recorder Installed

 

 

 

 

|

|

|

|

 

 

 

 

 

 

 

1)

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

A

-

0

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

|

|

|

|

|

 

 

 

 

 

 

 

2) ***

Cockpit Voice Recorder Not Equipped To Record Boom Microphones

D

-

0

Any in excess of those required by

14 CFR may be inoperative.

|

|

|

|

 

 

 

 

 

 

 


23

COMMUNICATIONS

 

 

 

 

 

 

 

 

 

 

 

 

9.

Boom Mikes (Flight Data Recorder Not Required By FAR)

 

 

 

COMBINED WITH ATA 23-8, REVISION 16.

|

|

 

 

 

 

 

 

 

10.

Avionics Master Switch

C

1

0

May be inoperative provided Both Left and Right Auxiliary Avionics Master Switches are operative.

|

|

 

 

 

 

 

 

 

11.

Radio Master Switch

C

1

0

May be inoperative provided the Emergency Radio Master Switches are operative.

 

 

 

 

 

 

 

 

12.

Prerecorded Passenger Announcement System

 

 

 

 

 

 

 

 

 

 

 

 

A)

Passenger Configuration

C

1

0

(O) May be inoperative provided alternate, normal, and emergency procedures, and/or operating restrictions are established and used.

 

 

 

 

 

 

 

 

B)

Cargo Configuration

D

1

0

 

 

 

 

 

 

 

 

 

13.

Push To Talk Switch

C

2

1

May be inoperative provided an operable Hand Mike is available on the affected side.

 

 

 

 

 

 

 

 

14.

***

Service Interphone System (Flight Deck To Cabin) (Cabin To Cabin) (Flight Deck To Ground)

C

1

0

(O) May be inoperative provided procedures are not dependent upon its use.

 

 

 

 

 

 

 

 


23

COMMMUNICATIONS

 

 

 

 

 

 

 

 

 

 

 

 

15.

Static Discharge Wicks

 

 

 

 

 

 

 

 

 

 

 

 

A)

S/N 567 And Earlier, Except TT447, 465, 471, 483, 521, And 582-733

C

-

-

The Wick on the Rudder and the outboard Wick on each Wing and Elevator must be installed.  Any one of the remaining Wicks may be missing.

 

 

 

 

 

 

 

 

B)

S/N TT447 , 465, 471, 483, 521, 568-581, And 734 And Later

C

-

-

The top Wick on the Rudder, the outboard Wick on each Control Surface, and the Ventral Fin Wick must be installed. A total of two Wicks except those listed above may be missing.

 

 

 

 

 

 

 

 

16.

High Frequency  (HF)

Communication System

 

D

 

 

 

C

-

 

 

 

-

-

 

 

 

1

Any in excess of those required by

14 CFR 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.

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23

COMMUNICATIONS

 

 

 

 

 

 

 

 

 

 

 

 

17.

***

Emergency Locator Transmitter (ELT)

 

 

 

 

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|

 

 

 

 

 

 

 

A)

Survival Type ELTs

D

-

-

Any in excess of those required by

14 CFR may be inoperative or missing.

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|

 

 

 

 

 

 

 

B)

Fixed ELTs

A

-

0

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

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|

 

 

 

 

 

 

 

 

 

D

-

-

Any in excess of those required by

14 CFR may be inoperative or missing.

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18.

Selective Call Systems (SELCAL)

C

-

0

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

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D

-

0

May be inoperative provided procedures do not require its use.

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A)

Channels

C

-

0

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

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D

-

0

May be inoperative provided procedures do not require its use.

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24

ELECTRICAL

 

 

 

 

|

 

 

 

 

 

 

 

1.

Batteries

 

 

 

 

|

 

 

 

 

 

 

 

A)

(SA226T And AT)

B

2

1

(M) Left Battery may be inoperative provided:

a)          Associated Battery Cable is disconnected from the Battery and SECURED, and

b)          A GPU is used for starting,

c)          Battery Overheat Switch remains grounded.

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B)

Batteries (SA226TC Effectivity 355 Thru 419)

B

2

1

(M) Right Battery may be inoperative provided:

a)          The associated Battery Cable is disconnected from the Battery and SECURED, and

b)          A GPU is used for starting,

c)          Battery Overheat Switch remains grounded.

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C)

Batteries (SA226TC Effectivity 201 Thru 354)

B

2

1

(M) One Battery may be inoperative provided:

a)          The associated Battery Cable is disconnected from the Battery and SECURED, and

b)          A GPU is used for starting,

c)          Battery Overheat Switch remains grounded.

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D)

Batteries (SA227 Aircraft)

B

2

1

(M) Right Battery may be inoperative provided:

a)          Associated Battery Cable is disconnected from the Battery and SECURED,

b)          A GPU is used for starting, and

c)          Battery Overheat Switch remains grounded.

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24

ELECTRICAL

 

 

 

 

|

 

 

 

 

 

 

 

2.

DC Voltmeter (Combination Indicator)

C

-

1

(O) May be inoperative for day VMC provided opposite Battery and DC Voltmeter are operative.

 

 

 

 

 

 

 

 

3.

DC Voltmeter (Applicable For Aircraft Without Combination Indicator)

C

1

1

(O) Any Selector position may be inoperative provided an alternate position or means remains on the Meter for determining the function of the failed position.

 

 

 

 

 

 

 

 

4.

Inverters (All Aircraft Except SA226-T SN’s 201-248 And SA226-AT, SN-002 Unless Modified To A DC Generator/Inverter System

C

-

1

One may be inoperative for day VMC.

 

NOTE:  With third Inverter                               modification, two may be                    inoperative provided operative              Inverter powers AC Bus.

 

 

 

 

 

 

 

 

5.

Alternator (AC System) (SA226T SN’s 201-248 And SA226AT, SN-002 Only)

C

2

1

One may be inoperative for day VMC provided the aircraft is operated in accordance with the AFM and within the “No Boost Pumps Required” envelope.

 

 

 

 

 

 

 

 

6.

AC Warning Lights

C

2

1

One may be inoperative provided AC Voltmeter is operative.

 

 

 

 

 

 

 

 

7.

AC Voltmeter

C

1

0

AC Voltmeter may be inoperative provided both AC Warning Lights are operative.

 

 

 

 

 

 

 

 

8.

Battery Disconnect Warning Lights

B

2

1

(M) One may be inoperative provided:

a)          The associated Battery Switch is in the OFF position,

b)          The associated Battery Cable is disconnected from the Battery and SECURED, and

c)          A GPU is used for starting.

 

 

 

 

 

 

 

 


24

ELECTRICAL

 

 

 

 

|

 

 

 

 

 

 

 

9.

Battery Overheat Warning Lights

B

2

1

(M) One may be inoperative provided:

a)          The associated Battery Cable is disconnected from the Battery and SECURED,

b)          A GPU is used for starting, and

c)          Battery Overheat Switch Wire is grounded to keep Battery Overheat Warning Lights OFF.

 

 

 

 

 

 

 

 

10.

Battery Temperature Indicating And Warning Lights System (Temperature Indications)

B

2

1

(M) One Temperature Indication may be inoperative provided:

a)          The associated Battery Cable is disconnected from the Battery and SECURED,

b)          A GPU is used for starting, and

c)          Associated temperature indication is operative.

 

 

 

 

 

 

 

 

11.

Auxiliary Battery Warning Lights

 

 

 

DELETED, REVISION 13c.

 

 

 

 

 

 

 

 

12.

DC Generator Warning Lights

C

2

0

May be inoperative provided Ammeters are monitored throughout the flight.

 

 

 

 

 

 

 

 


25

EQUIPMENT/ FURNISHINGS

 

 

 

 

 

 

 

 

 

 

 

 

1.

Cockpit Seat

B

2

1

Right side may be inoperative for single pilot operations provided right Seat remains unoccupied.

 

 

 

 

 

 

 

 

 

 

 

 

 

NOTE:  A Seat with an inoperative                  Seat Belt or Shoulder Harness              is considered to be inoperative.

 

 

 

 

 

 

 

 

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”.

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NOTE 1:  A Seat with an inoperative

                Seat Belt is considered

                inoperative.

 

 

 

 

 

 

 

 

 

 

 

 

 

NOTE 2:  Inoperative Seats do not                     affect the required number of                 Flight Attendants.

 

 

 

 

 

 

 

 

 

 

 

 

 

NOTE 3:  Affected Seat(s) may include

                the Seat(s) behind and/or

                adjacent outboard Seats.

 

 

 

 

 

 

 

 

 

 

 

 

 

(Continued)

 

 

 

 

 

 

 

 


25

EQUIPMENT/ FURNISHINGS

 

 

 

 

 

 

 

 

 

 

 

 

2.

Passenger Seat(s) (Continued)

 

 

 

 

 

 

 

 

 

 

 

 

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.

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|

 

 

 

 

 

 

 

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.

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25

EQUIPMENT/ FURNISHINGS

 

 

 

 

 

 

 

 

 

 

 

 

4.

ELT

 

 

 

RELOCATED TO ATA 23-17, REVISION 16.

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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.

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6.

Baggage Restraint Bars (Under Passenger Seats)

 

 

 

COMBINED WITH PASSENGER SEAT(S), REVISION 15.

 

 

 

 

 

 

 

 

7.

Crew Arm Rests

C

4

0

May be inoperative provided Arm Rest(s) can be secured in the DOWN position.

 

 

 

 

 

 

 

 

8.

Closet Restraining Net

C

1

0

As required by 14 CFR.

 

 

 

 

 

 

 

 

9.

Aft Cargo Tie-Down Net

C

-

0

As required by 14 CFR.

 

 

 

 

 

 

 

 

10.

Aft Cargo Tie-Down Rings

C

-

0

As required by 14 CFR.

 

 

 

 

 

 

 

 


25

EQUIPMENT/ FURNISHINGS

 

 

 

 

 

 

 

 

 

 

 

 

11.

Aft Cargo Blanket Liner Assembly

C

1

0

 

 

 

 

 

 

 

 

 

12.

Nose Cargo Blanket Liner Assembly

C

1

0

 

 

 

 

 

 

 

 

 

13.

***

EMS Equipment

C

1

0

(M) May be inoperative provided inoperative component(s) do not affect required aircraft equipment.

 

 

 

 

 

 

 

 

14.

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.

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D

-

-

Any in excess of those required by

14 CFR may be incomplete, missing, or inoperative.

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(Continued)

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25

EQUIPMENT/ FURNISHINGS

 

 

 

 

 

 

 

 

 

 

 

 

14.

Emergency Medical Equipment (Continued)

 

 

 

 

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|

 

 

 

 

 

 

 

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.

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D

-

-

Any in excess of those required by

14 CFR may be incomplete, missing, or inoperative.

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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.

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D

-

-

Any in excess of those required by

14 CFR may be incomplete, missing, or inoperative.

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15.

“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.

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25

EQUIPMENT/ FURNISHINGS

 

 

 

 

 

 

 

 

 

 

 

 

16. ***

Exterior Lavatory Door Ashtrays

 

 

 

 

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|

 

 

 

 

 

 

 

A)

Airplanes With More Than One Exterior Lavatory Door Ashtray Installed

A

-

-

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

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B)

 Airplanes With Only One Exterior Lavatory Door Ashtray Installed

A

1

0

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

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17. ***

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.

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18. ***

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.

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C

-

-

May be inoperative or missing provided Cargo Compartment remains EMPTY.

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25

EQUIPMENT/ FURNISHINGS

 

 

 

 

 

 

 

 

 

 

 

 

19.

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.

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NOTE:  If no Partitions are installed,

             the entire Overhead Storage

             Compartment is considered

             one Bin.

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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.

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(Continued)

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25

EQUIPMENT/ FURNISHINGS

 

 

 

 

 

 

 

 

 

 

 

 

19.

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

 

 

 

 

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NOTE 1:  If no partitions are installed, 

                the entire Overhead Storage

                Compartment is considered

                one Bin or Compartment.

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