U.S. Department of Transportation

Federal Aviation Administration

Washington, D.C.

 

Master Minimum Equipment List

 

 

 

Revision: 10a

Date: 09/24/ 2010

 

 

GULFSTREAM AEROSPACE

 

G-IV, (G400), (G300)

 

 

** FOR PART 91 OPERATIONS ONLY! **

Thomas L. Witts, Chairman

Flight Operations Evaluation Board (FOEB)

 

 

Federal Aviation Administration

Aircraft Evaluation Group

3960 Paramount Boulevard

Suite 100

Lakewood, California 90712-4137

 

 

 

Telephone:

(562) 627-5283

FAX:

(562) 627-5281

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

AIRCRAFT:

G-IV, (G400), (G300)

REVISION NO. 10a

DATE: 09/24/2010

PAGE NO.

I

 

TABLE OF CONTENTS

 

SYSTEM NO.

SYSTEM

PAGE NO.

 

--

Table of Contents

I

 

--

Log of Revisions

II, III, IV

 

--

Control Page

V, VI, VII, VIII

 

--

Highlights of Change

IX, X

 

--

Definitions

XI, XII, XIII, XIV,

 

--

Definitions

XV, XVI, XVII,

 

 

Definitions

XVIII, XIX

 

--

Preamble

XX, XXI

 

21

Air Conditioning

21-1 thru 21-7

 

22

Auto Flight

22-1, 2, 3

 

23

Communications

23-1 thru 23-11

 

24

Electrical Power

24-1 thru 24-10

 

25

Equipment/Furnishings

25-1 thru 25-15

 

26

Fire Protection

26-1 thru 26-5

 

27

Flight Controls

27-1, 2

 

28

Fuel

28-1 thru 28-5

 

29

Hydraulic Power

29-1, 2

 

30

Ice and Rain Protection

30-1, 2, 3

 

31

Indicating/Recording Systems

31-1, 2, 3

 

32

Landing Gear

32-1

 

33

Lights

33-1 thru 33-7

 

34

Navigation

34-1 thru 34-24

 

35

Oxygen

35-1, 2

 

36

Pneumatic

36-1, 2, 3

 

38

Water/Waste

38-1, 2

 

46

New Technology

46-1, 2

 

49

Airborne Auxiliary Power

49-1 thru 49-4

 

52

Doors

52-1, 2

 

71

Powerplant

71-1

73

Engine Fuel & Control

73-1

74

Ignition

74-1

76

Engine Controls

76-1

77

Engine Indicating

77-1, 2

78

Engine Exhaust

78-1

79

Engine Oil

79-1

80

Starting

80-1, 2

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

G-IV, (G400), (G300)

REVISION: 9

DATE: 12/19/2006

PAGE NO:

II

Log of Revisions

Rev No.

Date

Page Numbers

Initials

Original

02/08/1988

Original Issue

 

1

04/09/1990

ALL PAGES

 

2

09/10/1990

ALL PAGES

 

3

07/01/1991

HIGHLIGHTS OF REV.

 

3

07/01/1991

 21-1,21-3,21-4,23-1,23-2

 

3

07/01/1991

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

 

3

07/01/1991

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

 

3

07/01/1991

28-2,28-3,28-4,28-5,29-1

 

3

07/01/1991

29-2,30-1,30-2,31-1,32-1

 

3

07/01/1991

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

 

3

07/01/1991

34-2,34-3,34-4,34-5,35-1

 

3

07/01/1991

49-1,74-1,77-1

 

3a

12/28/1992

HIGHLIGHTS OF REV.

 

3a

12/28/1992

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

 

3a

12/28/1992

30-1,30-2,31-1,78-1

 

4

05/31/1996

HIGHLIGHTS OF REV.,DEFINITIONS

 

4

05/31/1996

21-1,21-2,21-3,21-4,21-5

 

4

05/31/1996

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

 

4

05/31/1996

23-3,23-4,23-5,24-1,24-2

 

4

05/31/1996

24-3,24-4,24-5,24-6,24-7

 

4

05/31/1996

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

 

4

05/31/1996

26-1,26-2,26-3,26-4,27-1

 

4

05/31/1996

28-1,28-2,28-3,28-4,28-5

 

4

05/31/1996

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

 

4

05/31/1996

31-1,32-1,33-1,33-2,33-3

 

4

05/31/1996

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

 

4

05/31/1996

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

 

4

05/31/1996

35-1,36-1,36-2,36-3,49-1

 

4

05/31/1996

49-2,49-3,52-1,71-1,73-1

 

4

05/31/1996

74-1,76-1,77-1,77-2,78-1

 

4

05/31/1996

79-1,80-1

 

5

10/11/2001

 HIGHLIGHTS OF REV.,DEFINITIONS

 

5

10/11/2001

21-1,21-2,21-3,21-4,21-5

 

5

10/11/2001

21-6,21-7,22-1,22-2,22-3

 

5

10/11/2001

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

 

5

10/11/2001

23-6,23-7,24-1,24-2,24-3

 

5

10/11/2001

24-4,24-5,24-6,24-7,24-8

 

5

10/11/2001

24-9,25-1,25-2,25-3,25-4

 

5

10/11/2001

25-5,25-6,25-7,25-8,25-9

 

5

10/11/2001

25-10,26-1,26-2,26-3,26-4

 

5

10/11/2001

26-5,27-1,28-1,28-2,28-3

 

5

10/11/2001

28-4,28-5,29-1,29-2,30-1

 

5

10/11/2001

30-2,30-3,31-1,31-2,33-1

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

G-IV, (G400), (G300)

REVISION: 9

DATE: 12/19/2006

PAGE NO:

III

Log of Revisions

Rev No.

Date

Page Numbers

Initials

5

10/11/2001

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

 

5

10/11/2001

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

 

5

10/11/2001

34-8,34-9,34-10,34-11,34-12

 

5

10/11/2001

34-13,34-14,34-15,34-16,34-17

 

5

10/11/2001

35-1,35-2,36-1,36-2,36-3

 

5

10/11/2001

38-1,38-2,49-1,49-2,49-3

 

5

10/11/2001

52-1,52-2,71-1,73-1,80-1

 

6

05/09/2003

HIGHLIGHTS OF REV.,DEFINITIONS

 

6

05/09/2003

21-1,21-2,21-3,21-4,21-5

 

6

05/09/2003

21-6,21-7,22-1,22-2,22-3

 

6

05/09/2003

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

 

6

05/09/2003

23-6,23-7,23-8,23-9,23-10

 

6

05/09/2003

23-11,23-12,24-1,24-2,24-3

 

6

05/09/2003

24-4,24-5,24-6,24-7,24-8

 

6

05/09/2003

24-9,25-1,25-2,25-3,25-4

 

6

05/09/2003

25-5,25-6,25-7,25-8,25-9

 

6

05/09/2003

25-10,26-1,26-3,26-5,27-1

 

6

05/09/2003

28-1,28-2,28-3,28-4,28-5

 

6

05/09/2003

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

 

6

05/09/2003

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

 

6

05/09/2003

33-3,33-4,33-5,34-1,34-2

 

6

05/09/2003

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

 

6

05/09/2003

34-8,34-9,34-10,34-11,34-12

 

6

05/09/2003

34-13,34-14,34-15,34-16,34-17

 

6

05/09/2003

34-18,34-19,35-1,35-2,36-1

 

6

05/09/2003

36-2,36-3,38-1,38-2,49-1

 

6

05/09/2003

49-2,49-3,52-1,52-2,71-1

 

6

05/09/2003

73-1,74-1,76-1,77-1,77-2

 

6

05/09/2003

78-1,79-1,80-1

 

7

08/25/2003

HIGHLIGHTS OF REV.,DEFINITIONS

 

7

08/25/2003

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

 

7

08/25/2003

23-7,23-8,23-9,23-10,23-11

 

7

08/25/2003

23-12,24-2,24-3,24-4,24-7

 

7

08/25/2003

24-9,25-1,25-3,25-4,25-5

 

7

08/25/2003

25-6,25-7,25-8,25-9,25-11

 

7

08/25/2003

25-12,25-13,26-1,26-2,26-3

 

7

08/25/2003

26-4,27-1,28-1,28-2,28-3

 

7

08/25/2003

28-4,28-5,30-1,30-3,31-2

 

7

08/25/2003

31-3,32-1,33-1,33-2,33-3

 

7

08/25/2003

33-4,33-5,34-1,34-2,34-3

 

7

08/25/2003

34-4,34-5,34-6,34-7,34-9

 

7

08/25/2003

34-11,34-12,34-13,34-14,34-15

 

7

08/25/2003

34-16,34-17,34-18,34-19,34-20

 

7

08/25/2003

38-2,49-3,52-1,52-2,74-1

 

7

08/25/2003

77-2,80-1,80-2

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

G-IV, (G400), (G300)

REVISION: 10a

DATE: 09/24/2010

PAGE NO:

IV

Log of Revisions

Rev No.

Date

Page Numbers

Initials

8

10/27/2005

HIGHLIGHTS OF REV.,DEFINITIONS

 

8

10/27/2005

21-1,21-2,21-3,21-4,21-5,21-6,21-7,22-1,22-2

 

8

10/27/2005

22-3, 23-1,23-2,23-3,23-4,23-5, 23-6,23-7,23-8

 

8

10/27/2005

23-9,23-10, 23-11,24-1,24-2,24-3,24-4, 24-6

 

8

10/27/2005

24-7,24-8,24-9,25-1, 25-2,25-3,25-4,25-5

 

8

10/27/2005

25-6, 25-7,25-8,25-9,25-10,25-11, 25-12,25-13

 

8

10/27/2005

25-14,25-15,26-1, 26-2,26-3,26-4, 26-5,27-1

 

8

10/27/2005

28-2,28-3,28-4,28-5,30-1, 30-2,30-3,31-1, 31-2

 

8

10/27/2005

31-3, 31-4,31-5,33-1,33-2,33-5, 33-6,33-7,34-1

 

8

10/27/2005

34-2,34-3, 34-4,34-5,34-6,34-7,34-8, 34-9

 

8

10/27/2005

34-10,34-11,34-12,34-13, 34-14,34-15, 34-16

 

8

10/27/2005

34-17, 34-18, 34-19,34-20,34-21, 34-22, 36-1

 

8

10/27/2005

36-2,38-1,38-2,49-1,49-2, 49-3,52-1, 52-2

 

8

10/27/2005

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

 

9

12/19/2006

HIGHLIGHTS OF REV., DEFINITIONS

 

9

12/19/2006

21-3, 21-4, 22-1, 22-3, 23-2, 23-3, 23-6, 23-7

 

9

12/19/2006

23-8, 23-9, 24-1, 24-2, 24-8, 25-1, 25-2, 25-3

 

9

12/19/2006

25-4, 25-5, 25-6, 25-8, 25-9, 25-10, 25-11

 

9

12/19/2006

25-13, 25-14, 25-15, 26-1, 26-3, 27-2, 29-2

 

9

12/19/2006

33-1, 33-4, 33-5, 33-7, 34-1, 34-4, 34-6, 34-7

 

9

12/19/2006

34-8, 34-9, 34-10, 34-11, 34-12, 34-13, 34-14

 

9

12/19/2006

34-15, 34-16, 34-18, 34-19, 34-22, 34-23, 35-1

 

9

12/19/2006

35-2, 36-3, 49-2, 49-3, 49-4, 52-2, 73-1

 

9

12/19/2006

77-2, 80-2

 

10

 02/25/2010

HIGHLIGHTS OF REV., DEFINITIONS

 

10

 02/25/2010

21-1, 21-2, 21-3, 21-4, 21-5, 12-6, 21-7, 22-1,

 

10

 02/25/2010

22-2, 23-2, 23-3, 32-4, 23-5, 23-6, 23-7, 23-8,

 

10

 02/25/2010

23-9, 23-10, 23-11, 24-1, 24-2, 24-3, 24-4, 24-6

 

10

 02/25/2010

24-7, 24-8, 24-9. 24-10, 25-1, 25-2, 25-3, 25-4,

 

10

 02/25/2010

25-5, 25-6, 25-7, 25-8, 25-9, 25-10, 25-11,

 

10

 02/25/2010

25-12, 25-13, 25-14, 25-15, 26-1, 26-4, 27-2,

 

10

 02/25/2010

28-1, 28-2, 28-3, 28-4, 29-2, 30-1, 30-2, 30-3,

 

10

 02/25/2010

31-1, 31-2, 31-3, 32-1, 33-1, 33-2, 33-3, 33-4,

 

10

 02/25/2010

33-5, 33-6, 33-7, 33-8, 33-9, 34-2, 34-3, 34-4

 

10

 02/25/2010

34-5, 34-6, 34-7, 34-8, 34-9, 34-10, 34-11

 

10

 02/25/2010

34-12, 34-13, 34-14, 34-15, 34-16, 34-17

 

10

 02/25/2010

34-18, 34-19, 34-20, 34-21, 34-22, 34-23

 

10

 02/25/2010

34-24, 35-1, 35-2, 36-1, 36-2, 46-1, 46-2,

 

10

 02/25/2010

49-1, 49-2, 49-3, 73-1, 74-1, 77-1, 77-2, 78-1,

 

10

 02/25/2010

79-1, 80-2

 

10a

09/24/2010

HIGHLIGHTS OF REV., DEFINITIONS

 

10a

09/24/2010

23-7, 23-8, 23-11, 25-2, 25-7, 25-8, 25-11,

 

10a

09/24/2010

25-12, 25-15, 26-1, 26-4, 31-1, 33-1, 33-2,

 

10a

09/24/2010

33-6, 34-11, 34-12, 34-13, 34-14, 34-15, 34-18

 

10a

09/24/2010

34-24, 36-2, 38-1, 38-2, 80-2

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

G-IV, (G400), (G300)

REVISION: 10a

DATE: 09/24/2010

PAGE NO:

V

Control Page

System

Page No.

Rev. No.

Current Date

Cover Page

-

10

02/25/2010

Table of Contents

I

10a

09/24/2010

Log of Revisions

II

9

12/19/2006

 

III

9

12/19/2006

 

IV

10a

09/24/2010

Control Page

V

10a

09/24/2010

 

VI

10a

09/24/2010

 

VII

10a

09/24/2010

 

VIII

10a

09/24/2010

Highlights of Change

IX

10a

09/24/2010

 

X

10a

09/24/2010

Definitions

XI

16

04/02/10

 

XII

16

04/02/10

 

XII

16

04/02/10

 

XIII

16

04/02/10

 

XIV

16

04/02/10

 

XV

16

04/02/10

 

XVI

16

04/02/10

 

XVII

16

04/02/10

 

XVIII

16

04/02/10

 

XIX

16

04/02/10

Preamble

XX

2

06/14/1989

 

XXI

2

06/14/1989

21

21-1

10

02/25/2010

 

21-2

10

02/25/2010

 

21-3

10

02/25/2010

 

21-4

10

02/25/2010

 

21-5

10

02/25/2010

 

21-6

10

02/25/2010

 

21-7

10

02/25/2010

22

22-1

10

02/25/2010

 

22-2

10

02/25/2010

 

22-3

9

12/19/2006

23

23-1

8

10/27/2005

 

23-2

10

02/25/2010

 

23-3

10

02/25/2010

 

23-4

10

02/25/2010

 

23-5

10

02/25/2010

 

23-6

10

02/25/2010

 

23-7

10a

09/24/2010

 

23-8

10a

09/24/2010

 

23-9

10

02/25/2010

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

G-IV, (G400), (G300)

REVISION: 10a

DATE: 09/24/2010

PAGE NO:

VI

Control Page

System

Page No.

Rev. No.

Current Date

 

23-10

10

02/25/2010

 

23-11

10a

09/24/2010

24

24-1

10

02/25/2010

 

24-2

10

02/25/2010

 

24-3

10

02/25/2010

 

24-4

10

02/25/2010

 

24-5

8

10/27/2005

 

24-6

10

02/25/2010

 

24-7

10

02/25/2010

 

24-8

10

02/25/2010

 

24-9

10

02/25/2010

 

24-10

10

02/25/2010

25

25-1

10

02/25/2010

 

25-2

10a

09/24/2010

 

25-3

10

02/25/2010

 

25-4

10

02/25/2010

 

25-5

10

02/25/2010

 

25-6

10

02/25/2010

 

25-7

10a

09/24/2010

 

25-8

10a

09/24/2010

 

25-9

10

02/25/2010

 

25-10

10

02/25/2010

 

25-11

10a

09/24/2010

 

25-12

10a

09/24/2010

 

25-13

10

02/25/2010

 

25-14

10

02/25/2010

 

25-15

10a

09/24/2010

26

26-1

10a

09/24/2010

 

26-2

8

10/27/2005

 

26-3

9

12/19/2006

 

26-4

10a

09/24/2010

 

26-5

8

10/27/2005

27

27-1

8

10/27/2005

 

27-2

10

02/25/2010

28

28-1

10

02/25/2010

 

28-2

10

02/25/2010

 

28-3

10

02/25/2010

 

28-4

10

02/25/2010

 

28-5

8

10/27/2005

29

29-1

6

05/09/2003

 

29-2

10

02/25/2010

30

30-1

10

02/25/2010

 

30-2

10

02/25/2010

 

30-3

10

02/25/2010

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

G-IV, (G400), (G300)

REVISION: 10a

DATE: 09/24/2010

PAGE NO:

VII

Control Page

System

Page No.

Rev. No.

Current Date

31

31-1

10a

09/24/2010

 

31-2

10

02/25/2010

 

31-3

10

02/25/2010

32

32-1

10

02/25/10

33

33-1

10a

09/24/2010

 

33-2

10a

09/24/2010

 

33-3

10

02/25/2010

 

33-4

10

02/25/2010

 

33-5

10

02/25/2010

 

33-6

10a

09/24/2010

 

33-7

10

02/25/2010

34

34-1

9

12/19/2006

 

34-2

10

02/25/2010

 

34-3

10

02/25/2010

 

34-4

10

02/25/2010

 

34-5

10

02/25/2010

 

34-6

10

02/25/2010

 

34-7

10

02/25/2010

 

34-8

10

02/25/2010

 

34-9

10

02/25/2010

 

34-10

10

02/25/2010

 

34-11

10a

09/24/2010

 

34-12

10a

09/24/2010

 

34-13

10a

09/24/2010

 

34-14

10a

09/24/2010

 

34-15

10a

09/24/2010

 

34-16

10

02/25/2010

 

34-17

10

02/25/2010

 

34-18

10a

09/24/2010

 

34-19

10

02/25/2010

 

34-20

10

02/25/2010

 

34-21

10

02/25/2010

 

34-22

10

02/25/2010

 

34-23

10

02/25/2010

 

34-24

10a

09/24/2010

35

35-1

10

02/25/2010

 

35-2

10

02/25/2010

36

36-1

10

02/25/2010

 

36-2

10a

09/24/2010

 

36-3

9

12/19/2006

38

38-1

10a

09/24/2010

 

38-2

10a

09/24/2010

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

G-IV, (G400), (G300)

REVISION: 10a

DATE: 09/24/2010

PAGE NO:

VIII

Control Page

System

Page No.

Rev. No.

Current Date

46

46-1

10

02/25/2010

 

46-2

10

02/25/2010

49

49-1

10

02/25/2010

 

49-2

10

02/25/2010

 

49-3

10

02/25/2010

 

49-4

9

12/19/2006

52

52-1

8

10/27/2005

 

52-2

9

12/19/2006

71

71-1

6

05/09/2003

73

73-1

10

02/25/2010

74

74-1

10

02/25/2010

76

76-1

6

05/09/2003

77

77-1

10

02/25/2010

 

77-2

10

02/25/2010

78

78-1

10

02/25/2010

79

79-1

10

02/25/2010

80

80-1

8

10/27/2005

 

80-2

10a

09/24/2010

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

G-IV, (G400), (G300)

REVISION NO. 10a

DATE: 09/24/2010

PAGE NO.

IX

HIGHLIGHTS OF CHANGE

 

This is an INTERIM revision to the Gulfstream Aerospace Corp. (GAC) G-IV, (G400), (G300) Master Minimum Equipment List (MMEL) which supersedes all previous revisions.

 

New updates from FAA Policy Letters 1 through 126 and Global Changes 39 through 162 have been incorporated in this revision. For a complete listing of FAA Policy Letters and Global Changes visit the Flight Standards Information Management System, (FSIMS) located at http://fsims.faa.gov/.

 

Removed Revision 10 Highlights of Change pages.

DEFINITIONS have been updated per Policy Letter 25, Revision 16.

Definition 1.e. corrects revision bar requirements.

Definition 21. deletes the Passenger Convenience item.

Definition 23.c. revises the Electronic Fault Alerting System for Airbus.

Definition 31. added HMV.

 

ATA 23 Communications

Item 13.1)b)  Page 23-7    Flight Attendant Visual and Audio Alerting System, updated       

                                          according to PL-9.  Updated NOTE 1.

Item 13.1)c)  Page 23-8    Flight Attendant Visual and Audio Alerting System, updated       

                                          according to PL-9.  Updated NOTE 1 and then in NOTE 2         

                                          changed the word “visual” to “audio”.

Item 19.        Page 23-11  Headsets, deleted the “NOTE”.

 

ATA 25 Equipment/Furnishings

Item 3.1)       Page 25-2    Recline Mechanism, replaced the word “seat” with “seat back”,                         updated according to PL-79.

Item 11.        Page 25-7    Storage Bin(s)/Cabin and Galley Storage Compartment/Closets,                      updated per PL104.

Item 12.        Page 25-8    Cargo Restraint Systems, updated according to PL-100.

Item 14.        Page 25-11  Galley/Cabin Waste Receptacles Access Doors/Cover,           

                                          updated according to PL-96.

Item 15.1)     Page 25-12  Exterior Lavatory Door Ashtray, the word “One” was added to

                                          first proviso according to PL-85.

Item 27.1)     Page 25-15  Non-Essential Equipment and Furnishings (NEF) - Changed    

                                          (Expired on December 31, 2007) to (Expired on April 30,           

                                          2008).

 

ATA 26 Fire Protection

Item 3.          Page 26-1    APU Fire Detection System, updated number installed from 2

                                          to 1.

Item 12.        Page 26-4    APU Fire Extinguishing System, updated number installed

                                          from 2 to 1 and required for dispatch from – to 0.

 

ATA 31 Indicating/Recording Systems

Item 2.          Page 31-1    Flight Data Recorder (FDR) Systems, updated according to

                                          PL-87.

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

G-IV, (G400), (G300)

REVISION NO. 10a

DATE: 09/24/2010

PAGE NO.

X

HIGHLIGHTS OF CHANGE

 

ATA 33 LIGHTS

Item 3.          Page 33-1.2 Passenger Lighted Information Signs, updated according to     

                                          PL-123.

Item 26.        Page 33-6    Dim and Test Annunciator Channels, updated list of switches.

 

ATA 34 NAVIGATION

Item 18.        Page 34-11  Traffic Alert and Collision Avoidance System (TCAS II),

                                          deleted a) Not required by 14 CFR in first proviso, updated       

                                          according to PL-32.

Item 18.        Page 34-12  Traffic Alert and Collision Avoidance System (TCAS II),

                                          deleted NOTE at top of page.

Item 18.5)     Page 34-12  Airspace Selection Function, added (Above/Normal/Below) to   

                                          the title.

Item 21.        Page 34-13  Altitude Alerting System, updated according to PL-39.

Item 22.        Page 34-14  Display Units, added *** to titles and add a new deferral for

                                          DU-885.

Item 32.        Page 34-18  Windshear Warning and Flight Guidance System (Reactive),

                                          updated repair category according to PL-67.

Item 33.        Page 34-18  Windshear Warning and Flight Guidance System (Predictive),

                                          updated repair category according to PL-67.

Item 45.        Page 34-24  Added Cursor Control Devices.

 

ATA 36 PNEUMATIC

Item 2.          Page 36-2    Bleed Air Hot Warning Systems, 1) Pressurized Configuration,            

                                          added, step for  “not operated in icing cond.” to proviso.

 

ATA 38 WATER/WASTE

Item 1.          Page 38-1    Potable Water Systems, deleted (O) in first proviso and

                                          changed (O) to (M) in second proviso per PL-83.

Item 4.          Page 38-2    Vacuum Toilet Holding Tank Indicator, added “***” to item         

                                          number as this is optional.

 

ATA 80 STARTING

Item 3.          Page 80-2    Start Valve Position Indications, added an (O) to second           

                                          proviso for AFM Limitations.

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

G-IV, (G400), (G300)

REVISION: 16

DATE: 04/02/2010

PAGE NO:

XI

DEFINITIONS

 

1. System Definitions.

 

System numbers are based on the Air Transport Association (ATA) Specification and items are numbered sequentially.

 

a. "Item" (Column 1) means the equipment, system, component, or function listed in the "Item" column. Repair interval categories (A, B, C, and D) are listed on right side of column 1. Repair intervals are described in definition 22.

 

b. "Number Installed" (Column 2) is the number (quantity) of items normally installed in the aircraft. This number represents the aircraft configuration considered in developing this MMEL. Should the number be a variable (e.g., passenger cabin items) a number is not required.

 

c. "Number Required for Dispatch" (Column 3) is the minimum number (quantity) of items required for operation provided the conditions specified in Column 4 are met.

 

NOTE: Where the MMEL shows a variable number required for dispatch, the MEL must reflect the actual number required for dispatch or an alternate means of configuration control approved by the Administrator.

 

d. "Remarks or Exceptions" (Column 4) in this column includes a statement either prohibiting or permitting operation with a specific number of items inoperative, provisos (conditions and limitations) for such operation, and appropriate notes.

 

e. A vertical bar (change bar) in the margin indicates a change, addition or deletion in the adjacent text for the current revision of that page only. The change bar is dropped at the next MMEL revision.

 

2. "Airplane/Rotorcraft Flight Manual" (AFM/RFM) is the document required for type certification and approved by the responsible FAA Aircraft Certification Office. The FAA approved AFM/RFM for the specific aircraft is listed on the applicable Type Certificate Data Sheet.

 

3. "As required by 14 CFR" means that the listed item is subject to certain provisions (restrictive or permissive) expressed in the Federal Aviation Regulations operating rules. The number of items required by the 14 CFR must be operative. When the listed item is not required by 14 CFR it may be inoperative for time specified by repair category. The term “14 CFR” may be substituted for “FAR” in MMELs or operator MELs.

 

4. Each inoperative item must be placarded to inform and remind the crewmembers and maintenance personnel of the equipment condition.

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

G-IV, (G400), (G300)

REVISION: 16

DATE: 04/02/2010

PAGE NO:

XII

DEFINITIONS

NOTE: To the extent practical, placards should be located adjacent to the control or indicator for the item affected; however, unless otherwise specified, placard wording and location will be determined by the operator.

 

5."-" symbol in Column 2 and/or Column 3 indicates a variable number (quantity) of the item installed.

 

6. "Deleted" in the remarks column after a sequence item indicates that the item was previously listed but is now required to be operative if installed in the aircraft.

 

7. As used in MMELs, "ER" refers to Extended Operations (ETOPS) of an airplane with operational approval to conduct ETOPS in accordance with the applicable regulations.

 

8. "Federal Aviation Regulations" (FAR) means the applicable portions of the Federal Aviation Act and Federal Aviation Regulations.

 

9. "Flight Day" means a 24 hour period (from midnight to midnight) either Universal Coordinated Time (UCT) or local time, as established by the operator, during which at least one flight is initiated for the affected aircraft.

 

10. "Icing Conditions" means an atmospheric environment that may cause ice to form on the aircraft (structural) or in the engine(s) (induction).

 

11. Alphabetical symbol in Column 4 indicates a proviso (condition or limitation) that must be complied with for operation with the listed item inoperative.

 

12. ”Inoperative" means a system and/or component malfunction to the extent that it does not accomplish its intended purpose and/or is not consistently functioning normally within its approved operating limit(s) or tolerance(s).

 

13. ”Notes:" in Column 4 provides additional information for crewmember or maintenance consideration. Notes are used to identify applicable material which is intended to assist with compliance, but do not relieve the operator of the responsibility for compliance with all applicable requirements. Notes are not a part of the provisos.

 

14. Inoperative components of an inoperative system: Inoperative items which are components of a system which is inoperative are usually considered components directly associated with and having no other function than to support that system. (Warning/caution systems associated with the inoperative system must be operative unless relief is specifically authorized per the MMEL).

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

G-IV, (G400), (G300)

REVISION: 16

DATE: 04/02/2010

PAGE NO:

XIII

DEFINITIONS

 

15. "(M)" symbol indicates a requirement for a specific maintenance procedure which must be accomplished prior to operation with the listed item inoperative. Normally these procedures are accomplished by maintenance personnel; however, other personnel may be qualified and authorized to perform certain functions. Procedures requiring specialized knowledge or skill, or requiring the use of tools or test equipment should be accomplished by maintenance personnel. The satisfactory accomplishment of all maintenance procedures, regardless of who performs them, is the responsibility of the operator. Appropriate procedures are required to be published as part of the operator's manual or MEL.

 

16. "(O)" symbol indicates a requirement for a specific operations procedure which must be accomplished in planning for and/or operating with the listed item inoperative. Normally these procedures are accomplished by the flight crew; however, other personnel may be qualified and authorized to perform certain functions. The satisfactory accomplishment of all procedures, regardless of who performs them, is the responsibility of the operator. Appropriate procedures are required to be published as a part of the operator's manual or MEL.

 

NOTE: The (M) and (O) symbols are required in the operator's MEL unless otherwise authorized by the Administrator.

 

17. "Deactivated" and "Secured" means that the specified component must be put into an acceptable condition for safe flight. An acceptable method of securing or deactivating will be established by the operator.

 

18. "Visual Flight Rules" (VFR) is as defined in 14 CFR Part 91. This precludes a pilot from filing an Instrument Flight Rules (IFR) flight plan.

 

19. "Visual Meteorological Conditions" (VMC) means the atmospheric environment is such that would allow a flight to proceed under the visual flight rules applicable to the flight. This does not preclude operating under Instrument Flight Rules.

 

20. "Visible Moisture" means an atmospheric environment containing water in any form that can be seen in natural or artificial light; for example, clouds, fog, rain, sleet, hail, or snow.

 

21. "Passenger Convenience Items" – Deleted, see NEF #30.

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

G-IV, (G400), (G300)

REVISION: 16

DATE: 04/02/2010

PAGE NO:

XIV

DEFINITIONS

 

22. Repair Intervals: All users of an MEL approved under 14 CFR 121, 125, 129 and 135 must effect repairs of inoperative systems or components, deferred in accordance with the MEL, at or prior to the repair times established by the following letter designators:

 

Category A. Items in this category shall be repaired within the time interval specified in the remarks column of the operator's approved MEL. For time intervals specified in "flight days," the day the malfunction was recorded in the aircraft maintenance record/logbook is excluded.  For all other time intervals (flights, flight legs, cycles, hours, etc), repair tracking begins at the point when the malfunction is deferred in accordance with the operator's approved MEL.

 

Category B. Items in this category shall be repaired within three (3) consecutive calendar days (72 hours), excluding the day the malfunction was recorded in the aircraft maintenance record/logbook. For example, if it were recorded at 10 a.m. on January 26th, the three day interval would begin at midnight the 26th and end at midnight the 29th.

 

Category C. Items in this category shall be repaired within ten (10) consecutive calendar days (240 hours), excluding the day the malfunction was recorded in the aircraft maintenance record/logbook. For example, if it were recorded at 10 a.m. on January 26th, the 10 day interval would begin at midnight the 26th and end at midnight February 5th.

 

Category D. Items in this category shall be repaired within one hundred and twenty (120) consecutive calendar days (2880 hours), excluding the day the malfunction was recorded in the aircraft maintenance log and/or record. The letter designators are inserted adjacent to Column 2.

 

An operator who has the authorization to use an MEL also has the authority to approve extensions to the maximum repair interval for category B and C items provided the responsible Flight Standards District Office (FSDO) is notified within 24 hours of the MEL extension.  The operator is not authorized to extend A and D items in the MEL. Misuse of the MEL extension authority may result in the operators OpSpecs/Mspecs being amended by removing the authority for the operator to use the MEL extension authority and/or use an MEL.

 

23. Electronic fault alerting system – General

 

New generation aircraft display system fault indications to the flight crew by use of computerized display systems. Each aircraft manufacturer has incorporated individual design philosophies in determining the data that would be represented. The following are customized definitions (specific to each manufacturer) to help determine the level of messages affecting the aircraft's dispatch status .When preparing the MEL document, operators are to select the proper Definition No. 23 for their aircraft, if appropriate.

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

G-IV, (G400), (G300)

REVISION: 16

DATE: 04/02/2010

PAGE NO:

XV

DEFINITIONS

 

a. BOEING (747-400, 757, 767, 777, 787)

 

Boeing airplanes equipped with Engine Indicating and Crew Alerting Systems (EICAS), provide different priority levels of system messages (WARNING, CAUTION, ADVISORY, STATUS and MAINTENANCE).Any messages that affects airplane dispatch status will be displayed at a STATUS message level or higher. The absence of an EICAS STATUS or higher level (WARNING, CAUTION, ADVISORY) indicates that the system/component is operating within its approved operating limits or tolerances.

 

System conditions that result only in a maintenance level message, i.e. no correlation with a higher level EICAS message, do not affect dispatch and do not require action other than as addressed within an operator’s standard maintenance program.

 

b. BOEING (B-717, MD-10, MD-11)

 

These aircraft are equipped with an alerting function which is a subsystem within the Electronic Instrument System (EIS).  The alerting function provides various levels of system condition alerts (WARNING, CAUTION, ADVISORY, MAINTENANCE and STATUS).  Alerts that affect aircraft dispatch will include WARNING, CAUTION, STATUS or MAINTENANCE level.  MAINTENANCE alerts are displayed on the status page of the EIS display panel under the maintenance heading.

 

A MAINTENANCE alert on the EIS indicates the presence of a system fault which can be identified by the Central Fault Display System (CFDS) interrogation.  The systems are designed to be fault tolerant, however, for any MAINTENANCE alert, the MEL must be verified for dispatch purposes.

 

c. AIRBUS (A-300-600, A-310, A-318/319/320/321, A-330, A-340, A-380)

 

Airbus aircraft equipped with Electronic Centralized Aircraft Monitoring (ECAM) provide different levels of system condition messages {WARNING (red), CAUTION (amber)}. On A318/319/320/321, A330 and A340, the ECAM STATUS page also provides MAINTENANCE STATUS messages.

 

Any message that affects airplane dispatch is displayed at the WARNING or CAUTION level.

For A318/319/320/321, MAINTENANCE STATUS messages may also affect airplane dispatch.

 

System faults that result only in messages on the Central Maintenance System (CMS) (for A330, A340 and A380) or on the Centralized Fault Display System (CFDS) (for A318/319/320/321) do not affect airplane dispatch and do not require action other than as addressed within the operator’s standard maintenance program.

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

G-IV, (G400), (G300)

REVISION: 16

DATE: 04/02/2010

PAGE NO:

XVI

DEFINITIONS

d. FOKKER (FK-100)

Fokker aircraft are equipped with Multi Function Display System (MFDS) which provides electronic message referring to the different priority levels of system information (WARNING (red), CAUTION (amber), AWARENESS (cyan) AND STATUS (white).  Any messages that affect aircraft dispatch will be at the WARNING, CAUTION or AWARENESS level.  In these cases the MEL must be verified for dispatch capability and maintenance may be required. System conditions that only require maintenance are not presented on the flight deck.  These maintenance indications/messages may be presented on the Maintenance & Test Panel (MAP) or the Centralized Fault Display Unit (CFDU) and by dedicated Built In Test Evaluation (BITE) of systems.

e. CANADAIR (CL-65, CL-604)

Canadair aircraft equipped with Engine Indication and Crew Alerting Systems (EICAS) provide four classes of messages (WARNING, CAUTION, ADVISORY, and STATUS). Any message that affects aircraft dispatch will be at the WARNING, CAUTION, or STATUS level.

System conditions that only require maintenance are not visible to the flight crew. These maintenance indications/messages are only activated by maintenance personnel using the Maintenance Diagnostics Computer.

f.  EMBRAER (EMB-135/145, ERJ-170 Series)

The EMB-135/145 and ERJ-170/190 are equipped with an Engine Indicating and Crew Alerting System (EICAS) that provides three different message levels: WARNING, CAUTION, and ADVISORY. The ERJ-170/190 Series add STATUS messagesFailures that effect dispatchability are presented to the flight crew at one of these levels.  Other failures may be presented only to the maintenance personnel on the Multi Function Display (MFD) maintenance pages or through the download of the Central Maintenance Computer (CMC).  System conditions that result only in a maintenance level message, i.e. no correlation with a higher level EICAS message, do not affect dispatch and do not require action other than as addressed within an operator's standard maintenance program.

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

G-IV, (G400), (G300)

REVISION: 16

DATE: 04/02/2010

PAGE NO:

XVII

DEFINITIONS

 

g. GULFSTREAM (G-IV, G-V, GV-SP, and GIV-X, G150 and G200)

 

GULFSTREAM airplanes equipped with EICAS provide different priority levels of system messages: WARNING (red), CAUTION (amber), ADVISORY, STATUS and MAINTENANCE (cyan or blue).  Any WARNING or CAUTION message affects airplane dispatch status and requires that the Airplane Flight Manual or the MEL be used to determine dispatch capability.  STATUS messages which indicate a system failure

 (e.g., FMS 1 fail) require that the Airplane Flight Manual or the MEL be used to determine dispatch capability.  MAINTENANCE messages do not affect airplane dispatch status. They indicate the presence of a system fault which can be identified by Maintenance Data Acquisition Unit (MDAU on the G-V) interrogation, Central Maintenance Computer (CMC on the GV-SP/GIV-X) interrogation or by reference to the Airplane Flight Manual.

 

Gulfstream mid-cabin airplanes (G-150, G-200) equipped with EICAS provide different priority levels of system messages: WARNING (red), CAUTION (amber), ADVISORY (green), and STATUS (white).  The Airplane Flight Manual prohibits take off with any WARNING message displayed.  CAUTION, ADVISORY and STATUS messages may affect airplane dispatch status and requires the Airplane Flight Manual or the MEL be used to determine dispatch capability.  The airplane may dispatch with CAUTION, ADVISORY and STATUS messages that indicate proper system operation and are not illuminated due to a system failure (i.e. FUEL STBY PUMP ON when the pump is selected ON, GND A/B OUT with LAND selected on the ground, or APU GEN OFF with the switch OFF).  MAINTENANCE and MAINTENANCE DATA STATUS messages do not affect airplane dispatch status.  They indicate the presence of a system fault which can be retrieved from the Maintenance Diagnostics Computer.  In all cases, the Airplane Flight Manual must be referenced and procedures compiled with for the displayed message prior to applying MEL dispatch relief.

 

h. De-HAVILLAND (DASH 8 SERIES 400)
 
Series 400 aircraft are equipped with a Caution/Warning Panel that annunciates all cautions and warnings. Advisory messages are displayed by the Electronic Indication System (EIS) or individual advisory lights supplied in the cockpit. "Class 1 failures" are failures that prevent continued operation of a specific Line Replacement Unit or channel and are annunciated via advisory messages: caution, warning or advisory lights in the flight compartment. Dispatch with such posted failures is to be in accordance with the MMEL. "Class 2 failures" are failures which do not prevent continued system function. These faults will not be annunciated to the flight crew and the absence of the higher level alert (warning, caution, advisory) indicates that the system/component is operating within its approved operating limits or tolerances.  Such faults would be evident during maintenance interrogation performed during maintenance activities. Class 2 faults do not affect dispatch and will be listed in the Fault Isolation Manual (FIM). Class 2 faults will be left to the discretion of the operators when these faults are to be rectified.

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

G-IV, (G400), (G300)

REVISION: 16

DATE: 04/02/2010

PAGE:

XVIII

DEFINITIONS

 

24. "Administrative control item" means an item listed by the operator in the MEL for tracking and informational purposes. It may be added to an operator's MEL by approval of the Principal Operations Inspector provided no relief is granted, or provided conditions and limitations are contained in an approved document (i.e. Structural Repair Manual, airworthiness directive, etc.). If relief other than that granted by an approved document is sought for an administrative control item, a request must be submitted to the Administrator. If the request results in review and approval by the FOEB, the item becomes an MMEL item rather than an administrative control item.

 

25. "***" symbol in Column 1 indicates an item which is not required by regulation but which may have been installed on some models of aircraft covered by this MMEL. This item may be included on the operator's MEL after the approving office has determined that the item has been installed on one or more of the operator's aircraft. The symbol, however, shall not be carried forward into the operator's MEL. It should be noted that neither this policy nor the use of this symbol provide authority to install or remove an item from an aircraft.

 

26. "Excess Items" means those items that have been installed that are redundant to the requirements of the 14 CFRs.

 

27. "Day of Discovery" is the calendar day an equipment/instrument malfunction was recorded in the aircraft maintenance log and or record. This day is excluded from the calendar days or flight days specified in the MMEL for the repair of an inoperative item of equipment. This provision is applicable to all MMEL items, i.e., categories "A, B, C, and D."

 

28. “Considered Inoperative”, as used in the provisos means that item must be treated for dispatch, taxi and flight purposes as though it were inoperative. The item shall not be used or operated until the original deferred item is repaired. Additional actins include: documenting the item on the dispatch release (if applicable), placarding, and complying with all remarks, exceptions, and related MMEL provisions, including any (M) and (O) procedures and observing the repair category.

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

G-IV, (G400), (G300)

REVISION: 16

DATE: 04/02/2010

PAGE:

XIX

DEFINITIONS

 

29. “Is not used” in the provisos, remarks or exceptions for an MMEL item may specify that another item relieved in the MMEL “is not used.” In such cases, crewmembers should not activate, actuate, or otherwise utilize that component or system under normal operations. It is not necessary for the operators to accomplish the (M) procedures associated with the item. However, operational requirements must be complied with, and an additional placard must be affixed, to the extent practical, adjacent to the control or indicator for the item that is not used to inform crewmembers that a component or system is not used under normal operations.

 

30. Nonessential equipment and furnishings (NEF) are those items installed on the aircraft as part of the original type certification, supplemental type certificate, or other form of alteration that have no effect on the safe operation of flight and would not be required by the applicable certification rules or operational rules.  They are those items that if inoperative, damaged or missing have no effect on the aircraft’s ability to be operated safely under all operational conditions.  These nonessential items may be installed in areas including, but not limited to, the passenger compartment, flight deck area, service areas, cargo areas, crew rest areas, lavatories, and galley areas.  NEF items are not items already identified in the MEL or CDL of the applicable aircraft.  They do not include items that are functionally required to meet the certification rule or for compliance with any operational rule.  Operator’s NEF process shall not provide for deferral of items within serviceable limits identified in the manufacturer’s maintenance manual or operator’s approved maintenance program such as wear limits, fuel/hydraulic leak rates, oil consumption, etc.  Cosmetic items that are fully serviceable but worn or soiled may be deferred under an operator’s NEF process.

 

31. As used in MMELs, Heavy Maintenance Visit (HMV) is a scheduled C-check/D-check or airworthiness maintenance program inspection where the aircraft is scheduled to be out of service for 4 or more days.

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

G-IV, (G400), (G300)

REVISION: 1

DATE: 07/05/1990

PAGE NO:

XX

PREAMBLE

(07/05/1990)

 

This preamble is applicable to, and will be included in, master minimum equipment lists (MMEL) issued under the provisions of Section 91.30(a) NEW Section 91.213(a)(2).It is not applicable to MMEL's issued under the provisions of Parts 121, 125, 129, and 135 of the FAR.

 

Except as provided in Section 91.30(d) NEW Section 91.213(d), or under the provisions of an approved MMEL, all equipment installed on an aircraft in compliance with the airworthiness standards or operating rules must be operative. Experience has shown that with the various levels of redundancy designed into modern aircraft, operation of every system or component installed may not be necessary when the remaining equipment can provide an acceptable level of safety.

 

An MMEL is developed by the FAA, with participation by the aviation industry, to improve aircraft utilization and thereby provide more convenient and economic air transportation for the public. The FAA-approved MMEL includes only those items of equipment which the Administrator finds may be inoperative and yet maintain an acceptable level of safety by appropriate conditions and limitations. The MMEL and FAA-issued letter of authorization are used as an MEL by an operator and permit operation of the aircraft with inoperative equipment.

 

The MMEL includes all items of installed equipment that are permitted to be inoperative. Equipment required by the FAR, and optional equipment in excess of FAR requirements, is included with appropriate conditions and limitations. For each listed item, the installed equipment configuration considered to be normal for the aircraft is specified. Items of equipment installed on aircraft (except for passenger convenience items such as galley equipment and passenger entertainment devices), such as "TCAS," windshear detection devices, and ground proximity warning systems (GPWS) that are in excess of what is required, and are not listed on the MMEL, must be operational for dispatch unless MMEL relief is sought through the FSDO having jurisdiction for the operator. If MMEL relief is sought, the operator must notify the FSDO who will make a request of the FOEB to convene and consider adding the equipment to the MMEL. The operator may then dispatch with the equipment disabled, or rendered inoperative, in accordance with all FAR. It is incumbent on the operator to endeavor to determine if O and/or M procedures for that equipment must be developed. If so, any procedures developed must comply with all FAR. Procedures developed to use the MMEL must not conflict with either the aircraft flight manual limitations, emergency procedures, or with airworthiness directives (AD), all of which take precedence over the MMEL and those procedures.

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

G-IV, (G400), (G300)

REVISION: 1

DATE: 07/05/1990

PAGE NO:

XXI

PREAMBLE

(07/05/1990)

 

The MEL provides for release of the aircraft for flight with inoperative equipment. When an item of equipment is discovered to be inoperative, it is reported by making an entry in the Aircraft Maintenance Record/Logbook as prescribed by 14 CFR. The item is then either repaired or may be deferred per the MEL or other approved means acceptable to the Administrator prior to further operation. MEL conditions and limitations do not relieve the operator from determining that the aircraft is in condition for safe operation with items of equipment inoperative.

 

When these requirements are met, an Airworthiness Release, Aircraft Maintenance Record/Logbook entry, or other approved documentation is issued as prescribed by 14 CFR. Such documentation is required prior to operation with any item of equipment inoperative.

 

Operators are responsible for exercising the necessary operational control to ensure that an acceptable level of safety is maintained. When operating with multiple inoperative items, the interrelationships between those items and the effect on aircraft operation and crew workload will be considered.

 

Operators are to establish a controlled and sound repair program including the parts, personnel, facilities, procedures, and schedules to ensure timely repair.

 

WHEN USING THE MEL, COMPLIANCE WITH THE STATED INTENT OF THE PREAMBLE, DEFINITIONS, AND THE CONDITIONS AND LIMITATIONS SPECIFIED IN THE MEL IS REQUIRED

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

 

AIRCRAFT:

G-IV, (G400), (G300)

REVISION NO: 10

DATE: 02/25/2010

PAGE NO:

21-1

 

 

1. SYSTEM,

SEQUENCE NUMBERS & ITEM

REPAIR CATEGORY

 

 

 

2. NUMBER INSTALLED

 

 

 

3. NUMBER REQUIRED FOR DISPATCH

 

 

 

4. REMARKS AND EXCEPTIONS

 

21

AIR CONDITIONING

 

 

 

 

 

 

 

 

 

 

 

 

1.

Cabin Altitude Indicator

C

1

0

May be inoperative provided:

a)      Cabin Pressure Selector Panel is operative, and

b)      Pressurization is operated in AUTO mode.

 

 

 

 

 

 

 

 

 

 

C

1

0

May be inoperative provided:

a)      Cabin Differential Pressure Indicator is operative, and

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

 

 

 

 

 

 

 

 

 

 

D

1

0

May be inoperative provided airplane is equipped with additional pneumatic three-in-one cabin pressurization monitoring instrument, and Cabin Altitude Indicator portion is fully operative.

 

 

 

 

 

 

 

 

 

 

C

1

0

(O) May be inoperative provided airplane is operated in unpressurized configuration.

 

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

 

AIRCRAFT:

G-IV, (G400), (G300)

REVISION NO: 10

DATE: 02/25/2010

PAGE NO:

21-2

 

 

1. SYSTEM,

SEQUENCE NUMBERS & ITEM

REPAIR CATEGORY

 

 

 

2. NUMBER INSTALLED

 

 

 

3. NUMBER REQUIRED FOR DISPATCH

 

 

 

4. REMARKS AND EXCEPTIONS

 

21

AIR CONDITIONING

 

 

 

 

 

 

 

 

 

 

 

 

2.

Cabin Differential Pressure Indicator

C

1

0

May be inoperative provided:

a)      Cabin Pressure Selector Panel is operative, and

b)      Pressurization is operated in AUTO mode.

 

 

 

 

 

 

 

 

 

 

C

1

0

May be inoperative provided:

a)      Cabin Altitude Indicator is operative, and

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

 

 

 

 

 

 

 

 

 

 

D

1

0

May be inoperative provided airplane is equipped with additional pneumatic three-in-one cabin pressurization monitoring instrument, and Cabin Differential Pressure portion is fully operative.

 

 

 

 

 

 

 

 

 

 

C

1

0

(O) May be inoperative provided airplane is operated in unpressurized configuration.

 

 

 

 

 

 

 

 

3.

Cabin Rate of Climb Indicator

D

1

0

 

 

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

 

AIRCRAFT:

G-IV, (G400), (G300)

REVISION NO: 10

DATE: 02/25/2010

PAGE NO:

21-3

 

 

1. SYSTEM,

SEQUENCE NUMBERS & ITEM

REPAIR CATEGORY

 

 

 

2. NUMBER INSTALLED

 

 

 

3. NUMBER REQUIRED FOR DISPATCH

 

 

 

4. REMARKS AND EXCEPTIONS

 

21

AIR CONDITIONING

 

 

 

 

 

 

 

 

 

 

 

 

4.

Automatic Pressurization Control System

C

1

0

(O) Except for ER operations, may be inoperative provided:

a)      Manual Pressurization Control System is operative,

b)      Cabin Altitude and Differential Pressure Indicators are operative,

c)      Cabin Rate of Climb Indicator is operative,

d)      Auto Pilot is operative, and

e)      Airplane is operated in accordance with AFM Limitations.

 

 

 

 

 

 

 

 

 

 

C

1

0

(O) Except for ER operations, may be inoperative provided airplane is operated in unpressurized configuration.

 

 

 

 

 

 

 

 

1)

Air Data System Input

C

2

1

(O) May be inoperative provided:

a)      Manual Pressurization Control System is operative,

b)      Cabin Altitude and Differential Pressure Indicators are operative,

c)      Cabin Rate of Climb Indicator is operative,

d)      Autopilot is operative, and

e)      Airplane is operated in accordance with AFM Limitations.

 

 

 

 

 

 

 

 

5

Cabin Altitude Pressure Warning System

C

1

0

May be inoperative provided:

a)      Cabin Altitude and Differential Pressure Indicators are operative,

b)      Cabin Oxygen ON Warning System is operative, and

c)      Airplane is operated in accordance with AFM Limitations.

 

 

 

 

 

 

 

 

 

 

C

1

0

May be inoperative provided airplane is operated in unpressurized configuration.

 

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

 

AIRCRAFT:

G-IV, (G400), (G300)

REVISION NO: 10

DATE: 02/25/2010

PAGE NO:

21-4

 

 

1. SYSTEM,

SEQUENCE NUMBERS & ITEM

REPAIR CATEGORY

 

 

 

2. NUMBER INSTALLED

 

 

 

3. NUMBER REQUIRED FOR DISPATCH

 

 

 

4. REMARKS AND EXCEPTIONS

 

21

AIR CONDITIONING

 

 

 

 

 

 

 

 

 

 

 

 

6.

Pressurization Outflow Valve Position Indicator

C

1

0

May be inoperative provided all other components of the pressurization system are operative.

 

 

 

 

 

 

 

 

7.

Cockpit Temperature Control Systems & Cabin Temperature Control Systems

C

4

0

(O) May be inoperative provided:

a)      Ram Air system is operative, and

b)      Airplane is operated in unpressurized configuration.

 

 

 

 

 

 

 

 

 

1)

Automatic System

C

2

0

May be inoperative provided;

a)      Associated manual control system is operative, and

b)      Associated temperature indicator is operative.

 

 

 

 

 

 

 

 

2)

Manual System

C

2

0

May be inoperative provided:

a)      Associated automatic control system is operative, and

b)      Associated temperature indicator is operative.

 

 

 

 

 

 

 

 

8.

Cockpit/Cabin Temperature Indicator

D

1

0

May be inoperative provided associated Automatic Temperature Control System is operative.

 

 

 

 

 

 

 

 

 

 

D

1

0

May be inoperative provided associated Manual Temperature Control System is operative.

 

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

 

AIRCRAFT:

G-IV, (G400), (G300)

REVISION NO: 10

DATE: 02/25/2010

PAGE NO:

21-5

 

 

1. SYSTEM,

SEQUENCE NUMBERS & ITEM

REPAIR CATEGORY

 

 

 

2. NUMBER INSTALLED

 

 

 

3. NUMBER REQUIRED FOR DISPATCH

 

 

 

4. REMARKS AND EXCEPTIONS

 

21

AIR CONDITIONING

 

 

 

 

 

 

 

 

 

 

 

 

9.

Environmental Control System (ECS) Packs

 

 

 

 

 

 

 

 

 

 

 

 

1)

Pressurized Configuration

C

2

1

Except for ER operations, may be inoperative provided:

a)      Inoperative ECS Pack is selected OFF,

b)      Bleed Air Isolation Valve is CLOSED and OPERATIVE, and

c)      Airplane is operated in accordance with AFM Limitations.

 

 

 

 

 

 

 

 

2)

Unpressurized Configuration

C

2

0

Except for ER operations, both may be inoperative provided outflow valve is operative.

 

 

 

 

 

 

 

 

10. ***

Three-in-one Cabin Pressurization Monitoring Instrument

C

1

0

May be inoperative provided primary Cabin Altitude and primary Cabin Differential Pressure Indicators are operative.

 

 

 

 

 

 

 

 

11.

Air Conditioning System Flow Control and Shutoff Valves

C

2

1

(M) Except for ER operations, may be inoperative provided:

a)      Affected Valve is CLOSED and deactivated electrically when associated Air Conditioning Pack is selected OFF, and

b)      Airplane is operated in accordance with AFM Limitations.

 

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

 

AIRCRAFT:

G-IV, (G400), (G300)

REVISION NO: 10

DATE: 02/25/2010

PAGE NO:

21-6

 

 

1. SYSTEM,

SEQUENCE NUMBERS & ITEM

REPAIR CATEGORY

 

 

 

2. NUMBER INSTALLED

 

 

 

3. NUMBER REQUIRED FOR DISPATCH

 

 

 

4. REMARKS AND EXCEPTIONS

 

21

AIR CONDITIONING

 

 

 

 

 

 

 

 

 

 

 

 

12.

Outflow Valve System

C

1

0

(M) (O) May be inoperative provided:

a)      Outflow valve is positioned to full OPEN position and electrically isolated,

b)      Airplane is operated in unpressurized configuration, and

c)      Extended overwater operations are not conducted.

 

 

 

 

 

 

 

 

13.

Cabin Pressurization Safety Valve

B

1

0

(O) May be inoperative provided:

a)      Cabin differential pressure and cabin altitude displays are operative,

b)      Selected cabin altitude is 1,000 feet higher than normal cabin altitude for the cruise flight level, and

c)      Automatic and Manual Pressurization Control Systems are operative.

 

 

 

 

 

 

 

 

 

 

C

1

0

(O) May be inoperative provided airplane is operated in unpressurized configuration.

 

 

 

 

 

 

 

 

14. ***

Cabin Remote Temperature Selector System

D

1

0

 

 

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

 

AIRCRAFT:

G-IV, (G400), (G300)

REVISION NO: 10

DATE: 02/25/2010

PAGE NO:

21-7

 

 

1. SYSTEM,

SEQUENCE NUMBERS & ITEM

REPAIR CATEGORY

 

 

 

2. NUMBER INSTALLED

 

 

 

3. NUMBER REQUIRED FOR DISPATCH

 

 

 

4. REMARKS AND EXCEPTIONS

 

21

AIR CONDITIONING

 

 

 

 

 

 

 

 

 

 

 

 

15. ***

Duct Temperature Selector System

D

1

0

 

 

 

 

 

 

 

 

 

16. ***

Right Hand Radio Rack Cooling Fan

B

1

0

 

 

 

 

 

 

 

 

 

17. ***

ECU Modulator Valve Indicator System

D

1

0

 

 

 

 

 

 

 

 

 

18.

***

Left Hand Radio Rack Cooling Fan

B

1

0

 

 

 

 

 

 

 

 

 

19.

Nose Radome Cooling System (includes fan, valve and communicator)

C

1

0

May be inoperative provided the outside air temperature is less than 90 deg. F (32 deg. C) during all ground operations.

 

 

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

 

AIRCRAFT:

G-IV, (G400), (G300)

REVISION NO: 10

DATE: 02/25/2010

PAGE NO:

22-1

 

 

1. SYSTEM,

SEQUENCE NUMBERS & ITEM

REPAIR CATEGORY

 

 

 

2. NUMBER INSTALLED

 

 

 

3. NUMBER REQUIRED FOR DISPATCH

 

 

 

4. REMARKS AND EXCEPTIONS

 

22

AUTO FLIGHT

 

 

 

 

 

 

 

 

 

 

 

 

1.

Flight Guidance Computers (FGC) (Autopilots/Flight Directors)

C

2

1

Except for ER operations or where en route operations or approach minimums require its use, may be inoperative provided flight time with one engine inoperative does not exceed one hour cruise from a suitable airport.

 

 

 

 

 

 

 

 

 

 

 

 

 

NOTE: Each FGC provides mach trim compensation, electric trim, yaw damper, autopilot, and flight director functions independent of the other FGC. Failure of the second FGC after dispatch would result in the complete loss of these functions, and AFM restrictions would apply.

 

 

 

 

 

 

 

 

 

 

B

2

0

Except for ER operations, may be inoperative provided:

a)      Automatic Cabin Pressurization System is operative,

b)      Flight time with one engine inoperative does not exceed one hour cruise from a suitable airport,

c)      Landing weather minimums are not dependent upon its use,

d)      Airplane is operated at or below FL 390, and

e)      Airplane is operated in accordance with AFM Limitations for Mach Trim and Yaw Damper.

 

 

 

 

 

 

 

 

 

 

 

 

 

NOTE: One FGC is required for MNPS, RVSM, RNP and PRNAV operations.

 

 

 

 

 

 

 

 

2.  ***

Auto-throttle Systems

D

2

0

 

 

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

 

AIRCRAFT:

G-IV, (G400), (G300)

REVISION NO: 10

DATE: 02/25/2010

PAGE NO:

22-2

 

 

1. SYSTEM,

SEQUENCE NUMBERS & ITEM

REPAIR CATEGORY

 

 

 

2. NUMBER INSTALLED

 

 

 

3. NUMBER REQUIRED FOR DISPATCH

 

 

 

4. REMARKS AND EXCEPTIONS

 

22

AUTO FLIGHT

 

 

 

 

 

 

 

 

 

 

 

 

3.  ***

Performance Computers (PZ)

C

2

0

 

 

 

 

 

 

 

 

 

4.

Yaw Damper System

C

1

0

(M) Except for ER operations, may be inoperative provided:

a)      Airplane is operated in accordance with AFM Limitations, and

b)      Procedures are established to deactivate Yaw Damper System.

 

 

 

 

 

 

 

 

5.

Control Wheel Autopilot Disconnect Buttons

C

2

1

May be inoperative provided:

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

b)      Approach minimums do not require the use of the autopilot, and

c)      Airplane is piloted from the side with operative button.

 

 

 

 

 

 

 

 

6.

Takeoff/Go-Around (TOGA) Buttons

C

2

0

May be inoperative provided alternate procedures are established and used.

 

 

 

 

 

 

 

 

 

 

 

 

 

NOTE: Autothrottles and Flight Director are unavailable for takeoff and go-around.

 

 

 

 

 

 

 

 

7.

Autothrottle Disconnect Buttons (on Thrust Lever Knobs)

C

2

0

May be inoperative provided autothrottle is not utilized.

 

 

 

 

 

 

 

 

8.

Autothrottle Engage/Disengage Switches (on Thrust Lever Stem)

C

2

0

May be inoperative provided Autothrottle is considered inoperative.

 

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

 

AIRCRAFT:

G-IV, (G400), (G300)

REVISION NO: 9

DATE: 12/19/2006

PAGE NO:

22-3

 

 

1. SYSTEM,

SEQUENCE NUMBERS & ITEM

REPAIR CATEGORY

 

 

 

2. NUMBER INSTALLED

 

 

 

3. NUMBER REQUIRED FOR DISPATCH

 

 

 

4. REMARKS AND EXCEPTIONS

 

22

AUTO FLIGHT

 

 

 

 

 

 

 

 

 

 

 

 

9.

Touch Control Steering Switches (TCS)

D

2

0

NOTE: If Honeywell HUD is installed and the left TCS is inoperative, the HUD TCS “clear” function will be inoperative.

 

 

 

 

 

 

 

 

10. ***

Remote Heading and Course Select Control System

C

-

0

May be inoperative provided manual Heading and Course Selectors are operative.

 



 

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

 

AIRCRAFT:

G-IV, (G400), (G300)

REVISION NO: 8

DATE: 10/27/2005

PAGE NO:

23-1

 

 

1. SYSTEM,

SEQUENCE NUMBERS & ITEM

REPAIR CATEGORY

 

 

 

2. NUMBER INSTALLED

 

 

 

3. NUMBER REQUIRED FOR DISPATCH

 

 

 

4. REMARKS AND EXCEPTIONS

 

23

COMMUNICATIONS

 

 

 

 

 

 

 

 

 

 

 

 

1.

Communications System (VHF and UHF)

C

-

-

Any in excess of those required by 14 CFR may be inoperative provided it is not powered by the Emergency AC Bus, Emergency DC Bus, Battery Bus, Battery Direct Bus, or the DC Transfer Bus and not required for emergency procedures.

 

 

 

 

 

 

 

 

1)

VHF Comm Control Panels

 

 

 

 

 

 

 

 

 

 

 

 

a)  ***

Frequency Transfer Light

C

-

0

 

 

 

 

 

 

 

 

 

b)  ***

Frequency Transfer Switch

C

-

0

 

 

 

 

 

 

 

 

 

c)  ***

Frequency Selector Knob

C

-

2

 

 

 

 

 

 

 

 

 

d)  ***

Frequency Indication

C

-

2

 

 

 

 

 

 

 

 

 

2.

Cockpit Voice Recorder (CVR) (With Flight Data Recorder (FDR) Installed)

A

1

0

May be inoperative provided:

a)      Flight Data Recorder (FDR) is operative, and

b)      Repairs are made within three (3) flight days.

 

 

 

 

 

 

 

 

 

Cockpit Voice Recorder (CVR) (Without Flight Data Recorder (FDR) Installed)

A

1

0

May be inoperative provided repairs are made within three (3) flight days.

 

 

 

 

 

 

 

 

 

 

 

 

 

(continued)

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

 

AIRCRAFT:

G-IV, (G400), (G300)

REVISION NO: 10

DATE: 02/25/2010

PAGE NO:

23-2

 

 

1. SYSTEM,

SEQUENCE NUMBERS & ITEM

REPAIR CATEGORY

 

 

 

2. NUMBER INSTALLED

 

 

 

3. NUMBER REQUIRED FOR DISPATCH

 

 

 

4. REMARKS AND EXCEPTIONS

 

23

COMMUNICATIONS

 

 

 

 

 

 

 

 

 

 

 

 

2.

Cockpit Voice Recorder (CVR) (installed for an Operator Other Than a Holder of an Air Carrier or Commercial Operator Certificate) (continued)

A

-

0

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

 

 

 

 

 

 

 

 

3.  ***

Selective Call System (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.

 

 

 

 

 

 

 

 

1)

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.

 

 

 

 

 

 

 

 

4.  ***

Emergency Locator Transmitters (ELT)

 

 

 

 

 

 

 

 

 

 

 

 

1)

***

Survival Type ELTs

D

-

-

Any in excess of those required by 14 CFR may be inoperative or missing.

 

 

 

 

 

 

 

 

2)

***

Fixed ELTs

A

-

0

(M) May be inoperative provided:

a)      System is deactivated, and

b)      Repairs are made within 90 days.

 

 

 

 

 

 

 

 

 

 

A

-

0

May be missing provided repairs are made within 90 days.

 

 

 

 

 

 

 

 

 

 

D

-

-

(M) Any in excess of those required by 14 CFR may be inoperative provided system is deactivated.

 

 

 

 

 

 

 

 

 

 

D

-

-

Any in excess of those required by 14 CFR may be missing.

 

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

 

AIRCRAFT:

G-IV, (G400), (G300)

REVISION NO: 10

DATE: 02/25/2010

PAGE NO:

23-3

 

 

1. SYSTEM,

SEQUENCE NUMBERS & ITEM

REPAIR CATEGORY

 

 

 

2. NUMBER INSTALLED

 

 

 

3. NUMBER REQUIRED FOR DISPATCH

 

 

 

4. REMARKS AND EXCEPTIONS

 

23

COMMUNICATIONS

 

 

 

 

 

 

 

 

 

 

 

 

5.  ***

Flitephone Systems

D

-

0

 

 

 

 

 

 

 

 

 

6.

Cockpit Speakers

C

2

0

May be inoperative provided:

a)      Affected speaker is not required for aural warnings, and

b)      An operative headset is provided for each person on cockpit duty.

 

 

 

 

 

 

 

 

7.  ***

Passenger Address System (PA)

 

 

 

 

 

 

 

 

 

 

 

 

 

Passenger Configuration

B

1

0

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

 

 

 

 

 

 

 

 

 

 

 

 

 

NOTE: Any station function(s) that are operative may be used.

 

 

 

 

 

 

 

 

 

 

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 are operative may be used.

 

 

 

 

 

 

 

 

***

Lavatory Speakers

C

-

-

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

 

 

 

 

 

 

 

 

 

Cargo Configuration

D

1

0

May be inoperative provided procedures do not require its use.

 

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

 

AIRCRAFT:

G-IV, (G400), (G300)

REVISION NO: 10

DATE: 02/25/2010

PAGE NO:

23-4

 

 

1. SYSTEM,

SEQUENCE NUMBERS & ITEM

REPAIR CATEGORY

 

 

 

2. NUMBER INSTALLED

 

 

 

3. NUMBER REQUIRED FOR DISPATCH

 

 

 

4. REMARKS AND EXCEPTIONS

 

23

COMMUNICATIONS

 

 

 

 

 

 

 

 

 

 

 

 

8.  ***

Satellite Communications (SATCOM) Systems

D

-

0

May be inoperative provided procedures do not require their use.

 

 

 

 

 

 

 

 

9.

***

Prerecorded Passenger Announcement Systems

D

-

0

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

 

 

 

 

 

 

 

 

10.

***

Hand Held Microphones

D

-

0

May be inoperative provided:

a)      Each cockpit crewmember uses a boom microphone, and

b)      Each (Control Wheel) Press-to-Talk Switch is operative.

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

 

AIRCRAFT:

G-IV, (G400), (G300)

REVISION NO: 10

DATE: 02/25/2010

PAGE NO:

23-5

 

 

1. SYSTEM,

SEQUENCE NUMBERS & ITEM

REPAIR CATEGORY

 

 

 

2. NUMBER INSTALLED

 

 

 

3. NUMBER REQUIRED FOR DISPATCH

 

 

 

4. REMARKS AND EXCEPTIONS

 

23

COMMUNICATIONS

 

 

 

 

 

 

 

 

 

 

 

 

11.

Boom Microphones

 

 

 

 

 

 

 

 

 

 

 

 

 

(Cockpit Voice Recorder with Flight Data Recorder installed)

 

 

 

 

 

 

 

 

 

 

 

 

1)

Cockpit Voice Recorder Equipped To Record Boom Microphone per 14 CFR 121.359(g), 135.151(d) or 125.227(e)

A

-

0

May be inoperative provided:

a)      Flight Data Recorder is operative, and

b)      Repairs are made within three (3) 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.

 

 

 

 

 

 

 

 

 

(Cockpit Voice Recorder without Flight Data Recorder Installed)

 

 

 

 

 

 

 

 

 

 

 

 

1)

Cockpit Voice Recorder Equipped To Record Boom Microphone per 14 CFR 121.359(g), 135.151(d), or 125.227(e)

A

-

0

May be inoperative provided repairs are made within three (3) flight days.

 

 

 

 

 

 

 

 

2) ***

Cockpit Voice Recorder Not Equipped to Record Boom Microphone

D

-

0

Any excess of those required by 14 CFR may be inoperative.

 

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

 

AIRCRAFT:

G-IV, (G400), (G300)

REVISION NO: 10

DATE: 02/25/2010

PAGE NO:

23-6

 

 

1. SYSTEM,

SEQUENCE NUMBERS & ITEM

REPAIR CATEGORY

 

 

 

2. NUMBER INSTALLED

 

 

 

3. NUMBER REQUIRED FOR DISPATCH

 

 

 

4. REMARKS AND EXCEPTIONS

 

23

COMMUNICATIONS

 

 

 

 

 

 

 

 

 

 

 

 

12. ***

Crewmember Interphone System(s)

 

 

 

 

 

 

 

 

 

 

 

 

1)

Passenger Configuration

 

 

 

 

 

 

 

 

 

 

 

 

a)

Flight Deck to Cabin, Cabin to Flight Deck Functions

B

-

0

(O) May be inoperative provided alternate communications procedures between the affected Flight Attendants station(s) are established and used.

 

 

 

 

 

 

 

 

 

 

 

 

 

NOTE: Any station function(s) that is operative may be used.

 

 

 

 

 

 

 

 

b) ***

Cabin to Cabin Functions

B

-

0

(O) May be inoperative provided alternate communication procedures between the affected fight attendant station(s) are established and used.

 

 

 

 

 

 

 

 

 

 

 

 

 

NOTE: Any station function(s) that is operative may be used.

 

 

 

 

 

 

 

 

c)  ***

Flight Deck to Ground Functions

C

-

0

May be inoperative provided alternate procedures are established and used.

 

 

 

 

 

 

 

 

 

 

D

-

0

May be inoperative provided procedures do not require its use.

 

 

 

 

 

 

 

 

 

 

D