U.S. Department of Transportation

Federal Aviation Administration

Washington, D.C.

 

Master Minimum Equipment List

 

 

Revision: 5

Date:  3/22/2010

 

 

“FOR PART 91 OPERATIONS ONLY”

 

GULFSTREAM

IA-GALAXY/G-200

Stephen L. Ford, Chairman

Flight Operations Evaluation Board (FOEB)

 

 

Federal Aviation Administration

Aircraft Evaluation Group, LGB-AEG

3960 Paramount Blvd, Suite 100

Lakewood, CA  90712-4137

 

 

 

Telephone:

(562)-627-5317

FAX:

(562) 627-5281

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

 

AIRCRAFT:

IA-GALAXY/G-200

REVISION NO. 5

DATE: 3/22/2010

PAGE NO.

I

 

 

TABLE OF CONTENTS

 

 

SYSTEM NO.

SYSTEM

PAGE NO.

 

 

--

Cover Page

-

 

 

--

Table of Contents

I

 

 

 

Log of Revisions

II, III

 

 

--

Control Page

IV, V, VI

 

 

--

Highlights of Change

VII,

 

 

--

Definitions

VIII, IX, X, XI, XII

 

 

--

Definitions

XIII, XIV, XV

 

 

--

Preamble

XVI, XVII

 

 

21

Air Conditioning

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

 

 

21

Air Conditioning

21-7, 8. 9. 10

 

 

22

Auto Flight

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

 

 

23

Communications

23-1, 2, 3, 4, 5, 6

 

 

23

Communications

23-7, 8, 9, 10, 11

 

 

23

Communications

23-12, 13

 

 

24

Electrical Power

24-1, 2

 

 

25

Equipment/Furnishings

25-1, 2, 3, 4, 5, 6

 

 

25

Equipment/Furnishings

25-7, 8, 9, 10, 11

 

 

25

Equipment/Furnishings

25-12, 13, 14

 

 

26

Fire Protection

26-1, 2, 3

 

 

27

Flight Controls

27-1, 2, 3, 4

 

 

28

Fuel

28-1, 2, 3

 

 

29

Hydraulic Power

29-1, 2

 

 

30

Ice and Rain Protection

30-1, 2, 3, 4

 

 

31

Indicating/Recording Systems

31-1, 2, 3

 

 

32

Landing Gear

32-1, 2

 

 

33

Lights

33-1, 2, 3, 4, 5

 

 

34

Navigation

34-1, 2, 3, 4, 5

 

 

34

Navigation

34-6, 7. 8, 9, 10

 

 

34

Navigation

34-11, 12, 13, 14

 

 

34

Navigation

34-15

 

 

35

Oxygen

35-1, 2

 

 

38

Water/Waste

38-1, 2

 

 

46

Electronic Flight Bag (EFB) Systems

46-1, 2

 

 

49

Airborne Auxiliary Power

49-1, 2

 

 

52

Doors

52-1, 2, 3

 

 

71

Powerplant

71-1

 

 

73

Engine Fuel & Control

73-1, 2

 

 

74

Ignition

74-1

 

 

76

Engine Controls

76-1

 

 

77

Engine Indicating

77-1

 

 

78

Engine Exhaust

78-1

 

 

79

Engine Oil

79-1

 

 

80

Starting

80-1

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

 

AIRCRAFT:

IA-GALAXY/G-200

REVISION NO. 5

DATE: 3/22/2010

PAGE NO.

II

 

 

Log of Revisions

 

 

Rev. No.

Date

Page Numbers

Initials

 

 

1

11/22/2002

HIGHLIGHTS OF REV., DEFINITIONS

 

 

 

1

11/22/2002

PREAMBLE, GUIDELINES

 

 

 

1

11/22/2002

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

 

 

 

1

11/22/2002

23-3, 23-4, 23-5, 23-6, 25-1, 25-2, 26-1

 

 

 

1

11/22/2002

27-1, 27-2, 31-1, 32-1, 33-1, 33-2, 33-3

 

 

 

1

11/22/2002

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

 

 

 

1

11/22/2002

34-8, 34-9, 34-10,34-11,34-12,35-1

 

 

 

2

11/14/2003

HIGHLIGHTS OF REV., DEFINITIONS

 

 

 

2

11/14/2003

GUIDELINES

 

 

 

2

11/14/2003

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

 

 

 

2

11/14/2003

23-1, 23-2, 23-3, 23-4, 23-5, 23-6, 24-1

 

 

 

2

11/14/2003

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

 

 

 

2

11/14/2003

25-6, 26-1, 26-2, 27-1, 27-2, 27-3, 28-1

 

 

 

2

11/14/2003

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

 

 

 

2

11/14/2003

30-3, 31-1, 31-2, 32-1, 33-1, 33-2, 33-3

 

 

 

2

11/14/2003

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

 

 

 

2

11/14/2003

34-7, 34-8, 34-9, 34-10, 34-11, 34-12

 

 

 

2

11/14/2003

35-1, 35-2, 38-1, 49-1, 52-1, 52-2, 71-1

 

 

 

2

11/14/2003

73-1, 74-1, 76-1, 77-1, 78-1, 79-1, 80-1

 

 

 

3

01/17/2006

HIGHLIGHTS OF REV., DEFINITIONS

 

 

 

3

01/17/2006

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

 

 

 

3

01/17/2006

22-2, 23-1, 23-2, 23-3, 23-4, 23-5, 24-1

 

 

 

3

01/17/2006

24-2, 25-1, 25-2, 25-3, 25-4, 25-5, 25-6

 

 

 

3

01/17/2006

25-7, 26-1, 26-2, 27-1, 27-2, 27-3, 27-4

 

 

 

3

01/17/2006

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

 

 

 

3

01/17/2006

30-2, 30-3, 31-1, 31-2, 32-1, 33-1, 33-2

 

 

 

3

01/17/2006

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

 

 

 

3

01/17/2006

34-8, 34-9, 34-10, 34-11, 34-12, 35-1

 

 

 

3

01/17/2006

35-2, 38-1, 49-1, 52-1, 52-2, 71-1, 73-1

 

 

 

3

01/17/2006

74-1, 77-1, 78-1, 79-1, 80-1

 

 

 

4

8/20/2007

HIGHLIGHTS OF REV., DEFINITIONS

 

 

 

4

8/20/2007

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

 

 

 

4

8/20/2007

21-8, 21-9, 21-10, 22-1, 22-2, 22-3, 22-4

 

 

 

4

8/20/2007

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

 

 

 

4

8/20/2007

23-6, 23-7, 23-8, 23-9, 23-10, 24-2, 25-2

 

 

 

4

8/20/2007

25-3, 25-4, 25-5, 25-6, 25-7, 25-8, 25-9

 

 

 

4

8/20/2007

25-10, 25-11, 25-12, 26-2, 26-3, 28-3

 

 

 

4

8/20/2007

29-2, 29-3, 30-4, 31-2, 31-3, 32-2, 33-3

 

 

 

4

8/20/2007

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

 

 

 

4

8/20/2007

34-8, 34-9, 34-10, 34-11, 34-12, 34-15

 

 

 

4

8/20/2007

35-1, 35-2, 38-1, 38-2. 49-2 52-2, 52-3

 

 

 

4

8/20/2007

73-2, 77-1, 80-1

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

 

AIRCRAFT:

IA-GALAXY/G-200

REVISION NO. 5

DATE: 3/22/2010

PAGE NO.

III

 

 

Log of Revisions

 

 

Rev. No.

Date

Page Numbers

Initials

 

 

5

3/22/2010

HIGHLIGHTS OF REV., DEFINITIONS

 

 

 

5

3/22/2010

PREAMBLE, GUIDELINES

 

 

 

5

3/22/2010

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

 

 

 

5

3/22/2010

21-8, 21-9, 21-10, 22-1, 22-2, 22-3, 22-4,

 

 

 

5

3/22/2010

23-2, 23-3, 23-5, 23-7, 23-8, 23-9, 23-10,

 

 

 

5

3/22/2010

23-11, 23-12, 23-13, 24-1, 24-2, 25-1, 25-2

 

 

 

5

3/22/2010

25-6, 25-10, 25-11, 25-12, 25-13, 25-14

 

 

 

5

3/22/2010

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

 

 

 

5

3/22/2010

29-1, 29-2, 30-1, 30-2, 30-3, 30-4, 31-1

 

 

 

5

3/22/2010

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

 

 

 

5

3/22/2010

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

 

 

 

5

3/22/2010

34-7, 34-8, 34-9, 34-10, 34-11, 34-12

 

 

 

5

3/22/2010

34-13, 34-14, 34-15, 35-1, 46-1, 46-2, 49-1

 

 

 

5

3/22/2010

52-1, 52-2, 52-3, 73-1, 73-2, 74-1, 77-1

 

 

 

5

3/22/2010

78-1, 79-1, 80-1

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

 

AIRCRAFT:

IA-GALAXY/G-200

REVISION NO. 5

DATE: 3/22/2010

PAGE NO:

IV

 

 

Control Page

 

 

System

Page No.

Rev. No.

Current Date

 

 

Cover Page

-

5

3/22/2010

 

 

Table of Contents

I

5

3/22/2010

 

 

Log of Revisions

II

5

3/22/2010

 

 

 

III

5

3/22/2010

 

 

Control Page

IV

5

3/22/2010

 

 

 

V

5

3/22/2010

 

 

 

VI

5

3/22/2010

 

 

Highlights of Change

VII

5

3/22/2010

 

 

Definitions

VIII

15

11/2/2009

 

 

 

IX

15

11/2/2009

 

 

 

X

15

11/2/2009

 

 

 

XI

15

11/2/2009

 

 

 

XII

15

11/2/2009

 

 

 

XIII

15

11/2/2009

 

 

 

XIV

15

11/2/2009

 

 

 

XV

15

11/2/2009

 

 

Preamble

XVI

2

7/05/1990

 

 

 

XVII

2

7/05/1990

 

 

21

21-1

5

3/22/2010

 

 

 

21-2

5

3/22/2010

 

 

 

21-3

5

3/22/2010

 

 

 

21-4

5

3/22/2010

 

 

 

21-5

5

3/22/2010

 

 

 

21-6

5

3/22/2010

 

 

 

21-7

5

3/22/2010

 

 

 

21-8

5

3/22/2010

 

 

 

21-9

5

3/22/2010

 

 

 

21-10

5

3/22/2010

 

 

22

22-1

5

3/22/2010

 

 

 

22-2

5

3/22/2010

 

 

 

22-3

5

3/22/2010

 

 

 

22-4

5

3/22/2010

 

 

 

22-5

4

8/20/2007

 

 

 

22-6

4

8/20/2007

 

 

23

23-1

4

8/20/2007

 

 

 

23-2

5

3/22/2010

 

 

 

23-3

5

3/22/2010

 

 

 

23-4

4

8/20/2007

 

 

 

23-5

5

3/22/2010

 

 

 

23-6

4

8/20/2007

 

 

 

23-7

5

3/22/2010

 

 

 

23-8

5

3/22/2010

 

 

 

23-9

5

3/22/2010

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

 

AIRCRAFT:

IA-GALAXY/G-200

REVISION NO. 5

DATE: 3/22/2010

PAGE NO:

V

 

 

Control Page

 

 

System

Page No.

Rev. No.

Current Date

 

 

 

23-10

5

3/22/2010

 

 

 

23-11

5

3/22/2010

 

 

 

23-12

5

3/22/2010

 

 

 

23-13

5

3/22/2010

 

 

24

24-1

5

3/22/2010

 

 

 

24-2

5

3/22/2010

 

 

25

25-1

5

3/22/2010

 

 

 

25-2

5

3/22/2010

 

 

 

25-3

4

8/20/2007

 

 

 

25-4

4

8/20/2007

 

 

 

25-5

4

8/20/2007

 

 

 

25-6

5

3/22/2010

 

 

 

25-7

4

8/20/2007

 

 

 

25-8

4

8/20/2007

 

 

 

25-9

4

8/20/2007

 

 

 

25-10

5

3/22/2010

 

 

 

25-11

5

3/22/2010

 

 

 

25-12

5

3/22/2010

 

 

 

25-13

5

3/22/2010

 

 

 

25-14

5

3/22/2010

 

 

26

26-1

3

1/17/2006

 

 

 

26-2

4

8/20/2007

 

 

 

26-3

4

8/20/2007

 

 

27

27-1

5

3/22/2010

 

 

 

27-2

5

3/22/2010

 

 

 

27-3

5

3/22/2010

 

 

 

27-4

5

3/22/2010

 

 

28

28-1

5

3/22/2010

 

 

 

28-2

5

3/22/2010

 

 

 

28-3

5

3/22/2010

 

 

29

29-1

5

3/22/2010

 

 

 

29-2

5

3/22/2010

 

 

30

30-1

5

3/22/2010

 

 

 

30-2

5

3/22/2010

 

 

 

30-3

5

3/22/2010

 

 

 

30-4

5

3/22/2010

 

 

31

31-1

5

3/22/2010

 

 

 

31-2

5

3/22/2010

 

 

 

31-3

4

8/20/2007

 

 

32

32-1

5

3/22/2010

 

 

 

32-2

5

3/22/2010

 

 

33

33-1

5

3/22/2010

 

 

 

33-2

5

3/22/2010

 

 

 

33-3

5

3/22/2010

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

 

AIRCRAFT:

IA-GALAXY/G-200

REVISION NO. 5

DATE: 3/22/2010

PAGE NO:

VI

 

 

Control Page

 

 

System

Page No.

Rev. No.

Current Date

 

 

 

33-4

5

3/22/2010

 

 

 

33-5

5

3/22/2010

 

 

34

34-1

5

3/22/2010

 

 

 

34-2

5

3/22/2010

 

 

 

34-3

5

3/22/2010

 

 

 

34-4

5

3/22/2010

 

 

 

34-5

5

3/22/2010

 

 

 

34-6

5

3/22/2010

 

 

 

34-7

5

3/22/2010

 

 

 

34-8

5

3/22/2010

 

 

 

34-9

5

3/22/2010

 

 

 

34-10

5

3/22/2010

 

 

 

34-11

5

3/22/2010

 

 

 

34-12

5

3/22/2010

 

 

 

34-13

5

3/22/2010

 

 

 

34-14

5

3/22/2010

 

 

 

34-15

5

3/22/2010

 

 

35

35-1

5

3/22/2010

 

 

 

35-2

4

8/20/2007

 

 

38

38-1

4

8/20/2007

 

 

 

38-2

4

8/20/2007

 

 

46

46-1

5

3/22/2010

 

 

 

46-2

5

3/22/2010

 

 

49

49-1

5

3/22/2010

 

 

 

49-2

4

8/20/2007

 

 

52

52-1

5

3/22/2010

 

 

 

52-2

5

3/22/2010

 

 

 

52-3

5

3/22/2010

 

 

71

71-1

3

1/17/2006

 

 

73

73-1

5

3/22/2010

 

 

 

73-2

5

3/22/2010

 

 

74

74-1

5

3/22/2010

 

 

76

76-1

2

11/14/2003

 

 

77

77-1

5

3/22/2010

 

 

78

78-1

5

3/22/2010

 

 

79

79-1

5

3/22/2010

 

 

80

80-1

5

3/22/2010

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

 

AIRCRAFT:

IA-GALAXY/G-200

REVISION NO. 5

DATE: 3/22/2010

PAGE NO:

VII

 

 

Highlights of Change

 

 

 

Revision 5

 

This is a standard revision to the IA-GALAXY/G-200 Master Minimum Equipment List (MMEL). The changes result from a public Flight Operations Evaluation Board (FOEB) meeting held on December 3, 2009 to consider approximately 174 changes proposed by operators and Gulfstream.

 

 

 

 

 

 

 

FAA Policy Letters 1 through 124 and Global Changes 39 through 159 have been incorporated. For a complete listing of FAA Policy Letters and Global Changes visit www.opspecs.com.

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

 

AIRCRAFT:

IA-GALAXY/G-200

REVISION NO: 15

DATE: 11/02/2009

PAGE NO:

VIII

 

 

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 revision of that page.

 

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 FAR" 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 FAR must be operative.  When the listed item is not required by FAR 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.

 

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.

U. S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

IA-GALAXY/G-200

REVISION NO: 15

DATE: 11/02/2009

PAGE NO:

IX

DEFINITIONS

 

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).

 

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.

U. S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

IA-GALAXY/G-200

REVISION NO: 15

DATE: 11/02/2009

PAGE NO:

X

DEFINITIONS

 

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" means those items related to passenger convenience, comfort or entertainment such as, but not limited to, galley equipment, movie equipment, ash trays, stereo equipment, overhead reading lamps, etc.

 

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 “calendar days” or "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.

U. S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

IA-GALAXY/G-200

REVISION NO: 15

DATE: 11/02/2009

PAGE:

XI

DEFINITIONS

 

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.

 

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.

U. S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

IA-GALAXY/G-200

REVISION NO: 15

DATE: 11/02/2009

PAGE:

XII

DEFINITIONS

 

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)

 

Airbus aircraft equipped with Electronic Centralized Aircraft Monitoring (ECAM) provide different levels of system condition messages (WARNING, CAUTION, STATUS, and ADVISORY). A-318/319/320/321, A-330, and A-340 also provide MAINTENANCE status messages.  Any message that effects airplane dispatchability will normally be at the WARNING, CAUTION or STATUS level.  MAINTENANCE messages (A-318/319/320/321, A-330, and A-340 only) are also indicated on ECAM Status Page below the white Maintenance label.  A MAINTENANCE status (Class II) message on ECAM indicates the presence of a system fault which can be identified by CFDS (A-318/319/320/321) or CMS (A-330/A-340) interrogation.  The systems are designed to be fault tolerant.  For A-318/319/320/321, MAINTNENACE status (Class II) do not affect dispatch but are listed in the MMEL.  Dispatch is allowed without specific conditions except for: 
-       BLUE RSVR MAINTENANCE status: If applicable, and 
-       AIR BLEED MAINTENANCE status: As applicable. 
 
For the A-330 and A-340, MAINTENANCE status messages do not affect dispatch.
 
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 affects 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.

U. S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

IA-GALAXY/G-200

REVISION NO: 15

DATE: 11/02/2009

PAGE:

XIII

DEFINITIONS

 

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.

 

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.

U. S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

IA-GALAXY/G-200

REVISION NO: 15

DATE: 11/02/2009

PAGE:

XIV

DEFINITIONS

 

h.  DEHAVILLAND  (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 are 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.

 

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."

U. S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

IA-GALAXY/G-200

REVISION NO: 15

DATE: 11/02/2009

PAGE:

XV

DEFINITIONS

 

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.

 

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.

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

IA-GALAXY/G-200)

REVISION: 2

DATE: 07/05/1990

PAGE NO:

XVI

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:

IA-GALAXY/G-200

REVISION NO: 2

DATE: 7/05/1990

PAGE NO:

XVII

PREAMBLE

(7/05/1990)

 

Suitable conditions and limitations in the form of placards, maintenance procedures, crew operating procedures, and other restrictions, as necessary, are required to be accomplished by the operator to ensure that an acceptable level of safety is maintained. Those procedures should be developed from guidance provided in the manufacturer's aircraft flight and/or maintenance manuals, manufacturer's recommendations, engineering specifications, and other appropriate sources. Procedures must not be contrary to any FAR. Wherever the statement "as required by FAR" appears in the MMEL, the operator must either list the specific FAR by part and section and carry the FAR on board the aircraft or specify the requirements and/or limitations to conduct the flight in accordance with the appropriate FAR.

 

The MMEL is intended to permit operations with inoperative items of equipment for the minimum period of time necessary until repairs can be accomplished. It is important that repairs be accomplished at the earliest opportunity in order to return the aircraft to its design level of safety and reliability. Inoperative equipment in all cases must be repaired, or inspected and deferred, by qualified maintenance personnel at the next required inspection Section 91.165(c), NEW Section 91.405(c). The repair intervals indicated by the Letters A, B, and C inserted adjacent to column 2 are NOT applicable to this MMEL.

 

The MMEL 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 records. The item is then either repaired or deferred per the MMEL or other approved means acceptable to the Administrator prior to further operation. In addition to the specific MMEL conditions and limitations, determination by the operator that the aircraft is in condition for safe operations under anticipated flight conditions must be made for all items of inoperative equipment. When these requirements are met, the aircraft may be considered airworthy and returned to service. 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 interrelationship between those items, and the effect on aircraft operation and crew workload, must be considered. Operators are expected to establish a controlled and sound repair program, including the parts, personnel, facilities, procedures, and schedules to ensure timely repair.

 

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

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

IA-GALAXY/G-200

REVISION NO: 5

DATE: 3/22/2010

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.

Ram Air Check Valve

C

1

0

(O) May be inoperative OPEN provided:

a)      Airplane is operated unpressurized, and

b)      Airplane is operated in accordance with AFM Limitations.

 

|

|

 

 

 

 

 

 

 

2.

Automatic Temperature Control Cabin

C

1

0

May be inoperative provided Manual Temperature Control Cabin is operative.

 

|

 

 

C

1

0

(O) May be inoperative provided:

a)      Airplane is operated unpressurized, and

b)      Airplane is operated in accordance with AFM Limitations.

 

|

|

 

 

 

 

 

 

 

3.

Automatic Temperature Control Cockpit

C

1

0

May be inoperative provided Manual Temperature Control Cockpit is operative.

 

 

 

 

C

1

0

(O) May be inoperative provided:

a)      Airplane is operated unpressurized, and

b)      Airplane is operated in accordance with AFM Limitations.

 

|

|

 

 

 

 

 

 

 

4.

Manual Temperature Control Cabin

C

1

0

May be inoperative provided Automatic Temperature Control Cabin is operative.

 

 

 

 

C

1

0

(O) May be inoperative provided:

a)      Airplane is operated unpressurized, and

b)      Airplane is operated in accordance with AFM Limitations.

 

|

|

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

IA-GALAXY/G-200

REVISION NO: 5

DATE: 3/22/2010

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

 

 

 

 

 

 

 

 

 

 

 

 

5.

Manual Temperature Control Cockpit

C

1

0

May be inoperative provided Automatic Temperature Control Cockpit is operative.

 

 

 

 

C

1

0

(O) May be inoperative provided:

a)      Airplane is operated unpressurized, and

b)      Airplane is operated in accordance with AFM Limitations.

 

|

|

 

 

 

 

 

 

 

6.

Air Conditioning Unit  

C

1

0

May be inoperative provided airplane is operated unpressurized with Bleed Air Source Selector in RAM.

 

 

|

 

 

 

 

 

 

 

 

 

 

 

 

NOTE: Heat will not be available on ground or in flight. Bleed Air Source Selector must be selected to RAM only.

 

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

IA-GALAXY/G-200

REVISION NO: 5

DATE: 3/22/2010

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

 

 

 

 

 

 

 

 

 

 

 

 

7.

Cabin Pressurization Control System

 

 

 

 

 

 

 

 

 

 

 

 

1)        

Automatic Mode

B

1

0

(O) May be inoperative provided:

a)      Airplane is operated unpressurized, and

b)      Airplane is operated in accordance with AFM Limitations.

 

l

|

 

 

 

 

 

 

 

2)        

Manual Mode

B

1

0

(O) May be inoperative provided:

a)      Airplane is operated unpressurized, and

b)      Airplane is operated in accordance with AFM Limitations.

 

|

|

 

 

 

 

 

 

 

 

8.

Outflow Valve

 

 

C

1

0

(M) (O) Except for over water operations, may be inoperative OPEN provided:

a)   Outflow valve is verified OPEN,

b)   Airplane is operated unpressurized, and

c)   Airplane is operated in accordance with AFM Limitations.

 

 

 |

|

|

 

 

 

 

 

 

 

 

 

 

 

C

1

0

(M) (O) Except for over water operations, may be inoperative CLOSED provided:

a)      Safety Valve is secured OPEN,

b)      Airplane is operated unpressurized, and

c)      Airplane is operated in accordance with AFM limitations.

|

|

|

|

|

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

IA-GALAXY/G-200

REVISION NO: 5

DATE: 3/22/2010

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

 

 

 

 

 

 

 

 

 

 

 

 

9.

Nose Cooling Fans

C

2

1

May be inoperative provided AFM procedures are followed for each flight.

|

 

 

 

 

 

 

 

10.

Bleed Pressure Regulator Shutoff Valves (PRSOV)

C

2

1

May be inoperative CLOSED provided the airplane is operated at or below FL250.

|


 

 

 

 

 

 

 

 

 

C

2

0

(O) May be inoperative provided:

a)      Airplane is operated unpressurized, and

b)      Airplane is operated in accordance with AFM Limitations.

|
l
|



 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

AIRCRAFT:

IA-GALAXY/G-200

REVISION NO: 5

DATE: 3/22/2010

PAGE NO:

21-5

 

SYSTEM

SEQUENCE &

NUMBERS

1. REPAIR CATEGORY

 

 

2. NUMBER INSTALLED

 

 

3. NUMBER REQUIRED FOR DISPATCH

 

 

4. REMARKS AND EXCEPTIONS

 

21

AIR CONDITIONING

 

 

 

 

 

 

 

 

 

 

 

 

 

 

11.

Pack Pressure Regulator Shutoff Valve (PRSOV)

C

1

0

(O) May be inoperative provided:

a)      Airplane is operated unpressurized, and

b)   Airplane is operated in accordance with AFM Limitations.


|
|


 

 

 

 

 

 

 

 

 

12.

High Pressure Valves

C

2

1

May be inoperative CLOSED provided:

a)      Both Low Pressure (LP) Regulator Shut Off Valves are operative, and

b)      Airplane is not operated above FL400.

 

 

 

 

 

 

 

 

 

 

 

 

C

2

0

(O) May be inoperative provided:

a)      Airplane is operated unpressurized, and

b)   Airplane is operated in accordance with AFM Limitations.

|
|
|


 

 

 

 

 

 

 

 

13.

Bleed Pressure/ Temperature HI Warning System

C

2

0

(M) (O) May be inoperative provided:

a)      Environmental Control System (ECS) switch is in RAM,

b)      Airplane is operated unpressurized, and

c)   Airplane is operated in accordance with AFM Limitations.

|


|
|


 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

AIRCRAFT:

IA-GALAXY/G-200

REVISION NO: 5

DATE: 3/22/2010

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

 

 

 

 

 

 

 

 

 

 

 

 

 

 

14.

Cabin Duct Temp HI Warning System 

C

1

0

(M) (O) May be inoperative provided:

a)      Environmental Control System (ECS) switch is in RAM,

b)   Airplane is operated unpressurized, and

c)   Airplane is operated in accordance with AFM Limitations.

 



|
|


 

 

 

 

 

 

 

 

 

15.

Cockpit Duct Temp HI Warning System

C

1

0

(M) (O) May be inoperative provided:

a)      Environmental Control System (ECS) switch is in RAM,

b)   Airplane is operated unpressurized, and

c)   Airplane is operated in accordance with AFM Limitations.

 



|
|


 

 

 

 

 

 

 

 

 

16.

Overhead Airflow Vents (Wemacs)

D

-

0

 

 

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

AIRCRAFT:

IA-GALAXY/G-200

REVISION NO: 5

DATE: 3/22/2010

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

 

 

 

 

 

 

 

 

 

 

 

 

 

 

17.

Cabin Pressurization System

C

1

0

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

|

 

 

 

 

 

 

 

 

 

 

18.

Cockpit/Cabin Temperature Indicators

D

2

0

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

|

 

 

 

 

 

 

 

 

 

19.

Cabin Altitude Rate of Climb Indicator

C

1

0

(O) May be inoperative provided:

a)   Cabin Differential Pressure Indication is operative,

b)   A chart to convert cabin differential pressure to cabin altitude is provided to the crew, and

c)   Automatic and Manual Mode of Cabin Pressurization System (CPCS) is operative.

|

 

 

 

 

 

 

 

 

 

 

 

 

C

1

0

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

l

 

 

 

 

 

 

 

 

 

20.

Cabin Altitude Indicator

C

1

0

(O) May be inoperative provided:

a)   Cabin Differential Pressure Indicator is operative,

b)   A Cabin Differential Pressure Chart from the AFM is used to calculate cabin altitude, and

c)   Computed Cabin Altitude is monitored during flight by crewmember.

 

 

 

 






 

 

 

 

 

 

 

 

 

 

(continued)

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

AIRCRAFT:

IA-GALAXY/G-200

REVISION NO: 5

DATE: 3/22/2010

PAGE NO:

21-8

 

1. SYSTEM,

SEQUENCE NUMBERS & ITEM

REPAIR CATEGORY

 

 

2. NUMBER INSTALLED

 

 

3. NUMBER REQUIRED FOR DISPATCH

 

 

4. REMARKS AND EXCEPTIONS

 

21

AIR CONDITIONING

 

 

 

 

 

 

 

 

 

 

 

 

 

 

20.

Cabin Altitude Indicator

(continued)

C

1

0

(O) May be inoperative provided:

a)      Airplane is operated unpressurized, and

b)   Airplane is operated in accordance with AFM Limitations.


|
|


 

 

 

 

 

 

 

 

 

21.

Cabin Differential Pressure Indicator

C

1

0

(O) May be inoperative provided:

a)   Cabin Altitude Indicator is operative,

b)   A Cabin Differential Pressure Chart from the AFM is used to calculate cabin differential pressure, and

c)   Computed Cabin Differential Pressure is monitored during flight by crewmember.

 

 

 

 







 

 

 

 

 

 

 

 

 

 

 

C

1

0

(O) May be inoperative provided:

a)      Airplane is operated unpressurized, and

b)   Airplane is operated in accordance with AFM Limitations.

 

|

|


 

 

 

 

 

 

 

 

 

22.

Cabin Altitude High Warning System

B

1

0

(O) May be inoperative provided:

a)   Cabin Differential Pressure Indicator is operative,

b)   A chart to convert cabin differential pressure to cabin altitude is provided to crew,

c)   Automatic and Manual Pressurization Modes are operative, and

d)   Cabin altitude is monitored during flight by crewmember.

|

 

 

 

 

 

 

 

 

 

 

 

C

1

0

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

l

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

AIRCRAFT:

IA-GALAXY/G-200

REVISION NO: 5

DATE: 3/22/2010

PAGE NO:

21-9

 

1. SYSTEM,

SEQUENCE NUMBERS & ITEM

REPAIR CATEGORY

 

 

2. NUMBER INSTALLED

 

 

3. NUMBER REQUIRED FOR DISPATCH

 

 

4. REMARKS AND EXCEPTIONS

 

21

AIR CONDITIONING

 

 

 

 

 

 

 

 

 

 

 

 

 

 

23.

Baggage Compartment Over Pressurization Warning System

C

1

0

May be inoperative provided AFM procedures are followed.




 

 

 

 

 

 

 

 

 

24.

Safety Valve

C

1

0

(M) (O) Except for over water operations, may be inoperative OPEN provided:

a)      Outflow Valve is secured OPEN,

b)      Airplane is operated unpressurized, and

c)      Airplane is operated in accordance with AFM Limitations.

 

 

l

|

|

 

 

 

 

 

 

 

 

 

 

 

 

 

C

1

0

(M)(O) Except for over water operations, may be inoperative CLOSED provided:

a)  Outflow Valve is secured OPEN,

b)  Airplane is operated unpressurized, and

c)  Airplane is operated in accordance with AFM Limitations

|

|

|

|

|

|

|

 

 

 

 

 

 

 

 

 

25.

Windshield Defog System

C

1

0

May be inoperative provided the windshield heating system is operative.


|

 

 

 

 

 

 

 

 

 

26.

Windshield Defog Switch

D

1

0

May be inoperative provided the windshield heating system is operative.


|

 

 

 

 

 

 

 

 

 

27.

HI Flow Pushbutton

D

1

0

 

 

 

 

 

 

 

 

 

 

 

28.

Automatic Pressurization Schedule

C

1

0

May be inoperative provided:

a)      Cabin Pressurization Pushbutton is placed in Manual Mode,

b)      Cabin Altimeter is operative,

c)      Cabin Vertical Speed Indicator is operative, and

d)      Cabin Differential Pressure Gauge is operative.








 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

AIRCRAFT:

IA-GALAXY/G-200

REVISION NO: 5

DATE: 3/22/2010

PAGE NO:

21-10

 

1. SYSTEM,

SEQUENCE NUMBERS & ITEM

REPAIR CATEGORY

 

 

2. NUMBER INSTALLED

 

 

3. NUMBER REQUIRED FOR DISPATCH

 

 

4. REMARKS AND EXCEPTIONS

 

21

AIR CONDITIONING

 

 

 

 

 

 

 

 

 

 

 

 

 

 

29.

Cabin Temperature Remote Controllers

D

-

0

 



 

 

 

 

 

 

 

 

 

30.

Emergency Pressurization System

C

1

0

(O) May be inoperative provided:

a)      Airplane is operated unpressurized, and

b)      Airplane is operated in accordance with AFM Limitations.


|

|


 

 

 

 

 

 

 

 

 

31.

Ditch Pushbutton

C

1

0

May be inoperative provided the outflow valve can be controlled by Manual Cabin Pressure operation.




 

 

 

 

 

 

 

 

 

32.

Dump Pushbutton

C

1

0

May be inoperative provided the outflow valve can be controlled by Manual Cabin Pressure operation.




 

 

 

 

 

 

 

 

 

33.

Baggage Pressurization System

C

1

0

May be inoperative provided:

a)      The airplane baggage compartment remains unpressurized, and

b)      BAGG PRESS Pushbutton is CLOSED.



 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

NOTE:  Pressure sensitive cargo is not carried in the baggage compartment.

 

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

AIRCRAFT:

IA-GALAXY/G-200

REVISION NO: 5

DATE: 3/22/2010

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 Director Systems

C

2

0

May be inoperative provided approach minimums do not require its use.

|

 

 

 

 

 

 

 

 

 

2.

Autopilot System

B

1

0

(M) May be inoperative except where enroute operations, RVSM operations, or approach minimums require its use provided AFM limitations are observed.

 

 

 

 

 

 

 

 

 

 

3.

Yaw Damper System

C

1

0

(M) May be inoperative provided airplane is operated in accordance with AFM limitations.

 

 

 

 

 

 

 

 

 

 

4.

MACH Trim

C

1

0

May be inoperative provided airplane is operated in accordance with AFM limitations.

 

 

 

 

 

 

 

 

 

 

5.

Control Wheel Autopilot Disconnect Buttons

C

2

1

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.

|


l
l

 

 

 

 

B

2

0

May be inoperative provided the autopilot is not used.

|

 

 

 

 

 

 

 

 

 

 

6.

Takeoff/Go-Around (TOGA) Buttons

C

2

0

May be inoperative provided autopilot is not utilized for coupled approaches.

|

 

 

 

 

 

 

 

 

 

7.

***

Auto Throttle System

 

C

-

0

 

 

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

AIRCRAFT:

IA-GALAXY/G-200

REVISION NO: 5

DATE: 3/22/2010

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

 

 

 

 

 

 

 

 

 

 

 

 

 

 

8.

Flight Control Computers (FCC)

C

2

1

(O) FCC may be inoperative provided contingency planned flight time, with one engine inoperative, does not exceed one hour cruise from a suitable airport.

|



 

 

 

 

 

 

 

 

 

 

 

 

 

 

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






 

 

 

 

 

 

 

 

 

 

 

A

2

0

(O) May be inoperative provided:

a)    Automatic Cabin Pressurization System is operative,

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

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

d)    Airplane is operated at or below FL280,

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

f)     Repairs are made within one (1) flight day.

|

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

AIRCRAFT:

IA-GALAXY/G-200

REVISION NO: 5

DATE: 3/22/2010

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.

Pitch Synchronization Pushbutton

C

2

0

 



 

 

 

 

 

 

 

 

 

10.

Alternate Autopilot Disconnect Switches

 

 

 

 

 

 

 

 

 

 

 

 

 

 

1)

Pitch Trim Switches

C

2

0

May be Inoperative provided:

a)      Control Wheel Autopilot Disconnect Button is operative, and

b)      Auto Pilot Gang Bar Disconnect is operative.

l

 

 

 

 

 

 

 

 

 

2)

TO/GA Buttons

C

2

0

May be Inoperative provided:

a)      Control Wheel Autopilot Disconnect Button is operative, and

b)   Auto Pilot Gang Bar Disconnect is operative.

l

 

 

 

 

 

 

 

 

 

3)

AHS Buttons

C

2

0

May be Inoperative provided:

a)      Control Wheel Autopilot Disconnect Button is operative, and

b)   Auto Pilot Gang Bar Disconnect is operative.

l

 

 

 

 

 

 

 

 

 

 

 

 

 

 

NOTE:  With optional IRS installed, AHS button selection will not cause the autopilot to disengage.

 

 

 

 

 

 

 

 

 

 

11.

V-Speed Automatic Synchronization and Upload System

C

1

0

May be inoperative provided V-speeds are manually input and crosschecked between each pilot station.




 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

AIRCRAFT:

IA-GALAXY/G-200

REVISION NO: 5

DATE: 3/22/2010

PAGE NO:

22-4

 

1. SYSTEM,

SEQUENCE NUMBERS & ITEM

REPAIR CATEGORY

 

 

2. NUMBER INSTALLED

 

 

3. NUMBER REQUIRED FOR DISPATCH

 

 

4. REMARKS AND EXCEPTIONS

 

22

AUTO FLIGHT

 

 

 

 

 

 

 

 

 

 

 

 

 

 

12.

Autopilot Coupler

 

 

 

 

 

 

 

 

 

 

 

 

 

 

1)

 Left Selection

C

1

0

May be inoperative provided contingency planned flight time, with one engine inoperative, does not exceed one hour cruise from a suitable airport.

 

 

 

 

 

 

 

 

 

 

 

 

 

2)

Right Selection

C

1

0

May be inoperative provided contingency planned flight time, with one engine inoperative, does not exceed one hour cruise from a suitable airport.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

3)

Left and Right

Selections

A

2

0

(O) May be inoperative provided:

a)   Automatic Cabin Pressurization System is operative,

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

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

d)   Airplane is operated at or below FL280,

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

f)    Repairs are made within one (1) flight day.

|

 

 

 

 

 

 

 

 

 

 

 

 

 



 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

AIRCRAFT:

IA-GALAXY/G-200

REVISION NO: 4

DATE: 8/20/2007

PAGE NO:

22-5

 

1. SYSTEM,

SEQUENCE NUMBERS & ITEM

REPAIR CATEGORY

 

 

2. NUMBER INSTALLED

 

 

3. NUMBER REQUIRED FOR DISPATCH

 

 

4. REMARKS AND EXCEPTIONS

 

22

AUTO FLIGHT

 

 

 

 

 

 

 

 

 

 

 

 

 

 

13.

Flight Control Panel, Altitude Guidance Modes

 

 

 

 

 

 

 

 

 

 

 

 

 

 

1)

Vertical Navigation (VNAV) Mode Selector Switch

C

1

0

May be inoperative provided vertical navigation mode is considered inoperative and not used during autopilot operations.





 

 

 

 

 

 

 

 

 

2)

Vertical Speed (VS) Mode Selector Switch

C

1

0

May be inoperative provided vertical speed mode is considered inoperative and not used during autopilot operations.




 

 

 

 

 

 

 

 

 

3)

Flight Level Change (FLC) Mode Selector Switch

C

1

0

May be inoperative provided flight level change mode is considered inoperative and not used during autopilot operations.




 

 

 

 

 

 

 

 

 

4)

Pitch Mode (PIT)

C

1

0

May be inoperative provided pitch mode is considered inoperative and not used during autopilot operations.




 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

AIRCRAFT:

IA-GALAXY/G-200

REVISION NO: 4

DATE: 8/20/2007

PAGE NO:

22-6

 

1. SYSTEM,

SEQUENCE NUMBERS & ITEM

REPAIR CATEGORY

 

 

2. NUMBER INSTALLED

 

 

3. NUMBER REQUIRED FOR DISPATCH

 

 

4. REMARKS AND EXCEPTIONS

 

22

AUTO FLIGHT

 

 

 

 

 

 

 

 

 

 

 

 

 

 

14.

Flight Control Panel, Lateral Guidance Modes

 

 

 

 

 

 

 

 

 

 

 

 

 

 

1)

BANK Mode Selector Switch

C

1

0

May be inoperative provided autopilot operations do not require bank selection.



 

 

 

 

 

 

 

 

 

2)

Navigation (NAV) Mode Selector Switch

C

1

0

May be inoperative provided NAV mode autopilot operations are not required.



 

 

 

 

 

 

 

 

 

3)

Back Course (BC) Mode Selector Switch

C

1

0

May be inoperative provided Back Course operations are not conducted.



 

 

 

 

 

 

 

 

 

4)

Approach (APPR) Mode Selector Switch

C

1

0

May be inoperative provided Approach Mode operations are not conducted.



 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

AIRCRAFT:

IA-GALAXY/G-200

REVISION NO: 4

DATE: 8/20/2007

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.

Communication Systems ( VHF and UHF)

D

-

-

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

 

 

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

AIRCRAFT:

IA-GALAXY/G-200

REVISION NO: 5

DATE: 3/22/2010

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.

Passenger Address (PA) System

 

 

 

 

 

 

 

 

 

 

 

 

 

 

1)

Passenger Configuration

B

1

0

(O) May be inoperative provided:

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

b)   Flight attendant alerting system (audio and visual) operates normally.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

NOTE: Any station function(s) that operates normally 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 operate normally may be used.

 

 

 

 

 

 

 

 

 

 

 

2)

Lavatory Speakers

C

1

0

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

l

 

 

 

 

 

 

 

 

 

3.

Cockpit Speakers

C

2

0

May be inoperative provided the affected crewmember has available an operative headset.

l

 

 

 

 

 

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

AIRCRAFT:

IA-GALAXY/G-200

REVISION NO: 5

DATE: 3/22/2010

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

 

 

 

 

 

 

 

 

 

 

 

 

 

 

4.

Hand Held Microphones

C

-

0

May be inoperative provided the affected cockpit crewmember:

a)      Uses a boom microphone (headset), and

b)   Associated Control Wheel Push-to-Talk Switch is operative.

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NOTE:  An optional Side Panel Console Mounted Push-to-Talk (PTT) Switch may be used in lieu of an operative Control Wheel Push-to-Talk Switch where installed.






 

 

 

 

 

 

 

 

 

5.

Radio Tuning Units (RTU)

C

2

0

May be inoperative provided direct tuning is available from each FMS and is operative.

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6.

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.

 

 

 

 

 

 

 

 

 

 

 

Cockpit Voi