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Revision: |
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Date: 10/09/2009 |
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DEPARTMENT OF TRANSPORTATION |
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FEDERAL AVIATION ADMINISTRATION |
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WASHINGTON , D.C. |
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MASTER MINIMUM EQUIPMENT LIST |
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TWIN COMMANDER AIRCRAFT 680T/680V/680W/681/690/690A 690B/690C/690D/695/695A/695B |
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Roman A. Buettner |
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Chairman, Flight Operations Evaluation Board (FOEB) |
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Federal Aviation Administration |
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Kansas City Aircraft Evaluation Group |
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DOT Building , Room 332 |
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901 Locust Street |
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Kansas City , MO 64106-2641 |
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Telephone: |
(816)-329-3233 |
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FAX: |
(816)-329-3241 |
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| U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION |
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| AIRCRAFT: TWIN COMMANDER AIRCRAFT 680T/680V/680W/681/690/690A 690B/690C/690D/695/695A/695B |
REVISION NO: 7a
DATE: 10/09/2009 |
PAGE NO:
I |
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| TABLE OF CONTENTS |
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| SYSTEM NO. |
SYSTEM |
PAGE NO. |
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| -- |
Cover Page |
-- |
| -- |
Table of Contents |
I |
| -- |
Log of Revisions |
II, III |
| -- |
Control Page(s) |
IV, V |
| -- |
Highlights of Change |
VI |
| -- |
Definitions |
VII |
| -- |
Preamble |
VIII |
| -- |
Guidelines for (O) & (M) Procedures |
IX, X, XI, |
| -- |
Guidelines for (O) & (M) Procedures |
XII, XIII |
| 21 |
Air Conditioning |
21-1, 2 |
| 22 |
Autopilot |
22-1 |
| 23 |
Communications |
23-1 THRU 4 |
| 24 |
Electrical |
24-1 |
| 25 |
Equipment/Furnishings |
25-1 THRU 5 |
| 26 |
Fire Protection |
26-1 |
| 27 |
Flight Controls |
27-1 |
| 28 |
Fuel |
28-1 |
| 30 |
Ice & Rain Protection |
30-1, 2 |
| 31 |
Indicating/Recording Systems |
31-1, 2 |
| 32 |
Landing Gear |
32-1 |
| 33 |
Lights |
33-1, 2 |
| 34 |
Navigation |
34-1 THRU 16 |
| 35 |
Oxygen |
35-1 |
| 38 |
Water/Waste |
38-1 |
| 46 |
Information Systems |
46-1, 2 |
| 52 |
Doors |
52-1 |
| 61 |
Propellers |
61-1 |
| 73 |
Engine Fuel & Control |
73-1 |
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| U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION |
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| AIRCRAFT: TWIN COMMANDER AIRCRAFT 680T/680V/680W/681/690/690A 690B/690C/690D/695/695A/695B |
REVISION NO: 6
DATE: 03/31/2003 |
PAGE NO:
II |
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| Log of Revisions |
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| Rev No. |
Date |
Page Numbers |
Initials |
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| 1 |
09/08/1982 |
Complete Reissue |
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| 2 |
05/29/1984 |
Complete Reissue |
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| 3 |
07/22/1988 |
Complete Reissue |
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| 4 |
03/29/1989 |
Complete Reissue |
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| 5 |
06/22/1989 |
HIGHLIGHTS OF REV., DEFINITIONS |
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| 5 |
06/22/1989 |
PREAMBLE |
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| 5a |
04/17/1991 |
HIGHLIGHTS OF REV., DEFINITIONS |
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| 5a |
04/17/1991 |
23-1, 23-2 |
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| 5b |
08/22/1994 |
HIGHLIGHTS OF REV., DEFINITIONS |
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| 5b |
08/22/1994 |
GUIDELINES |
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| 5b |
08/22/1994 |
21-1, 21-2, 22-1, 23-1, 23-2 |
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| 5b |
08/22/1994 |
24-1, 25-1, 25-2, 26-1, 27-1 |
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| 5b |
08/22/1994 |
28-1, 30-1, 30-2, 31-1, 32-1 |
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| 5b |
08/22/1994 |
33-1, 33-2, 34-1, 34-2, 34-3 |
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| 5b |
08/22/1994 |
34-4, 35-1, 52-1, 73-1 |
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| 5c |
04/16/1996 |
HIGHLIGHTS OF REV., DEFINITIONS |
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| 5c |
04/16/1996 |
GUIDELINES |
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| 5c |
04/16/1996 |
21-1, 21-2, 22-1, 23-1, 23-2 |
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| 5c |
04/16/1996 |
24-1, 25-1, 25-2, 26-1, 27-1 |
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| 5c |
04/16/1996 |
28-1, 30-1, 30-2, 31-1, 32-1 |
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| 5c |
04/16/1996 |
33-1, 33-2, 34-1, 34-2,34-3 |
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| 5c |
04/16/1996 |
34-4, 34-5, 34-6, 35-1, 52-1 |
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| 5c |
04/16/1996 |
61-1, 73-1 |
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| 5d |
08/04/1997 |
HIGHLIGHTS OF REV., DEFINITIONS |
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| 5d |
08/04/1997 |
34-1, 34-2, 34-3, 34-4, 34-5 |
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| 5d |
08/04/1997 |
34-6 |
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| 6 |
03/31/2003 |
HIGHLIGHTS OF REV., DEFINITIONS |
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| 6 |
03/31/2003 |
GUIDELINES |
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| 6 |
03/31/2003 |
21-1, 21-2, 22-1, 23-1, 23-2 |
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| 6 |
03/31/2003 |
23-3, 24-1, 25-1, 25-2, 26-1 |
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| 6 |
03/31/2003 |
27-1, 30-2, 31-1, 31-2, 33-1 |
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| 6 |
03/31/2003 |
34-1, 34-2, 34-3, 34-4, 34-5 |
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| 6 |
03/31/2003 |
34-6, 34-7, 34-8, 34-9, 34-10 |
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| 6 |
03/31/2003 |
52-1, 61-1 |
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| U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION |
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| AIRCRAFT: TWIN COMMANDER AIRCRAFT 680T/680V/680W/681/690/690A 690B/690C/690D/695/695A/695B |
REVISION NO: 7a
DATE: 10/09/2009 |
PAGE NO:
III |
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| Log of Revisions |
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| Rev No. |
Date |
Page Numbers |
Initials |
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| 7 |
09/09/2009 |
COVER PAGE, TABLE OF CONTENTS, |
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| 7 |
09/09/2009 |
LOG OF REVISIONS, CONTROL PAGES, |
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| 7 |
09/09/2009 |
HIGHLIGHTS OF CHANGE, DEFINITIONS, |
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| 7 |
09/09/2009 |
PREAMBLE, GUIDELINES FOR (O) & (M), |
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| 7 |
09/09/2009 |
22-1, 23-1, 23-2, 23-3, 23-4, |
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| 7 |
09/09/2009 |
24-1, 25-1, 25-2, 25-3, 25-4, |
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| 7 |
09/09/2009 |
25-5, 26-1, 30-2, 31-1, 31-2, |
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| 7 |
09/09/2009 |
33-1, 33-2, 34-2, 34-3, 34-4, |
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| 7 |
09/09/2009 |
34-5, 34-6, 34-7, 34-8, 34-9, |
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| 7 |
09/09/2009 |
34-10, 34-11, 34-12, 34-13, |
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| 7 |
09/09/2009 |
34-14, 34-15, 34-16, 35-1, |
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| 7 |
09/09/2009 |
38-1, 46-1, 46-2 |
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| 7a |
10/09/2009 |
COVER PAGE, TABLE OF CONTENTS, |
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| 7a |
10/09/2009 |
LOG OF REVISIONS, CONTROL PAGES, |
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| 7a |
10/09/2009 |
HIGHLIGHTS OF CHANGE, DEFINITIONS, |
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| 7a |
10/09/2009 |
PREAMBLE, GUIDELINES FOR (O) & (M), |
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| 7a |
10/09/2009 |
30-2, 46-2 |
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| U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION |
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| AIRCRAFT: TWIN COMMANDER AIRCRAFT 680T/680V/680W/681/690/690A 690B/690C/690D/695/695A/695B |
REVISION NO: 7a
DATE: 10/09/2009 |
PAGE NO:
IV |
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| Control Page |
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| System |
Page No. |
Rev. No. |
Current Date |
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| Cover Page |
- |
7a |
10/09/2009 |
| Table of Contents |
I |
7a |
10/09/2009 |
| Log of Revisions |
II |
6 |
03/31/2003 |
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III |
7a |
10/09/2009 |
| Control Page |
IV |
7a |
10/09/2009 |
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V |
7a |
10/09/2009 |
| Highlights of Change |
VI |
7a |
10/09/2009 |
| Definitions |
VII |
7a |
10/09/2009 |
| Preamble |
VIII |
7a |
10/09/2009 |
| Guidelines for (O) & (M) Procedures |
IX |
7a |
10/09/2009 |
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X |
7a |
10/09/2009 |
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XI |
7a |
10/09/2009 |
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XII |
7a |
10/09/2009 |
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XIII |
7a |
10/09/2009 |
| 21 |
21-1 |
6 |
03/31/2003 |
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21-2 |
6 |
03/31/2003 |
| 22 |
22-1 |
7 |
09/09/2009 |
| 23 |
23-1 |
7 |
09/09/2009 |
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23-2 |
7 |
09/09/2009 |
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23-3 |
7 |
09/09/2009 |
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23-4 |
7 |
09/09/2009 |
| 24 |
24-1 |
7 |
09/09/2009 |
| 25 |
25-1 |
7 |
09/09/2009 |
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25-2 |
7 |
09/09/2009 |
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25-3 |
7 |
09/09/2009 |
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25-4 |
7 |
09/09/2009 |
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25-5 |
7 |
09/09/2009 |
| 26 |
26-1 |
7 |
09/09/2009 |
| 27 |
27-1 |
6 |
03/31/2003 |
| 28 |
28-1 |
6 |
03/31/2003 |
| 30 |
30-1 |
5c |
04/16/1996 |
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30-2 |
7a |
10/09/2009 |
| 31 |
31-1 |
7 |
09/09/2009 |
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31-2 |
7 |
09/09/2009 |
| 32 |
32-1 |
5c |
04/16/1996 |
| 33 |
33-1 |
7 |
09/09/2009 |
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33-2 |
7 |
09/09/2009 |
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| U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION |
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| AIRCRAFT: TWIN COMMANDER AIRCRAFT 680T/680V/680W/681/690/690A 690B/690C/690D/695/695A/695B |
REVISION NO: 7a
DATE: 10/09/2009 |
PAGE NO:
V |
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| Control Page |
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| System |
Page No. |
Rev. No. |
Current Date |
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| 34 |
34-1 |
6 |
03/31/2003 |
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34-2 |
7 |
09/09/2009 |
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34-3 |
7 |
09/09/2009 |
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34-4 |
7 |
09/09/2009 |
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34-5 |
7 |
09/09/2009 |
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34-6 |
7 |
09/09/2009 |
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34-7 |
7 |
09/09/2009 |
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34-8 |
7 |
09/09/2009 |
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34-9 |
7 |
09/09/2009 |
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34-10 |
7 |
09/09/2009 |
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34-11 |
7 |
09/09/2009 |
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34-12 |
7 |
09/09/2009 |
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34-13 |
7 |
09/09/2009 |
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34-14 |
7 |
09/09/2009 |
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34-15 |
7 |
09/09/2009 |
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34-16 |
7 |
09/09/2009 |
| 35 |
35-1 |
7 |
09/09/2009 |
| 38 |
38-1 |
7 |
09/09/2009 |
| 46 |
46-1 |
7 |
09/09/2009 |
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46-2 |
7a |
10/09/2009 |
| 52 |
52-1 |
6 |
03/31/2003 |
| 61 |
61-1 |
6 |
03/31/2003 |
| 73 |
73-1 |
5c |
04/16/1996 |
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| U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION |
||
| AIRCRAFT: TWIN COMMANDER AIRCRAFT 680T/680V/680W/681/690/690A 690B/690C/690D/695/695A/695B |
REVISION NO: 7a
DATE: 10/09/2009 |
PAGE NO:
VI |
| HIGHLIGHTS OF CHANGE |
||
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Cover Page
|
Updated to reflect Revision 7a. |
| Table Of Contents
|
Updated to incorporate Revision 7a Page Number changes only. |
| Log Of Revisions
|
Updated to incorporate Revision 7a changes. |
| Control Pages
|
Updated to incorporate Revision 7a changes. |
| Highlights Of Change
|
Updated to incorporate Revision 7a changes. |
| Definitions
|
Updated to reflect revised Page Number only.
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| Preamble |
Updated to reflect revised Page Number only.
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| Guidelines (O & M)
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Updated to reflect revised Page Numbers only. |
| ATA 30-12
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Revised SYSTEM ITEM title by deleting “Engine Inlet Anti-Ice Systems” and adding “Generator Inlet Deicer Installation”, which was inadvertently omitted in Revision 7. No change in relief.
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| ATA 46-1 |
Added “1. Electronic Flight Bag Systems (EFBs), (Continued)”, to the SYSTEM ITEM column. No change in relief. |
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| U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION |
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| AIRCRAFT: TWIN COMMANDER AIRCRAFT 680T/680V/680W/681/690/690A 690B/690C/690D/695/695A/695B |
REVISION NO: 7a
DATE: 10/09/2009 |
PAGE NO:
VII |
| DEFINITIONS |
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The Definitions must be inserted here in each Minimum Equipment List (MEL) from current FAA MMEL Policy Letter 25, entitled “Policy Concerning MMEL Definitions”, and from current FAA MMEL Policy Letter 70, entitled “Definitions Required in MELs”.
| U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION |
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| AIRCRAFT: TWIN COMMANDER AIRCRAFT 680T/680V/680W/681/690/690A 690B/690C/690D/695/695A/695B |
REVISION NO: 7a
DATE: 10/09/2009 |
PAGE NO:
VIII |
| PREAMBLE |
||
The applicable Preamble must be inserted here in each Minimum Equipment List (MEL) from current FAA MMEL Policy Letter 34, entitled “MMEL and MEL PREAMBLE”, or from current FAA Policy Letter 36, entitled “14 CFR Part 91 MEL Approval & Preamble”, for Part 91 MEL approvals.
| U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION |
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| AIRCRAFT: TWIN COMMANDER AIRCRAFT 680T/680V/680W/681/690/690A 690B/690C/690D/695/695A/695B |
REVISION NO: 7a
DATE: 10/09/2009 |
PAGE NO:
IX |
| Guidelines for (O) & (M) Procedures |
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The FOEB has identified a need for certain procedures to provide an adequate level of safety while providing relief for the following items. These procedures must be established by the operator. The following guidelines are to help establish these required procedures:
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21-1 |
(M) Maintenance procedure to ensure no fuel leak or electrical/mechanical fault exists that may cause additional damage.
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| 21-4 |
(M) Maintenance procedure to ensure that the Dump Valve is secured in the OPEN position.
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| 22-1 |
(M) Maintenance procedure to ensure no electrical or mechanical fault exists that will have an adverse effect on any flight control function.
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| 22-2 |
(M) Maintenance procedure to ensure no electrical or mechanical fault exists that will have an adverse effect on any flight control function.
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| 23-4-A
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(O) Operations procedure to ensure PA System is not required by 14 CFR and passengers are appropriately briefed.
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| 23-7 |
(O) Operations procedure to ensure SATCOM Voice or Data Link operates normally, alternate procedures are established and used, and SATCOM coverage is available over the intended route of flight.
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| 23-8 |
(O) Operations procedure to establish and use alternate procedures.
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| 23-8-A |
(O) Operations procedure to establish and use alternate procedures.
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| 25-2-A
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(M) Maintenance procedure to ensure Seat is secured in the FULL UPRIGHT position.
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| 25-2-B
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(O) Operations procedure to ensure baggage is not stowed under Seat with inoperative Restraining Bar, Seat is properly placarded, and flight crew is alerted.
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| 25-2-C-1
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(M) Maintenance procedure to ensure Seat is secured in the FULL UPRIGHT position if an Armrest is missing.
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| U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION |
||
| AIRCRAFT: TWIN COMMANDER AIRCRAFT 680T/680V/680W/681/690/690A 690B/690C/690D/695/695A/695B |
REVISION NO: 7a
DATE: 10/09/2009 |
PAGE NO:
X |
| Guidelines for (O) & (M) Procedures |
||
|
25-5-B
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(M) Maintenance procedure to ensure inoperative System is deactivated. Applies to both provisos.
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| 25-7-A
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(O) Operations procedure to ensure AED is resealed in a manner that will identify it as a Unit that cannot be mistaken for a fully serviceable Unit.
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| 25-7-B
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(O) Operations procedure to ensure EMK is resealed in a manner that will identify it as a Unit that cannot be mistaken for a fully serviceable Unit.
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| 25-7-C
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(O) Operations procedure to ensure FAK is resealed in a manner that will identify it as a Unit that cannot be mistaken for a fully serviceable Unit.
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| 25-8
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(M) Maintenance procedure to ensure acceptable cargo loading limits from an approved source is maintained.
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| 27-3 |
(M) Maintenance procedure to ensure that the failure of the Electrical Pitch Trim will not affect the operation of the Manual Trims or other flight controls.
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| 31-2 |
(O) Operations procedure for recording flight time.
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| 32-1 |
(O) Operations procedure to prevent movement of the aircraft when stopped or parked.
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| 33-3 |
(O) Operations procedure to ensure PA System operates normally and is used to notify passengers when Signs are turned ON or OFF.
|
| 33-3-A |
(O) Operations procedure to ensure that alternate procedures are used for passenger briefings.
|
| 34-19 |
(O) Operations procedure to ensure any combination of three Gyro or INS (IRU) Stabilized Compass Systems are operative.
(O) Operations procedure to ensure two Gyro or Compass Systems operate normally, and the airplane is operated with dual independent navigation capability.
(O) Operations procedure to ensure at least two Stabilized Directional Gyro Systems are installed and operate normally.
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| U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION |
||
| AIRCRAFT: TWIN COMMANDER AIRCRAFT 680T/680V/680W/681/690/690A 690B/690C/690D/695/695A/695B |
REVISION NO: 7a
DATE: 10/09/2009 |
PAGE NO:
XI |
| Guidelines for (O) & (M) Procedures |
||
|
34-20-A-1
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(O) Operations procedure to ensure alternate procedures are established and used.
|
| 34-20-A-1-a |
(O) Operations procedure to ensure alternate procedures are established and used.
|
| 34-20-A-1-d |
(O) Operations procedure to ensure alternate procedures are established and used.
(O) Operations procedure to ensure alternate procedures are established and used and advisory callouts are not required by 14 CFR.
|
| 34-20-A-1-e
|
(O) Operations procedure to ensure alternate procedures are established and used.
(O) Operations procedure to ensure alternate procedures are established and used and Windshear Detection and Avoidance System (Predictive) operates normally.
|
| 34-20-A-2 |
(O) Operations procedure to ensure alternate procedures are established and used.
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| 34-20-B-1
|
(O) Operations procedure to ensure alternate procedures are established and used.
|
| 34-20-B-1-a |
(O) Operations procedure to ensure alternate procedures are established and used.
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| 34-20-B-1-d
|
(O) Operations procedure to ensure alternate procedures are established and used.
(O) Operations procedure to ensure alternate procedures are established and used and advisory callouts are not required by 14 CFR.
|
| 34-20-B-1-e |
(O) Operations procedure to ensure alternate procedures are established and used.
|
| 34-20-C-1
|
(O) Operations procedure to ensure alternate procedures are established and used.
|
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| U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION |
||
| AIRCRAFT: TWIN COMMANDER AIRCRAFT 680T/680V/680W/681/690/690A 690B/690C/690D/695/695A/695B |
REVISION NO: 7a
DATE: 10/09/2009 |
PAGE NO:
XII |
| Guidelines for (O) & (M) Procedures |
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34-21 |
(M) Maintenance procedure to ensure System is deactivated and SECURED. Applies to both provisos.
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| 34-22 |
(M) Maintenance procedure to ensure System is deactivated and SECURED. Applies to both provisos.
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| 34-22-B
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(O) Operations procedure to ensure TA Visual Display and Audio Functions are operative, TA ONLY Mode is selected by the crew, and enroute or approach procedures do not require use of the RA Display System.
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| 34-22-C
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(O) Operations procedure to ensure RA Visual Display and Audio Functions are operative, and enroute or approach procedures do not require use of the TA Display System.
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| 34-25-A
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(O) Operations procedure to ensure current aeronautical charts are used, status and suitability of navigation facilities to be used are verified, and Approach Navigation Radios are manually tuned and identified.
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| 34-26-A
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(O) Operations procedure to ensure current aeronautical charts are used, status and suitability of navigation facilities to be used are verified, and Approach Navigation Radios are manually tuned and identified.
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| 34-31 |
(O) Operations procedure to ensure Autopilot with Altitude Hold is operative and enroute operations do not require use of the Altitude Alerting System.
(O) Operations procedure to ensure aircraft is operated with a Second in Command and enroute operations do not require use of the Altitude Alerting System.
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| 34-32-A-1
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(O) Operations procedure to ensure alternate procedures are established and used.
(O) Operations procedure to ensure alternate procedures are established and used and Windshear Detection and Avoidance System (Predictive) operates normally.
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| U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION |
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| AIRCRAFT: TWIN COMMANDER AIRCRAFT 680T/680V/680W/681/690/690A 690B/690C/690D/695/695A/695B |
REVISION NO: 7a
DATE: 10/09/2009 |
PAGE NO:
XIII |
| Guidelines for (O) & (M) Procedures |
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34-32-A-2
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(O) Operations procedure to ensure alternate procedures are established and used.
(O) Operations procedure to ensure alternate procedures are established and used and Windshear Warning and Flight Guidance System (Reactive) operates normally.
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| 34-32-B-1 |
(O) Operations procedure to ensure alternate procedures are established and used.
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| 34-32-B-2
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(O) Operations procedure to ensure alternate procedures are established and used.
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| 38-1 |
(M) Maintenance procedure to ensure associated Components are deactivated or isolated and System Components do not have leaks.
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| 46-1-A
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(O) Operations procedure to ensure alternate procedures are established and used.
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| 46-1-B |
(O) Operations procedure to ensure alternate procedures are established and used.
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| 46-1-C |
(O) Operations procedure to ensure alternate procedures are established and used.
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| 46-1-D |
(M) Maintenance procedure to ensure associated EFB and hardware is secured by an alternate means or removed from the aircraft.
(O) Operations procedure to ensure alternate procedures are established and used.
(M) Maintenance procedure to ensure associated EFB and hardware is secured by an alternate means or removed from the aircraft.
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| U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION |
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| AIRCRAFT: TWIN COMMANDER AIRCRAFT 680T/680V/680W/681/690/690A 690B/690C/690D/695/695A/695B |
REVISION NO: 6
DATE: 03/31/2003 |
PAGE NO:
21-1 |
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| 1. SYSTEM, SEQUENCE NUMBERS & ITEM |
REPAIR CATEGORY |
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2. NUMBER INSTALLED |
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3. NUMBER REQUIRED FOR DISPATCH |
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4. REMARKS AND EXCEPTIONS |
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| 21 |
AIR CONDITIONING |
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| 1. |
Combustion Heater |
C |
1 |
0 |
(M) |
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| 2. |
Defog Blower |
C |
1 |
0 |
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| 3. |
Pressurization Controller |
C |
1 |
0 |
May be inoperative for unpressurized flight. |
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| 4. |
Safety Valve |
C |
1 |
0 |
(M) May be inoperative provided: a) Airplane remains unpressurized, and b) Dump Valve is blocked OPEN. |
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| 5. |
Outflow Valve |
C |
1 |
0 |
May be inoperative provided: a) Airplane remains unpressurized, and b) Dump Valve is OPEN. |
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| 6. |
Altitude Warning |
C |
1 |
0 |
May be inoperative for unpressurized flight. |
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C |
1 |
0 |
May be inoperative for pressurized flight at or below 10,000 feet MSL. |
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| 7. |
Cabin Rate Of Climb |
C |
1 |
0 |
May be inoperative for unpressurized flight. |
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C |
1 |
0 |
May be inoperative for pressurized flight provided Differential Pressure/Cabin Altitude Indicator is operative. |
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| 8. |
Differential Pressure/Cabin Altitude Indicator |
C |
1 |
0 |
May be inoperative for unpressurized flight. |
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| 9. |
Baggage Compartment Heater |
C |
1 |
0 |
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| U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION |
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| AIRCRAFT: TWIN COMMANDER AIRCRAFT 680T/680V/680W/681/690/690A 690B/690C/690D/695/695A/695B |
REVISION NO: 6
DATE: 03/31/2003 |
PAGE NO:
21-2 |
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| 1. SYSTEM, SEQUENCE NUMBERS & ITEM |
REPAIR CATEGORY |
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2. NUMBER INSTALLED |
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3. NUMBER REQUIRED FOR DISPATCH |
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4. REMARKS AND EXCEPTIONS |
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| 21 |
AIR CONDITIONING |
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| 10. |
Air Conditioning System (Freon) |
C |
1 |
0 |
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| U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION |
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| AIRCRAFT: TWIN COMMANDER AIRCRAFT 680T/680V/680W/681/690/690A 690B/690C/690D/695/695A/695B |
REVISION NO: 7
DATE: 09/09/2009 |
PAGE NO:
22-1 |
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| 1. SYSTEM, SEQUENCE NUMBERS & ITEM |
REPAIR CATEGORY |
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2. NUMBER INSTALLED |
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3. NUMBER REQUIRED FOR DISPATCH |
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4. REMARKS AND EXCEPTIONS |
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| 22 |
AUTOPILOT |
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| 1. |
Autopilot System |
C |
- |
0 |
(M) May be inoperative provided operations do not require its use. |
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NOTE: For RVSM operations, the Altitude Hold Function must be operative. |
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| 2. |
Yaw Damper |
C |
1 |
0 |
(M) |
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| 3. |
Autopilot Disconnect Functions (Quick Release Controls) |
C
B
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2
2
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1
0
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One may be inoperative provided: a) Autopilot is not used below 1,500 feet AGL, and b) Approach minimums do not require the use of the Autopilot.
May be inoperative provided Autopilot is not used. |
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| U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION |
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| AIRCRAFT: TWIN COMMANDER AIRCRAFT 680T/680V/680W/681/690/690A 690B/690C/690D/695/695A/695B |
REVISION NO: 7
DATE: 09/09/2009 |
PAGE NO:
23-1 |
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| 1. SYSTEM, SEQUENCE NUMBERS & ITEM |
REPAIR CATEGORY |
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2. NUMBER INSTALLED |
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3. NUMBER REQUIRED FOR DISPATCH |
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4. REMARKS AND EXCEPTIONS |
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| 23 |
COMMUNICATIONS |
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| 1. |
Communications System (VHF And UHF) |
D |
- |
- |
Any in excess of those required by 14 CFR may be inoperative provided it is not powered by any Emergency Power Source and not required for emergency procedures. |
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| 2. |
Cockpit Speaker |
C |
2 |
0 |
May be inoperative provided two operative Headsets are available to the flight crew. |
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| 3. |
Audio Amplifier |
C |
2 |
0 |
May be inoperative provided two operative Headsets are available to the flight crew. |
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| 4. |
Passenger Address System (PA) |
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| A) |
Passenger Configuration |
C
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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. |
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| B) |
Cargo Configuration |
D
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1
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0
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May be inoperative provided procedures do not require its use. |
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| U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION |
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| AIRCRAFT: TWIN COMMANDER AIRCRAFT 680T/680V/680W/681/690/690A 690B/690C/690D/695/695A/695B |
REVISION NO: 7
DATE: 09/09/2009 |
PAGE NO:
23-2 |
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| 1. SYSTEM, SEQUENCE NUMBERS & ITEM |
REPAIR CATEGORY |
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2. NUMBER INSTALLED |
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3. NUMBER REQUIRED FOR DISPATCH |
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4. REMARKS AND EXCEPTIONS |
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| 23 |
COMMUNICATIONS |
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| 5. |
Cockpit Voice Recorder (CVR) |
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| A) |
For Air Carrier And Commercial Operators |
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| 1) |
With Flight Data Recorder (FDR) Installed |
A |
1 |
0 |
May be inoperative provided: a) Flight Data Recorder (FDR) operates normally, and b) Repairs are made within three flight days. |
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| 2) |
Without Flight Data Recorder (FDR) Installed |
A |
1 |
0 |
May be inoperative provided repairs are made within three flight days. |
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| B) |
For Operators Other Than Air Carriers And Commercial Operators |
A |
1 |
0 |
May be inoperative provided repairs are made in accordance with applicable sections of 14 CFR. |
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| 6. |
Boom Microphones |
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| A) |
Cockpit Voice Recorder With Flight Data Recorder Installed |
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| 1) |
Cockpit Voice Recorder Equipped To Record Boom Microphone Per 14 CFR 135.151(d) |
A |
- |
0 |
May be inoperative provided: a) Flight Data Recorder (FDR) operates normally, and b) Repairs are made within three flight days. |
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| 2) *** |
Cockpit Voice Recorder Not Equipped To Record Boom Microphone |
D |
- |
0 |
Any in excess of those required by 14 CFR may be inoperative. |
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(Continued) |
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| U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION |
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| AIRCRAFT: TWIN COMMANDER AIRCRAFT 680T/680V/680W/681/690/690A 690B/690C/690D/695/695A/695B |
REVISION NO: 7
DATE: 09/09/2009 |
PAGE NO:
23-3 |
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| 1. SYSTEM, SEQUENCE NUMBERS & ITEM |
REPAIR CATEGORY |
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2. NUMBER INSTALLED |
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3. NUMBER REQUIRED FOR DISPATCH |
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4. REMARKS AND EXCEPTIONS |
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| 23 |
COMMUNICATIONS |
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| 6. |
Boom Microphones (Continued) |
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| B) |
Cockpit Voice Recorder Without Flight Data Recorder Installed |
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| 1) |
Cockpit Voice Recorder Equipped To Record Boom Microphone Per 14 CFR 135.151(d) |
A |
- |
0 |
May be inoperative provided repairs are made within three flight days. |
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| 2) *** |
Cockpit Voice Recorder Not Equipped To Record Boom Microphones |
D |
- |
0 |
Any in excess of those required by 14 CFR may be inoperative. |
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| 7. |
High Frequency (HF) Communication System |
D
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-
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-
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Any in excess of those required by 14 CFR may be inoperative. |
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C |
- |
1 |
(O) May be inoperative while conducting operations that require two LRCS provided: a) SATCOM Voice or Data Link operates normally, b) Alternate procedures are established and used, c) SATCOM coverage is available over the intended route of flight, and d) If INMARSAT Codes are not available while using SATCOM Voice prior coordination with the appropriate ATS facility is required. |
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(Continued) |
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| U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION |
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| AIRCRAFT: TWIN COMMANDER AIRCRAFT 680T/680V/680W/681/690/690A 690B/690C/690D/695/695A/695B |
REVISION NO: 7
DATE: 09/09/2009 |
PAGE NO:
23-4 |
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| 1. SYSTEM, SEQUENCE NUMBERS & ITEM |
REPAIR CATEGORY |
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2. NUMBER INSTALLED |
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3. NUMBER REQUIRED FOR DISPATCH |
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4. REMARKS AND EXCEPTIONS |
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| 23 |
COMMUNICATIONS |
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| 7. |
High Frequency (HF) Communication System (Continued) |
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NOTE: SATCOM is to be used only as a backup to normal HF communications unless otherwise authorized by the appropriate ATS facilities. |
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| 8. |
Selective Call Systems (SELCAL) |
C |
- |
0 |
(O) May be inoperative provided alternate procedures are established and used. |
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D |
- |
0 |
May be inoperative provided procedures do not require its use. |
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| A) |
Channels |
C |
- |
0 |
(O) May be inoperative provided alternate procedures are established and used. |
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D |
- |
0 |
May be inoperative provided procedures do not require its use. |
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| U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION |
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| AIRCRAFT: TWIN COMMANDER AIRCRAFT 680T/680V/680W/681/690/690A 690B/690C/690D/695/695A/695B |
REVISION NO: 7
DATE: 09/09/2009 |
PAGE NO:
24-1 |
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| 1. SYSTEM, SEQUENCE NUMBERS & ITEM |
REPAIR CATEGORY |
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2. NUMBER INSTALLED |
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3. NUMBER REQUIRED FOR DISPATCH |
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4. REMARKS AND EXCEPTIONS |
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| 24 |