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U.S. Department of Transportation Federal Aviation Administration Washington , D.C. |
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| Master Minimum Equipment List |
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| Revision: 14b |
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| Date: 08/27/2010 |
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| Hawker Beechcraft Corporation |
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| Beechcraft Model 200 and F90
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| Applicable Models: 200 / 200C / 200CT / 200T / A100-1 / A200 / A200C / A200CT B200 / B200C / B200CT / B200T / B200GT / B200CGT and F90 |
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| Johnathon A Vetter, Chairman |
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| Flight Operations Evaluation Board (FOEB) |
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| Federal Aviation Administration |
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| 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: Beechcraft Model 200 and F-90 |
REVISION NO: 14b DATE: 08/27/2010 |
PAGE NO. I |
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| TABLE OF CONTENTS |
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| SYSTEM NO. |
SYSTEM |
PAGE NO. |
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Table of Contents |
I |
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Log of Revisions |
II, III, IV |
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Control Page |
V, VI, VII |
| -- |
Highlights of Change |
VIII |
| -- |
Definitions |
IX |
| -- |
Preamble |
X |
| -- |
Guidelines for (O) & (M) Procedures |
XI THRU XVIII |
| 21 |
Air Conditioning |
21-1, 2, 3 |
| 22 |
Auto Flight |
22-1, 2, 3 |
| 23 |
Communications |
23-1 THRU 23-6 |
| 24 |
Electrical Power |
24-1, 2 |
| 25 |
Equipment/Furnishings |
25-1 THRU 25-7 |
| 26 |
Fire Protection |
26-1, 2 |
| 27 |
Flight Controls |
27-1 |
| 28 |
Fuel |
28-1, 2 |
| 30 |
Ice and Rain Protection |
30-1, 2, 3, 4, 5 |
| 31 |
Indicating/Recording Systems |
31-1, 2 |
| 32 |
Landing Gear |
32-1 |
| 33 |
Lights |
33-1, 2, 3 |
| 34 |
Navigation |
34-1 THRU 34-15 |
| 35 |
Oxygen |
35-1 |
| 37 |
Vacuum/Pressure |
37-1 |
| 46 |
Information Systems |
46-1, 2 |
| 52 |
Doors |
52-1 |
| 61 |
Propellers |
61-1 |
| 73 |
Engine Fuel & Control |
73-1 |
| 77 |
Engine Indicating |
77-1 |
| 79 |
Engine Oil |
79-1 |
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| U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION |
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| AIRCRAFT: Beechcraft Model 200 and F-90 |
REVISION NO: 10 DATE: 04/08/2002 |
PAGE NO: II |
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| Log of Revisions |
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| Rev No. |
Date |
Page Numbers |
Initials |
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| 0 |
02/27/1980 |
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| 1 |
11/04/1981 |
Pen & Ink change to add Beech |
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B200C after the 200CT |
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| 2 |
02/01/1982 |
Pen & Ink change to include |
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Beech F-90 |
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| 3 |
11/10/1983 |
All pages |
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| 4 |
07/30/1984 |
28-1 |
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| 5 |
03/09/1988 |
All pages |
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| 6 |
07/07/1988 |
Page 21-2 |
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| 7 |
03/16/1989 |
All pages |
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| 8 |
06/19/1989 |
DEFINITIONS, PREAMBLE |
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| 8a |
04/16/1991 |
HIGHLIGHTS OF REV., DEFINITIONS |
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| 8a |
04/16/1991 |
23-1 |
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| 8b |
01/13/1992 |
HIGHLIGHTS OF REV., GUIDELINES |
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| 8b |
01/13/1992 |
22-1 |
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| 9 |
07/08/1994 |
HIGHLIGHTS OF REV., DEFINITIONS |
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| 9 |
07/08/1994 |
GUIDELINES |
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| 9 |
07/08/1994 |
21-1, 21-2, 22-1, 23-1, 23-2 |
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| 9 |
07/08/1994 |
24-1, 25-1, 25-2, 26-1, 27-1 |
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| 9 |
07/08/1994 |
28-1, 28-2, 30-1, 30-2, 31-1 |
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| 9 |
07/08/1994 |
32-1, 33-1, 33-2, 34-1, 34-2 |
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| 9 |
07/08/1994 |
34-3, 34-4, 34-5, 34-6, 35-1 |
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| 9 |
07/08/1994 |
52-1, 61-1 |
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| 9a |
08/17/1994 |
HIGHLIGHTS OF REV. |
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| 9a |
08/17/1994 |
23-2 |
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| 9b |
10/20/1994 |
HIGHLIGHTS OF REV. |
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| 9b |
10/20/1994 |
35-1 |
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| 9c |
03/17/1999 |
HIGHLIGHTS OF REV., DEFINITIONS |
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| 9c |
03/17/1999 |
GUIDELINES |
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| 9c |
03/17/1999 |
23-1, 25-1, 25-2, 26-1, 33-1 |
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| 9c |
03/17/1999 |
33-2, 34-1, 34-2, 34-3, 34-4 |
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| 9c |
03/17/1999 |
34-5, 34-6, 34-7, 61-1 |
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| 9d |
10/12/1999 |
HIGHLIGHTS OF REV., DEFINITIONS |
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| 9d |
10/12/1999 |
PREAMBLE, GUIDELINES |
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| 9d |
10/12/1999 |
34-7, 61-1 |
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| 9e |
09/27/2000 |
HIGHLIGHTS OF REV., DEFINITIONS |
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| 9e |
09/27/2000 |
GUIDELINES |
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| 9e |
09/27/2000 |
33-2, 34-1, 34-2, 34-3, 34-4 |
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| 9e |
09/27/2000 |
34-5, 34-6, 34-7, 34-8, 34-9 |
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| 10 |
04/08/2002 |
HIGHLIGHTS OF REV., DEFINITIONS |
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| 10 |
04/08/2002 |
GUIDELINES |
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| 10 |
04/08/2002 |
21-1, 21-2, 22-1, 23-1, 23-2 |
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| 10 |
04/08/2002 |
23-3, 24-1, 25-1, 25-2, 25-3 |
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| U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION |
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| AIRCRAFT: Beechcraft Model 200 and F-90 |
REVISION NO: 13 DATE: 8/17/2004 |
PAGE NO: III |
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| Log of Revisions |
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| Rev No. |
Date |
Page Numbers |
Initials |
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| 10 |
04/08/2002 |
26-1, 26-2, 27-1, 28-1, 28-2 |
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| 10 |
04/08/2002 |
30-1, 30-2, 31-1, 32-1, 33-1 |
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| 10 |
04/08/2002 |
33-2, 34-1, 34-2, 34-3, 34-4 |
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| 10 |
04/08/2002 |
34-5, 34-6, 34-7, 34-8, 34-9 |
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| 10 |
04/08/2002 |
34-10, 34-11, 35-1, 52-1, 61-1 |
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| 11 |
03/31/2003 |
HIGHLIGHTS OF REV., DEFINITIONS |
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| 11 |
03/31/2003 |
GUIDELINES |
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| 11 |
03/31/2003 |
21-1, 21-2, 21-3, 22-1, 22-2 |
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| 11 |
03/31/2003 |
23-1, 23-2, 23-3, 23-4, 24-1 |
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| 11 |
03/31/2003 |
24-2, 25-1, 25-2, 25-3, 25-4 |
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| 11 |
03/31/2003 |
25-5, 26-1, 26-2, 26-3, 27-1 |
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| 11 |
03/31/2003 |
27-2, 28-1, 28-2, 30-1, 30-2 |
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| 11 |
03/31/2003 |
30-3, 31-1, 32-1, 33-1, 33-2 |
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| 11 |
03/31/2003 |
33-3, 34-1, 34-2, 34-3, 34-4 |
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| 11 |
03/31/2003 |
34-5, 34-6, 34-7, 34-8, 34-9 |
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| 11 |
03/31/2003 |
34-10, 34-11, 34-12, 34-13, 34-14 |
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| 11 |
03/31/2003 |
34-15, 34-16, 35-1, 37-1, 52-1 |
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| 11 |
03/31/2003 |
61-1, 77-1, 79-1 |
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| 12 |
11/03/2003 |
HIGHLIGHTS OF REV., DEFINITIONS |
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| 12 |
11/03/2003 |
GUIDELINES |
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| 12 |
11/03/2003 |
21-1, 21-2, 21-3, 22-1, 22-2 |
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| 12 |
11/03/2003 |
23-1, 23-2, 23-3, 23-4, 23-5 |
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| 12 |
11/03/2003 |
23-6, 24-1, 24-2, 25-1, 25-2 |
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| 12 |
11/03/2003 |
25-3, 25-4, 25-5, 26-1, 26-2 |
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| 12 |
11/03/2003 |
26-3, 27-1, 27-2, 28-1, 28-2 |
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| 12 |
11/03/2003 |
30-1, 30-2, 30-3, 30-4, 32-1 |
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| 12 |
11/03/2003 |
33-1, 33-2, 33-3, 34-1, 34-2 |
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| 12 |
11/03/2003 |
34-3, 34-4, 34-5, 34-6, 34-7 |
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| 12 |
11/03/2003 |
34-8, 34-9, 34-10, 34-11 |
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| 12 |
11/03/2003 |
34-12, 34-13, 34-14, 34-15 |
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| 12 |
11/03/2003 |
34-16, 35-1, 37-1, 52-1 |
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| 12 |
11/03/2003 |
61-1, 77-1, 79-1 |
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| 12a |
02/25/2004 |
HIGHLIGHTS OF REV., DEFINITIONS |
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| 12a |
02/25/2004 |
GUIDELINES |
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| 12a |
02/25/2004 |
27-1, 79-1 |
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| 13 |
08/17/2004 |
HIGHLIGHTS OF REV., DEFINITIONS |
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| 13 |
08/17/2004 |
GUIDELINES |
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| 13 |
08/17/2004 |
21-3, 22-1, 22-2, 23-2, 24-1 |
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| 13 |
08/17/2004 |
24-2, 25-3, 25-4, 26-3, 27-1 |
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| 13 |
08/17/2004 |
28-2, 30-1, 30-2, 30-3, 30-4 |
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| 13 |
08/17/2004 |
30-5, 34-1, 34-2, 34-3, 34-4 |
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| 13 |
08/17/2004 |
34-5, 34-6, 34-7, 34-8, 34-9 |
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| 13 |
08/17/2004 |
34-10, 34-11, 34-12, 34-13 |
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| 13 |
08/17/2004 |
34-14, 34-15, 34-16, 34-17 |
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| U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION |
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| AIRCRAFT: Beechcraft Model 200 and F-90 |
REVISION NO: 14b DATE: 08/27/2010 |
PAGE NO: IV |
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| Log of Revisions |
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| Rev No. |
Date |
Page Numbers |
Initials |
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| 14 |
09/16/2008 |
HIGHLIGHTS OF REV., DEFINITIONS |
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| 14 |
09/16/2008 |
GUIDELINES |
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| 14 |
09/16/2008 |
21-1, 21-2, 21-3, 22-1, 22-2, 23-1, 23-2, 23-3, |
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| 14 |
09/16/2008 |
23-4, 23-5, 23-6, 24-1, 24-2, 25-2, 25-3, 25-4, |
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| 14 |
09/16/2008 |
25-5, 25-6, 25-7, 26-2, 27-1, 28-1, 28-2, 30-2, |
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| 14 |
09/16/2008 |
30-3, 30-4, 30-5, 31-1, 31-2,32-1, 33-1, 33-2, |
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| 14 |
09/16/2008 |
33-3, 34-1, 34-2, 34-3, 34-4, 34-5, 34-6, 34-7, |
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| 14 |
09/16/2008 |
34-8, 34-9, 34-10, 34-11, 34-12, 34-13, 34-14, |
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| 14 |
09/16/2008 |
34-16, 35-1, 46-1, 46-2, 52-1, 61-1, 73-1, 77-1 |
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| 14 |
09/16/2008 |
79-1 |
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| 14a |
06/04/2010 |
Highlights of Change, Definitions, Preamble |
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| 14a |
06/04/2010 |
Guidelines for (O) & (M), 21-2, 22-1, 34-5, 37-1 |
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| 14b |
08/27/2010 |
Highlights of Change, 22-1, 22-2, 22-3, 27-1, |
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| 14b |
08/27/2010 |
28-1, 30-1, 30-2, 34-1, 34-2, 34-4, 34-5, 34-6, |
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| 14b |
08/27/2010 |
34-7, 34-8, 34-9, 34-10, 34-11, 34-12, 34-13, |
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| 14b |
08/27/2010 |
34-14, 34-15, 37-1, 46-2, 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: Beechcraft Model 200 and F-90 |
REVISION NO: 14b DATE: 08/27/2010 |
PAGE NO: V |
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| Control Page |
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| System |
Page No. |
Rev. No. |
Current Date |
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| Cover Page |
- |
14b |
08/27/2010 |
| Table of Contents |
I |
14b |
08/27/2010 |
| Log of Revisions |
II |
10 |
04/08/2002 |
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III |
13 |
08/17/2004 |
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IV |
14b |
08/27/2010 |
| Control Page |
V |
14b |
08/27/2010 |
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VI |
14b |
08/27/2010 |
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VII |
14b |
08/27/2010 |
| Highlights of Change |
VIII |
14b |
08/27/2010 |
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VIIIa |
14b |
08/27/2010 |
| Definitions |
IX |
14a |
06/04/2010 |
| Preamble |
X |
14a |
06/04/2010 |
| Guidelines for (O) & (M) Procedures |
XI |
14b |
08/27/2010 |
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XII |
14b |
08/27/2010 |
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XIII |
14b |
08/27/2010 |
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XIV |
14b |
08/27/2010 |
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XV |
14b |
08/27/2010 |
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XVI |
14b |
08/27/2010 |
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XVII |
14b |
08/27/2010 |
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XVIII |
14b |
08/27/2010 |
| 21 |
21-1 |
14 |
09/16/2008 |
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21-2 |
14a |
06/04/2010 |
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21-3 |
14 |
09/16/2008 |
| 22 |
22-1 |
14b |
08/27/2010 |
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22-2 |
14b |
08/27/2010 |
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22-3 |
14b |
08/27/2010 |
| 23 |
23-1 |
14 |
09/16/2008 |
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23-2 |
14 |
09/16/2008 |
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23-3 |
14 |
09/16/2008 |
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23-4 |
14 |
09/16/2008 |
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23-5 |
14 |
09/16/2008 |
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23-6 |
14 |
09/16/2008 |
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| U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION |
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| AIRCRAFT: Beechcraft Model 200 and F-90 |
REVISION NO: 14b DATE: 08/27/2010 |
PAGE NO: VI |
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| Control Page |
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| System |
Page No. |
Rev. No. |
Current Date |
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| 24 |
24-1 |
14 |
09/16/2008 |
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24-2 |
14 |
09/16/2008 |
| 25 |
25-1 |
12 |
11/03/2003 |
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25-2 |
14 |
09/16/2008 |
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25-3 |
14 |
09/16/2008 |
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25-4 |
14 |
09/16/2008 |
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25-5 |
14 |
09/16/2008 |
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25-6 |
14 |
09/16/2008 |
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25-7 |
14 |
09/16/2008 |
| 26 |
26-1 |
12 |
11/03/2003 |
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26-2 |
14 |
09/16/2008 |
| 27 |
27-1 |
14b |
08/27/2010 |
| 28 |
28-1 |
14b |
08/27/2010 |
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28-2 |
14 |
09/16/2008 |
| 30 |
30-1 |
14b |
08/27/2010 |
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30-2 |
14b |
08/27/2010 |
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30-3 |
14 |
09/16/2008 |
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30-4 |
14 |
09/16/2008 |
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30-5 |
14 |
09/16/2008 |
| 31 |
31-1 |
14 |
09/16/2008 |
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31-2 |
14 |
09/16/2008 |
| 32 |
32-1 |
14 |
09/16/2008 |
| 33 |
33-1 |
14 |
09/16/2008 |
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33-2 |
14 |
09/16/2008 |
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33-3 |
14 |
09/16/2008 |
| 34 |
34-1 |
14b |
08/27/2010 |
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34-2 |
14b |
08/27/2010 |
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34-3 |
14 |
09/16/2008 |
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34-4 |
14b |
08/27/2010 |
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34-5 |
14b |
08/27/2010 |
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34-6 |
14b |
08/27/2010 |
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34-7 |
14b |
08/27/2010 |
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34-8 |
14b |
08/27/2010 |
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34-9 |
14b |
08/27/2010 |
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34-10 |
14b |
08/27/2010 |
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34-11 |
14b |
08/27/2010 |
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34-12 |
14b |
08/27/2010 |
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34-13 |
14b |
08/27/2010 |
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34-14 |
14b |
08/27/2010 |
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34-15 |
14b |
08/27/2010 |
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| U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION |
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| AIRCRAFT: Beechcraft Model 200 and F-90 |
REVISION NO: 14b DATE: 08/27/2010 |
PAGE NO: VII |
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| Control Page |
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| System |
Page No. |
Rev. No. |
Current Date |
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| 35 |
35-1 |
14 |
09/16/2008 |
| 37 |
37-1 |
14b |
08/27/2010 |
| 46 |
46-1 |
14 |
09/16/2008 |
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46-2 |
14b |
08/27/2010 |
| 52 |
52-1 |
14b |
08/27/2010 |
| 61 |
61-1 |
14b |
08/27/2010 |
| 73 |
73-1 |
14 |
09/16/2008 |
| 77 |
77-1 |
14 |
09/16/2008 |
| 79 |
79-1 |
14 |
09/16/2008 |
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| U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION |
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| AIRCRAFT: Beechcraft Model 200 and F-90 |
REVISION NO: 14b DATE: 08/27/2010 |
PAGE NO. VIII |
| HIGHLIGHTS OF CHANGE |
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| The following changes are the Highlights of Changes for Revision 14a. |
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| Definitions |
Revised to reference the source document for definitions to avoid duplication of changes published to definitions policy letter. |
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| Preamble |
Revised to reference the source document for Preambles, both certificated operators and Part 91 operators, to discontinue publication of duplicate MMELs for differences in the Preambles. |
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| 21-8 |
Delete duplicate relief for Instrument Air Bleed Shutoff Valves and add cross-reference to Chapter 37. |
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| 22-2 |
Yaw Damper (F-90 with STC SA4130NM) correct error for Number Required to “0” |
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| 22-3 |
Add applicability for Garmin GFC-700 AFCS to maintain at least 1 Control Wheel Disconnect Button for Garmin autopilot system. |
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| 34-13 |
Specify applicability of Remarks to Class A TAWS and TCAS II only. |
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| 37-2 |
Instrument Air Valves Remarks changed to add an (M) procedure per duplicate 21-8 relief to secure valve because a malfunctioning valve is unreliable to simply switch OFF. |
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| The following changes are the Highlights of Changes for Revision 14b. |
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Revision 14b incorporates Model 200 HDC MMEL Revision 2. |
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| 22-2 |
Yaw Damper (200 HDC) Added model. |
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| 22-6 |
Flight Director relief relocated to chapter 22 |
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| 22-6-a |
Flight Director Mode Selection Panel Annunciator Lamps become Sub-Item |
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| 27-4 |
Add RVSM NOTE |
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| 28-1 |
Add applicability for 200HDC to Standby Boost Pump |
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| 30-2 |
Revise Ice Vane Annunciator Remarks to verify operative. |
|
|
|
| 30-5 |
Revise Pitot Heat Remarks to correct format and separate relief criteria. |
|
|
|
| U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION |
||
| AIRCRAFT: Beechcraft Model 200 and F-90 |
REVISION NO: 14b DATE: 08/27/2010 |
PAGE NO. VIIIa |
| HIGHLIGHTS OF CHANGE |
||
|
|
|
| 34-1 & 2 |
Revised Remarks to stipulate Electronic Air Data System instead of EFIS to correct unnecessary exclusion of Proline 2 equipped aircraft. |
|
|
|
| 34-4 |
Revised Turn/Slip Remarks to remove EFIS restriction because not applicable for right side instruments and Day VFR is mitigation for left side. |
|
|
|
| 34-8 |
Navigation Equipment reformatted into sub items and Remarks revised to address operational considerations: VOR/ILS TACAN Systems, Glide Slope, Marker Beacon System, DME, RNAV, ADF, RMI and FMS are Navigation Equipment sub items. |
|
|
|
| 34-9-1 |
Add relief for Radar Stabilization to WX Radar. |
|
|
|
| 34-11 |
Radar Altimeter relief renumbered and Remarks changed to accommodate variable installations. |
|
|
|
| 34-12 |
Altitude Alerting System relief renumbered |
| 34-13 |
Gyro-magnetic Compass System relief renumbered |
| 34-14 |
Non-Stabilized Magnetic Compass relief renumbered |
| 34-15 & 16 |
Traffic Alert Collision Avoidance System relief renumbered |
| 34-17 |
TAWS/GPWS relief renumbered |
| 34-18 |
Traffic Awareness System (TCAD/TAS relief renumbered |
| 34-19 |
Ground Proximity Altitude Advisory System (GPAAS) relief renumbered |
|
|
|
| 34-20 |
Standby Attitude Indicator relief renumbered and Remarks revised to account for Standby Attitude Indicator required by Type Design Approvals. |
|
|
|
| 34-21 |
Flight Profile Advisory System relief renumbered |
| 34-22 |
Independent Multi-Function Display relief renumbered |
| 34-23 & 24 |
Windshear relief renumbered |
|
|
|
| 34-25 |
ADS-B relief renumbered and undated per PL-105 |
|
|
|
| 37-2 |
Instrument Air Valves Remarks changed to (O) procedure because no mechanical means to secure valve closed. Valve must be powered closed. |
|
|
|
| 46-3 |
XM Weather System is renumbered to 3. to allow relief to be used for non-IFIS-5000 independent systems and changed to Category D. |
|
|
|
| 52-6 |
Added 200 HDC Baggage Pod Door Warning Light |
|
|
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| 61-1 |
Add applicability to Reverse not Ready to exclude A200CT. |
|
|
|
| U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION |
||
| AIRCRAFT: Beechcraft Model 200 and F-90 |
REVISION NO: 14a DATE: 06/04/2010 |
PAGE: IX |
| DEFINITIONS |
||
The Definitions must be inserted here in each Minimum Equipment List (MEL) from current FAA MMEL Policy Letter PL-25, MMEL DEFINITIONS in accordance with current FAA MMEL Policy Letter PL-70, DEFINITIONS REQUIRED IN MELs.
| U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION |
||
| AIRCRAFT: Beechcraft Model 200 and F-90 |
REVISION NO: 14a DATE: 06/04/2010 |
PAGE NO. X |
| PREAMBLE |
||
The applicable Preamble must be inserted here in each Minimum Equipment List (MEL) from current FAA MMEL Policy Letter PL-34, MMEL AND MEL PREAMBLE or PL-36, FAR PART 91MEL APPROVAL AND PREAMBLE.
| U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION |
||
| AIRCRAFT: Beechcraft Model 200 and F-90 |
REVISION NO: 14b DATE: 08/27/2010 |
PAGE NO. XI |
| Guidelines for (O) & (M) Procedures |
||
The FOEB has identified a need for certain procedures to provide an adequate level of safety while providing relief for the following items. These procedures must be established by the operator. The following guidelines are to help establish these required procedures:
| 21-1 |
(O) Procedure to ensure compliance with regulations, operational requirements and passenger briefing information for unpressurized flight.
|
| 21-2 |
(M) Maintenance procedure to ensure the Safety Valve (Dump) is secured in the open position.
|
| (O) Procedure to ensure compliance with regulations, operational requirements and passenger briefing information for unpressurized flight.
|
|
| 21-3 |
(M) Maintenance procedure to ensure the Safety Valve (Dump) is secured in the open position.
|
| (O) Procedure to ensure compliance with regulations, operational requirements and passenger briefing information for unpressurized flight
|
|
| 21-4,5,6 |
(O) Procedure to ensure compliance with regulations, operational requirements and passenger briefing information for unpressurized flight.
|
| 21-7 |
(M) Maintenance procedure to determine Bleed Air Shutoff Valve(s) are secure in the closed position.
|
| (O) Procedure to ensure compliance with regulations, operational requirements and passenger briefing information for unpressurized flight.
|
|
| 21-9 |
(M) Maintenance procedure to determine Bleed Air Shutoff Valve(s) are secure in the closed position.
|
| (O) Procedure to ensure compliance with regulations, operational requirements and passenger briefing information for unpressurized flight.
|
|
| 21-14 |
(M) Maintenance procedure to deactivate and secure Air Conditioner. |
| 21-16-1 |
(O) Procedure to verify affected Environmental and Instrument Bleed Air Valves are selected OFF and verified closed prior to each flight.
|
| U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION |
||
| AIRCRAFT: Beechcraft Model 200 and F-90 |
REVISION NO: 14b DATE: 08/27/2010 |
PAGE NO. XII |
| Guidelines for (O) & (M) Procedures |
||
| 21-16-2 |
(O) Procedure to verify affected Environmental and Instrument Bleed Air Valves are selected OFF and verified closed prior to each flight.
|
| 21-18 & 19 |
(O) Procedure to ensure compliance with regulations, operational requirements and passenger briefing information for unpressurized flight.
|
| 22-1 |
(M) Maintenance procedure to deactivate the autopilot and ensure no electrical or mechanical fault exists that will have an adverse affect on any Flight Control function.
|
| 22-2 |
(M) Maintenance procedure to deactivate the Yaw Damper and ensure no electrical or mechanical fault exists that will have an adverse affect on any Flight Control function.
|
| 22-3 |
(M) Maintenance procedure to deactivate & secure autopilot and electric trim.
|
| 22-4 |
(O) Procedure to establish alternate method to accomplish a go-around.
|
| 22-5 |
(O) Operations procedure to verify prior to departure, the proper Autopilot Mode Annunciation is displayed on the pilot's panels(s).
|
| 22-6-a |
(O) Operations procedure to verify, prior to departure, the proper Autopilot Mode Annunciation is displayed on the pilot's panels(s).
|
| 22-7 |
(O) Operations procedure to verify, prior to departure, the proper Autopilot Mode Annunciation is displayed on the pilot's panel(s).
|
| 23-2-1 |
(O) Operations procedure to specify how passengers will be briefed for normal and emergency operation.
|
| 23-3 |
(O) Operations procedure to ensure aural warnings are available. NOTE: An acceptable test would be to activate the Stall Warning System.
|
| 23-10 |
(O) Operations procedure to ensure SATCOM Data Link System operates normally.
|
| 23-11 |
(O) Operations procedure to ensure passengers are briefed prior to departure.
|
| 23-16 |
(O) Procedure to provide alternate means to maintain contact with aircraft. |
| 23-16-1 |
(O) Procedure to provide alternate means to maintain contact with aircraft. |
| 24-7 |
(M) Maintenance procedure to deactivate and secure the Cabin AC Power System. |
| U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION |
||
| AIRCRAFT: Beechcraft Model 200 and F-90 |
REVISION NO: 14b DATE: 08/27/2010 |
PAGE NO. XIII |
| Guidelines for (O) & (M) Procedures |
||
| 24-8 |
(M) Maintenance procedure to disconnect and remove the Standby Battery. |
| 24-9 |
(M) Maintenance procedure to placard and secure access to the aircraft External Power Receptacle.
|
| 24-10 |
(O) Operations procedure to verify connection and disconnection of External Power Supply.
|
| 24-12 |
(O) Operations procedure to verify Generator Bus Tie Relay is CLOSED and both DC GEN Annunciators are operative prior to departure.
|
| 25-1-1 |
(M) Maintenance procedure to secure the affected Arm Rest(s) in the full up or full down position.
|
| 25-1-4 |
(M) Maintenance procedure to secure the affected Seat in a position acceptable to the flight crew allowing for full Flight Control movement and normal pilot visibility.
|
| 25-2-1 |
(M) Maintenance procedure to secure Seat in the full upright position.
|
| 25-5-2-a |
(M) Maintenance procedure to disconnect Remote Switch and verify ELT is armed.
|
| 25-10 |
(M) Maintenance procedure to ensure the affected Receptacle is empty and secured to prevent use.
|
| (O) Operations procedure to ensure a sufficient number of Receptacles are available for the flight.
|
|
| 25-11 |
(M) Maintenance procedure to ensure inoperative Cargo Restraints are isolated from use and Cargo Loading Limits are observed for remaining restraints.
|
| 25-12 |
(M) Maintenance procedure to secure the affected compartment closed.
|
| (M) Maintenance procedure to remove the affected compartment door(s)
|
|
| (O) Operations procedure to ensure crew awareness and passenger briefing regarding use of affected storage compartment.
|
|
| 25-12-1 |
(M) Maintenance procedure to ensure door latch is operable.
|
| 25-13 |
(M) Maintenance procedure to remove or deactivate/secure inoperative System or equipment.
|
| (O) Operations procedure to ensure crew awareness of inoperative equipment. |
| U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION |
||
| AIRCRAFT: Beechcraft Model 200 and F-90 |
REVISION NO: 14b DATE: 08/27/2010 |
PAGE NO. XIV |
| Guidelines for (O) & (M) Procedures |
||
| 25-14 |
(M) Maintenance procedure to deactivate and secure the inoperative System.
|
| 25-18 |
(M) Maintenance procedure to secure the Cockpit and/or Cabin Partition Doors / Curtains in the full open position or to remove Doors / Curtains.
|
| 26-4 |
(O) Operations procedure to ensure Lavatory is locked closed and accessed only by crewmembers.
|
| (M) Maintenance Procedure to ensure Lavatory Waste Receptacle is empty and Door is placarded.
|
|
| 27-1 |
(O) Procedure to provide method to check trim tab for full range of motion and ensure there is no restriction to movement.
|
| 27-2 |
(O) Procedure to provide method to verify full flap travel and correct intermediate flap settings.
|
| 27-4 27-4-3 |
(M) Maintenance procedure to deactivate the Electric Trim and ensure Manual Trim is operative.
|
| 28-1 |
(M) Procedure to deactivated and secure affected Standby Fuel Boost Pump.
|
| 28-5 |
(M) Maintenance procedure to ensure there are no fuel leaks or restrictions to fuel flow associated with the Fuel Counter / Totalizer malfunction.
|
| 28-6 |
(O) Operations procedure to ensure the quantity and balance of fuel on board meets the regulatory requirements for the intended flight and fuel balance is maintained throughout flight.
|
| 28-9 |
(O) Operations procedure to ensure Standby Electric Boost Pump is turned on and verified operative.
|
| (M) Procedure to determine there is no fuel leak, the Low Pressure Pump has disconnected (shaft has sheared), pump failure did not introduce debris into the fuel system, and the Fuel Pressure Low annunciator is extinguished by use of the Standby Electric Fuel Pump with the engine operating at takeoff power.
|
|
| 30-2 |
(O) Operations procedure to verify operation of the Anti-Ice Vanes prior to each departure. |
| (M) Maintenance procedure to secure Anti-Ice Vanes in the full extended position. |
|
| (O) Operations procedure to ensure that Surface Temperatures and Ice Vane Extended Performance Charts are considered. |
|
| (M) Maintenance procedure to secure the Anti-Ice Vanes in the full extended position. |
| U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION |
||
| AIRCRAFT: Beechcraft Model 200 and F-90 |
REVISION NO: 14b DATE: 08/27/2010 |
PAGE NO. XV |
| Guidelines for (O) & (M) Procedures |
||
| 30-5-1 |
(O) Procedure to verify each pitot mast heat is operative prior to each flight.
|
| 30-10-1-a |
(O) Operations procedure to ensure aircraft is not operated in visible moisture 5 degrees Celsius or below.
|
| (M) Maintenance procedure to manually extend and secure the Anti-Ice Vanes in the fully extended position.
|
|
| (O) Operations procedure to ensure Ice Vanes Extended performance data is used.
|
|
| 30-10-1-b |
(O) Operations procedure to ensure that is not operated in visible moisture 5 degrees Celsius or below.
|
| 30-10- 2- a & -b |
(M) Maintenance procedure to ensure the Anti-Ice Vanes are secured in the fully extended position.
|
| (O) Procedure to ensure that Surface Temperatures and Performance Charts with Ice Vanes Extended are considered.
|
|
| 30-10-2-c |
(M) Maintenance procedure to manually extend and secure the Anti-Ice Vanes in the fully extended position.
|
| 31-2 |
(O) Operations procedure to record flight time.
|
| 31-7 |
(O) Establish alternate procedure to collect engine trend monitoring data. |
| 32-1 |
(O) Operations procedure to prevent movement of aircraft when stopped or parked.
|
| 32-2 |
(M) Maintenance procedure to deactivate Brake Deice and ensure Rudder Boost remains operative.
|
| 32-5 |
(M) Maintenance procedure to verify proper hydraulic fluid level prior to first flight of each day.
|
| 32-6 |
(O) Operations procedure to ensure flight crew awareness of the requirement to manually release the Down Lock Latch.
|
| 33-1 |
(O) Operations procedure to identify minimum sufficient operative lighting for the crew to perform required duties and for passengers to locate items and move safely about the cabin during night operations.
|
| U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION |
||
| AIRCRAFT: Beechcraft Model 200 and F-90 |
REVISION NO: 14b DATE: 08/27/2010 |
PAGE NO. XVI |
| Guidelines for (O) & (M) Procedures |
||
| 33-4 |
(O) Operations procedure to appropriately brief the passengers.
|
|
| 34-2-1 |
(O) Operations procedure to ensure crew awareness of specific airspeed information.
|
|
| 34-8-3-a |
(O) Procedure to ensure current navigation charts are available and used, status of applicable Navigation Facilities are verified, Navigation Radios are tuned manually, and flight planning is not predicated on use FMS guidance in the terminal area.
|
|
| 34-10-1&2 |
(O) Procedure to determine the Multi-Function Processing Unit is operative.
|
|
| 34-11 |
(M) Procedure to deactivate and secure the Radar Altimeter System.
|
|
| (O) Alternate procedure for terrain clearance awareness and approach minimums awareness with the radar altimeter inoperative.
|
||
| 34-12 |
(O) Operations procedure to verify Autopilot with Altitude Hold is operative.
|
|
| 34-13 |
(O) Operations procedure to ensure equipment configuration and flight crew awareness of the need to manually slave Directional Gyro.
|
|
| 34-14 |
(O) Operations procedure that identifies the required sources of magnetic heading information needed to be available and operative.
|
|
| 34-15 |
(M) Maintenance procedure to deactivate and secure the TCAS II System.
|
|
| 34-15-2 |
(O) Operations procedure to ensure TA ONLY Mode is selected by the crew and TA visual display and audio functions are operative.
|
|
| 34-15-3 |
(O) Operations procedure to ensure RA visual display and audio functions are operative.
|
|
| 34-16 |
(M) Maintenance procedure to deactivate and secure the TCAS I System.
|
|
| 34-17 |
(O) Procedure to ensure pilot planning and awareness of terrain clearance.
|
|
| U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION |
||
| AIRCRAFT: Beechcraft Model 200 and F-90 |
REVISION NO: 14b DATE: 08/27/2010 |
PAGE NO. XVII |
| Guidelines for (O) & (M) Procedures |
||
| 34-17-1 |
(O) Procedure to ensure alternate means of terrain awareness with inoperative GPWS.
|
| 34-17-1-a |
O) Procedure to ensure alternate means of crew awareness with inoperative Mode(s).
|
| 34-17-1-b |
(O) Procedure to ensure alternate means of terrain awareness with inoperative GPWS.
|
| 34-17-1-d |
(O) Procedure to ensure alternate means of crew awareness with inoperative advisory callout(s).
|
| 34-17-1-e |
(O) Procedures for windshear avoidance when Windshear Warning and Flight Guidance System is inoperative. Procedure should include a review of windshear avoidance and windshear recovery procedures.
|
| 34-17-2 |
(O) Procedure to ensure alternate means of terrain awareness with inoperative FLTA/PDA Modes.
|
| 34-22 |
(O) Operations procedure must identify all systems and functions affected by the inoperative MFD specific to each installation and provide for MEL deferral of those affected systems.
|
| 34-23 |
(O) Establish alternate procedures for use when Windshear Warning and Flight Guidance System is inoperative. Procedure should include a review of windshear avoidance and windshear recovery procedures.
|
| 34-24 |
(O) Establish alternate procedures for use when Windshear Detection and Avoidance System is inoperative. Procedure should include a review of windshear avoidance and windshear recovery procedures.
|
| 35-2 |
(M) Maintenance procedure to ensure a qualified crew member is stationed inside the aircraft to monitor the Internal Oxygen Gauge during servicing.
|
| U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION |
||
| AIRCRAFT: Beechcraft Model 200 and F-90 |
REVISION NO: 14b DATE: 08/27/2010 |
PAGE NO. XVIII |
| Guidelines for (O) & (M) Procedures |
||
| 35-3 |
(M) Maintenance procedure to block and placard affected Seat and to block flow of oxygen from the inoperative Mask.
|
| 37-2 |
(O) Operations procedure to determine Bleed Air Shutoff Valve is in the closed position prior to each departure.
|
| 46-1
|
(O) Procedure to ensure all the aeronautical information required for the flight is available in paper form or dual redundant electronic form.
|
| 46-1-1 |
(O) Procedure to ensure adequate battery power supply for the EFB is available for the duration of the flight plus one hour or all the aeronautical information required for the flight is available in paper form.
|
| 46-1-2 |
(M) Procedure to secure the EFB in a useable position by other means and if unable to secure the EFB, then remove the EFB from the aircraft.
(O) Procedure to ensure all the aeronautical information required for the flight is available in paper form or dual redundant electronic form if the EFB is removed.
|
| 46-1-3 |
(O) Procedure to provide alternate source of information normally provided through EFB data connection.
|
| 46-2-1 & 2 |
(O) Procedure to ensure all the aeronautical information required for the flight is available in paper form or dual redundant electronic form.
|
| 46-2-3 & 4 |
(O) Procedure to provide any required information normally provided through the CMU or Third VHF Radio.
|
| 52-2 |
(O) Operations procedure to inspect the Cargo Door Latching Mechanism to ensure the Door is latched prior to each departure.
|
| 52-3 |
(O) Operations procedure to inspect, using adequate Light, the Cabin Door Latching Mechanism to ensure the Door is latched prior to each departure.
|
| 52-4 |
(O) Operations procedure to ensure crew awareness that the Cabin Door must be lowered manually to prevent damage to personnel or the aircraft.
|
| 73-1 |
(M) Procedure to ensure there are no fuel leaks associated with the Fuel Flow Indicator malfunction.
|
| 79-1 |
(O) Operations procedure to monitor corresponding Oil Pressure Gauge.
|
| U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION |
|||||
| AIRCRAFT: Beechcraft Model 200 and F-90 |
REVISION NO: 14 DATE: 09/16/2008 |
PAGE NO: 21-1 |
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| 1. SYSTEM, SEQUENCE NUMBERS & ITEM |
REPAIR CATEGORY |
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|
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2. NUMBER INSTALLED |
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3. NUMBER REQUIRED FOR DISPATCH |
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|
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4. REMARKS AND EXCEPTIONS |
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| 21 |
AIR CONDITIONING |
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| 1. |
Pressurization Controller |
C |
1 |
0 |
(O) May be inoperative for unpressurized flight. |
|
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|
|
|
|
|
|
|
| 2. |
Safety Valve (Dump) |
C |
1 |
0 |
(M)(O) May be inoperative provided: a) Airplane remains unpressurized, and b) Safety Valve (Dump) is blocked open. |
|
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|
|
| 3. |
Outflow Valve |
C |
1 |
0 |
(M)(O) May be inoperative provided: a) Airplane remains unpressurized, and b) Safety Valve (Dump) is blocked open. |
|
|
|
|
|
|
|
|
|
| 4. |
Cabin Altitude Warning (ALT WARN) |
C |
1 |
0 |
May be inoperative for pressurized flight at or below 10,000 feet MSL. |
|
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|
|
|
C |
1 |
0 |
(O) May be inoperative for unpressurized flight. |
|
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| 5. |
Cabin Rate of Climb Indicator |
C |
1 |
0 |
May be inoperative for pressurized flight provided CABIN ALTITUDE/ DIFFERENTIAL PRESSURE Indicator is operative. |
|
|
|
|
|
|
|
|
|
|
|
|
C |
1 |
0 |
(O) May be inoperative for unpressurized flight. |
|
|
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|
|
|
|
|
|
| 6. |
Cabin Altitude/ Differential Pressure Indicator |
C |
1 |
0 |
(O) May be inoperative for unpressurized flight provided Safety Valve (Dump) is OPEN. |
|
|
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|
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| U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION |
|||||
| AIRCRAFT: Beechcraft Model 200 and F-90 |
REVISION NO: 14a DATE: 06/04/2010 |
PAGE NO: 21-2 |
|||
| 1. SYSTEM, SEQUENCE NUMBERS & ITEM |
REPAIR CATEGORY |
||||
|
|
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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|
|
|
|
|
|
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|
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|
|
| 7. |
Bleed Air Shutoff Valves (Environmental) (3 Position Switch) |
C |
2 |
1 |
(M) One may be inoperative in the ENVIR OFF Position for pressurized flight. |
|
|
|
|
|
|
|
|
|
|
|
|
C |
2 |
0 |
(M)(O) May be inoperative in the ENVIR OFF position for unpressurized flight. |
|
|
|
|
|
|
|
|
|
| 8. |
Bleed Air Shutoff Valves (Pneumatic Instrument Air) (3 Position Switch) |
|
|
|
DELETED; Revision 14a, See Chapter 37 |
|
|
|
|
|
|
|
|
|
| 9. |
Bleed Air Shutoff Valves (2 Position switch) |
C |
2 |
1 |
(M) One may be inoperative in the closed position for pressurized flight. |
|
|
|
|
|
|
|
|
|
|
|
|
C |
2 |
0 |
(M)(O) May be inoperative in closed position for unpressurized flight. |
|
|
|
|
|
|
|
|
|
| 10. |
AUTOMATIC Temperature Controller |
C |
1 |
0 |
May be inoperative provided MANUAL Temperature Controller is operative. |
|
|
|
|
|
|
|
|
|
| 11. |
MANUAL Temperature Controller |
C |
1 |
0 |
May be inoperative provided AUTOMATIC Controller is operative. |
|
|
|
|
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|
|
| 12. |
Electric Heat |
C |
1 |
0 |
|
|
|
|
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| 13. |
Ventilation Blower |
|
|
|
DELETED REVISION 9. |
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| 14. |
Air Conditioner |
C |
1 |
0 |
(M) |
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| 15. *** |
Aft Blower |
C |
1 |
0 |
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| U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION |
|||||
| AIRCRAFT: Beechcraft Model 200 and F-90 |
REVISION NO: 14 DATE: 09/16/2008 |
PAGE NO: 21-3 |
|||
| 1. SYSTEM, SEQUENCE NUMBERS & ITEM |
REPAIR CATEGORY |
||||
|
|
2. NUMBER INSTALLED |
||||
|
|
3. NUMBER REQUIRED FOR DISPATCH |
||||
|
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4. REMARKS AND EXCEPTIONS |
||||
| 21 |
AIR CONDITIONING |
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| 16. |
L or R BL AIR FAIL Annunciator System |
|
|
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|
|
| 1) |
Annunciator Fails to Illuminate |
C |
2 |
1 |
(O) One may be inoperative provided: a) Environmental and Instrument Bleed Air Valves on the inoperative side are verified closed before each flight, and b) Aircraft is not operative into known or forecast icing conditions. |
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NOTE: Rudder Boost will be inoperative. |
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| 2) |
Annunciator Remains Illuminated |
C |
2 |
1 |
(O) One may be inoperative provided: a) Environmental and instrument Bleed Air Valves on the inoperative side are verified closed before each flight, and b) Aircraft is not operated into known or forecast icing conditions. |
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NOTE: Rudder Boost will be inoperative. |
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| 17. *** |
Ground Air Cooling System |
C |
1 |
0 |
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| 18. |
Bleed Air OFF Annunciator System |
C |
1 |
0 |
(O) May be inoperative for unpressurized flight. |
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| 19. |
Cabin Door Seal System |
C |
1 |
0 |
(O) May be inoperative for unpressurized flight. |
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| 20. |
Cabin Temperature Indicator System |
C |
1 |
0 |
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| U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION |
|||||
| AIRCRAFT: Beechcraft Model 200 and F-90 |
REVISION NO: 14b DATE: 08/27/2010 |
PAGE NO: 22-1 |
|||
| 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 |
||||
| 22 |
AUTO FLIGHT |
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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: RVSM is not authorized. |
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| 2. |
Yaw Damper (200 Series except 200HDC, 200T with Tip Tanks or STC SA3519NM & F90 except STC SA4130NM) |
C |
1 |
0 |
(M) May be inoperative provided aircraft is operated at or below 17,000 ft Pressure Altitude. |
| |
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(200T with Tip Tanks) |
C |
1 |
0 |
(M) May be inoperative provided aircraft is operated at or below 7,000 ft MSL. |
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(200 Series with STC SA3519NM) |
C |
1 |
0 |
(M) |
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(F-90 with STC SA4130NM) |
C |
1 |
0 |
(M) |
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(200 HDC Only) |
C |
1 |
0 |
(M) May be inoperative provided aircraft is operated at or below 25,000 ft Pressure Altitude. |
| | | |
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| 3. |
Autopilot Control Wheel Disconnect Switches (AP/YD/TRIM DISC) |
C |
2 |
1 |
One may be inoperative on the non-flying pilot side provided: a) Autopilot is not used below 1,500 feet AGL, and b) Approach minimums do not require the use of the autopilot |
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(Except Garmin GFC-700 AFCS equipped) |
B |
- |
0 |
May be inoperative provided: a) Autopilot is not used, and b) Second level switch trim interrupt function remains operative. |
| | |
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(Continued) |
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| U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION |
|||||
| AIRCRAFT: Beechcraft Model 200 and F-90 |
REVISION NO: 14b DATE: 08/27/2010 |
PAGE NO: 22-2 |
|||
| 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 |
||||
| 22 |
AUTO FLIGHT |
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| 3. |
Autopilot Control Wheel Disconnect Switches (Continued) |
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| | | | |
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(Except Garmin GFC-700 AFCS equipped) |
B |
- |
0 |
(M) May be inoperative provided: a) Autopilot is considered inoperative, b) Electric Elevator Trim is considered inoperative, and c) Yaw Damper is considered inoperative. |
| | |
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| 4. |
Autopilot Go-Around Switch |
C |
1 |
0 |
(O) May be inoperative provided: a) Approach minimums do not require its use, and b) Alternate procedures are established and used to disconnect Autopilot and establish initial pitch and wings level attitude. |
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| 5. |
Autopilot Mode Selector/Annunciator (Except Collins Proline 21 equipped) |
C |
1 |
0 |
(O) May be inoperative provided the affected Mode(s) is/are selected momentarily prior to departure to verify that proper Mode Annunciation is displayed on the pilot’s EFIS Display or Remote Annunciator Panel. |
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| 6. |
Flight Director System |
C |
1 |
0 |
May be inoperative provided approach procedures do not require its use. |
| | |
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NOTE: Any operative Mode may be used. |
| | |
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| a) |
Flight Director Mode Selector Panel Annunciator Lamps (Except Collins Proline 21 equipped) |
C |
1 |
0 |
(O) May be inoperative provided the affected Mode(s) is/are selected momentarily prior to departure to verify that proper Mode Annunciator is displayed on the Pilot’s EFIS Display or Remote Annunciator Panel. |
| |
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|
| U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION |
|||||
| AIRCRAFT: Beechcraft Model 200 and F-90 |
REVISION NO: 14b DATE: 08/27/2010 |
PAGE NO: 22-3 |
|||
| 1. SYSTEM, SEQUENCE NUMBERS & ITEM |
REPAIR CATEGORY |
||||
|
|
2. NUMBER INSTALLED |
||||
|
|
3. NUMBER REQUIRED FOR DISPATCH |
||||
|
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4. REMARKS AND EXCEPTIONS |
||||
| 22 |
AUTO FLIGHT |
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| 7. |
Autopilot/Flight Guidance Panel Lamps (Except Collins Proline 21 equipped) |
C |
1 |
0 |
(O) May be inoperative provided the affected Mode(s) is/are selected momentarily prior to departure to verify that proper Mode Annunciator is displayed on pilot’s EFIS Display or Remote Annunciator Panel. |
|
| U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION |
|||||
| AIRCRAFT: Beechcraft Model 200 and F-90 |
REVISION NO: 14 DATE: 09/16/2008 |
PAGE NO: 23-1 |
|||
| 1. SYSTEM, SEQUENCE NUMBERS & ITEM |
REPAIR CATEGORY |
||||
|
|
2. NUMBER INSTALLED |
||||
|
|
3. NUMBER REQUIRED FOR DISPATCH |
||||
|
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4. REMARKS AND EXCEPTIONS |
||||
| 23 |
COMMUNICATIONS |
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|
| 1. |
Communications System (VHF, UHF) |
D |
- |
- |
Any in excess of those required by FAR may be inoperative provided it is not powered by Emergency Power Source and not required for Emergency Procedures. |
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| 2. |
Passenger Address System (PA) |
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|
|
| 1) |
Passenger Configuration |
C |
1 |
0 |
(O) May be inoperative provided alternate normal and emergency procedures and/or operating restrictions are established and used. . |
|
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| 2) |
Cargo Configuration |
D |
1 |
0 |
May be inoperative provided procedures do not require its use. |
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| 3. |
Cockpit Speakers System (Including Audio Amp.) |
C |
2 |
0 |
(O) May be inoperative provided: a) Two operative Headsets are available to the flight crew, and b) Aural warnings are available. |
|
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| 4. |
Audio Amplifiers |
|
|
|
DELETED Rev.14, Combine with Cockpit Speakers. |
|
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|
| 5. |
Static Discharge Wicks |
C |
- |
- |
One Wick may be missing or broken from: 1) Each Wing (includes Aileron), 2) Each side of Horizontal Stabilizer, and 3) Vertical Stabilizer |
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|
|
NOTE: A Maximum of three (3) Static Wicks may be broken or missing. |
|
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|
| U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION |
|||||
| AIRCRAFT: Beechcraft Model 200 and F-90 |
REVISION NO: 14 DATE: 09/16/2008 |
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 |
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|
| 6. |
Boom Microphones (includes headset mic) |
|
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|
|
|
| 1) |
With FDR and Cockpit Voice Recorder Equipped To Record Boom Microphone |
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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|
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|
|
| 2) |
With Only Cockpit Voice Recorder Equipped To Record Boom Microphone |
A |
- |
0 |
May be inoperative provided repairs are made within three flight days. |
|
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|
| 3) *** |
Without Cockpit Voice Recorder Equipped To Record Boom Microphone |
D |
- |
0 |
Any in excess of those required by FAR may be inoperative. |
|
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|
|
| U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION |
|||||
| AIRCRAFT: Beechcraft Model 200 and F-90 |
REVISION NO: 14 DATE: 09/16/2008 |
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 |
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|
|
| 7. |
Cockpit Voice Recorder (CVR) |
|
|
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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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|
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|
|
| 3) |
For Operators Other Than Air Carriers and Commercial Operators |
A |
1 |
0 |
May be inoperative provided repairs are made in accordance with applicable FARs. |
|
|
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|
|
| 8. *** |
Passenger Call System |
C |
1 |
0 |
|
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|
| 9. *** |
Voice Activated Interphone System (cockpit to cabin) |
D |
1 |
0 |
|
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|
| U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION |
|||||
| AIRCRAFT: Beechcraft Model 200 and F-90 |
REVISION NO: 14 DATE: 09/16/2008 |
PAGE NO: 23-4 |
|||
| 1. SYSTEM, SEQUENCE NUMBERS & ITEM |
REPAIR CATEGORY |
||||
|
|
2. NUMBER INSTALLED |
||||
|
|
3. NUMBER REQUIRED FOR DISPATCH |
||||
|
|
4. REMARKS AND EXCEPTIONS |
||||
| 23 |
COMMUNICATIONS |
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|
|
| 10. |
High Frequency (HF) Communication System |
D |
- |
- |
Any in excess of those required by FAR 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.
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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|
|
| 11. *** |
Recorded Passenger Briefing System |
D |
1 |
0 |
(O) May be inoperative provided passengers are appropriately briefed prior to each departure. |
|
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|
|
| 12. *** |
Flight Phone System |
D |
1 |
0 |
|
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|
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|
|
|
| 13. *** |
Ground Communications Power System |
D |
1 |
0 |
|
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|
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|
|
| U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION |
|||||
| AIRCRAFT: Beechcraft Model 200 and F-90 |
REVISION NO: 14 DATE: 09/16/2008 |
PAGE NO: 23-5 |
|||
| 1. SYSTEM, SEQUENCE NUMBERS & ITEM |
REPAIR CATEGORY |
||||
|
|
2. NUMBER INSTALLED |
||||
|
|
3. NUMBER REQUIRED FOR DISPATCH |
||||
|
|
4. REMARKS AND EXCEPTIONS |
||||
| 23 |
COMMUNICATIONS |
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|
| 14. |
Push-to-Talk Switches |
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|
|
|
| 1) |
Aircraft Equipped With Separate Hand Microphone Plug-In (Second-in-command Required) |
C |
2 |
1 |
One may be inoperative provided Hand Held Microphone on affected side is operative. |
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|
|
|
| 2) |
Aircraft Equipped With Separate Hand Microphone Plug-In (Second-In-Command Not Required) |
C |
2 |
1 |
Right side may be inoperative. |
|
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|
|
|
|
|
|
| 3) |
Aircraft Without Separate Hand Microphone Plug-In. (Second-In-Command Not Required) |
C |
2 |
1 |
Right side may be inoperative. |
|
|
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|
|
| 15. |
Hand Held Microphone |
C |
2 |
1 |
Right side may be inoperative. |
|
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|
|
|
|
|
C |
2 |
1 |
One may be inoperative provided Boom Microphone and Push-to-Talk Switch are operative on side with inoperative Microphone. |
|
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|
|
|
|
|
|
|
| U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION |
|||||
| AIRCRAFT: Beechcraft Model 200 and F-90 |
REVISION NO: 14 DATE: 09/16/2008 |
PAGE NO: 23-6 |
|||
| 1. SYSTEM, SEQUENCE NUMBERS & ITEM |
REPAIR CATEGORY |
||||
|
|
2. NUMBER INSTALLED |
||||
|
|
3. NUMBER REQUIRED FOR DISPATCH |
||||
|
|
4. REMARKS AND EXCEPTIONS |
||||
| 23 |
COMMUNICATIONS |
|
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|
|
|
| 16. |
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. |
|
|
|
|
|
|
|
|
|
| 1) |
Channels |
C |
- |
0 |
(O) May be inoperative provided alternate procedures are established and use. |
|
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|
|
|
|
|
|
|
|
|
D |
- |
0 |
May be inoperative provided procedures do not require its use. |
|
|
|
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|
|
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|
|
| U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION |
|||||
| AIRCRAFT: Beechcraft Model 200 and F-90 |
REVISION NO: 14 DATE: 09/16/2008 |
PAGE NO: 24-1 |
|||
| 1. SYSTEM, SEQUENCE NUMBERS & ITEM |
REPAIR CATEGORY |
||||
|
|
2. NUMBER INSTALLED |
||||
|
|
3. NUMBER REQUIRED FOR DISPATCH |
||||
|
|
4. REMARKS AND EXCEPTIONS |
||||
| 24 |
ELECTRICAL POWER |
|
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|
|
|
|
| 1. |
DC Generator Caution Lights |
B |
2 |
1 |
One may be inoperative provided corresponding Load Meter is monitored. |
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|
|
| 2. |
Inverters (Except SN BB-1769, BB-1834, BB-1843, BL-148 and After, BY-1 and after, and BZ-1 and after) |
B |
2 |
1 |
One may be inoperative for day VFR. |
|
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|
|
|
| 3. |
Inverters Warning Light (Except SN BB-1769, BB-1834, BB-1843, BL-148 and After, BY-1 and after, and BZ-1 and after) |
B |
2 |
1 |
One may be inoperative provided both Inverters are operative. |
|
|
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|
|
|
|
|
|
| 4. |
DC Load Meter |
|
|
|
DELETED, Revision 14 |
|
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|
|
|
|
|
|
|
| 5. |
AC Volt/Frequency Meter (Except SN BB-1769, BB-1834, BB-1843, BL-148 and After, BY-1 and after, and BZ-1 and after) |
B |
1 |
0 |
May be inoperative provided Inverter Warning Light is operative. |
|
|
|
|
|
|
|
|
|
| 6. *** |
Battery Temperature Indicating System |
C |
1 |
0 |
May be inoperative provided the Standard Battery Charge Annunciator System is operative. |
|
|
|
|
|
|
|
|
|
| U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION |
|||||
| AIRCRAFT: Beechcraft Model 200 and F-90 |
REVISION NO: 14 DATE: 09/16/2008 |
PAGE NO: 24-2 |
|||
| 1. SYSTEM, SEQUENCE NUMBERS & ITEM |
REPAIR CATEGORY |
||||
|
|
2. NUMBER INSTALLED |
||||
|
|
3. NUMBER REQUIRED FOR DISPATCH |
||||
|
|
4. REMARKS AND EXCEPTIONS |
||||
| 24 |
ELECTRICAL POWER |
|
|
|
|
|
|
|
|
|
|
|
|
|
| 7. *** |
Cabin AC Power System |
C |
- |
0 |
(M) |
|
|
|
|
|
|
|
|
|
| 8. |
EFIS Standby Power |
B |
1 |
0 |
(M) May be inoperative provided: a) Airplane is operated in day VMC only, and b) Standby Battery is disconnected and removed. |
|
|
|
|
|
|
|
|
|
| 9. |
External Power System |
C |
1 |
0 |
(M) |
|
|
|
|
|
|
|
|
|
| 10. |
External Power Annunciator |
C |
1 |
0 |
(O) |
|
|
|
|
|
|
|
|
|
| 11. |
L or R GEN BUS TIE Relay (Model F90 Only) |
B |
2 |
1 |
One may be inoperative for day VMC operations provided both DC GEN Annunciators/Caution Lights are operative. |
|
|
|
|
|
|
|
|
|
| 12. |
L or GEN BUS TIE Annunciator (Model F90 Only) |
B |
2 |
0 |
(O) May be inoperative provided: a) Generator Bus Tie Relay is verified closed prior to each departure, and b) Both DC GEN Annunciators/ Caution Lights are operative. |
|
|
|
|
|
|
|
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| U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION |
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| AIRCRAFT: Beechcraft Model 200 and F-90 |
REVISION NO: 12 DATE: 11/03/2003 |
PAGE NO: 25-1 |
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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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| 25 |
EQUIPMENT/ FURNISHINGS |
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| 1. |
Crew Seats |
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| 1) |
Arm Rests |
C |
- |
0 |
(M) May be inoperative provided the affected Arm Rest(s) is/are stowed and secured in the full up or full down position and is/are acceptable to the flight crew. |
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| 2) |
Lumbar Support |
C |
- |
0 |
May be inoperative provided the Seat configuration is acceptable to the flight crew. |
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| 3) |
Shoulder Harness |
B |
2 |
1 |
Right side may be inoperative provided Seat is not occupied. |
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| 4) |
Seat Adjustment |
A |
- |
0 |
(M) May be inoperative provided: a) Seat(s) is/are locked in a position that permits normal pilot visibility, b) Full Flight Control movement is available, c) Position of the affected Seat(s) is/are acceptable to the flight crew, and d) Repairs are made within one flight day. |
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| U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION |
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| AIRCRAFT: Beechcraft Model 200 and F-90 |
REVISION NO: 14 DATE: 09/16/2008 |
PAGE NO: 25-2 |
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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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| 25 |
EQUIPMENT/ FURNISHINGS |
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| 2. |
Passenger Seat(s) |
D |
- |
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May be inoperative provided: a) Seat does not block an Emergency Exit, b) Seat does not restrict any passenger from access to the main aircraft aisle, and c) Affected seat(s) are blocked and placarded “DO NOT OCCUPY”. |
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NOTE 1: A seat with an inoperative seat belt is considered inoperative. |
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NOTE 2: Affected seat(s) may include the seat(s) behind. |
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| 1) |
Recline Mechanism |
D |
- |
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(M) May be inoperative and seat occupied provided seat is secured in the full upright position. |
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D |
- |
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May be inoperative and seat occupied provided seat is immovable in the full upright position |
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| 2) |
Armrest |
D |
- |
- |
May be inoperative or missing and Seat occupied provided: a) Armrest does not block an Emergency Exit, b) Armrest does not restrict any passenger from access to the main aircraft aisle, and c) For an Armrest with a recline mechanism, seat is secure in the full upright position. |
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| U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION |
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| AIRCRAFT: Beechcraft Model 200 and F-90 |
REVISION NO: 14 DATE: 09/16/2008 |
PAGE NO: 25-3 |
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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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| 25 |
EQUIPMENT/ FURNISHINGS |
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| 3. *** |
Floatation Equipment |
D |
- |
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Any in excess of those required by FAR may be inoperative or missing. |
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| 4. |
Emergency Medical Equipment |
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| 1) *** |
Automatic External Defibrillator (AED) and/or Associated Equipment |
D |
- |
- |
May be incomplete, missing, or inoperative. |
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| 2) *** |
Emergency Medical Kit (EMK) and/or Associated Equipment |
D |
- |
- |
May be incomplete, missing or inoperative. |
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| 3) |
First Aid Kit (FAK) and/or Associated Equipment |
D |
- |
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Any in excess of those required by FAR may be incomplete, missing or inoperative. |
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| 5. |
Emergency Locator Transmitter (ELT) |
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| 1) |
Survival Type ELTs |
D |
- |
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Any in excess of those required by FAR may be inoperative or missing. |
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| 2) |
Fixed ELTs |
A |
- |
0 |
May be inoperative or missing provided repairs are made within 90 days. |
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D |
- |
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Any in excess of those required by FAR may be inoperative or missing. |
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| a) *** |
Remote Switch |
D |
1 |
0 |
(M) May be inoperative provided: a) Remote switch is disconnected from the ELT, and b) ELT switch is placed in the ARM position. |
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| U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION |
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| AIRCRAFT: Beechcraft Model 200 and F-90 |
REVISION NO: 14 DATE: 09/16/2008 |
PAGE NO: 25-4 |
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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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| 25 |
EQUIPMENT/ FURNISHINGS |
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| 6. |
Non-Essential Equipment & Furnishings (NEF) |
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0 |
May be inoperative, damaged, or missing provided that the item(s) is deferred in accordance with the operator’s NEF deferral program. The NEF program, procedures, and processes are outlined in the operators (insert name) Manual. (M) and (O) procedures, if required, must be available to the flight crew and included in the operator’s appropriate document.
NOTE: Exterior Lavatory Door Ash Trays are not considered NEF Items. |
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| 7. *** |
Electric Toilet |
C |
1 |
0 |
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| 8. |
“Fasten Seat Belt While Seated” Sign or Placard |
C |
- |
- |
One or more Signs or Placards may be illegible or missing provided a legible Sign or Placard is visible from each occupied Passenger Seat. |
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| U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION |
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| AIRCRAFT: Beechcraft Model 200 and F-90 |
REVISION NO: 14 DATE: 09/16/2008 |
PAGE NO: 25-5 |
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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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| 25 |
EQUIPMENT/ FURNISHINGS |
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| 9. *** |
Exterior Lavatory Door Ashtrays |
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| 1) |
Airplanes With More Than One Exterior Lavatory Door Ashtray Installed |
A |
- |
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One may be missing provided it is replaced within 10 calendar days. |
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| 2) |
Airplanes With Only One Exterior Lavatory Door Ashtray Installed |
A |
1 |
0 |
May be missing provided it is replaced within 3 calendar days. |
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| 10. *** |
Waste Receptacle Access Doors/Covers |
C |
- |
- |
(M)(O) May be inoperative provided: a) The container is empty and the access is secured to prevent waste introduction into the compartment, and b) Procedures are established to ensure that sufficient Waste Receptacles are available to accommodate all waste that may be generated on a flight. |
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| 11. *** |
Cargo Restraint Systems |
C |
- |
- |
(M) May be inoperative or missing provided acceptable cargo loading limits from an approved source, i.e., an Approved Cargo Loading Manual, Cargo Handling Manual, or Weight and Balance Document are observed. |
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C |
- |
- |
May be inoperative or missing provided Cargo Compartment remains empty. |
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| U.S. DEPARTMENT OF TRANSPORTATION MA |