DEPARTMENT OF TRANSPORTATION
Revision: 5
Date: 05/30/2002
FEDERAL AVIATION ADMINISTRATION
WASHINGTON, D.C.
M A S T E R
M I N I M U M
E Q U I P M E N T
L I S T
HAWKER SIDDELEY HS-125
(SERIES 1 THROUGH 800XP)
/S/
ROD LALLEY, CHAIRMAN, FLIGHT
OPERATIONS EVALUATION BOARD (FOEB)
FEDERAL AVIATION ADMINISTRATION
FLIGHT STANDARDS DIVISION
SEATTLE AIRCRAFT EVALUATION GROUP
1601 LIND AVE. S.W.
RENTON, WASHINGTON 98055-4056
TELEPHONE: (425)227-2280
FAX: (425)227-1270
FEDERAL AVIATION ADMINISTRATION
MASTER MINIMUM EQUIPMENT LIST
Page: I
Revision: 5
Date: 05/30/2002
HAWKER SIDDELEY HS-125
(SERIES 1 THROUGH 800XP)
Table of Contents
SYSTEM NO.
---------21
21
22
23
24
24
25
26
27
28
29
30
30
31
32
33
34
34
34
34
35
49
52
56
73
74
SYSTEM
PAGE
Table of Contents
Log of Revisions
Control Page
Highlights of Change
Highlights of Change
Highlights of Change
Definitions
Definitions
Preamble
Air Conditioning
Air Conditioning
Auto Flight
Communications
Electrical Power
Electrical Power
Equipment/Furnishings
Fire Protection
Flight Controls
Fuel
Hydraulic Power
Ice and Rain Protection
Ice and Rain Protection
Indicating/Recording Systems
Landing Gear
Lights
Navigation
Navigation
Navigation
Navigation
Oxygen
Airborne Auxiliary Power
Doors
Windows
Engine Fuel & Control
Ignition
I, II
III, IV
V, VI, VII
VIII, IX, X, XI
XII, XIII, XIV, XV
XVI
XVII, XVIII, XIX, XX
XXI, XXII, XXIII, XXIV
XXV, XXVI
21-1, 2, 3, 4, 5
21-6 THRU 10
22-1, 2, 3, 4, 5
23-1, 2, 3, 4, 5
24-1, 2, 3, 4, 5
24-6
25-1, 2, 3, 4
26-1, 2, 3
27-1, 2, 3, 4, 5
28-1, 2, 3, 4, 5
29-1, 2
30-1, 2, 3, 4, 5
30-6
31-1, 2
32-1
33-1, 2, 3, 4, 5
34-1, 2, 3, 4, 5
34-6 THRU 10
34-11 THRU 15
34-16
35-1, 2
49-1
52-1, 2
56-1
73-1, 2
74-1
FEDERAL AVIATION ADMINISTRATION
MASTER MINIMUM EQUIPMENT LIST
Page: II
Revision: 5
Date: 05/30/2002
HAWKER SIDDELEY HS-125
(SERIES 1 THROUGH 800XP)
Table of Contents
SYSTEM NO.
77
78
79
80
SYSTEM
PAGE
Engine Indicating
Engine Exhaust
Engine Oil
Starting
77-1
78-1
79-1
80-1
FEDERAL AVIATION ADMINISTRATION
MASTER MINIMUM EQUIPMENT LIST
Page: III
Revision: 5
Date: 05/30/2002
HAWKER SIDDELEY HS-125
(SERIES 1 THROUGH 800XP)
Log of Revisions
---------------------------------------------------------------------¦ REV.NO. ¦ DATE
¦ PAGE NUMBERS
¦ INITIALS ¦
---------------------------------------------------------------------¦ ORIGINAL ¦
¦
¦
¦
¦ 1
¦ 04/02/1987 ¦ Complete Revision
¦
¦
¦ 2
¦ 03/06/1992 ¦ ALL PAGES
¦
¦
¦ 3
¦ 09/07/1993 ¦ HIGHLIGHTS OF REV.,DEFINITIONS ¦
¦
¦ 3
¦ 09/07/1993 ¦ 21-1,21-2,21-3,21-4,21-5
¦
¦
¦ 3
¦ 09/07/1993 ¦ 21-6,21-7,22-1,22-2,22-3
¦
¦
¦ 3
¦ 09/07/1993 ¦ 23-1,23-2,23-3,24-1,24-2
¦
¦
¦ 3
¦ 09/07/1993 ¦ 24-3,24-4,24-5,25-1,25-2
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¦ 3
¦ 09/07/1993 ¦ 25-3,26-1,26-2,26-3,27-1
¦
¦
¦ 3
¦ 09/07/1993 ¦ 27-2,27-3,28-1,28-2,28-3
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¦ 3
¦ 09/07/1993 ¦ 28-4,28-5,29-1,29-2,30-1
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¦
¦ 3
¦ 09/07/1993 ¦ 30-2,30-3,30-4,30-5,30-6
¦
¦
¦ 3
¦ 09/07/1993 ¦ 31-1,32-1,33-1,33-2,33-3
¦
¦
¦ 3
¦ 09/07/1993 ¦ 33-4,34-1,34-2,34-3,34-4
¦
¦
¦ 3
¦ 09/07/1993 ¦ 34-5,34-6,34-7,34-8,34-9
¦
¦
¦ 3
¦ 09/07/1993 ¦ 34-10,34-11,35-1,35-2,38-1
¦
¦
¦ 3
¦ 09/07/1993 ¦ 49-1,52-1,56-1,73-1,73-2
¦
¦
¦ 3
¦ 09/07/1993 ¦ 74-1,77-1,78-1,79-1,80-1
¦
¦
¦ 3a
¦ 10/02/1996 ¦ HIGHLIGHTS OF REV.,DEFINITIONS ¦
¦
¦ 3a
¦ 10/02/1996 ¦ 21-1,21-3
¦
¦
¦ 4
¦ 03/10/1998 ¦ HIGHLIGHTS OF REV.,DEFINITIONS ¦
¦
¦ 4
¦ 03/10/1998 ¦ 21-1,21-2,21-3,21-4,21-5
¦
¦
¦ 4
¦ 03/10/1998 ¦ 21-6,21-7,21-8,22-1,22-2
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¦
¦ 4
¦ 03/10/1998 ¦ 22-3,22-4,23-1,23-2,23-3
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¦
¦ 4
¦ 03/10/1998 ¦ 23-4,24-1,24-2,24-3,24-4
¦
¦
¦ 4
¦ 03/10/1998 ¦ 24-5,24-6,25-1,25-2,25-3
¦
¦
¦ 4
¦ 03/10/1998 ¦ 27-1,27-2,27-3,27-4,28-1
¦
¦
¦ 4
¦ 03/10/1998 ¦ 28-2,28-3,28-4,29-1,29-2
¦
¦
¦ 4
¦ 03/10/1998 ¦ 30-1,30-2,30-3,30-4,30-5
¦
¦
¦ 4
¦ 03/10/1998 ¦ 30-6,31-1,33-1,33-2,33-3
¦
¦
¦ 4
¦ 03/10/1998 ¦ 33-4,33-5,34-1,34-2,34-3
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¦
¦ 4
¦ 03/10/1998 ¦ 34-4,34-5,34-6,34-7,34-8
¦
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¦ 4
¦ 03/10/1998 ¦ 34-9,34-10,34-11,34-12,34-13
¦
¦
¦ 4
¦ 03/10/1998 ¦ 34-14,35-1,35-2,49-1,52-1
¦
¦
¦ 4
¦ 03/10/1998 ¦ 77-1,78-1
¦
¦
¦ 4a
¦ 12/22/1999 ¦ HIGHLIGHTS OF REV.,DEFINITIONS ¦
¦
¦ 4a
¦ 12/22/1999 ¦ 34-11
¦
¦
¦ 4b
¦ 01/28/2002 ¦ HIGHLIGHTS OF REV.,DEFINITIONS ¦
¦
¦ 4b
¦ 01/28/2002 ¦ 52-2
¦
¦
¦ 5
¦ 05/30/2002 ¦ HIGHLIGHTS OF REV.,DEFINITIONS ¦
¦
¦ 5
¦ 05/30/2002 ¦ PREAMBLE
¦
¦
¦ 5
¦ 05/30/2002 ¦ 21-1,21-2,21-3,21-4,21-5
¦
¦
¦ 5
¦ 05/30/2002 ¦ 21-6,21-7,21-8,21-9,21-10
¦
¦
----------------------------------------------------------------------
FEDERAL AVIATION ADMINISTRATION
MASTER MINIMUM EQUIPMENT LIST
Page: IV
Revision: 5
Date: 05/30/2002
HAWKER SIDDELEY HS-125
(SERIES 1 THROUGH 800XP)
Log of Revisions
---------------------------------------------------------------------¦ REV.NO. ¦ DATE
¦ PAGE NUMBERS
¦ INITIALS ¦
---------------------------------------------------------------------¦ 5
¦ 05/30/2002 ¦ 22-1,22-2,22-3,22-4,22-5
¦
¦
¦ 5
¦ 05/30/2002 ¦ 23-1,23-2,23-3,23-4,23-5
¦
¦
¦ 5
¦ 05/30/2002 ¦ 24-1,24-2,24-3,24-4,24-5
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¦ 5
¦ 05/30/2002 ¦ 25-1,25-2,25-3,25-4,26-1
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¦
¦ 5
¦ 05/30/2002 ¦ 26-2,27-2,27-3,27-4,27-5
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¦ 5
¦ 05/30/2002 ¦ 28-1,28-2,28-3,28-4,28-5
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¦ 5
¦ 05/30/2002 ¦ 29-1,29-2,30-1,30-2,30-3
¦
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¦ 5
¦ 05/30/2002 ¦ 30-4,30-5,30-6,31-1,31-2
¦
¦
¦ 5
¦ 05/30/2002 ¦ 32-1,33-1,33-2,33-4,33-5
¦
¦
¦ 5
¦ 05/30/2002 ¦ 34-1,34-2,34-3,34-4,34-5
¦
¦
¦ 5
¦ 05/30/2002 ¦ 34-6,34-9,34-10,34-11,34-12
¦
¦
¦ 5
¦ 05/30/2002 ¦ 34-13,34-14,34-15,34-16,35-1
¦
¦
¦ 5
¦ 05/30/2002 ¦ 35-2,38-1,49-1,52-2,56-1
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¦ 5
¦ 05/30/2002 ¦ 73-1,73-2,77-1
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----------------------------------------------------------------------
FEDERAL AVIATION ADMINISTRATION
Page: V
Revision: 5
Date: 05/30/2002
MASTER MINIMUM EQUIPMENT LIST
HAWKER SIDDELEY HS-125
(SERIES 1 THROUGH 800XP)
Control Page
SYSTEM
PAGE
Cover Page
Table of Contents
I
II
III
IV
V
VI
VII
VIII
IX
X
XI
XII
XIII
XIV
XV
XVI
XVII
XVIII
XIX
XX
XXI
XXII
XXIII
XXIV
XXV
XXVI
21-1
21-2
21-3
21-4
21-5
21-6
21-7
21-8
21-9
21-10
22-1
22-2
22-3
Log of Revisions
Control Page
Highlights of Change
Definitions
Preamble
21
22
REV NO.
5
5
5
5
5
5
5
5
5
5
5
5
5
5
5
5
5
6
6
6
6
6
6
6
6
2
2
5
5
5
5
5
5
5
5
5
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5
5
5
CURRENT DATE
05/30/2002
05/30/2002
05/30/2002
05/30/2002
05/30/2002
05/30/2002
05/30/2002
05/30/2002
05/30/2002
05/30/2002
05/30/2002
05/30/2002
05/30/2002
05/30/2002
05/30/2002
05/30/2002
05/30/2002
01/31/1995
01/31/1995
01/31/1995
01/31/1995
01/31/1995
01/31/1995
01/31/1995
01/31/1995
06/14/1989
06/14/1989
05/30/2002
05/30/2002
05/30/2002
05/30/2002
05/30/2002
05/30/2002
05/30/2002
05/30/2002
05/30/2002
05/30/2002
05/30/2002
05/30/2002
05/30/2002
FEDERAL AVIATION ADMINISTRATION
Page: VI
Revision: 5
Date: 05/30/2002
MASTER MINIMUM EQUIPMENT LIST
HAWKER SIDDELEY HS-125
(SERIES 1 THROUGH 800XP)
Control Page
SYSTEM
23
24
25
26
27
28
29
30
31
PAGE
22-4
22-5
23-1
23-2
23-3
23-4
23-5
24-1
24-2
24-3
24-4
24-5
24-6
25-1
25-2
25-3
25-4
26-1
26-2
26-3
27-1
27-2
27-3
27-4
27-5
28-1
28-2
28-3
28-4
28-5
29-1
29-2
30-1
30-2
30-3
30-4
30-5
30-6
31-1
31-2
REV NO.
5
5
5
5
5
5
5
5
5
5
5
5
4
5
5
5
5
5
5
3
4
5
5
5
5
5
5
5
5
5
5
5
5
5
5
5
5
5
5
5
CURRENT DATE
05/30/2002
05/30/2002
05/30/2002
05/30/2002
05/30/2002
05/30/2002
05/30/2002
05/30/2002
05/30/2002
05/30/2002
05/30/2002
05/30/2002
03/10/1998
05/30/2002
05/30/2002
05/30/2002
05/30/2002
05/30/2002
05/30/2002
09/07/1993
03/10/1998
05/30/2002
05/30/2002
05/30/2002
05/30/2002
05/30/2002
05/30/2002
05/30/2002
05/30/2002
05/30/2002
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05/30/2002
05/30/2002
05/30/2002
05/30/2002
05/30/2002
05/30/2002
05/30/2002
05/30/2002
05/30/2002
FEDERAL AVIATION ADMINISTRATION
Page: VII
Revision: 5
Date: 05/30/2002
MASTER MINIMUM EQUIPMENT LIST
HAWKER SIDDELEY HS-125
(SERIES 1 THROUGH 800XP)
Control Page
SYSTEM
PAGE
32
33
32-1
33-1
33-2
33-3
33-4
33-5
34-1
34-2
34-3
34-4
34-5
34-6
34-7
34-8
34-9
34-10
34-11
34-12
34-13
34-14
34-15
34-16
35-1
35-2
49-1
52-1
52-2
56-1
73-1
73-2
74-1
77-1
78-1
79-1
80-1
34
35
49
52
56
73
74
77
78
79
80
REV NO.
5
5
5
4
5
5
5
5
5
5
5
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4
4
5
5
5
5
5
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5
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4
5
5
5
5
3
5
4
3
3
CURRENT DATE
05/30/2002
05/30/2002
05/30/2002
03/10/1998
05/30/2002
05/30/2002
05/30/2002
05/30/2002
05/30/2002
05/30/2002
05/30/2002
05/30/2002
03/10/1998
03/10/1998
05/30/2002
05/30/2002
05/30/2002
05/30/2002
05/30/2002
05/30/2002
05/30/2002
05/30/2002
05/30/2002
05/30/2002
05/30/2002
03/10/1998
05/30/2002
05/30/2002
05/30/2002
05/30/2002
09/07/1993
05/30/2002
03/10/1998
09/07/1993
09/07/1993
FEDERAL AVIATION ADMINISTRATION
MASTER MINIMUM EQUIPMENT LIST
Page: VIII
Revision: 5
Date: 05/30/2002
HAWKER SIDDELEY HS-125
(SERIES 1 THROUGH 800XP)
Highlights of Change
EFFECTIVE ABOVE DATE, the HS-125 Master Minimum Equipment List has been
revised. Please replace affected pages with revision 5 for a complete
up-to-date MMEL.
ATA 21 AIR CONDITIONING
Item 21-10-3:
Number of item changed.
Item 21-10-5:
Expanded Title.
Item 21-10-6:
Expanded Title and added subitem 1) to Title.
Item 21-10-9:
Moved item 21-60-7, Rev. 5.
Item 21-10-10: New Item.
Item 21-10-11: New Item.
Item 21-10-12: New Item.
Item 21-10-13: New Item.
Item 21-10-14: Item has moved from item 21-30-9, Rev 5.
Item 21-10-15: Expanded Title.
Item 21-20-2:
Expanded Title and added proviso c).
Item 21-21-1:
Added "***".
Item 21-30-9:
Item moved to item 21-10-14.
Item 21-50-1:
Deleted reference to flight insepection aircraft.
Item 21-60-4:
Expanded Title.
Item 21-60-5:
Item moved to item 21-10-15.
Item 21-60-6:
New Item.
Item 21-60-7:
Item moved from item 21-10-9.
FEDERAL AVIATION ADMINISTRATION
MASTER MINIMUM EQUIPMENT LIST
Page: IX
Revision: 5
Date: 05/30/2002
HAWKER SIDDELEY HS-125
(SERIES 1 THROUGH 800XP)
Highlights of Change
ATA 22 AUTO PILOT
Item 22-10-1:
Added two notes.
Item 22-10-2:
New Item.
Item 22-10-5:
Added "***".
Item 22-10-7:
New Item.
Item 22-20-2:
Deleted Item, Rev. 5.
Item 22-20-3:
Deleted Item, Rev. 5.
Item 22-20-4:
Expanded Title and added (O) procedure. 1st proviso
deleted.
Item 22-20-5:
Clarify aircraft model in title and proviso revised.
Item 22-20-6:
Clarify aircraft model in title and proviso revised.
Item 22-20-7:
Clarify title and added notes.
Item 22-20-8:
Item moved to ATA 27-30-5, Rev. 5.
Item 22-20-9:
New Item.
ATA 23 COMMUNICATIONS
Item 23-05-1:
Item 23-10-1:
Item 23-10-2:
Title and provisos revised.
To aliegn with PL-95.
Deleted reference to Flight Inspection Aircraft.
Item 23-10-3:
New Item.
Item 23-30-1:
Changed repair interval from "B" to "C".
Item 23-50-3:
Revised Per PL-58, Rev. 3, dated July 12, 2001.
Item 23-50-4:
New Item.
Item 23-50-5:
New Item.
FEDERAL AVIATION ADMINISTRATION
MASTER MINIMUM EQUIPMENT LIST
Page: X
Revision: 5
Date: 05/30/2002
HAWKER SIDDELEY HS-125
(SERIES 1 THROUGH 800XP)
Highlights of Change
ATA 24 ELECTRICAL
Item 23-70-1:
Revised Per PL-29, Rev. 3, dated, Aug. 15, 1997.
Item 23-70-2:
Added Subitems 1 and 2, changed repair interval.
Item 24-20-1:
Repair interval changed to "C"
Item 24-20-7:
Changed title to clarify aircraft model.
Item 24-20-8,
Sub-item 2: Added proviso a) for clarification.
Item 24-30-6:
Changed title to clarify aircraft model.
Item 24-30-9:
Changed title to clarify aircraft model.
Proviso "b" added.
Item 24-30-10: Expanded Title and added "***".
Item 24-30-12: Added "***".
ATA 25
EQUIPMENT/FURNISHINGS
Item 25-10-2: New Item.
Item 25-20-1: Title Revised Per PL-79, Rev. 2, dated March 1, 2001.
Item 25-20-2: Repair Interval changed Per PL73, Rev. 2, dated 9/19/2001.
Item 25-60-5: New Item.
ATA 26 FIRE PROTECTION
Item 26-10-1: Changed title to clarify aircraft model.
Item 26-20-4: Title changed to clarify aircraft model and revised Per
PL-75, Rev.1 dated Aug. 15, 1997.
FEDERAL AVIATION ADMINISTRATION
MASTER MINIMUM EQUIPMENT LIST
Page: XI
Revision: 5
Date: 05/30/2002
HAWKER SIDDELEY HS-125
(SERIES 1 THROUGH 800XP)
Highlights of Change
ATA 27
FLIGHT CONTROLS
Item 27-30-1: Added notes for clarification.
Item 27-30-2: Changed title to clarify aircraft model.
Item 27-30-3: Changed title to clarify aircraft model.
Item 27-30-4: Changed title to clarify aircraft model.
Item 27-30-5: New Item.
ATA 24 ELECTRICAL
Item 23-70-1:
Revised Per PL-29, Rev. 3, dated, Aug. 15, 1997.
Item 23-70-2:
Added Subitems 1 and 2, changed repair interval.
Item 24-20-1:
Repair interval changed to "C"
Item 24-20-7:
Changed title to clarify aircraft model.
Item 24-20-8,
Sub-item 1:
Item 24-30-6:
Changed title to clarify aircraft model.
Item 24-30-9:
Changed title to clarify aircraft model.
Proviso "b" added.
Added proviso a) for clarification.
FEDERAL AVIATION ADMINISTRATION
MASTER MINIMUM EQUIPMENT LIST
Page: XII
Revision: 5
Date: 05/30/2002
HAWKER SIDDELEY HS-125
(SERIES 1 THROUGH 800XP)
Highlights of Change
ATA 28
FUEL
Item 27-60-3:
New Item.
Item 28-20-2:
Title changed to clarify aircraft model.
Item 28-20-3:
Title changed to clarify aircraft model.
Item 28-20-4:
Title changed to clarify aircraft model.
Item 28-20-5:
Title changed to clarify aircraft model.
Item 28-20-6:
Title changed to clarify aircraft model.
Item 28-22-1:
Title changed to clarify aircraft model.
Item 28-43-2:
Title changed to clarify aircraft model.
Item 28-43-3:
Title changed to clarify aircraft model.
Item 28-43-4:
Title changed to clarify aircraft model.
Item 28-45-2:
Added "***" and changed number installed to a "-".
ATA 29 HYDRAULIC POWER
Item 29-30-5:
Title changed to clarify aircraft model.
Item 29-30-6:
New Item.
Item 29-30-7:
New Item added back into the MMEL with proviso added.
ATA 30
ICE AND RAIN PROTECTION
Item 30-10-2:
Minor change to proviso b) subitem 1) and subitem 2
title change to clarify aircraft model.
Item 30-10-4:
Title changed to clarify aircraft model.
Item 30-10-5:
Title changed to clarify aircraft model.
Item 30-10-6:
Added "***".
FEDERAL AVIATION ADMINISTRATION
MASTER MINIMUM EQUIPMENT LIST
Page: XIII
Revision: 5
Date: 05/30/2002
HAWKER SIDDELEY HS-125
(SERIES 1 THROUGH 800XP)
Highlights of Change
Item 30-20-3:
Title changed to clarify aircraft model.
Item 30-20-4:
Title changed to clarify aircraft model.
Item 30-30-1:
Minor change to title and note added.
Item 30-30-2:
Title changed to clarify aircraft model.
Item 30-30-3:
Title changed to clarify aircraft model.
Item 30-30-4:
Minor change to title. Added the word "Mast".
Item 30-30-5:
New Item.
Item 30-30-6:
New Item.
Item 30-40-1:
Title change in subitem 1) and 2) to clarify aircraft
model.
Item 30-40-2:
Expanded proviso and added a note.
Item 30-40-3:
Title changed to clarify aircraft model.
Item 30-80-1:
Added procedures in proviso.
ATA 31
INDICATING/RECORDING SYSTEMS
Item 31-30-1:
Change to reflect Policy Letter 87.
Item 31-40-1:
Added "***".
Item 31-50-1:
New Item.
ATA 32 LANDING GEAR
Item 32-32-1:
New Item.
FEDERAL AVIATION ADMINISTRATION
MASTER MINIMUM EQUIPMENT LIST
Page: XIV
Revision: 5
Date: 05/30/2002
HAWKER SIDDELEY HS-125
(SERIES 1 THROUGH 800XP)
Highlights of Change
ATA 33 LIGHTS
Item 33-10-1:
Revised to reflect PL-77, Rev 2, dated, Aug. 15, 1997.
Item 33-10-2:
Title changed to clarify aircraft model and # installed
changed from "2" to a dash.
Item 33-10-3:
Title changed to clarify aircraft model.
Item 33-20-2:
Number installed changed from "2" to dash.
Item 33-40-5:
Deleted reference to flight at night, revised title and
added 2nd proviso.
Item 33-50-1:
Expanded proviso.
ATA 34
NAVIGATION
Item 34-9-1:
Subitems 1 and 2 titles changed to clarify aircraft model.
Item 34-9-2:
Added "***".
Item 34-9-3:
Added "***".
Item 34-9-4:
Added "***".
Item 34-10-2: Changed to reflect Policy Letter 39.
Added note.
Item 34-10-3: Minor correction to subitem 4) proviso.
Item 34-10-8: Expanded title for clarity.
FEDERAL AVIATION ADMINISTRATION
MASTER MINIMUM EQUIPMENT LIST
Page: XV
Revision: 5
Date: 05/30/2002
HAWKER SIDDELEY HS-125
(SERIES 1 THROUGH 800XP)
Highlights of Change
Item 34-20-1: Added note.
Item 34-20-2: Added the word Indication to subitem 1).
provisos.
Reformatted
Item 34-20-4: Expanded title.
Item 34-40-4: Added Terrain Awareness Warning System to title.
Item 34-50-2: Added proviso and changed number required for dispatch.
Item 34-50-3: Revised Per PL-3, Rev. 2, dated Aug. 15, 1997.
Item 34-50-4: Revised Per PL-76, Rev. 2, dated Oct 16, 2001.
Item 34-50-8: New Item.
Item 34-60-1: Revised Per PL-32, Rev 5, dated April 6, 2000.
Item 34-70-1: Added "MFD" to title.
Item 34-70-2: Added "MFD" to title.
Item 34-70-3: Added "MFD" to title.
Item 34-70-4: Added subitem 1) to title.
Item 34-70-7: Added *** for optional equipment.
Item 34-70-10: New Item.
Item 34-70-13: New Item.
ATA 35 OXYGEN
Item 35-00-1:
Deleted (M) procedure.
Item 35-20-1:
Deleted (M) procedure and minor change to proviso c).
FEDERAL AVIATION ADMINISTRATION
MASTER MINIMUM EQUIPMENT LIST
Page: XVI
Revision: 5
Date: 05/30/2002
HAWKER SIDDELEY HS-125
(SERIES 1 THROUGH 800XP)
Highlights of Change
ATA 49
AIRBORNE AUXILIARY POWER
Item 49-10-1: Added Load Control Valve to title.
Item 49-10-2: Minor change to subitem 1) title and added subitem 2).
ATA 52 DOORS
Item 52-70-5:
New Item.
Item 52-70-6:
New Item.
ATA 56 WINDOWS
Item 56-10-1:
Deleted from MMEL, Revision 5.
FOEB does not allow
Item 56-10-2:
Deleted from MMEL, Revision 5.
relief for cracked windows.
FOEB does not allow
ATA 73
ENGINE FUEL AND CONTROL
Item 73-22-1: Changed title to reflect aircraft model and added TFE-731
Engine Only to title. Proviso revised accordingly.
Item 73-23-1: Changed title to reflect aircraft model.
Item 73-31-1: Changed repair interval.
ATA 77 ENGINE INDICATIONS
Item 77-10-2:
Added TFE-731 Engines to subitem 1) title and added "RPM"
to subitem 2) and 3) title.
Item 77-32-3:
New Item.
FEDERAL AVIATION ADMINISTRATION
MASTER MINIMUM EQUIPMENT LIST
Page: XVII
Revision: 6
Date: 01/31/1995
HAWKER SIDDELEY HS-125
(SERIES 1 THROUGH 800XP)
Definitions
1.
System Definitions.
System numbers are based on the Air Transport Association (ATA)
Specification Number 100 and items are numbered sequentially.
a.
"Item" (Column 1) means the equipment, system,
component, or function listed in the "Item"
column.
b.
"Number Installed" (Column 2) is the number
(quantity) of items normally installed in the
aircraft. This number represents the aircraft
configuration considered in developing this MMEL.
Should the number be a variable (e.g., passenger
cabin items) a number is not required.
c.
"Number Required for Dispatch" (Column 3) is the
minimum number (quantity) of items required for
operation provided the conditions specified in
Column 4 are met.
¦
NOTE: Where the MMEL shows a variable number required for
dispatch, the MEL must reflect the actual number required for
dispatch or an alternate means of configuration control approved
by the Administrator.
d.
"Remarks or Exceptions" (Column 4) in this column
includes a statement either prohibiting or
permitting operation with a specific number of
items inoperative, provisos (conditions and
limitations) for such operation, and appropriate
notes.
e.
A vertical bar (change bar) in the margin
indicates a change, addition or deletion in the
adjacent text for the current revision of that
page only. The change bar is dropped at the next
revision of that page.
2. "Airplane/Rotorcraft Flight Manual" (AFM/RFM) is the document
required for type certification and approved by the responsible
FAA Aircraft Certification Office. The FAA approved AFM/RFM for
the specific aircraft is listed on the applicable Type
FEDERAL AVIATION ADMINISTRATION
MASTER MINIMUM EQUIPMENT LIST
Page: XVIII
Revision: 6
Date: 01/31/1995
HAWKER SIDDELEY HS-125
(SERIES 1 THROUGH 800XP)
Definitions
Certificate Data Sheet.
3. "As required by FAR" means that the listed item is subject to
certain provisions (restrictive or permissive) expressed in the
Federal Aviation Regulations operating rules. The number of
items required by the FAR must be operative. When the listed
item is not required by FAR it may be inoperative for time
specified by repair category.
4. Each inoperative item must be placarded to inform and remind
the crewmembers and maintenance personnel of the equipment
condition.
NOTE: To the extent practical, placards should be located
adjacent to the control or indicator for the item affected;
however, unless otherwise specified, placard wording and location
will be determined by the operator.
5. "-" symbol in Column 2 and/or Column 3 indicates a variable
number (quantity) of the item installed.
¦
6. "Deleted" in the remarks column after a sequence item
indicates that the item was previously listed but is now required
to be operative if installed in the aircraft.
7. "ER" refers to extended range operations of a two-engine
airplane which has a type design approval for ER operations and
complies with the provisions of Advisory Circular 120-42A.
8. "Federal Aviation Regulations" (FAR) means the applicable
portions of the Federal Aviation Act and Federal Aviation
Regulations.
9. "Flight Day" means a 24 hour period (from midnight to
midnight) either Universal Coordinated Time (UCT) or local time,
as established by the operator, during which at least one flight
is initiated for the affected aircraft.
10. "Icing Conditions" means an atmospheric environment that may
cause ice to form on the aircraft or in the engine(s).
11. Alphabetical symbol in Column 4 indicates a proviso
(condition or limitation) that must be complied with for
¦
FEDERAL AVIATION ADMINISTRATION
MASTER MINIMUM EQUIPMENT LIST
Page: XIX
Revision: 6
Date: 01/31/1995
HAWKER SIDDELEY HS-125
(SERIES 1 THROUGH 800XP)
Definitions
operation with the
listed item inoperative.
12. "Inoperative" means a system and/or component malfunction to
the extent that it does not accomplish its intended purpose
and/or is not consistently functioning normally within its
approved operating limit(s) or tolerance(s).
13. "Notes:" in Column 4 provides additional information for
crewmember or maintenance consideration. Notes are used to
identify applicable material which is intended to assist with
compliance, but do not relieve the operator of the responsibility
for compliance with all applicable requirements. Notes are not a
part of the provisos.
14. Inoperative components of an inoperative system:
Inoperative items which are components of a system which is
inoperative are usually considered components directly associated
with and having no other function than to support that system.
(Warning/caution systems associated with the inoperative system
must be operative unless relief is specifically authorized per
the MMEL).
15. "(M)" symbol indicates a requirement for a specific
maintenance procedure which must be accomplished prior to
operation with the listed item inoperative. Normally these
procedures are accomplished by maintenance personnel; however,
other personnel may be qualified and authorized to perform
certain functions. Procedures requiring specialized knowledge or
skill, or requiring the use of tools or test equipment should be
accomplished by maintenance personnel. The satisfactory
accomplishment of all maintenance procedures, regardless of
who performs them, is the responsibility of the operator.
Appropriate procedures are required to be published as part of
the operator's manual or MEL.
16. "(O)" symbol indicates a requirement for a specific
operations procedure which must be accomplished in planning for
and/or operating with the listed item inoperative. Normally
these procedures are accomplished by the flight crew; however,
other personnel may be qualified and authorized to perform
certain functions. The satisfactory accomplishment of all
procedures, regardless of who performs them, is the
responsibility of the operator. Appropriate procedures are
FEDERAL AVIATION ADMINISTRATION
MASTER MINIMUM EQUIPMENT LIST
Page: XX
Revision: 6
Date: 01/31/1995
HAWKER SIDDELEY HS-125
(SERIES 1 THROUGH 800XP)
Definitions
required to be published as a part of the operator's manual or
MEL.
NOTE: The (M) and (O) symbols are required in the operator's MEL
unless otherwise authorized by the Administrator.
17. "Deactivated" and "Secured" means that the specified
component must be put into an acceptable condition for safe
flight. An acceptable method of securing or deactivating will be
established by the operator.
18. "Visual Flight Rules" (VFR) is as defined in FAR Part 91.
This precludes a pilot from filing an Instrument Flight Rules
(IFR) flight plan.
19. "Visual Meteorological Conditions" (VMC) means the
atmospheric environment is such that would allow a flight to
proceed under the visual flight rules applicable to the flight.
This does not preclude operating under Instrument Flight Rules.
20. "Visible Moisture" means an atmospheric environment
containing water in any form that can be seen in natural or
artificial light; for example, clouds, fog, rain, sleet, hail, or
snow.
21. "Passenger Convenience Items" means those items related to
passenger convenience, comfort or entertainment such as, but not
limited to, galley equipment, movie equipment, ash trays, stereo
equipment, overhead reading lamps, etc.
22. Repair Intervals: All users of an MEL approved under FAR
121, 125, 129 and 135 must effect repairs of inoperative systems
or components, deferred in accordance with the MEL, at or prior
to the repair times established by the following letter
designators:
Category A. Items in this category shall be repaired within
the time interval specified in the remarks column of the
operator's approved MEL.
Category B. Items in this category shall be repaired within
three (3) consecutive calendar days (72 hours), excluding the day
the malfunction was recorded in the aircraft maintenance
FEDERAL AVIATION ADMINISTRATION
MASTER MINIMUM EQUIPMENT LIST
Page: XXI
Revision: 6
Date: 01/31/1995
HAWKER SIDDELEY HS-125
(SERIES 1 THROUGH 800XP)
Definitions
record/logbook. For example, if it were recorded at 10 a.m. on
January 26th, the three day interval would begin at midnight the
26th and end at midnight the 29th.
Category C. Items in this category shall be repaired within
ten (10) consecutive calendar days (240 hours), excluding the day
the malfunction was recorded in the aircraft maintenance
record/logbook. For example, if it were recorded at 10 a.m. on
January 26th, the 10 day interval would begin at midnight the
26th and end at midnight February 5th.
Category D. Items in this category shall be repaired within
one hundred and twenty (120) consecutive calendar days (2880
hours), excluding the day the malfunction was recorded in the
aircraft maintenance log and/or record.
The letter designators are inserted adjacent to Column 2.
23. Electronic fault alerting system - General
¦
¦
New generation aircraft display system fault indications to the ¦
flight crew by use of computerized display systems. Each
¦
aircraft manufacturer has incorporated individual design
¦
philosophies in determining the data that would be
¦
represented. The following are customized definitions (specific¦
to each manufacturer) to help determine the level of messages
¦
affecting the aircraft's dispatch status. When preparing the
¦
MEL document, operators are to select the proper Definition No. ¦
23 for their aircraft, if appropriate.
¦
¦
a.
BOEING (B-757/767, B-747-400, B-777)
¦
¦
Boeing airplanes equipped with Engine Indicating and Crew
¦
Alerting Systems (EICAS), provide different priority levels of ¦
system messages (WARNING, CAUTION, ADVISORY, STATUS and
¦
MAINTENANCE). Any messages that affects airplane dispatch
¦
status will be displayed at a STATUS message level or higher. ¦
The absence of an EICAS STATUS or higher level (WARNING,
¦
CAUTION, ADVISORY) indicates that the system/component is
¦
operating within its approved operating limits or tolerances.
¦
¦
System conditions that result only in a maintenance level
¦
message, i.e. no correlation with a higher level EICAS message, ¦
FEDERAL AVIATION ADMINISTRATION
MASTER MINIMUM EQUIPMENT LIST
Page: XXII
Revision: 6
Date: 01/31/1995
HAWKER SIDDELEY HS-125
(SERIES 1 THROUGH 800XP)
Definitions
do not affect dispatch and do not require action other than as
addressed within an operators standard maintenance program.
¦
¦
¦
b.
DOUGLAS (MD-11)
¦
¦
Some Douglas aircraft are equipped with an alerting function
¦
which is a subsystem within the Electronic Instrument System
¦
(EIS). The alerting function provides various levels of system ¦
condition alerts (WARNING, CAUTION, ADVISORY, MAINTENANCE and
¦
STATUS).
¦
¦
Alerts that affect aircraft dispatch will include WARNING,
¦
CAUTION, STATUS or MAINTENANCE level. MAINTENANCE alerts are
¦
displayed on the status page of the EIS display panel under the ¦
maintenance heading.
¦
¦
A MAINTENANCE alert on the EIS indicates the presence of a
¦
system fault which can be identified by the Central Fault
¦
Display System (CFDS) interrogation. The systems are designed ¦
to be fault tolerant, however, for any MAINTENANCE alert, the
¦
MEL must be verified for dispatch purposes.
¦
¦
c.
AIRBUS (A-300-600, A-310, A-320/319/321, A-330, A-340
¦
¦
Airbus aircraft equipped with Electronic Centralized Aircraft
¦
Monitoring (ECAM) provide different levels of system condition ¦
messages (WARNING, CAUTION, STATUS, and ADVISORY). A-320/319/
¦
321, A-330, and A-340 also provide MAINTENANCE status messages. ¦
¦
Any message that effects airplane dispatchability will normally ¦
be at the WARNING, CAUTION or STATUS level. MAINTENANCE
¦
messages (A-320/319/321, A-330, and A-340 only) are also
¦
indicated on ECAM Status Page below the white Maintenance label.¦
¦
A MAINTENANCE status (Class II) message on ECAM indicates the
¦
presence of a system fault which can be identified by CFDS
¦
(A-320/319/321) or CMS (A-330/A-340) interrogation. The systems ¦
are designed to be fault tolerant, however for any MAINTENANCE ¦
status (Class II) message, the A-320/319/321 MEL must be
¦
verified for dispatch capability. For the A-330 and A-340,
¦
MAINTENANCE status messages do not affect dispatch.
¦
d.
FOKKER
(FK-100)
¦
FEDERAL AVIATION ADMINISTRATION
MASTER MINIMUM EQUIPMENT LIST
Page: XXIII
Revision: 6
Date: 01/31/1995
HAWKER SIDDELEY HS-125
(SERIES 1 THROUGH 800XP)
Definitions
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
System conditions that only require maintenance are not
¦
presented on the flight deck. These maintenance
¦
indications/messages may be presented on the Maintenance & Test ¦
Panel (MAP) or the Centralized Fault Display Unit (CFDU) and by ¦
dedicated Built In Test Evaluation (BITE) of systems.
¦
Fokker aircraft are equipped with Multi Function Display System
(MFDS) which provides electronic message referring to the
different priority levels of system information (WARNING (red),
CAUTION (amber), AWARENESS (cyan) AND STATUS (white). Any
messages that affects aircraft dispatch will be at the WARNING,
CAUTION or AWARENESS level. In these cases the MEL must be
verified for dispatch capability and maintenance may be
required.
24. "Administrative control item" means an item listed by the
operator in the MEL for tracking and informational purposes. It
may be added to an operator's MEL by approval of the Principal
Operations Inspector provided no relief is granted, or provided
conditions and limitations are contained in an approved document
(i.e. Structural Repair Manual, airworthiness directive, etc.).
If relief other than that granted by an approved document is
sought for an administrative control item, a request must be
submitted to the Administrator. If the request results in review
and approval by the FOEB, the item becomes an MMEL item rather
than an administrative control item.
25. "***" symbol in Column 1 indicates an item which is not
required by regulation but which may have been installed on some
models of aircraft covered by this MMEL. This item may be
included on the operator's MEL after the approving office has
determined that the item has been installed on one or more of the
operator's aircraft. The symbol, however, shall not be carried
forward into the operator's MEL. It should be noted that neither
this policy nor the use of this symbol provide authority to
install or remove an item from an aircraft.
26. "Excess Items" means those items that have been installed
that are redundant to the requirements of the FARs.
27. "Day of Discovery" is the calendar day an
equipment/instrument malfunction was recorded in the aircraft
FEDERAL AVIATION ADMINISTRATION
MASTER MINIMUM EQUIPMENT LIST
Page: XXIV
Revision: 6
Date: 01/31/1995
HAWKER SIDDELEY HS-125
(SERIES 1 THROUGH 800XP)
Definitions
maintenance log and or record. This day is excluded from the
calendar days or flight days specified in the MMEL for the
repair of an inoperative item of equipment. This provision is
applicable to all MMEL items, i.e., categories "A, B, C, and
D."
FEDERAL AVIATION ADMINISTRATION
MASTER MINIMUM EQUIPMENT LIST
Page: XXV
Revision: 2
Date: 06/14/1989
HAWKER SIDDELEY HS-125
(SERIES 1 THROUGH 800XP)
Preamble
(Effective 6/14/89)
The following is applicable for authorized certificate holders operating
under Federal Aviation Regulations (FAR) Parts 121, 125, 129, 135: The
FAR require that all equipment installed on an aircraft in compliance
with the Airworthiness Standards and the Operating Rules must be
operative. However, the Rules also permit the publication of a Minimum
Equipment List (MEL) where compliance with certain equipment
requirements is not necessary in the interests of safety under all
operating conditions. Experience has shown that with the various levels
of redundancy designed into aircraft, operation of every system or
installed component may not be necessary when the remaining operative
equipment can provide an acceptable level of safety. A Master Minimum
Equipment List (MMEL) is developed by the FAA, with participation by the
aviation industry, to improve aircraft utilization and thereby provide
more convenient and economic air transportation for the public. The FAA
approved MMEL includes those items of equipment related to airworthiness
and operating regulations and other items of equipment which the
Administrator finds may be inoperative and yet maintain an acceptable
level of safety by appropriate conditions and limitations; it does not
contain obviously required items such as wings, flaps, and rudders. The
MMEL is the basis for development of individual operator MELs which take
into consideration the operator's particular aircraft equipment
configuration and operational conditions. Operator MELs, for
administrative control, may include items not contained in the
MMEL; however, relief for administrative control items must be
approved by the Administrator. An operator's MEL may differ in
format from the MMEL, but cannot be less restrictive than the MMEL.
The individual operator's MEL, when approved and authorized, permits
operation of the aircraft with inoperative equipment.
Equipment not required by the operation being conducted and equipment in
excess of FAR requirements are included in the MEL with appropriate
conditions and limitations. The MEL must not deviate from the Aircraft
Flight Manual Limitations, Emergency Procedures or with Airworthiness
Directives. It is important to remember that all equipment related to
the airworthiness and the operating regulations of the aircraft not
listed on the MMEL must be operative.
FEDERAL AVIATION ADMINISTRATION
MASTER MINIMUM EQUIPMENT LIST
Page: XXVI
Revision: 2
Date: 06/14/1989
HAWKER SIDDELEY HS-125
(SERIES 1 THROUGH 800XP)
Preamble
(Effective 6/14/89)
Suitable conditions and limitations in the form of placards, maintenance
procedures, crew operating procedures and other restrictions as
necessary are specified in the MEL to ensure that an acceptable level of
safety is maintained.
The MEL is intended to permit operation with inoperative items of
equipment for a period of time until repairs can be accomplished. It is
important that repairs be accomplished at the earliest opportunity. In
order to maintain an acceptable level of safety and reliability the MMEL
establishes limitations on the duration of and conditions for operation
with inoperative equipment. The MEL provides for release of the
aircraft for flight with inoperative equipment. When an item of
equipment is discovered to be inoperative, it is reported by making an
entry in the Aircraft Maintenance Record/Logbook as prescribed by FAR.
The item is then either repaired or may be deferred per the MEL or other
approved means acceptable to the Administrator prior to further
operation. MEL conditions and limitations, do not relieve the operator
from determining that the aircraft is in condition for safe operation
with items of equipment inoperative.
When these requirements are met, an Airworthiness Release, Aircraft
Maintenance Record/Logbook entry, or other approved documentation is
issued as prescribed by FAR. Such documentation is required prior to
operation with any item of equipment inoperative.
Operators are responsible for exercising the necessary operational
control to ensure that an acceptable level of safety is maintained.
When operating with multiple inoperative items, the interrelationships
between those items and the effect on aircraft operation and crew
workload will be considered.
Operators are to establish a controlled and sound repair program
including the parts, personnel, facilities, procedures, and schedules to
ensure timely repair.
WHEN USING THE MEL, COMPLIANCE WITH THE STATED INTENT OF THE PREAMBLE,
DEFINITIONS, AND THE CONDITIONS AND LIMITATIONS SPECIFIED IN THE MEL IS
REQUIRED.
------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION
¦
¦
¦
¦
MASTER MINIMUM EQUIPMENT LIST
¦
¦ FEDERAL AVIATION ADMINISTRATION
¦
¦ --------------------------------------------------------------------------- ¦
¦ AIRCRAFT:
¦ REVISION NO: 5
¦ PAGE:
¦
¦
HAWKER SIDDELEY HS-125
¦
¦
¦
¦
(SERIES 1 THROUGH 800XP)
¦ DATE: 05/30/2002
¦ 21-1
¦
¦ --------------------------------------------------------------------------- ¦
¦
1. ¦ 2. NUMBER INSTALLED
¦
¦ SYSTEM &
¦
-------------------------------------------- ¦
¦ SEQUENCE
ITEM
¦
¦ 3. NUMBER REQUIRED FOR DISPATCH
¦
¦ NUMBERS
¦
¦
--------------------------------------- ¦
¦ ------------------------- ¦
¦
¦ 4. REMARKS OR EXCEPTIONS
¦
¦ 21 AIR CONDITIONING
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 10-1 Engine Main Air
C ¦ 2 ¦ 1 ¦ (M)(O)One may be inoperative for
¦
¦
Valves
¦
¦
¦ pressurized flight provided:
¦
¦
¦
¦
¦
a) Valve is secured closed, and
¦
¦
¦
¦
¦
b) Cockpit auxiliary heating
¦
¦
¦
¦
¦
system operates normally.
¦
¦
¦
¦
¦
¦
¦
C ¦ 2 ¦ 0 ¦ (M)(O)May be inoperative provided:
¦
¦
¦
¦
¦
a) Flight is conducted in an
¦
¦
¦
¦
¦
unpressurized configuration,
¦
¦
¦
¦
¦
b) Both valves are secured
¦
¦
¦
¦
¦
closed, and
¦
¦
¦
¦
¦
c) Both ram air and dump valves
¦
¦
¦
¦
¦
operate normally.
¦
¦
¦
¦
¦
¦
¦ 10-2 Engine Main Air
C ¦ 2 ¦ 1 ¦ (O)One may be inoperative provided:
¦
¦
Valve Position
¦
¦
¦
a) Both engine main air valves
¦
¦
Indicators
¦
¦
¦
operate normally.
¦
¦
¦
¦
¦
OR
¦
¦
¦
¦
¦
b) If one engine main air valve
¦
¦
¦
¦
¦
is inoperative, the indica¦
¦
¦
¦
¦
tor associated with the
¦
¦
¦
¦
¦
operative valve operates
¦
¦
¦
¦
¦
normally.
¦
¦
¦
¦
¦
¦
¦
C ¦ 2 ¦ 0 ¦ (M)(O)May be inoperative provided:
¦
¦
¦
¦
¦
a) Flight is conducted in an
¦
¦
¦
¦
¦
unpressurized configuration,
¦
¦
¦
¦
¦
b) Both engine main air valves
¦
¦
¦
¦
¦
are secured closed, and
¦
¦
¦
¦
¦
c) Ram air and dump valves
¦
¦
¦
¦
¦
operate normally.
¦
¦
¦
¦
¦
¦
¦ 10-3 Refrigeration Unit C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided:
| ¦
¦
System/Air Cycle
¦
¦
¦
a) Flight is conducted in an
| ¦
¦
Machine
¦
¦
¦
unpressurized configuration, | ¦
¦
¦
¦
¦
and
¦
¦
¦
¦
¦
b) Ram air and dump valves
¦
¦
¦
¦
¦
operate normally.
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
-------------------------------------------------------------------------------
------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION
¦
¦
¦
¦
MASTER MINIMUM EQUIPMENT LIST
¦
¦ FEDERAL AVIATION ADMINISTRATION
¦
¦ --------------------------------------------------------------------------- ¦
¦ AIRCRAFT:
¦ REVISION NO: 5
¦ PAGE:
¦
¦
HAWKER SIDDELEY HS-125
¦
¦
¦
¦
(SERIES 1 THROUGH 800XP)
¦ DATE: 05/30/2002
¦ 21-2
¦
¦ --------------------------------------------------------------------------- ¦
¦
1. ¦ 2. NUMBER INSTALLED
¦
¦ SYSTEM &
¦
-------------------------------------------- ¦
¦ SEQUENCE
ITEM
¦
¦ 3. NUMBER REQUIRED FOR DISPATCH
¦
¦ NUMBERS
¦
¦
--------------------------------------- ¦
¦ ------------------------- ¦
¦
¦ 4. REMARKS OR EXCEPTIONS
¦
¦ 21 AIR CONDITIONING
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 10-4 Footwarmer and
C ¦ 1 ¦ 0 ¦ May be inoperative provided
¦
¦
Windscreen
¦
¦
¦ windscreen heating system operates
¦
¦
Demister Valve
¦
¦
¦ normally.
¦
¦
¦
¦
¦
¦
¦ 10-5 Cockpit
C ¦ - ¦ 0 ¦
¦
¦ *** Ventilation Fans
¦
¦
¦
¦
¦
(Excluding Hawker
¦
¦
¦
| ¦
¦
800XP Fitted with
¦
¦
¦
| ¦
¦
Collins Proline 21
¦
¦
¦
| ¦
¦
Avionics)
¦
¦
¦
| ¦
¦
¦
¦
¦
¦
¦ 10-6 Two Way Cabin
C ¦ 1 ¦ 0 ¦
| ¦
¦
Flood Valve
¦
¦
¦
| ¦
¦
(Series 3 Through
¦
¦
¦
| ¦
¦
700, and 800B)
¦
¦
¦
| ¦
¦
¦
¦
¦
¦
¦
1) Cabin Flood
C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided:
| ¦
¦
Valve
¦
¦
¦
a) LH or RH cabin valve
| ¦
¦
(Series 800A
¦
¦
¦
operates normally.
| ¦
¦
and 800XP)
¦
¦
¦
OR
| ¦
¦
¦
¦
¦
b) Flight is conducted
| ¦
¦
¦
¦
¦
in an unpressurized
| ¦
¦
¦
¦
¦
configuration.
| ¦
¦
¦
¦
¦
¦
¦ 10-7 Ram Air Shut-Off
C ¦ 1 ¦ 0 ¦ (M)(O)May be inoperative for
¦
¦
Valve
¦
¦
¦ pressurized flight provided:
¦
¦
¦
¦
¦
a) Valve is secured fully
¦
¦
¦
¦
¦
closed, and
¦
¦
¦
¦
¦
b) Dump Valve operates
¦
¦
¦
¦
¦
normally.
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
-------------------------------------------------------------------------------
------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION
¦
¦
¦
¦
MASTER MINIMUM EQUIPMENT LIST
¦
¦ FEDERAL AVIATION ADMINISTRATION
¦
¦ --------------------------------------------------------------------------- ¦
¦ AIRCRAFT:
¦ REVISION NO: 5
¦ PAGE:
¦
¦
HAWKER SIDDELEY HS-125
¦
¦
¦
¦
(SERIES 1 THROUGH 800XP)
¦ DATE: 05/30/2002
¦ 21-3
¦
¦ --------------------------------------------------------------------------- ¦
¦
1. ¦ 2. NUMBER INSTALLED
¦
¦ SYSTEM &
¦
-------------------------------------------- ¦
¦ SEQUENCE
ITEM
¦
¦ 3. NUMBER REQUIRED FOR DISPATCH
¦
¦ NUMBERS
¦
¦
--------------------------------------- ¦
¦ ------------------------- ¦
¦
¦ 4. REMARKS OR EXCEPTIONS
¦
¦ 21 AIR CONDITIONING
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 10-8 Rear Baggage
C ¦ 1 ¦ 0 ¦ (M)May be inoperative provided:
¦
¦ *** Pannier Heating
¦
¦
¦
a) Inlet and outlet valves are
¦
¦
System
¦
¦
¦
verified closed, and
¦
¦
¦
¦
¦
b) Pannier heating is selected
¦
¦
¦
¦
¦
OFF.
¦
¦
¦
¦
¦
¦
¦ 10-9 Refrigeration Unit
¦
¦
¦ Moved to ATA-21-60-7, Rev. 5.
| ¦
¦
Bypass Valve (RBV)
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 10-10 Overhead Air
D ¦ - ¦ 0 ¦
| ¦
¦
Flow Distribution
¦
¦
¦
| ¦
¦
Vents (Punkah
¦
¦
¦
| ¦
¦
Louvers)
¦
¦
¦
| ¦
¦
¦
¦
¦
¦
¦ 10-11 Cabin Floor
C ¦ 2 ¦ 0 ¦ (O)May be inoperative provided:
| ¦
¦
Valve
¦
¦
¦
a) Cabin flood valve operates
| ¦
¦
(Series 800A
¦
¦
¦
normally.
| ¦
¦
and 800XP)
¦
¦
¦
OR
| ¦
¦
¦
¦
¦
b) Flight is conducted in an
| ¦
¦
¦
¦
¦
unpressurized configuration. | ¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 10-12 Cabin Flood
C ¦ 1 ¦ 0 ¦
| ¦
¦
Valve Indicator
¦
¦
¦
| ¦
¦
(Series 800A
¦
¦
¦
| ¦
¦
and 800XP)
¦
¦
¦
| ¦
¦
¦
¦
¦
¦
¦ 10-13 Cabin Floor
C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided:
| ¦
¦
Valve Indicator
¦
¦
¦
a) Cabin flood valve is
| ¦
¦
(Series 800A
¦
¦
¦
verified to operate
| ¦
¦
and 800XP)
¦
¦
¦
normally.
| ¦
¦
¦
¦
¦
OR
| ¦
¦
¦
¦
¦
b) Flight is conducted in an
| ¦
¦
¦
¦
¦
unpressurized configuration. | ¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
-------------------------------------------------------------------------------
------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION
¦
¦
¦
¦
MASTER MINIMUM EQUIPMENT LIST
¦
¦ FEDERAL AVIATION ADMINISTRATION
¦
¦ --------------------------------------------------------------------------- ¦
¦ AIRCRAFT:
¦ REVISION NO: 5
¦ PAGE:
¦
¦
HAWKER SIDDELEY HS-125
¦
¦
¦
¦
(SERIES 1 THROUGH 800XP)
¦ DATE: 05/30/2002
¦ 21-4
¦
¦ --------------------------------------------------------------------------- ¦
¦
1. ¦ 2. NUMBER INSTALLED
¦
¦ SYSTEM &
¦
-------------------------------------------- ¦
¦ SEQUENCE
ITEM
¦
¦ 3. NUMBER REQUIRED FOR DISPATCH
¦
¦ NUMBERS
¦
¦
--------------------------------------- ¦
¦ ------------------------- ¦
¦
¦ 4. REMARKS OR EXCEPTIONS
¦
¦ 21 AIR CONDITIONING
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 10-14 Flow Control
C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided:
| ¦
¦
Valve (Series
¦
¦
¦
a) Flight is conducted in an
| ¦
¦
1 Through 800)/
¦
¦
¦
unpressurized configuration, | ¦
¦
Pressure
¦
¦
¦
b) Ram air and dump valves
| ¦
¦
Regulating Shut¦
¦
¦
operate normally, and
| ¦
¦
off Valve (PRSOV)
¦
¦
¦
c) RH main air valve is closed. | ¦
¦
(Series 800XP)
¦
¦
¦
| ¦
¦
¦
¦
¦
¦
¦ 10-15 HP Air Valve
C ¦ 2 ¦ 1 ¦ (O)One may be inoperative provided: | ¦
¦
(Series 1 Through
¦
¦
¦
a) Main air valve on the
| ¦
¦
800XP) With
¦
¦
¦
affected side is secured in
| ¦
¦
TFE-731 Engines
¦
¦
¦
the closed position, and
| ¦
¦
Only)
¦
¦
¦
b) Cockpit auxilliary heating
| ¦
¦
¦
¦
¦
system operates normally.
| ¦
¦
¦
¦
¦
¦
¦
C ¦ 2 ¦ 0 ¦ (O)May be inoperative provided:
| ¦
¦
¦
¦
¦
a) Flight is conducted in an
| ¦
¦
¦
¦
¦
unpressurized configuration, | ¦
¦
¦
¦
¦
b) Both Main Air Valves are
| ¦
¦
¦
¦
¦
secured in the closed
| ¦
¦
¦
¦
¦
position, and
| ¦
¦
¦
¦
¦
c) Both ram air and dump valves | ¦
¦
¦
¦
¦
operate normally.
| ¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
-------------------------------------------------------------------------------
------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION
¦
¦
¦
¦
MASTER MINIMUM EQUIPMENT LIST
¦
¦ FEDERAL AVIATION ADMINISTRATION
¦
¦ --------------------------------------------------------------------------- ¦
¦ AIRCRAFT:
¦ REVISION NO: 5
¦ PAGE:
¦
¦
HAWKER SIDDELEY HS-125
¦
¦
¦
¦
(SERIES 1 THROUGH 800XP)
¦ DATE: 05/30/2002
¦ 21-5
¦
¦ --------------------------------------------------------------------------- ¦
¦
1. ¦ 2. NUMBER INSTALLED
¦
¦ SYSTEM &
¦
-------------------------------------------- ¦
¦ SEQUENCE
ITEM
¦
¦ 3. NUMBER REQUIRED FOR DISPATCH
¦
¦ NUMBERS
¦
¦
--------------------------------------- ¦
¦ ------------------------- ¦
¦
¦ 4. REMARKS OR EXCEPTIONS
¦
¦ 21 AIR CONDITIONING
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 20-1 Cabin
¦
¦
¦ Moved to Item 34-10-10, Rev. 5.
| ¦
¦
Recirculating Fan
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 20-2 Flight Deck Heat
C ¦ 1 ¦ 0 ¦ (O)May be inoperative closed
| ¦
¦
Valve/Auxiliary
¦
¦
¦ provided flight is conducted at or | ¦
¦
Heating Valve
¦
¦
¦ below FL 250.
| ¦
¦
¦
¦
¦
¦
¦
C ¦ 1 ¦ 0 ¦ (O)May be inoperative closed
¦
¦
¦
¦
¦ provided:
¦
¦
¦
¦
¦
a) Flight is conducted in an
¦
¦
¦
¦
¦
unpressurized configuration,
¦
¦
¦
¦
¦
and
¦
¦
¦
¦
¦
b) Ram air and dump valves
¦
¦
¦
¦
¦
operate normally.
¦
¦
¦
¦
¦
¦
¦ 20-3 Flight Deck
C ¦ - ¦ 0 ¦
¦
¦
Recirculating Fan
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 20-4 Mixing Valves
C ¦ 2 ¦ 1 ¦
¦
¦
(TFE 731 Engine
¦
¦
¦
¦
¦
Only)
C ¦ 2 ¦ 0 ¦ (O)May be inoperative provided:
¦
¦
¦
¦
¦
a) Flight is conducted in an
¦
¦
¦
¦
¦
unpressurized configuration,
¦
¦
¦
¦
¦
and
¦
¦
¦
¦
¦
b) Ram air and dump valves
¦
¦
¦
¦
¦
operate normally.
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
-------------------------------------------------------------------------------
------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION
¦
¦
¦
¦
MASTER MINIMUM EQUIPMENT LIST
¦
¦ FEDERAL AVIATION ADMINISTRATION
¦
¦ --------------------------------------------------------------------------- ¦
¦ AIRCRAFT:
¦ REVISION NO: 5
¦ PAGE:
¦
¦
HAWKER SIDDELEY HS-125
¦
¦
¦
¦
(SERIES 1 THROUGH 800XP)
¦ DATE: 05/30/2002
¦ 21-6
¦
¦ --------------------------------------------------------------------------- ¦
¦
1. ¦ 2. NUMBER INSTALLED
¦
¦ SYSTEM &
¦
-------------------------------------------- ¦
¦ SEQUENCE
ITEM
¦
¦ 3. NUMBER REQUIRED FOR DISPATCH
¦
¦ NUMBERS
¦
¦
--------------------------------------- ¦
¦ ------------------------- ¦
¦
¦ 4. REMARKS OR EXCEPTIONS
¦
¦ 21 AIR CONDITIONING
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 30-1 Cabin Altitude
C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided:
¦
¦
Warning Light/
¦
¦
¦
a) Cabin altimeter operates
¦
¦
Annunciator
¦
¦
¦
normally, and
¦
¦
¦
¦
¦
b) Cabin altitude aural warning
¦
¦
¦
¦
¦
operates normally.
¦
¦
¦
¦
¦
OR
¦
¦
C ¦
¦
¦
c) Flight is conducted in an
¦
¦
¦
¦
¦
unpressurized configuration,
¦
¦
¦
¦
¦
and
¦
¦
¦
¦
¦
d) Ram air and dump valves
¦
¦
¦
¦
¦
operate normally.
¦
¦
¦
¦
¦
¦
¦ 30-2 Cabin Altitude
C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided:
¦
¦
Aural Warning
¦
¦
¦
a) Cabin altimeter operates
¦
¦
¦
¦
¦
normally, and
¦
¦
¦
¦
¦
b) Cabin altitude warning
¦
¦
¦
¦
¦
annunciator/light operates
¦
¦
¦
¦
¦
normally.
¦
¦
¦
¦
¦
OR
¦
¦
C ¦
¦
¦
c) Flight is conducted in an
¦
¦
¦
¦
¦
unpressurized configuration,
¦
¦
¦
¦
¦
and
¦
¦
¦
¦
¦
d) Ram air and dump valves
¦
¦
¦
¦
¦
operate normally.
¦
¦
¦
¦
¦
¦
¦ 30-3 Automatic Cabin
C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided:
¦
¦
Pressure
¦
¦
¦
a) Manual pressure control
¦
¦
Controller
¦
¦
¦
system operates normally,
¦
¦
¦
¦
¦
and
¦
¦
¦
¦
¦
b) Cabin altitude, differential
¦
¦
¦
¦
¦
pressure and rate of climb
¦
¦
¦
¦
¦
indicators operate normally.
¦
¦
¦
¦
¦
OR
¦
¦
C ¦
¦
¦
c) Flight is conducted in an
¦
¦
¦
¦
¦
unpressurized configuration,
¦
¦
¦
¦
¦
and
¦
¦
¦
¦
¦
d) Ram air and dump valves
¦
¦
¦
¦
¦
operate normally.
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
-------------------------------------------------------------------------------
------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION
¦
¦
¦
¦
MASTER MINIMUM EQUIPMENT LIST
¦
¦ FEDERAL AVIATION ADMINISTRATION
¦
¦ --------------------------------------------------------------------------- ¦
¦ AIRCRAFT:
¦ REVISION NO: 5
¦ PAGE:
¦
¦
HAWKER SIDDELEY HS-125
¦
¦
¦
¦
(SERIES 1 THROUGH 800XP)
¦ DATE: 05/30/2002
¦ 21-7
¦
¦ --------------------------------------------------------------------------- ¦
¦
1. ¦ 2. NUMBER INSTALLED
¦
¦ SYSTEM &
¦
-------------------------------------------- ¦
¦ SEQUENCE
ITEM
¦
¦ 3. NUMBER REQUIRED FOR DISPATCH
¦
¦ NUMBERS
¦
¦
--------------------------------------- ¦
¦ ------------------------- ¦
¦
¦ 4. REMARKS OR EXCEPTIONS
¦
¦ 21 AIR CONDITIONING
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 30-4 Fan Operated
C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided dump
¦
¦
Venturi
¦
¦
¦ valve operates normally.
¦
¦
¦
¦
¦
¦
¦ 30-5 Outflow/Safety
C ¦ 2 ¦ 0 ¦ (O)May be inoperative provided:
¦
¦
Valves
¦
¦
¦
a) Flight is conducted in an
¦
¦
¦
¦
¦
unpressurized configuration,
¦
¦
¦
¦
¦
and
¦
¦
¦
¦
¦
b) Ram air and dump valves
¦
¦
¦
¦
¦
operate normally.
¦
¦
¦
¦
¦
¦
¦ 30-6 Cabin Pressure
¦
¦
¦
¦
¦
Instruments
¦
¦
¦
¦
¦
(Triple Indicator
¦
¦
¦
¦
¦
or Separate
¦
¦
¦
¦
¦
Indicators)
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
1) Cabin
C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided:
¦
¦
Altimeter
¦
¦
¦
a) Cabin differential pressure
¦
¦
Indicator
¦
¦
¦
indicator operates normally,
¦
¦
¦
¦
¦
and
¦
¦
¦
¦
¦
b) A chart is provided to the
¦
¦
¦
¦
¦
flight crew to convert cabin
¦
¦
¦
¦
¦
differential pressure to
¦
¦
¦
¦
¦
cabin altitude.
¦
¦
¦
¦
¦
OR
¦
¦
C ¦
¦
¦
c) Flight is conducted in an
¦
¦
¦
¦
¦
unpressurized configuration,
¦
¦
¦
¦
¦
and
¦
¦
¦
¦
¦
d) Ram air and dump valves
¦
¦
¦
¦
¦
operate normally.
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ (Continued)
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
-------------------------------------------------------------------------------
------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION
¦
¦
¦
¦
MASTER MINIMUM EQUIPMENT LIST
¦
¦ FEDERAL AVIATION ADMINISTRATION
¦
¦ --------------------------------------------------------------------------- ¦
¦ AIRCRAFT:
¦ REVISION NO: 5
¦ PAGE:
¦
¦
HAWKER SIDDELEY HS-125
¦
¦
¦
¦
(SERIES 1 THROUGH 800XP)
¦ DATE: 05/30/2002
¦ 21-8
¦
¦ --------------------------------------------------------------------------- ¦
¦
1. ¦ 2. NUMBER INSTALLED
¦
¦ SYSTEM &
¦
-------------------------------------------- ¦
¦ SEQUENCE
ITEM
¦
¦ 3. NUMBER REQUIRED FOR DISPATCH
¦
¦ NUMBERS
¦
¦
--------------------------------------- ¦
¦ ------------------------- ¦
¦
¦ 4. REMARKS OR EXCEPTIONS
¦
¦ 21 AIR CONDITIONING
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 30-6 Cabin Pressure
¦
¦
¦
¦
¦
Instruments
¦
¦
¦
¦
¦
(Triple Indicator
¦
¦
¦
¦
¦
or Separate
¦
¦
¦
¦
¦
Indicators)
¦
¦
¦
¦
¦
(Cont'd)
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
2) Cabin
C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided:
¦
¦
Differential
¦
¦
¦
a) Cabin altimeter operates
¦
¦
Pressure
¦
¦
¦
normally, and
¦
¦
Indicator
¦
¦
¦
b) A chart is provided to the
¦
¦
¦
¦
¦
flight crew to convert cabin
¦
¦
¦
¦
¦
altitude to cabin
¦
¦
¦
¦
¦
differential pressure.
¦
¦
¦
¦
¦
OR
¦
¦
C ¦
¦
¦
c) Flight is conducted in an
¦
¦
¦
¦
¦
unpressurized configuration,
¦
¦
¦
¦
¦
and
¦
¦
¦
¦
¦
d) Ram air and dump valves
¦
¦
¦
¦
¦
operate normally.
¦
¦
¦
¦
¦
¦
¦
3) Cabin Rate of
C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided:
¦
¦
Climb Indicator
¦
¦
¦
a) All remaining instruments
¦
¦
¦
¦
¦
and functions of the press¦
¦
¦
¦
¦
urization system operate
¦
¦
¦
¦
¦
normally.
¦
¦
¦
¦
¦
OR
¦
¦
C ¦
¦
¦
b) Flight is conducted in an
¦
¦
¦
¦
¦
unpressurized configuration,
¦
¦
¦
¦
¦
and
¦
¦
¦
¦
¦
c) Ram air and dump valves
¦
¦
¦
¦
¦
operate normally.
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
-------------------------------------------------------------------------------
------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION
¦
¦
¦
¦
MASTER MINIMUM EQUIPMENT LIST
¦
¦ FEDERAL AVIATION ADMINISTRATION
¦
¦ --------------------------------------------------------------------------- ¦
¦ AIRCRAFT:
¦ REVISION NO: 5
¦ PAGE:
¦
¦
HAWKER SIDDELEY HS-125
¦
¦
¦
¦
(SERIES 1 THROUGH 800XP)
¦ DATE: 05/30/2002
¦ 21-9
¦
¦ --------------------------------------------------------------------------- ¦
¦
1. ¦ 2. NUMBER INSTALLED
¦
¦ SYSTEM &
¦
-------------------------------------------- ¦
¦ SEQUENCE
ITEM
¦
¦ 3. NUMBER REQUIRED FOR DISPATCH
¦
¦ NUMBERS
¦
¦
--------------------------------------- ¦
¦ ------------------------- ¦
¦
¦ 4. REMARKS OR EXCEPTIONS
¦
¦ 21 AIR CONDITIONING
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 30-9 Flow Control Valve
¦
¦
¦ Moved to 21-10-14, Rev. 5.
| ¦
¦
¦
¦
¦
¦
¦ 30-10 Automatic
C ¦ 2 ¦ 0 ¦ (O)May be inoperative provided:
¦
¦
Pressures
¦
¦
¦
a) Flight is conducted in an
¦
¦
Regulator
¦
¦
¦
unpressurized configuration,
¦
¦
¦
¦
¦
and
¦
¦
¦
¦
¦
b) Ram air dump valves operate
¦
¦
¦
¦
¦
normally.
¦
¦
¦
¦
¦
¦
¦ 50-1 Auxiliary Cooling C ¦ - ¦ 0 ¦ (M)(O)May be inoperative provided
| ¦
¦ *** Pack
¦
¦
¦ cabin ambient temperature is at a
| ¦
¦
¦
¦
¦ level suitable for cooling.
| ¦
¦
¦
¦
¦
¦
¦ 60-1 Temperature
¦
¦
¦
¦
¦
Control System
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
1) Automatic
C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided the
¦
¦
¦
¦
¦ manual control system operates
¦
¦
¦
¦
¦ normally.
¦
¦
¦
¦
¦
¦
¦
2) Manual
C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided the
¦
¦
¦
¦
¦ automatic control system operates
¦
¦
¦
¦
¦ normally.
¦
¦
¦
¦
¦
¦
¦ 60-2 Cabin Temperature C ¦ 1 ¦ 0 ¦
¦
¦
Indicator
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
-------------------------------------------------------------------------------
------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION
¦
¦
¦
¦
MASTER MINIMUM EQUIPMENT LIST
¦
¦ FEDERAL AVIATION ADMINISTRATION
¦
¦ --------------------------------------------------------------------------- ¦
¦ AIRCRAFT:
¦ REVISION NO: 5
¦ PAGE:
¦
¦
HAWKER SIDDELEY HS-125
¦
¦
¦
¦
(SERIES 1 THROUGH 800XP)
¦ DATE: 05/30/2002
¦ 21-10
¦
¦ --------------------------------------------------------------------------- ¦
¦
1. ¦ 2. NUMBER INSTALLED
¦
¦ SYSTEM &
¦
-------------------------------------------- ¦
¦ SEQUENCE
ITEM
¦
¦ 3. NUMBER REQUIRED FOR DISPATCH
¦
¦ NUMBERS
¦
¦
--------------------------------------- ¦
¦ ------------------------- ¦
¦
¦ 4. REMARKS OR EXCEPTIONS
¦
¦ 21 AIR CONDITIONING
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 60-3 Cabin Duct
C ¦ 1 ¦ 0 ¦
¦
¦
Temperature
¦
¦
¦
¦
¦
Indicator
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 60-4 Turbine Unit
C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided:
¦
¦
Bypass Valve
¦
¦
¦
a) Flight is conducted in an
¦
¦
(Series 1 Through
¦
¦
¦
unpressurized configuration, | ¦
¦
800)/Low Limit
¦
¦
¦
and
| ¦
¦
Temp Control Valve
¦
¦
¦
b) Ram air and dump valves
| ¦
¦
(Series 800XP)
¦
¦
¦
operate normally.
| ¦
¦
¦
¦
¦
¦
¦ 60-5 Cabin Flood
¦
¦
¦
¦
¦
Control
¦
¦
¦ Deleted in Rev. 5.
| ¦
¦
Valve/Flood Flow
¦
¦
¦
¦
¦
Valve
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 60-6 Cabin/VIP
D ¦ - ¦ 0 ¦ (O)May be inoperative provided the | ¦
¦
Temperature
¦
¦
¦ temperature control system
| ¦
¦
Control Switch
¦
¦
¦ operates normally from the
| ¦
¦
¦
¦
¦ cockpit.
| ¦
¦
¦
¦
¦
¦
¦ 60-7 Refrigeration Unit C ¦ 1 ¦ 0 ¦ (O)May be inoperative
| ¦
¦
Bypass Valve (RBV)
¦
¦
¦ provided:
| ¦
¦
(Series 1 Through
¦
¦
¦
a) Ram air and dump valves
| ¦
¦
800)/Cabin
¦
¦
¦
operate normally, and
| ¦
¦
Temperature Control ¦
¦
¦
b) Flight is conducted in an
| ¦
¦
Valve (Series
¦
¦
¦
unpressurized configuration. | ¦
¦
800XP)
¦
¦
¦
| ¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
-------------------------------------------------------------------------------
------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION
¦
¦
¦
¦
MASTER MINIMUM EQUIPMENT LIST
¦
¦ FEDERAL AVIATION ADMINISTRATION
¦
¦ --------------------------------------------------------------------------- ¦
¦ AIRCRAFT:
¦ REVISION NO: 5
¦ PAGE:
¦
¦
HAWKER SIDDELEY HS-125
¦
¦
¦
¦
(SERIES 1 THROUGH 800XP)
¦ DATE: 05/30/2002
¦ 22-1
¦
¦ --------------------------------------------------------------------------- ¦
¦
1. ¦ 2. NUMBER INSTALLED
¦
¦ SYSTEM &
¦
-------------------------------------------- ¦
¦ SEQUENCE
ITEM
¦
¦ 3. NUMBER REQUIRED FOR DISPATCH
¦
¦ NUMBERS
¦
¦
--------------------------------------- ¦
¦ ------------------------- ¦
¦
¦ 4. REMARKS OR EXCEPTIONS
¦
¦ 22 AUTO FLIGHT
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 10-1 Autopilot System
B ¦ 1 ¦ 0 ¦ May be inoperative provided
| ¦
¦
¦
¦
¦ approach minimums do not require
¦
¦
¦
¦
¦ its use.
| ¦
¦
¦
¦
¦
¦
¦
C ¦ - ¦ 1 ¦
| ¦
¦
¦
¦
¦
¦
¦
B ¦ - ¦ 0 ¦ NOTE 1: Any mode which functions
| ¦
¦
¦
¦
¦
normally may be used.
| ¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ NOTE 2: For operations within RVSM | ¦
¦
¦
¦
¦
airspace, the following
| ¦
¦
¦
¦
¦
items must be operating:
| ¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
a) 2 ADC's
| ¦
¦
¦
¦
¦
b) 1 ATC Transponder
| ¦
¦
¦
¦
¦
c) 1 A/P Altitude Hold
| ¦
¦
¦
¦
¦
function, and
| ¦
¦
¦
¦
¦
d) 1 Altitude Alerter.
| ¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ NOTE 3: Flying below, above or
| ¦
¦
¦
¦
¦
crossing RVSM airspace does | ¦
¦
¦
¦
¦
not require the above items | ¦
¦
¦
¦
¦
to be operating.
| ¦
¦
¦
¦
¦
¦
¦ 10-2 Yaw Damp/AutoC ¦ 1 ¦ 0 ¦ May be inoperative provided both
| ¦
¦
pilot Controller
¦
¦
¦ Autopilot Control Wheel disengage
| ¦
¦
Disconnect Switch
¦
¦
¦ switches operate normally.
| ¦
¦
Bar (Collins
¦
¦
¦
| ¦
¦
Avionics Equipped
¦
¦
¦
| ¦
¦
Aircraft Only)
¦
¦
¦
| ¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
-------------------------------------------------------------------------------
------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION
¦
¦
¦
¦
MASTER MINIMUM EQUIPMENT LIST
¦
¦ FEDERAL AVIATION ADMINISTRATION
¦
¦ --------------------------------------------------------------------------- ¦
¦ AIRCRAFT:
¦ REVISION NO: 5
¦ PAGE:
¦
¦
HAWKER SIDDELEY HS-125
¦
¦
¦
¦
(SERIES 1 THROUGH 800XP)
¦ DATE: 05/30/2002
¦ 22-2
¦
¦ --------------------------------------------------------------------------- ¦
¦
1. ¦ 2. NUMBER INSTALLED
¦
¦ SYSTEM &
¦
-------------------------------------------- ¦
¦ SEQUENCE
ITEM
¦
¦ 3. NUMBER REQUIRED FOR DISPATCH
¦
¦ NUMBERS
¦
¦
--------------------------------------- ¦
¦ ------------------------- ¦
¦
¦ 4. REMARKS OR EXCEPTIONS
¦
¦ 22 AUTO FLIGHT
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 10-3 Autopilot Control C ¦ 2 ¦ 1 ¦ (O)One may be inoperative provided
¦
¦
Wheel Disengage
¦
¦
¦ autopilot is not used below 1,500
¦
¦
Switches
¦
¦
¦ feet AGL.
¦
¦
¦
¦
¦
¦
¦
C ¦ 2 ¦ 0 ¦ May be inoperative provided auto¦
¦
¦
¦
¦ pilot is not used.
¦
¦
¦
¦
¦
¦
¦ 10-4 Autopilot
C ¦ - ¦ 0 ¦ May be inoperative provided:
¦
¦
Disconnect
¦
¦
¦
a) Autopilot is not used below
¦
¦
Annunciator Lights
¦
¦
¦
1,500 feet AGL, and
¦
¦
¦
¦
¦
b) All remaining A/P disengage¦
¦
¦
¦
¦
ment alerts operate
¦
¦
¦
¦
¦
normally.
¦
¦
C ¦
¦
¦
OR
¦
¦
¦
¦
¦
c) Autopilot is not used.
¦
¦
¦
¦
¦
¦
¦ 10-5 Touch Control
C ¦ 2 ¦ 0 ¦ (O)May be inoperative provided
¦
¦ *** Steering (TCS)
¦
¦
¦ system is verified OFF.
| ¦
¦
¦
¦
¦
¦
¦ 10-6 Go Around (GA)
C ¦ 2 ¦ 1 ¦ One may be inoperative provided
¦
¦
Switches
¦
¦
¦ approach minimums do not require
¦
¦
¦
¦
¦ its use.
¦
¦
¦
¦
¦
¦
¦
C ¦ 2 ¦ 0 ¦ (O)May be inoperative provided:
¦
¦
¦
¦
¦
a) Autopilot is not used for
¦
¦
¦
¦
¦
approach below 500 feet AGL,
¦
¦
¦
¦
¦
and
¦
¦
¦
¦
¦
b) Alternate procedures are
¦
¦
¦
¦
¦
established and used.
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
-------------------------------------------------------------------------------
------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION
¦
¦
¦
¦
MASTER MINIMUM EQUIPMENT LIST
¦
¦ FEDERAL AVIATION ADMINISTRATION
¦
¦ --------------------------------------------------------------------------- ¦
¦ AIRCRAFT:
¦ REVISION NO: 5
¦ PAGE:
¦
¦
HAWKER SIDDELEY HS-125
¦
¦
¦
¦
(SERIES 1 THROUGH 800XP)
¦ DATE: 05/30/2002
¦ 22-3
¦
¦ --------------------------------------------------------------------------- ¦
¦
1. ¦ 2. NUMBER INSTALLED
¦
¦ SYSTEM &
¦
-------------------------------------------- ¦
¦ SEQUENCE
ITEM
¦
¦ 3. NUMBER REQUIRED FOR DISPATCH
¦
¦ NUMBERS
¦
¦
--------------------------------------- ¦
¦ ------------------------- ¦
¦
¦ 4. REMARKS OR EXCEPTIONS
¦
¦ 22 AUTO FLIGHT
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 10-7 Pitch/Roll Switch C ¦ 2 ¦ 1 ¦ (O) May be inoperative provided
| ¦
¦
(Series 800 and
¦
¦
¦ Autopilot Controller operates
| ¦
¦
800XP Only with
¦
¦
¦ normally.
| ¦
¦
Collins A/P)
¦
¦
¦
| ¦
¦
¦
¦
¦
¦
¦ 10-8 A/P Flap
C ¦ 2 ¦ 1 ¦
| ¦
¦
Annuciator
¦
¦
¦
| ¦
¦
(Honeywell Equipped ¦
¦
¦
| ¦
¦
Aircraft Only)
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
C ¦ 2 ¦ 0 ¦ (O)May be inoperative provided the | ¦
¦
¦
¦
¦ autopilot flight director is not
| ¦
¦
¦
¦
¦ used with flaps extended.
| ¦
¦
¦
¦
¦
¦
¦ 20-1 Yaw Damper System C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided the
¦
¦
¦
¦
¦ airplane is operated in accordance
¦
¦
¦
¦
¦ with AFM Limitations.
¦
¦
¦
¦
¦
¦
¦ 20-2 Aileron Out-of¦
¦
¦ Deleted Revision 5.
| ¦
¦
Trim Annunciators
¦
¦
¦
| ¦
¦
¦
¦
¦
¦
¦ 20-3 Elevator Out-of¦
¦
¦ Deleted Revision 5.
| ¦
¦
Trim Annunciators
¦
¦
¦
| ¦
¦
¦
¦
¦
¦
¦ 20-4 Autopilot Trim
C ¦ 2 ¦ 0 ¦ (O)May be inoperative provided
| ¦
¦
Annunciators
¦
¦
¦ autopilot is not used.
| ¦
¦
(Aircraft With
¦
¦
¦
| ¦
¦
Digital Avionics
¦
¦
¦
| ¦
¦
Only)
¦
¦
¦
| ¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
-------------------------------------------------------------------------------
------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION
¦
¦
¦
¦
MASTER MINIMUM EQUIPMENT LIST
¦
¦ FEDERAL AVIATION ADMINISTRATION
¦
¦ --------------------------------------------------------------------------- ¦
¦ AIRCRAFT:
¦ REVISION NO: 5
¦ PAGE:
¦
¦
HAWKER SIDDELEY HS-125
¦
¦
¦
¦
(SERIES 1 THROUGH 800XP)
¦ DATE: 05/30/2002
¦ 22-4
¦
¦ --------------------------------------------------------------------------- ¦
¦
1. ¦ 2. NUMBER INSTALLED
¦
¦ SYSTEM &
¦
-------------------------------------------- ¦
¦ SEQUENCE
ITEM
¦
¦ 3. NUMBER REQUIRED FOR DISPATCH
¦
¦ NUMBERS
¦
¦
--------------------------------------- ¦
¦ ------------------------- ¦
¦
¦ 4. REMARKS OR EXCEPTIONS
¦
¦ 22 AUTO FLIGHT
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 20-5 Autopilot Aileron
¦
¦
¦
¦
¦
Trim Indicator
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
1) Series 1
C ¦ 1 ¦ 0 ¦ May be inoperative provided
| ¦
¦
Through 700
¦
¦
¦ autopilot is not used.
| ¦
¦
Only
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 20-6 Autopilot Elevator
¦
¦
¦
¦
¦
Trim Indicator
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
1) Series 1
C ¦ 1 ¦ 0 ¦ May be inoperative provided
| ¦
¦
Through 700
¦
¦
¦ autopilot is not used.
| ¦
¦
Only
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
-------------------------------------------------------------------------------
------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION
¦
¦
¦
¦
MASTER MINIMUM EQUIPMENT LIST
¦
¦ FEDERAL AVIATION ADMINISTRATION
¦
¦ --------------------------------------------------------------------------- ¦
¦ AIRCRAFT:
¦ REVISION NO: 5
¦ PAGE:
¦
¦
HAWKER SIDDELEY HS-125
¦
¦
¦
¦
(SERIES 1 THROUGH 800XP)
¦ DATE: 05/30/2002
¦ 22-5
¦
¦ --------------------------------------------------------------------------- ¦
¦
1. ¦ 2. NUMBER INSTALLED
¦
¦ SYSTEM &
¦
-------------------------------------------- ¦
¦ SEQUENCE
ITEM
¦
¦ 3. NUMBER REQUIRED FOR DISPATCH
¦
¦ NUMBERS
¦
¦
--------------------------------------- ¦
¦ ------------------------- ¦
¦
¦ 4. REMARKS OR EXCEPTIONS
¦
¦ 22 AUTO FLIGHT
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 20-7 Guidance
C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided:
¦
¦
Controller
¦
¦
¦
a) Approach minimums do not
¦
¦
(Honeywell
¦
¦
¦
require its use, and
¦
¦
SPZ-8000 and
¦
¦
¦
b) AFM limitations are
| ¦
¦
Collins APS-85 and
¦
¦
¦
observed.
| ¦
¦
Collins Proline
¦
¦
¦
| ¦
¦
21 Equipped
¦
¦
¦ NOTE 1: Autopilot and yaw damper
| ¦
¦
Aircraft)
¦
¦
¦
will not be available.
| ¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ NOTE 2: For operations within RVSM | ¦
¦
¦
¦
¦
airspace, the following
| ¦
¦
¦
¦
¦
items must be operating:
| ¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
a) 2 ADC's
| ¦
¦
¦
¦
¦
b) 1 ATC Transponder
| ¦
¦
¦
¦
¦
c) 1 A/P Altitude Hold
| ¦
¦
¦
¦
¦
Function, and
| ¦
¦
¦
¦
¦
d) 1 Altitude Alerter.
| ¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ NOTE 3: Flying below, above or
| ¦
¦
¦
¦
¦
crossing RVSM airspace does | ¦
¦
¦
¦
¦
not require the above items | ¦
¦
¦
¦
¦
to be operating.
| ¦
¦
¦
¦
¦
¦
¦ 20-8 Mach Trim System
¦
¦
¦ Moved this item to ATA 27-30-5,
| ¦
¦
¦
¦
¦ Revision 5.
| ¦
¦
¦
¦
¦
¦
¦ 20-9 Mode Select
C ¦ - ¦ 0 ¦ May be inoperative provided
| ¦
¦
Panel
¦
¦
¦ autopilot is not used.
| ¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
-------------------------------------------------------------------------------
------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION
¦
¦
¦
¦
MASTER MINIMUM EQUIPMENT LIST
¦
¦ FEDERAL AVIATION ADMINISTRATION
¦
¦ --------------------------------------------------------------------------- ¦
¦ AIRCRAFT:
¦ REVISION NO: 5
¦ PAGE:
¦
¦
HAWKER SIDDELEY HS-125
¦
¦
¦
¦
(SERIES 1 THROUGH 800XP)
¦ DATE: 05/30/2002
¦ 23-1
¦
¦ --------------------------------------------------------------------------- ¦
¦
1. ¦ 2. NUMBER INSTALLED
¦
¦ SYSTEM &
¦
-------------------------------------------- ¦
¦ SEQUENCE
ITEM
¦
¦ 3. NUMBER REQUIRED FOR DISPATCH
¦
¦ NUMBERS
¦
¦
--------------------------------------- ¦
¦ ------------------------- ¦
¦
¦ 4. REMARKS OR EXCEPTIONS
¦
¦ 23 COMMUNICATIONS
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 05-1 Radio Management
C ¦ 2 ¦ 1 ¦ (O)One may be inoperative provided:
¦
¦
Unit (RMU)/
¦
¦
¦
a) Remaining RMU/RTU operates
¦
¦
Radio Tuning Unit
¦
¦
¦
normally,
¦
¦
(RTU)
¦
¦
¦
b) Alternate procedures are
¦
¦
¦
¦
¦
established and used.
¦
¦
¦
¦
¦
¦
¦ 10-1 Communications
D ¦ - ¦ - ¦ Any in excess of those required by | ¦
¦
System (VHF, UHF)
¦
¦
¦ FAR may be inoperative provided it | ¦
¦
¦
¦
¦ is not powered by the Emergency AC | ¦
¦
¦
¦
¦ Bus, Emergency DC Bus, Battery Bus, | ¦
¦
¦
¦
¦ Battery Direct Bus, or the TC
| ¦
¦
¦
¦
¦ Transfer Bus and not required for
| ¦
¦
¦
¦
¦ emergency procedures.
| ¦
¦
¦
¦
¦
¦
¦
1) VHF Comm
¦
¦
¦
| ¦
¦
¦
¦
¦
| ¦
¦
a) Frequency
C ¦ - ¦ 0 ¦
| ¦
¦
Transfer Light ¦
¦
¦
| ¦
¦
¦
¦
¦
¦
¦
b) Frequency
C ¦ - ¦ 0 ¦
| ¦
¦
Transfer
¦
¦
¦
| ¦
¦
Switch
¦
¦
¦
| ¦
¦
¦
¦
¦
¦
¦
c) Frequency
C ¦ - ¦ 0 ¦
| ¦
¦
Selector
¦
¦
¦
| ¦
¦
Knob
¦
¦
¦
| ¦
¦
¦
¦
¦
¦
¦
d) Frequency
C ¦ - ¦ 0 ¦
| ¦
¦
Indication
¦
¦
¦
| ¦
¦
¦
¦
¦
¦
¦
2) HF Comm
¦
¦
¦ (O)May be inoperative while cond| ¦
¦
¦
¦
¦ ucting operations that require two | ¦
¦
¦
¦
¦ LRCS provided:
| ¦
¦
¦
¦
¦
a) SATCOM (High or Low Gain)
| ¦
¦
¦
¦
¦
Data Link system operates
| ¦
¦
¦
¦
¦
normally, and
| ¦
¦
¦
¦
¦
b) SATCOM Data Link Commuica| ¦
¦
¦
¦
¦
tion operates normally over | ¦
¦
¦
¦
¦
the intended route of
| ¦
¦
¦
¦
¦
Flight.
| ¦
¦
¦
¦
¦
¦
-------------------------------------------------------------------------------
------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION
¦
¦
¦
¦
MASTER MINIMUM EQUIPMENT LIST
¦
¦ FEDERAL AVIATION ADMINISTRATION
¦
¦ --------------------------------------------------------------------------- ¦
¦ AIRCRAFT:
¦ REVISION NO: 5
¦ PAGE:
¦
¦
HAWKER SIDDELEY HS-125
¦
¦
¦
¦
(SERIES 1 THROUGH 800XP)
¦ DATE: 05/30/2002
¦ 23-2
¦
¦ --------------------------------------------------------------------------- ¦
¦
1. ¦ 2. NUMBER INSTALLED
¦
¦ SYSTEM &
¦
-------------------------------------------- ¦
¦ SEQUENCE
ITEM
¦
¦ 3. NUMBER REQUIRED FOR DISPATCH
¦
¦ NUMBERS
¦
¦
--------------------------------------- ¦
¦ ------------------------- ¦
¦
¦ 4. REMARKS OR EXCEPTIONS
¦
¦ 23 COMMUNICATIONS
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 10-2 Audio Control
C ¦ - ¦ 2 ¦ (O)Any in excess of those required
¦
¦
Panels
¦
¦
¦ at pilot and copilot's seat
| ¦
¦
¦
¦
¦ positions may be inoperative
| ¦
¦
¦
¦
¦ provided alternate procedures are
¦
¦
¦
¦
¦ established and used.
¦
¦
¦
¦
¦
¦
¦ 10-3 Standby Nav/Comm
C ¦ 1 ¦ 0 ¦ May be inoperative provided primary | ¦
¦
Controller
¦
¦
¦ means for tuning Nav/Comm radios
| ¦
¦
(Clearance
¦
¦
¦ operates normally.
| ¦
¦
Delivery Unit)
¦
¦
¦
| ¦
¦
¦
¦
¦
¦
¦ 20-1 Selective Call
C ¦ - ¦ 0 ¦
¦
¦ *** System (SELCAL)
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 20-2 ACARS System
C ¦ 1 ¦ 0 ¦ May be inoperative provided
¦
¦ ***
¦
¦
¦ alternate procedures are
¦
¦
¦
¦
¦ established and used.
¦
¦
¦
¦
¦
¦
¦ 20-3 AFIS (VHF/SAT)
C ¦ - ¦ 0 ¦ May be inoperative provided
¦
¦ ***
¦
¦
¦ alternate procedures are
¦
¦
¦
¦
¦ established and used.
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
-------------------------------------------------------------------------------
------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION
¦
¦
¦
¦
MASTER MINIMUM EQUIPMENT LIST
¦
¦ FEDERAL AVIATION ADMINISTRATION
¦
¦ --------------------------------------------------------------------------- ¦
¦ AIRCRAFT:
¦ REVISION NO: 5
¦ PAGE:
¦
¦
HAWKER SIDDELEY HS-125
¦
¦
¦
¦
(SERIES 1 THROUGH 800XP)
¦ DATE: 05/30/2002
¦ 23-3
¦
¦ --------------------------------------------------------------------------- ¦
¦
1. ¦ 2. NUMBER INSTALLED
¦
¦ SYSTEM &
¦
-------------------------------------------- ¦
¦ SEQUENCE
ITEM
¦
¦ 3. NUMBER REQUIRED FOR DISPATCH
¦
¦ NUMBERS
¦
¦
--------------------------------------- ¦
¦ ------------------------- ¦
¦
¦ 4. REMARKS OR EXCEPTIONS
¦
¦ 23 COMMUNICATIONS
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 30-1 Passenger Address
¦
¦
¦
¦
¦
System
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
1) Passenger
C ¦ 1 ¦ 0 ¦ (0)May be inoperative provided:
| ¦
¦
Configuration
¦
¦
¦
a) Alternate, normal and emer¦
¦
¦
¦
¦
gency procedures, and/or
¦
¦
¦
¦
¦
operating restrictions are
¦
¦
¦
¦
¦
established and used, and
¦
¦
¦
¦
¦
b) Flight Deck/Cabin Interphone
¦
¦
¦
¦
¦
system operates normally.
¦
¦
¦
¦
¦
¦
¦
2) Cargo
D ¦ 1 ¦ 0 ¦
¦
¦
Configuration
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 30-2 Cabin Chimes
C ¦ - ¦ 0 ¦ (O)May be inoperative provided:
¦
¦
¦
¦
¦
a) Passenger address system
¦
¦
¦
¦
¦
operates normally.
¦
¦
¦
¦
¦
OR
¦
¦
C ¦
¦
¦
b) Alternate procedures are
¦
¦
¦
¦
¦
established and used.
¦
¦
¦
¦
¦
¦
¦ 30-3 Prerecorded
C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided
¦
¦ *** Passenger
¦
¦
¦ alternate procedures are
¦
¦
Announcement
¦
¦
¦ established and used.
¦
¦
System
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 30-4 Flight Deck
C ¦ - ¦ 0 ¦ May be inoperative provided:
¦
¦
Speakers
¦
¦
¦
a) Procedures do not require
¦
¦
¦
¦
¦
their use, and
¦
¦
¦
¦
¦
b) Headsets are installed and
¦
¦
¦
¦
¦
operate normally.
¦
¦
¦
¦
¦
¦
¦ 30-5 Emergency Locator D ¦ - ¦ - ¦ As required by FAR.
| ¦
¦ *** Transmitter (ELT)
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
-------------------------------------------------------------------------------
------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION
¦
¦
¦
¦
MASTER MINIMUM EQUIPMENT LIST
¦
¦ FEDERAL AVIATION ADMINISTRATION
¦
¦ --------------------------------------------------------------------------- ¦
¦ AIRCRAFT:
¦ REVISION NO: 5
¦ PAGE:
¦
¦
HAWKER SIDDELEY HS-125
¦
¦
¦
¦
(SERIES 1 THROUGH 800XP)
¦ DATE: 05/30/2002
¦ 23-4
¦
¦ --------------------------------------------------------------------------- ¦
¦
1. ¦ 2. NUMBER INSTALLED
¦
¦ SYSTEM &
¦
-------------------------------------------- ¦
¦ SEQUENCE
ITEM
¦
¦ 3. NUMBER REQUIRED FOR DISPATCH
¦
¦ NUMBERS
¦
¦
--------------------------------------- ¦
¦ ------------------------- ¦
¦
¦ 4. REMARKS OR EXCEPTIONS
¦
¦ 23 COMMUNICATIONS
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 40-1 Service Interphone C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided:
¦
¦
System (Flight
¦
¦
¦
a) Alternate procedures are
¦
¦
Deck to Cabin)
¦
¦
¦
established and used, and
¦
¦
(Cabin to Flight
¦
¦
¦
b) PA system operates normally.
¦
¦
Deck) (Flight Deck
¦
¦
¦
¦
¦
to Ground)
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
C ¦ - ¦ 0 ¦ As required by FAR.
| ¦
¦
¦
¦
¦
¦
¦ 50-1 Headsets
C ¦ - ¦ 1 ¦ One may be inoperative at either
¦
¦
¦
¦
¦ pilot's station provided speaker
¦
¦
¦
¦
¦ system operates normally.
¦
¦
¦
¦
¦
¦
¦ 50-2 Microphones
C ¦ - ¦ - ¦ Any in excess of those required by
¦
¦
¦
¦
¦ FAR may be inoperative.
¦
¦
¦
¦
¦
¦
¦ 50-3 Boom Microphones
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
1) Cockpit Voice
A ¦ - ¦ 0 ¦ May be inoperative provided:
¦
¦
Recorder
¦
¦
¦
a) Flight Data Recorder (FDR)
¦
¦
Equipped To
¦
¦
¦
operates normally, and
¦
¦
Record Boom
¦
¦
¦
b) Repairs are made within
¦
¦
Microphone Per
¦
¦
¦
three flight days.
¦
¦
FAR 121.359(e),
¦
¦
¦
¦
¦
135.151(d) or
¦
¦
¦
¦
¦
125.227(e)
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ *** 2) Cockpit Voice
D ¦ - ¦ 0 ¦ Any in excess of those required by | ¦
¦
Recorder Not
¦
¦
¦ FAR may be inoperative.
| ¦
¦
Equipped to
¦
¦
¦
¦
¦
Record Boom
¦
¦
¦
¦
¦
Microphone
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 50-4 Glareshield
D ¦ 2 ¦ 0 ¦ (O)May be inoperative provided
| ¦
¦ *** Microphone
¦
¦
¦ alternate procedures are
| ¦
¦
Switches
¦
¦
¦ established and used.
| ¦
¦
¦
¦
¦
¦
¦ 50-5 Flight Deck
D ¦ 1 ¦ 0 ¦ (O)May be inoperative provided
| ¦
¦ *** Interphone System
¦
¦
¦ alternate procedures are
| ¦
¦
¦
¦
¦ established and used.
| ¦
¦
¦
¦
¦
¦
-------------------------------------------------------------------------------
------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION
¦
¦
¦
¦
MASTER MINIMUM EQUIPMENT LIST
¦
¦ FEDERAL AVIATION ADMINISTRATION
¦
¦ --------------------------------------------------------------------------- ¦
¦ AIRCRAFT:
¦ REVISION NO: 5
¦ PAGE:
¦
¦
HAWKER SIDDELEY HS-125
¦
¦
¦
¦
(SERIES 1 THROUGH 800XP)
¦ DATE: 05/30/2002
¦ 23-5
¦
¦ --------------------------------------------------------------------------- ¦
¦
1. ¦ 2. NUMBER INSTALLED
¦
¦ SYSTEM &
¦
-------------------------------------------- ¦
¦ SEQUENCE
ITEM
¦
¦ 3. NUMBER REQUIRED FOR DISPATCH
¦
¦ NUMBERS
¦
¦
--------------------------------------- ¦
¦ ------------------------- ¦
¦
¦ 4. REMARKS OR EXCEPTIONS
¦
¦ 23 COMMUNICATIONS
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 60-1 Static Dischargers C ¦ - ¦ - ¦ One discharger from each group or
¦
¦
¦
¦
¦ area may be missing.
¦
¦
¦
¦
¦
¦
¦ 70-1 Cockpit Voice
C ¦ - ¦ 0 ¦ As required by FAR.
| ¦
¦
Recorder (CVR)
¦
¦
¦
¦
¦
System
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
1) Cockpit Voice
A ¦ - ¦ 0 ¦ May be inoperative provided repairs | ¦
¦
Recorder
¦
¦
¦ are made within three flight days. | ¦
¦
Equipped To
¦
¦
¦
| ¦
¦
Record Boom
¦
¦
¦
| ¦
¦
Microphone
¦
¦
¦
| ¦
¦
¦
¦
¦
¦
¦ *** 2) Cockpit Voice
D ¦ - ¦ 0 ¦ Any in excess of those required by | ¦
¦
Recorder Not
¦
¦
¦ FAR may be inoperative.
| ¦
¦
Equipped To
¦
¦
¦
| ¦
¦
Record Boom
¦
¦
¦
| ¦
¦
Microphone
¦
¦
¦
| ¦
¦
¦
¦
¦
¦
¦ 70-2 Flight Phone
¦
¦
¦
| ¦
¦ ***
¦
¦
¦
¦
¦
1) Cockpit
D ¦ - ¦ 0 ¦
| ¦
¦
¦
¦
¦
¦
¦
2) Cabin
D ¦ - ¦ 0 ¦
| ¦
¦
¦
¦
¦
¦
¦ 70-3 Satellite
D ¦ - ¦ 0 ¦ (O)May be inoperative provided:
¦
¦ *** Communications
¦
¦
¦
a) Alternate procedures are
¦
¦
Systems (SATCOM)
¦
¦
¦
established and used.
¦
¦
¦
¦
¦
OR
¦
¦
¦
¦
¦
b) Procedures do not require
¦
¦
¦
¦
¦
its use.
¦
¦
¦
¦
¦
¦
¦ 80-1 Heads Up
D ¦ - ¦ 0 ¦ (O)May be inoperative provided
¦
¦ *** Technology Inc.,
¦
¦
¦ alternate procedures are
| ¦
¦
Checklist System
¦
¦
¦ established and used.
| ¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ NOTE: Any activation switch which
¦
¦
¦
¦
¦
functions normally may be
¦
¦
¦
¦
¦
used.
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
-------------------------------------------------------------------------------
------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION
¦
¦
¦
¦
MASTER MINIMUM EQUIPMENT LIST
¦
¦ FEDERAL AVIATION ADMINISTRATION
¦
¦ --------------------------------------------------------------------------- ¦
¦ AIRCRAFT:
¦ REVISION NO: 5
¦ PAGE:
¦
¦
HAWKER SIDDELEY HS-125
¦
¦
¦
¦
(SERIES 1 THROUGH 800XP)
¦ DATE: 05/30/2002
¦ 24-1
¦
¦ --------------------------------------------------------------------------- ¦
¦
1. ¦ 2. NUMBER INSTALLED
¦
¦ SYSTEM &
¦
-------------------------------------------- ¦
¦ SEQUENCE
ITEM
¦
¦ 3. NUMBER REQUIRED FOR DISPATCH
¦
¦ NUMBERS
¦
¦
--------------------------------------- ¦
¦ ------------------------- ¦
¦
¦ 4. REMARKS OR EXCEPTIONS
¦
¦ 24 ELECTRICAL POWER
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 20-1 AC Main Inverters C ¦ 2 ¦ 1 ¦ (O)One may be inoperative provided: | ¦
¦
¦
¦
¦
a) Standby inverter is verified
¦
¦
¦
¦
¦
to operate normally before
¦
¦
¦
¦
¦
each departure, and
¦
¦
¦
¦
¦
b) Both AC alternators operate | ¦
¦
¦
¦
¦
normally.
| ¦
¦
¦
¦
¦
¦
¦ 20-3 Standby Inverter
C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided both
¦
¦
¦
¦
¦ main inverters operate normally.
¦
¦
¦
¦
¦
¦
¦ 20-4 Inverter Fail
C ¦ 2 ¦ 0 ¦ (O)May be inoperative provided:
¦
¦
Lights/
¦
¦
¦
a) Auto-changeover system
¦
¦
Annunciators
¦
¦
¦
operates normally,
¦
¦
¦
¦
¦
b) Both main inverters operate
¦
¦
¦
¦
¦
normally, and
¦
¦
¦
¦
¦
c) AC voltmeter is installed
¦
¦
¦
¦
¦
and operates normally.
¦
¦
¦
¦
¦
¦
¦ 20-5 Standby Inverter
C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided
¦
¦
"ON" Light/
¦
¦
¦ standby inverter is verified to
¦
¦
Annunciator
¦
¦
¦ operate normally before each
¦
¦
¦
¦
¦ departure.
¦
¦
¦
¦
¦
¦
¦ 20-6 AC Voltmeter
C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided:
¦
¦
¦
¦
¦
a) All inverters operate
¦
¦
¦
¦
¦
normally,and
¦
¦
¦
¦
¦
b) All AC system annunciators
¦
¦
¦
¦
¦
operate normally.
¦
¦
¦
¦
¦
¦
¦ 20-7 AC Frequency Meter C ¦ - ¦ 0 ¦ May be inoperative provided elec¦
¦
(Series 600 and
¦
¦
¦ trical busbar fail lights operate
| ¦
¦
700 Only)
¦
¦
¦ normally.
| ¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
-------------------------------------------------------------------------------
------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION
¦
¦
¦
¦
MASTER MINIMUM EQUIPMENT LIST
¦
¦ FEDERAL AVIATION ADMINISTRATION
¦
¦ --------------------------------------------------------------------------- ¦
¦ AIRCRAFT:
¦ REVISION NO: 5
¦ PAGE:
¦
¦
HAWKER SIDDELEY HS-125
¦
¦
¦
¦
(SERIES 1 THROUGH 800XP)
¦ DATE: 05/30/2002
¦ 24-2
¦
¦ --------------------------------------------------------------------------- ¦
¦
1. ¦ 2. NUMBER INSTALLED
¦
¦ SYSTEM &
¦
-------------------------------------------- ¦
¦ SEQUENCE
ITEM
¦
¦ 3. NUMBER REQUIRED FOR DISPATCH
¦
¦ NUMBERS
¦
¦
--------------------------------------- ¦
¦ ------------------------- ¦
¦
¦ 4. REMARKS OR EXCEPTIONS
¦
¦ 24 ELECTRICAL POWER
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 20-8 AC Generator
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
1) Aircraft with
C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided:
¦
¦
One AC
¦
¦
¦
a) AFM Limitations are
¦
¦
Generator
¦
¦
¦
observed,
¦
¦
¦
¦
¦
b) Windshield fluid de-icing
¦
¦
¦
¦
¦
system is installed and
¦
¦
¦
¦
¦
operates normally, and
¦
¦
¦
¦
¦
c) Aircraft is not operated in
¦
¦
¦
¦
¦
known or forecast icing
¦
¦
¦
¦
¦
conditions.
¦
¦
¦
¦
¦
¦
¦
2) Aircraft with
C ¦ 2 ¦ 1 ¦ (O)One may be inoperative provided: | ¦
¦
Two AC
¦
¦
¦
a) Both Main AC inverters
| ¦
¦
Generators
¦
¦
¦
operate normally, and
| ¦
¦
¦
¦
¦
b) Aircraft is not operated in
¦
¦
¦
¦
¦
known or forecast icing
¦
¦
¦
¦
¦
conditions.
¦
¦
¦
¦
¦
¦
¦ 20-9 AC Generator Fail
¦
¦
¦
¦
¦
Warning Light/
¦
¦
¦
¦
¦
Annunciator(s)
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
1) Aircraft with
C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided both
¦
¦
One AC
¦
¦
¦ windshield heating systems operate
¦
¦
Generator
¦
¦
¦ normally.
¦
¦
¦
¦
¦
¦
¦
2) Aircraft with
C ¦ 2 ¦ 0 ¦ (O)May be inoperative provided:
¦
¦
Two AC
¦
¦
¦
a) Both AC generators operate
¦
¦
Generators
¦
¦
¦
normally, and
¦
¦
¦
¦
¦
b) Auto-changeover system
¦
¦
¦
¦
¦
operates normally.
¦
¦
¦
¦
¦
¦
¦ 10. Engine Driven
¦
¦
¦ Deleted, Rev. 3.
¦
¦
Generators
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
-------------------------------------------------------------------------------
------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION
¦
¦
¦
¦
MASTER MINIMUM EQUIPMENT LIST
¦
¦ FEDERAL AVIATION ADMINISTRATION
¦
¦ --------------------------------------------------------------------------- ¦
¦ AIRCRAFT:
¦ REVISION NO: 5
¦ PAGE:
¦
¦
HAWKER SIDDELEY HS-125
¦
¦
¦
¦
(SERIES 1 THROUGH 800XP)
¦ DATE: 05/30/2002
¦ 24-3
¦
¦ --------------------------------------------------------------------------- ¦
¦
1. ¦ 2. NUMBER INSTALLED
¦
¦ SYSTEM &
¦
-------------------------------------------- ¦
¦ SEQUENCE
ITEM
¦
¦ 3. NUMBER REQUIRED FOR DISPATCH
¦
¦ NUMBERS
¦
¦
--------------------------------------- ¦
¦ ------------------------- ¦
¦
¦ 4. REMARKS OR EXCEPTIONS
¦
¦ 24 ELECTRICAL POWER
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 21-1 115 VAC/60 Hz
C ¦ 1 ¦ 0 ¦ May be inoperative provided pro¦
¦
System (FAA Flight
¦
¦
¦ cedures are not dependent upon its
¦
¦
Inspection
¦
¦
¦ use.
¦
¦
Aircraft Only)
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 30-2 DC Generator Fail C ¦ 2 ¦ 0 ¦ (O)May be inoperative provided:
¦
¦
Lights/
¦
¦
¦
a) Both ammeters operate
¦
¦
Annunciators
¦
¦
¦
normally, and
¦
¦
¦
¦
¦
b) DC voltmeter operates
¦
¦
¦
¦
¦
normally.
¦
¦
¦
¦
¦
¦
¦ 30-3 APU Generator
C ¦ 1 ¦ 0 ¦
¦
¦
¦
¦
¦
¦
¦ 30-4 APU Generator Fail C ¦ 1 ¦ 0 ¦
¦
¦
Light/Annunciator
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 30-5 APU Generator
C ¦ 1 ¦ 0 ¦ May be inoperative provided APU
¦
¦
Overheat Light/
¦
¦
¦ generator is not used.
¦
¦
Annunciator
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 30-6 Battery NO CHARGE C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided
¦
¦
Light (Series 1
¦
¦
¦ battery is verified to be charging | ¦
¦
Through 700
¦
¦
¦ normally.
| ¦
¦
Only)
¦
¦
¦
| ¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
-------------------------------------------------------------------------------
------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION
¦
¦
¦
¦
MASTER MINIMUM EQUIPMENT LIST
¦
¦ FEDERAL AVIATION ADMINISTRATION
¦
¦ --------------------------------------------------------------------------- ¦
¦ AIRCRAFT:
¦ REVISION NO: 5
¦ PAGE:
¦
¦
HAWKER SIDDELEY HS-125
¦
¦
¦
¦
(SERIES 1 THROUGH 800XP)
¦ DATE: 05/30/2002
¦ 24-4
¦
¦ --------------------------------------------------------------------------- ¦
¦
1. ¦ 2. NUMBER INSTALLED
¦
¦ SYSTEM &
¦
-------------------------------------------- ¦
¦ SEQUENCE
ITEM
¦
¦ 3. NUMBER REQUIRED FOR DISPATCH
¦
¦ NUMBERS
¦
¦
--------------------------------------- ¦
¦ ------------------------- ¦
¦
¦ 4. REMARKS OR EXCEPTIONS
¦
¦ 24 ELECTRICAL POWER
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 30-7 Bus Tie Contactor C ¦ 1 ¦ 0 ¦ (M)May be inoperative provided:
¦
¦
System (Split Bus
¦
¦
¦
a) Bus Tie contactor is
¦
¦
Tie Contactor
¦
¦
¦
verified open before each
¦
¦
Aircraft Only)
¦
¦
¦
departure,
¦
¦
¦
¦
¦
b) Both engine driven DC gener¦
¦
¦
¦
¦
ators operate normally, and
¦
¦
¦
¦
¦
c) PS1 AND PS2 voltage is
¦
¦
¦
¦
¦
normal.
¦
¦
¦
¦
¦
¦
¦ 30-8 DC Bus Tie Light/ C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided:
¦
¦
Annunciator
¦
¦
¦
a) Bus Tie system operates
¦
¦
¦
¦
¦
normally,
¦
¦
¦
¦
¦
b) Both ammeters operate
¦
¦
¦
¦
¦
normally,and
¦
¦
¦
¦
¦
c) Generator fail lights/
¦
¦
¦
¦
¦
annunciators operate
¦
¦
¦
¦
¦
normally.
¦
¦
¦
¦
¦
¦
¦ 30-9 Battery Contactor C ¦ 2 ¦ 1 ¦ (M)(O)One may be inoperative
¦
¦
Annunciators
¦
¦
¦ provided:
¦
¦
(Series 800 and
¦
¦
¦
a) Emergency contactor operates | ¦
¦
800XP Only)
¦
¦
¦
normally before each
| ¦
¦
¦
¦
¦
departure, and
¦
¦
¦
¦
¦
b) Battery contactor operates
¦
¦
¦
¦
¦
normally before each
¦
¦
¦
¦
¦
departure.
¦
¦
¦
¦
¦
¦
¦ 30-10 Emergency Power
¦
¦
¦ Deleted Revision 5.
| ¦
¦
Packs
¦
¦
¦
| ¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
-------------------------------------------------------------------------------
------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION
¦
¦
¦
¦
MASTER MINIMUM EQUIPMENT LIST
¦
¦ FEDERAL AVIATION ADMINISTRATION
¦
¦ --------------------------------------------------------------------------- ¦
¦ AIRCRAFT:
¦ REVISION NO: 5
¦ PAGE:
¦
¦
HAWKER SIDDELEY HS-125
¦
¦
¦
¦
(SERIES 1 THROUGH 800XP)
¦ DATE: 05/30/2002
¦ 24-5
¦
¦ --------------------------------------------------------------------------- ¦
¦
1. ¦ 2. NUMBER INSTALLED
¦
¦ SYSTEM &
¦
-------------------------------------------- ¦
¦ SEQUENCE
ITEM
¦
¦ 3. NUMBER REQUIRED FOR DISPATCH
¦
¦ NUMBERS
¦
¦
--------------------------------------- ¦
¦ ------------------------- ¦
¦
¦ 4. REMARKS OR EXCEPTIONS
¦
¦ 24 ELECTRICAL POWER
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 30-11 Battery
¦
¦
¦
¦
¦
Temperature
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
1) Indicator
C ¦ - ¦ 0 ¦ (M)May be inoperative provided
¦
¦
¦
¦
¦ battery hot caution annunciators
¦
¦
¦
¦
¦ operate normally.
¦
¦
¦
¦
¦
¦
¦
2) BATT HOT
C ¦ - ¦ 0 ¦ (O)May be inoperative provided:
¦
¦
Caution
¦
¦
¦
a) Indicator operates normally,
¦
¦
Annunciators
¦
¦
¦
and
¦
¦
¦
¦
¦
b) Battery temperatures are
¦
¦
¦
¦
¦
monitored in flight.
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ NOTE: Not required for lead acid
¦
¦
¦
¦
¦
battery systems.
¦
¦
¦
¦
¦
¦
¦ 30-12 Battery Heater
A ¦ 2 ¦ 0 ¦ (O)May be inoperative provided:
¦
¦ ***
Muffs
¦
¦
¦
a) Battery temperature gauge
| ¦
¦
¦
¦
¦
operates normally,
¦
¦
¦
¦
¦
b) Battery temperature is
¦
¦
¦
¦
¦
monitored by the flightcrew
¦
¦
¦
¦
¦
to ensure temperature
¦
¦
¦
¦
¦
remains above -10 degrees C
¦
¦
¦
¦
¦
at all times, and
¦
¦
¦
¦
¦
c) Repairs are made within two
¦
¦
¦
¦
¦
flight days.
¦
¦
¦
¦
¦
¦
¦ 30-15 FIS Power
C ¦ 1 ¦ 0 ¦ May be inoperative provided pro¦
¦
Recovery System
¦
¦
¦ cedures are not dependent upon its
¦
¦
(FAA Flight
¦
¦
¦ use.
¦
¦
Inspection
¦
¦
¦
¦
¦
Aircraft Only)
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
-------------------------------------------------------------------------------
------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION
¦
¦
¦
¦
MASTER MINIMUM EQUIPMENT LIST
¦
¦ FEDERAL AVIATION ADMINISTRATION
¦
¦ --------------------------------------------------------------------------- ¦
¦ AIRCRAFT:
¦ REVISION NO: 4
¦ PAGE:
¦
¦
HAWKER SIDDELEY HS-125
¦
¦
¦
¦
(SERIES 1 THROUGH 800XP)
¦ DATE: 03/10/1998
¦ 24-6
¦
¦ --------------------------------------------------------------------------- ¦
¦
1. ¦ 2. NUMBER INSTALLED
¦
¦ SYSTEM &
¦
-------------------------------------------- ¦
¦ SEQUENCE
ITEM
¦
¦ 3. NUMBER REQUIRED FOR DISPATCH
¦
¦ NUMBERS
¦
¦
--------------------------------------- ¦
¦ ------------------------- ¦
¦
¦ 4. REMARKS OR EXCEPTIONS
¦
¦ 24 ELECTRICAL POWER
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 50-1 AC Bus Fail
C ¦ 3 ¦ 2 ¦ (O)One may be inoperative provided:
¦
¦
Lights/
¦
¦
¦
a) Standby inverter is verified
¦
¦
Annunciators
¦
¦
¦
to operate normally before
¦
¦
¦
¦
¦
each departure,
¦
¦
¦
¦
¦
b) Inverter associated with the
¦
¦
¦
¦
¦
inoperative light/annun¦
¦
¦
¦
¦
ciator operates normally,
¦
¦
¦
¦
¦
and
¦
¦
¦
¦
¦
c) Voltmeter operates normally.
¦
¦
¦
¦
¦
¦
¦ 50-2 26 VAC Bus Fail
¦
¦
¦
¦
¦ *** Annunciators
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
1) INST 1/26 VAC - C ¦ 1 ¦ 0 ¦ (O)May be inoperative OFF provided:
¦
¦
XS1 Fail
¦
¦
¦
a) Affected 26 VAC Instrument
¦
¦
¦
¦
¦
Transformer is verified to
¦
¦
¦
¦
¦
operate normally, and
¦
¦
¦
¦
¦
b) Alternate procedures are
¦
¦
¦
¦
¦
established and used.
¦
¦
¦
¦
¦
¦
¦
2) INST 2/26 VAC- C ¦ 1 ¦ 0 ¦ (O)May be inoperative OFF provided:
¦
¦
XSE Fail
¦
¦
¦
a) Affected 26 VAC Instrument
¦
¦
¦
¦
¦
Transformer is verified to
¦
¦
¦
¦
¦
operate normally, and
¦
¦
¦
¦
¦
b) Alternate procedures are
¦
¦
¦
¦
¦
established and used.
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
-------------------------------------------------------------------------------
------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION
¦
¦
¦
¦
MASTER MINIMUM EQUIPMENT LIST
¦
¦ FEDERAL AVIATION ADMINISTRATION
¦
¦ --------------------------------------------------------------------------- ¦
¦ AIRCRAFT:
¦ REVISION NO: 5
¦ PAGE:
¦
¦
HAWKER SIDDELEY HS-125
¦
¦
¦
¦
(SERIES 1 THROUGH 800XP)
¦ DATE: 05/30/2002
¦ 25-1
¦
¦ --------------------------------------------------------------------------- ¦
¦
1. ¦ 2. NUMBER INSTALLED
¦
¦ SYSTEM &
¦
-------------------------------------------- ¦
¦ SEQUENCE
ITEM
¦
¦ 3. NUMBER REQUIRED FOR DISPATCH
¦
¦ NUMBERS
¦
¦
--------------------------------------- ¦
¦ ------------------------- ¦
¦
¦ 4. REMARKS OR EXCEPTIONS
¦
¦ 25 EQUIPMENT/FURNISHINGS ¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 10-1 Pilot(s) Seat
C ¦ 2 ¦ 0 ¦ (M)May be inoperative provided:
¦
¦
Adjustment System
¦
¦
¦
a) Position of the seat(s)
¦
¦
¦
¦
¦
permits normal pilot
¦
¦
¦
¦
¦
visibility and full flight
¦
¦
¦
¦
¦
control movement, and
¦
¦
¦
¦
¦
b) Seat(s) is secured with
¦
¦
¦
¦
¦
mechanical stops.
¦
¦
¦
¦
¦
¦
¦ 10-2 Cockpit
D ¦ - ¦ 0 ¦ NOTE: Items such as yoke clips,
| ¦
¦
Convenience Items
¦
¦
¦
side panel holders, coffee
| ¦
¦
¦
¦
¦
cup holders, and control yoke | ¦
¦
¦
¦
¦
plastic covers may be
| ¦
¦
¦
¦
¦
inoperative or missing.
| ¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
-------------------------------------------------------------------------------
------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION
¦
¦
¦
¦
MASTER MINIMUM EQUIPMENT LIST
¦
¦ FEDERAL AVIATION ADMINISTRATION
¦
¦ --------------------------------------------------------------------------- ¦
¦ AIRCRAFT:
¦ REVISION NO: 5
¦ PAGE:
¦
¦
HAWKER SIDDELEY HS-125
¦
¦
¦
¦
(SERIES 1 THROUGH 800XP)
¦ DATE: 05/30/2002
¦ 25-2
¦
¦ --------------------------------------------------------------------------- ¦
¦
1. ¦ 2. NUMBER INSTALLED
¦
¦ SYSTEM &
¦
-------------------------------------------- ¦
¦ SEQUENCE
ITEM
¦
¦ 3. NUMBER REQUIRED FOR DISPATCH
¦
¦ NUMBERS
¦
¦
--------------------------------------- ¦
¦ ------------------------- ¦
¦
¦ 4. REMARKS OR EXCEPTIONS
¦
¦ 25 EQUIPMENT/FURNISHINGS ¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 20-1 Passenger Seats
C ¦ - ¦ - ¦ May be inoperative provided:
| ¦
¦
(Including Seat
¦
¦
¦
a) Seat does not block an
| ¦
¦
Backs and Armrests) ¦
¦
¦
Emergency Exit,
| ¦
¦
¦
¦
¦
b) Seat does not restrict any
| ¦
¦
¦
¦
¦
passenger from access to the | ¦
¦
¦
¦
¦
main aircraft asisle, and
| ¦
¦
¦
¦
¦
c) Affected seat(s) are blocked | ¦
¦
¦
¦
¦
and placarded "DO NOT
| ¦
¦
¦
¦
¦
OCCUPY"
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ NOTE 1: A seat with an inoperative
¦
¦
¦
¦
¦
seatbelt is considered
¦
¦
¦
¦
¦
inoperative.
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ NOTE 2: Inoperative seats do not
¦
¦
¦
¦
¦
affect the required number
¦
¦
¦
¦
¦
of flight attendants.
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ NOTE 3: Affected seat(S) may
| ¦
¦
¦
¦
¦
include the seat(s) behind | ¦
¦
¦
¦
¦
and/or adjacent outboard
| ¦
¦
¦
¦
¦
Seats.
¦
¦
¦
¦
¦
¦
¦
1) Recline
C ¦ - ¦ - ¦ May be inoperative and seat
| ¦
¦
Mechanism
¦
¦
¦ occupied provided seat is secured
| ¦
¦
¦
¦
¦ in the up-right position.
| ¦
¦
¦
¦
¦
¦
¦
2) Underseat
C ¦ - ¦ - ¦ (O)May be inoperative provided:
| ¦
¦
Baggage
¦
¦
¦
a) Baggage is not stowed under | ¦
¦
¦
¦
¦
seat with inoperative
| ¦
¦
¦
¦
¦
restraining bar,
| ¦
¦
¦
¦
¦
b) Associated seat is placarded | ¦
¦
¦
¦
¦
"DO NOT STOW BAGGAGE UNDER
| ¦
¦
¦
¦
¦
THIS SEAT", and
| ¦
¦
¦
¦
¦
c) Procedures are established
| ¦
¦
¦
¦
¦
to alert Cabin Crew of
| ¦
¦
¦
¦
¦
inoperative restraining
| ¦
¦
¦
¦
¦
bar.
| ¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
-------------------------------------------------------------------------------
------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION
¦
¦
¦
¦
MASTER MINIMUM EQUIPMENT LIST
¦
¦ FEDERAL AVIATION ADMINISTRATION
¦
¦ --------------------------------------------------------------------------- ¦
¦ AIRCRAFT:
¦ REVISION NO: 5
¦ PAGE:
¦
¦
HAWKER SIDDELEY HS-125
¦
¦
¦
¦
(SERIES 1 THROUGH 800XP)
¦ DATE: 05/30/2002
¦ 25-3
¦
¦ --------------------------------------------------------------------------- ¦
¦
1. ¦ 2. NUMBER INSTALLED
¦
¦ SYSTEM &
¦
-------------------------------------------- ¦
¦ SEQUENCE
ITEM
¦
¦ 3. NUMBER REQUIRED FOR DISPATCH
¦
¦ NUMBERS
¦
¦
--------------------------------------- ¦
¦ ------------------------- ¦
¦
¦ 4. REMARKS OR EXCEPTIONS
¦
¦ 25 EQUIPMENT/FURNISHINGS ¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 20-2 Flight Inspection D ¦ 1 ¦ 0 ¦ May be inoperative provided pro¦
¦
Panel System (FAA
¦
¦
¦ cedures are not dependent upon its
¦
¦
Flight Inspection
¦
¦
¦ use.
¦
¦
Aircraft Only)
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 25-1 Cockpit Sun Visors C ¦ - ¦ 0 ¦ May be inoperative.
¦
¦
¦
¦
¦
¦
¦ 60-1 Overwater
D ¦ - ¦ - ¦ Any in excess of that required by
| ¦
¦
Equipment
¦
¦
¦ FAR may be inoperative.
¦
¦
¦
¦
¦
¦
¦ 60-2 First Aid Kits
D ¦ - ¦ - ¦ Any in excess of those required by | ¦
¦
¦
¦
¦ FAR may be inoperative.
¦
¦
¦
¦
¦
¦
¦ 60-3 Passenger
¦ - ¦ 0 ¦ Passenger convenience items, as
¦
¦
Convenience
¦
¦
¦ expressed in this MMEL, are those
¦
¦
Items(s)
¦
¦
¦ related to passenger convenience,
¦
¦
¦
¦
¦ comfort or entertainment such as,
¦
¦
¦
¦
¦ but not limited to: galley equip¦
¦
¦
¦
¦ ment, movie equipment, ash trays,
¦
¦
¦
¦
¦ stereo equipment, overhead lamps,
¦
¦
¦
¦
¦ etc. Items addressed elsewhere in
¦
¦
¦
¦
¦ this document shall not be
¦
¦
¦
¦
¦ included. (M) and (O) procedures
¦
¦
¦
¦
¦ may be required and included in the
¦
¦
¦
¦
¦ air carrier's appropriate document.
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ NOTE: Lavatory door ash trays are
¦
¦
¦
¦
¦
not considered convenience
¦
¦
¦
¦
¦
items.
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
-------------------------------------------------------------------------------
------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION
¦
¦
¦
¦
MASTER MINIMUM EQUIPMENT LIST
¦
¦ FEDERAL AVIATION ADMINISTRATION
¦
¦ --------------------------------------------------------------------------- ¦
¦ AIRCRAFT:
¦ REVISION NO: 5
¦ PAGE:
¦
¦
HAWKER SIDDELEY HS-125
¦
¦
¦
¦
(SERIES 1 THROUGH 800XP)
¦ DATE: 05/30/2002
¦ 25-4
¦
¦ --------------------------------------------------------------------------- ¦
¦
1. ¦ 2. NUMBER INSTALLED
¦
¦ SYSTEM &
¦
-------------------------------------------- ¦
¦ SEQUENCE
ITEM
¦
¦ 3. NUMBER REQUIRED FOR DISPATCH
¦
¦ NUMBERS
¦
¦
--------------------------------------- ¦
¦ ------------------------- ¦
¦
¦ 4. REMARKS OR EXCEPTIONS
¦
¦ 25 EQUIPMENT/FURNISHINGS ¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 60-4 Observer Seat
A ¦ - ¦ - ¦ May be inoperative provided:
¦
¦
(Including
¦
¦
¦
a) A passenger seat in the
¦
¦
Associated
¦
¦
¦
passenger cabin is available
¦
¦
Equipment)
¦
¦
¦
to an FAA inspector for the
¦
¦
¦
¦
¦
performance of official
¦
¦
¦
¦
¦
duties.
¦
¦
¦
¦
¦
OR
¦
¦
A ¦
¦
¦
b) Second observer seat is is
¦
¦
¦
¦
¦
available, functional, and
¦
¦
¦
¦
¦
acceptable, including
¦
¦
¦
¦
¦
peripheral equipment, to an
¦
¦
¦
¦
¦
FAA inspector for the
¦
¦
¦
¦
¦
performance of official
¦
¦
¦
¦
¦
duties, and
¦
¦
¦
¦
¦
c) Operations are limited to
¦
¦
¦
¦
¦
not more than two flight
¦
¦
¦
¦
¦
days before repairs are
¦
¦
¦
¦
¦
made.
¦
¦
¦
¦
¦
¦
¦
1) Audio Control
A ¦ 1 ¦ 0 ¦ May be inoperative provided:
¦
¦
Panel
¦
¦
¦
a) Occupant of seat is not
¦
¦
¦
¦
¦
performing official duties,
¦
¦
¦
¦
¦
b) Alternate communication
¦
¦
¦
¦
¦
procedures are established
¦
¦
¦
¦
¦
and used, and
¦
¦
¦
¦
¦
c) Operations are limited to
¦
¦
¦
¦
¦
not more than two flight
¦
¦
¦
¦
¦
days before repairs are
¦
¦
¦
¦
¦
made.
¦
¦
¦
¦
¦
¦
¦ 60-5 Emergency Vision
C ¦ 2 ¦ 0 ¦
| ¦
¦ *** Assurance System
¦
¦
¦
| ¦
¦
(EVAS)
¦
¦
¦
| ¦
¦
(STC # SA00892LA)
¦
¦
¦
| ¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
-------------------------------------------------------------------------------
------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION
¦
¦
¦
¦
MASTER MINIMUM EQUIPMENT LIST
¦
¦ FEDERAL AVIATION ADMINISTRATION
¦
¦ --------------------------------------------------------------------------- ¦
¦ AIRCRAFT:
¦ REVISION NO: 5
¦ PAGE:
¦
¦
HAWKER SIDDELEY HS-125
¦
¦
¦
¦
(SERIES 1 THROUGH 800XP)
¦ DATE: 05/30/2002
¦ 26-1
¦
¦ --------------------------------------------------------------------------- ¦
¦
1. ¦ 2. NUMBER INSTALLED
¦
¦ SYSTEM &
¦
-------------------------------------------- ¦
¦ SEQUENCE
ITEM
¦
¦ 3. NUMBER REQUIRED FOR DISPATCH
¦
¦ NUMBERS
¦
¦
--------------------------------------- ¦
¦ ------------------------- ¦
¦
¦ 4. REMARKS OR EXCEPTIONS
¦
¦ 26 FIRE PROTECTION
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 10-1 Engine Fire Warning ¦
¦
¦
¦
¦
Lights/Annunciators ¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
1) Series 1
C ¦ 2 ¦ 0 ¦ May be inoperative provided
| ¦
¦
Through 700
¦
¦
¦ HP cock lights operate normally.
| ¦
¦
Only
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
2) Series 800 and C ¦ - ¦ 0 ¦ May be inoperative provided HP
| ¦
¦
800XP Only
¦
¦
¦ cock lights operate normally.
| ¦
¦
¦
¦
¦
¦
¦ 10-2 HP Cock Fire
C ¦ 2 ¦ 0 ¦ May be inoperative provided
¦
¦
Warning Lights
¦
¦
¦ engine fire warning system
¦
¦
¦
¦
¦ operates normally.
¦
¦
¦
¦
¦
¦
¦ 15-1 APU Fire
C ¦ 1 ¦ 0 ¦ May be inoperative provided APU is
¦
¦
Detection System
¦
¦
¦ not used.
¦
¦
¦
¦
¦
¦
¦
1) Warning Bell
C ¦ 1 ¦ 0 ¦ (M)(O)May be inoperative for
¦
¦
¦
¦
¦ ground operations provided:
¦
¦
¦
¦
¦
a) APU Fire warning annunciator
¦
¦
¦
¦
¦
operates normally, and
¦
¦
¦
¦
¦
b) System is continuously
¦
¦
¦
¦
¦
monitored at the cockpit
¦
¦
¦
¦
¦
control panel.
¦
¦
¦
¦
¦
¦
¦
2) Warning
¦
¦
¦
¦
¦
Annunciator
C ¦ 1 ¦ 0 ¦ (M)(O)May be inoperative for
¦
¦
¦
¦
¦ ground operations provided:
¦
¦
¦
¦
¦
a) APU Fire warning bell
¦
¦
¦
¦
¦
operates normally, and
¦
¦
¦
¦
¦
b) System is continuously
¦
¦
¦
¦
¦
monitored at the cockpit
¦
¦
¦
¦
¦
control panel.
¦
¦
¦
¦
¦
¦
¦ 15-2 APU Fire
C ¦ 1 ¦ 0 ¦ (M)May be inoperative provided:
¦
¦
Detection Test
¦
¦
¦
a) Failure is verified to be in
¦
¦
System
¦
¦
¦
the light circuit, and
¦
¦
¦
¦
¦
b) System operation is verified
¦
¦
¦
¦
¦
once each flight day.
¦
¦
¦
¦
¦
OR
¦
¦
C ¦
¦
¦
c) APU is not used.
¦
-------------------------------------------------------------------------------
------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION
¦
¦
¦
¦
MASTER MINIMUM EQUIPMENT LIST
¦
¦ FEDERAL AVIATION ADMINISTRATION
¦
¦ --------------------------------------------------------------------------- ¦
¦ AIRCRAFT:
¦ REVISION NO: 5
¦ PAGE:
¦
¦
HAWKER SIDDELEY HS-125
¦
¦
¦
¦
(SERIES 1 THROUGH 800XP)
¦ DATE: 05/30/2002
¦ 26-2
¦
¦ --------------------------------------------------------------------------- ¦
¦
1. ¦ 2. NUMBER INSTALLED
¦
¦ SYSTEM &
¦
-------------------------------------------- ¦
¦ SEQUENCE
ITEM
¦
¦ 3. NUMBER REQUIRED FOR DISPATCH
¦
¦ NUMBERS
¦
¦
--------------------------------------- ¦
¦ ------------------------- ¦
¦
¦ 4. REMARKS OR EXCEPTIONS
¦
¦ 26 FIRE PROTECTION
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 20-1 APU Fire
C ¦ 1 ¦ 0 ¦ May be inoperative provided APU is
¦
¦
Extinguisher System ¦
¦
¦ not used.
¦
¦
¦
¦
¦
¦
¦ 20-2 APU Extinguisher
C ¦ 1 ¦ 0 ¦ (M)(O)May be missing provided:
¦
¦
Pressure Relief
¦
¦
¦
a) Indicator readings or other
¦
¦
Discharge Indicator ¦
¦
¦
acceptable means are used to
¦
¦
¦
¦
¦
verify adequate charge.
¦
¦
¦
¦
¦
OR
¦
¦
C ¦
¦
¦
b) APU is not used.
¦
¦
¦
¦
¦
¦
¦ 20-3 Engine Fire
C ¦ 2 ¦ 0 ¦ (M)May be inoperative provided an
¦
¦
Extinguisher Relief ¦
¦
¦ acceptable procedure is used to
| ¦
¦
Discharge Indicators ¦
¦
¦ verify bottle charge is adequate
¦
¦
¦
¦
¦ before each departure.
¦
¦
¦
¦
¦
¦
¦ 20-4 Portable Fire
D ¦ - ¦ - ¦ (M)Any in excess of those required
¦
¦
Extinguishers
¦
¦
¦ by FAR may be unserviceable or
¦
¦
¦
¦
¦ missing provided:
¦
¦
¦
¦
¦
a) Inoperative fire exting| ¦
¦
¦
¦
¦
uisher is tagged
| ¦
¦
¦
¦
¦
inoperative, removed from
| ¦
¦
¦
¦
¦
location, and placed out of | ¦
¦
¦
¦
¦
sight so it can not be
| ¦
¦
¦
¦
¦
mistaken for a fuctional
| ¦
¦
¦
¦
¦
unit, and
| ¦
¦
¦
¦
¦
b) Required distribution is
| ¦
¦
¦
¦
¦
maintained.
| ¦
¦
¦
¦
¦
¦
¦ 30-1 Forward/Aft
C ¦ - ¦ 0 ¦ May be inoperative provided:
¦
¦
Baggage Smoke
¦
¦
¦
a) Associated compartment
¦
¦
Detection Systems
¦
¦
¦
remains empty.
¦
¦
¦
¦
¦
OR
¦
¦
C ¦
¦
¦
b) Only non-combustible
¦
¦
¦
¦
¦
materials are carried.
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
-------------------------------------------------------------------------------
------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION
¦
¦
¦
¦
MASTER MINIMUM EQUIPMENT LIST
¦
¦ FEDERAL AVIATION ADMINISTRATION
¦
¦ --------------------------------------------------------------------------- ¦
¦ AIRCRAFT:
¦ REVISION NO: 3
¦ PAGE:
¦
¦
HAWKER SIDDELEY HS-125
¦
¦
¦
¦
(SERIES 1 THROUGH 800XP)
¦ DATE: 09/07/1993
¦ 26-3
¦
¦ --------------------------------------------------------------------------- ¦
¦
1. ¦ 2. NUMBER INSTALLED
¦
¦ SYSTEM &
¦
-------------------------------------------- ¦
¦ SEQUENCE
ITEM
¦
¦ 3. NUMBER REQUIRED FOR DISPATCH
¦
¦ NUMBERS
¦
¦
--------------------------------------- ¦
¦ ------------------------- ¦
¦
¦ 4. REMARKS OR EXCEPTIONS
¦
¦ 26 FIRE PROTECTION
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 30-2 Toilet Smoke
C ¦ - ¦ - ¦ (M)(O)May be inoperative provided:
¦
¦ *** Detection System
¦
¦
¦
a) Toilet waste bin fire
¦
¦
¦
¦
¦
extinguisher system operates
¦
¦
¦
¦
¦
normally.
¦
¦
¦
¦
¦
OR
¦
¦
C ¦
¦
¦
b) Toilet waste receptacle is
¦
¦
¦
¦
¦
empty,
¦
¦
¦
¦
¦
c) Toilet door is locked closed
¦
¦
¦
¦
¦
and placarded "INOPERATIVE ¦
¦
¦
¦
¦
DO NOT ENTER," and
¦
¦
¦
¦
¦
d) Toilet is not used for any
¦
¦
¦
¦
¦
purpose.
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ NOTE 1: These provisos are not in¦
¦
¦
¦
¦
tended to prohibit inspec¦
¦
¦
¦
¦
tions by crewmembers.
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ NOTE 2: A toilet smoke detector
¦
¦
¦
¦
¦
system is not required for
¦
¦
¦
¦
¦
all-cargo operations.
¦
¦
¦
¦
¦
¦
¦ 30-3 Rear Baggage
C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided:
¦
¦ *** Panier Smoke
¦
¦
¦
a) Compartment remains empty,
¦
¦
Detection System
¦
¦
¦
and
¦
¦
¦
¦
¦
b) Pannier heating is selected
¦
¦
¦
¦
¦
OFF.
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
-------------------------------------------------------------------------------
------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION
¦
¦
¦
¦
MASTER MINIMUM EQUIPMENT LIST
¦
¦ FEDERAL AVIATION ADMINISTRATION
¦
¦ --------------------------------------------------------------------------- ¦
¦ AIRCRAFT:
¦ REVISION NO: 4
¦ PAGE:
¦
¦
HAWKER SIDDELEY HS-125
¦
¦
¦
¦
(SERIES 1 THROUGH 800XP)
¦ DATE: 03/10/1998
¦ 27-1
¦
¦ --------------------------------------------------------------------------- ¦
¦
1. ¦ 2. NUMBER INSTALLED
¦
¦ SYSTEM &
¦
-------------------------------------------- ¦
¦ SEQUENCE
ITEM
¦
¦ 3. NUMBER REQUIRED FOR DISPATCH
¦
¦ NUMBERS
¦
¦
--------------------------------------- ¦
¦ ------------------------- ¦
¦
¦ 4. REMARKS OR EXCEPTIONS
¦
¦ 27 FLIGHT CONTROLS
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 10-1 Aileron Trim
B ¦ 1 ¦ 0 ¦ (M)(O)May be inoperative provided:
¦
¦
Position Indicator
¦
¦
¦
a) Aileron trim system operates
¦
¦
¦
¦
¦
normally, and
¦
¦
¦
¦
¦
b) Aileron trim is visually
¦
¦
¦
¦
¦
verified to be centered
¦
¦
¦
¦
¦
before each departure.
¦
¦
¦
¦
¦
¦
¦ 20-1 Rudder Trim
B ¦ 1 ¦ 0 ¦ (M)(O)May be inoperative provided:
¦
¦
Position Indicator
¦
¦
¦
a) Rudder trim system operates
¦
¦
¦
¦
¦
normally, and
¦
¦
¦
¦
¦
b) Rudder trim is visually
¦
¦
¦
¦
¦
verified to be centered
¦
¦
¦
¦
¦
before each departure.
¦
¦
¦
¦
¦
¦
¦ 20-2 Rudder Pedal
C ¦ 2 ¦ 0 ¦ May be inoperative provided adjust¦
¦
Adjustment System
¦
¦
¦ ment can be secured in a position
¦
¦
¦
¦
¦ which suits individual pilot's
¦
¦
¦
¦
¦ requirement.
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
-------------------------------------------------------------------------------
------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION
¦
¦
¦
¦
MASTER MINIMUM EQUIPMENT LIST
¦
¦ FEDERAL AVIATION ADMINISTRATION
¦
¦ --------------------------------------------------------------------------- ¦
¦ AIRCRAFT:
¦ REVISION NO: 5
¦ PAGE:
¦
¦
HAWKER SIDDELEY HS-125
¦
¦
¦
¦
(SERIES 1 THROUGH 800XP)
¦ DATE: 05/30/2002
¦ 27-2
¦
¦ --------------------------------------------------------------------------- ¦
¦
1. ¦ 2. NUMBER INSTALLED
¦
¦ SYSTEM &
¦
-------------------------------------------- ¦
¦ SEQUENCE
ITEM
¦
¦ 3. NUMBER REQUIRED FOR DISPATCH
¦
¦ NUMBERS
¦
¦
--------------------------------------- ¦
¦ ------------------------- ¦
¦
¦ 4. REMARKS OR EXCEPTIONS
¦
¦ 27 FLIGHT CONTROLS
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 30-1 Electrical
C ¦ 1 ¦ 0 ¦ (M)(O)May be inoperative provided:
¦
¦
Elevator Trim
¦
¦
¦
a) Manual trim operates
¦
¦
System
¦
¦
¦
normally, and
¦
¦
¦
¦
¦
b) Associated circuit breakers
¦
¦
¦
¦
¦
are pulled and collared.
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ NOTE 1: For operations within RVSM | ¦
¦
¦
¦
¦
airspace, the following
| ¦
¦
¦
¦
¦
items must be operating:
| ¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
a) 2 ADC's
| ¦
¦
¦
¦
¦
b) 1 ATC Transponder
| ¦
¦
¦
¦
¦
c) 1 A/P altitude hold
| ¦
¦
¦
¦
¦
Function, and
| ¦
¦
¦
¦
¦
d) 1 Altitude Alerter
| ¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ NOTE 2: Flying below, above or
| ¦
¦
¦
¦
¦
crossing RVSM airspace does | ¦
¦
¦
¦
¦
not require the above items | ¦
¦
¦
¦
¦
to be operating.
| ¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ NOTE 3: Mach Trim System may be
| ¦
¦
¦
¦
¦
affected.
| ¦
¦
¦
¦
¦
¦
¦ 30-2 Stall Warning/
¦
¦
¦
¦
¦
Identification
¦
¦
¦
¦
¦
Systems
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
1) Series 1
B ¦ 2 ¦ 1 ¦ (M)(O)One may be inoperative
| ¦
¦
Through 700
¦
¦
¦ provided:
| ¦
¦
Only
¦
¦
¦
a) Remaining stall test channel
¦
¦
¦
¦
¦
operates normally, and
¦
¦
¦
¦
¦
b) Remaining stall detector
¦
¦
¦
¦
¦
pneumatic system is verified
¦
¦
¦
¦
¦
to operate normally before
¦
¦
¦
¦
¦
each departure.
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ (Continued)
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
-------------------------------------------------------------------------------
------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION
¦
¦
¦
¦
MASTER MINIMUM EQUIPMENT LIST
¦
¦ FEDERAL AVIATION ADMINISTRATION
¦
¦ --------------------------------------------------------------------------- ¦
¦ AIRCRAFT:
¦ REVISION NO: 5
¦ PAGE:
¦
¦
HAWKER SIDDELEY HS-125
¦
¦
¦
¦
(SERIES 1 THROUGH 800XP)
¦ DATE: 05/30/2002
¦ 27-3
¦
¦ --------------------------------------------------------------------------- ¦
¦
1. ¦ 2. NUMBER INSTALLED
¦
¦ SYSTEM &
¦
-------------------------------------------- ¦
¦ SEQUENCE
ITEM
¦
¦ 3. NUMBER REQUIRED FOR DISPATCH
¦
¦ NUMBERS
¦
¦
--------------------------------------- ¦
¦ ------------------------- ¦
¦
¦ 4. REMARKS OR EXCEPTIONS
¦
¦ 27 FLIGHT CONTROLS
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 30-2 Stall Warning/
¦
¦
¦
¦
¦
Identification
¦
¦
¦
¦
¦
Systems
¦
¦
¦
¦
¦
(Cont'd)
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
2) (Series 800
B ¦ 3 ¦ 2 ¦ (O)One stall warning and/or
| ¦
¦
and 800XP
¦
¦
¦ identification channel may be
| ¦
¦
Only)
¦
¦
¦ inoperative provided:
| ¦
¦
¦
¦
¦
a) Inoperative channel is
¦
¦
¦
¦
¦
inhibited by pulling and
¦
¦
¦
¦
¦
collaring the associated
¦
¦
¦
¦
¦
STALL INDENT circuit breaker
¦
¦
¦
¦
¦
(SSU and STALL IDENT amber
¦
¦
¦
¦
¦
annunciators illuminated if
¦
¦
¦
¦
¦
IDENT 1 or 2 is inhibited),
¦
¦
¦
¦
¦
b) Before each departure,
¦
¦
¦
¦
¦
normal operation of the
¦
¦
¦
¦
¦
remaining channels is
¦
¦
¦
¦
¦
confirmed by independently
¦
¦
¦
¦
¦
pressing the cockpit TEST
¦
¦
¦
¦
¦
buttons,
¦
¦
¦
¦
¦
c) Before each departure,
¦
¦
¦
¦
¦
normal operation of the
¦
¦
¦
¦
¦
stick pusher is confirmed
¦
¦
¦
¦
¦
(stall valves A and B OPEN
¦
¦
¦
¦
¦
with red annunciators
¦
¦
¦
¦
¦
illuminated) by pressing the
¦
¦
¦
¦
¦
two operative TEST buttons
¦
¦
¦
¦
¦
simultaneously, and
¦
¦
¦
¦
¦
d) Lights erroneously on due to
¦
¦
¦
¦
¦
system failure are
¦
¦
¦
¦
¦
deactivated.
¦
¦
¦
¦
¦
¦
¦ 30-3 Stick Shaker
C ¦ 2 ¦ 1 ¦ One may be inoperative provided:
¦
¦
Motors (Series
¦
¦
¦
a) Both stall warning channels
¦
¦
800 and 800XP
¦
¦
¦
operate normally, and
| ¦
¦
Only)
¦
¦
¦
b) Remaining stick shaker
| ¦
¦
¦
¦
¦
system operates normally.
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
-------------------------------------------------------------------------------
------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION
¦
¦
¦
¦
MASTER MINIMUM EQUIPMENT LIST
¦
¦ FEDERAL AVIATION ADMINISTRATION
¦
¦ --------------------------------------------------------------------------- ¦
¦ AIRCRAFT:
¦ REVISION NO: 5
¦ PAGE:
¦
¦
HAWKER SIDDELEY HS-125
¦
¦
¦
¦
(SERIES 1 THROUGH 800XP)
¦ DATE: 05/30/2002
¦ 27-4
¦
¦ --------------------------------------------------------------------------- ¦
¦
1. ¦ 2. NUMBER INSTALLED
¦
¦ SYSTEM &
¦
-------------------------------------------- ¦
¦ SEQUENCE
ITEM
¦
¦ 3. NUMBER REQUIRED FOR DISPATCH
¦
¦ NUMBERS
¦
¦
--------------------------------------- ¦
¦ ------------------------- ¦
¦
¦ 4. REMARKS OR EXCEPTIONS
¦
¦ 27 FLIGHT CONTROLS
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 30-4 Stall Warning
C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided both
¦
¦
Autopilot
¦
¦
¦ stall warning channels operate
| ¦
¦
Disconnect System
¦
¦
¦ normally.
| ¦
¦
(Series 800 and
¦
¦
¦
| ¦
¦
800XP Only)
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 30-5 Mach Trim System
C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided:
| ¦
¦
(Series 800XP)
¦
¦
¦
a) Mechanical elevator trim
| ¦
¦
¦
¦
¦
system operates normally,
| ¦
¦
¦
¦
¦
and
| ¦
¦
¦
¦
¦
b) AFM speed limitations are
| ¦
¦
¦
¦
¦
observed.
| ¦
¦
¦
¦
¦
¦
¦ 50-1 Flap Position
C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided:
¦
¦
Indicator
¦
¦
¦
a) Flap position is visually
¦
¦
¦
¦
¦
verified at 0 degrees before
¦
¦
¦
¦
¦
each departure,
¦
¦
¦
¦
¦
b) AFM procedures for flap 0
¦
¦
¦
¦
¦
degree take-off and landing
¦
¦
¦
¦
¦
are observed, and
| ¦
¦
¦
¦
¦
c) Flaps are not operated
| ¦
¦
¦
¦
¦
enroute.
| ¦
¦
¦
¦
¦
¦
¦ 50-2 Flap Handle
C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided flap | ¦
¦
Select Position
¦
¦
¦ position indicator operates
| ¦
¦
Indicator
¦
¦
¦ normally.
| ¦
¦
¦
¦
¦
¦
¦
C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided AFM | ¦
¦
¦
¦
¦ limitations for flap 0 degree
| ¦
¦
¦
¦
¦ takeoff and landing are observed.
| ¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
-------------------------------------------------------------------------------
------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION
¦
¦
¦
¦
MASTER MINIMUM EQUIPMENT LIST
¦
¦ FEDERAL AVIATION ADMINISTRATION
¦
¦ --------------------------------------------------------------------------- ¦
¦ AIRCRAFT:
¦ REVISION NO: 5
¦ PAGE:
¦
¦
HAWKER SIDDELEY HS-125
¦
¦
¦
¦
(SERIES 1 THROUGH 800XP)
¦ DATE: 05/30/2002
¦ 27-5
¦
¦ --------------------------------------------------------------------------- ¦
¦
1. ¦ 2. NUMBER INSTALLED
¦
¦ SYSTEM &
¦
-------------------------------------------- ¦
¦ SEQUENCE
ITEM
¦
¦ 3. NUMBER REQUIRED FOR DISPATCH
¦
¦ NUMBERS
¦
¦
--------------------------------------- ¦
¦ ------------------------- ¦
¦
¦ 4. REMARKS OR EXCEPTIONS
¦
¦ 27 FLIGHT CONTROLS
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 60-1 Air Brake Position C ¦ - ¦ 0 ¦ (O)May be inoperative provided:
¦
¦
Indicator
¦
¦
¦
a) Airbrakes are verified to
¦
¦
¦
¦
¦
operate normally,
¦
¦
¦
¦
¦
b) Airbrakes are visually
¦
¦
¦
¦
¦
verified to be retracted
¦
¦
¦
¦
¦
before each departure, and
¦
¦
¦
¦
¦
c) Takeoff warning system
¦
¦
¦
¦
¦
operates normally.
¦
¦
¦
¦
¦
¦
¦ 60-2 Control Column
C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided
¦
¦
Lock System
¦
¦
¦ system is secured unlocked.
¦
¦
¦
¦
¦
¦
¦ 60-3 Rudder Gust Lock
D ¦ 1 ¦ 0 ¦ (O)May be inoperative provided
| ¦
¦
Flapper Door
¦
¦
¦ alternate procedures are
| ¦
¦
¦
¦
¦ established and used.
| ¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
-------------------------------------------------------------------------------
------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION
¦
¦
¦
¦
MASTER MINIMUM EQUIPMENT LIST
¦
¦ FEDERAL AVIATION ADMINISTRATION
¦
¦ --------------------------------------------------------------------------- ¦
¦ AIRCRAFT:
¦ REVISION NO: 5
¦ PAGE:
¦
¦
HAWKER SIDDELEY HS-125
¦
¦
¦
¦
(SERIES 1 THROUGH 800XP)
¦ DATE: 05/30/2002
¦ 28-1
¦
¦ --------------------------------------------------------------------------- ¦
¦
1. ¦ 2. NUMBER INSTALLED
¦
¦ SYSTEM &
¦
-------------------------------------------- ¦
¦ SEQUENCE
ITEM
¦
¦ 3. NUMBER REQUIRED FOR DISPATCH
¦
¦ NUMBERS
¦
¦
--------------------------------------- ¦
¦ ------------------------- ¦
¦
¦ 4. REMARKS OR EXCEPTIONS
¦
¦ 28 FUEL
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 20-1 Fuel Booster Pumps C ¦ 2 ¦ 1 ¦ (O)One may be inoperative provided:
¦
¦
¦
¦
¦
a) Crossfeed and wing transfer
¦
¦
¦
¦
¦
valves operate normally,
¦
¦
¦
¦
¦
b) Aircraft is operated in
¦
¦
¦
¦
¦
accordance with AFM
¦
¦
¦
¦
¦
supplement procedure,
¦
¦
¦
¦
¦
c) L.P. fuel warning system
¦
¦
¦
¦
¦
operates normally,
¦
¦
¦
¦
¦
d) Both fuel quantity indic¦
¦
¦
¦
¦
ators operate normally, and
¦
¦
¦
¦
¦
e) RPM indicators operate
¦
¦
¦
¦
¦
normally.
¦
¦
¦
¦
¦
¦
¦ 20-2 Wing Transfer
C ¦ 1 ¦ 0 ¦ (M)(O)May be inoperative provided
¦
¦
Magnetic Indicator
¦
¦
¦ transfer valve is verified to
¦
¦
(Series 1 Through
¦
¦
¦ operate normally before each
| ¦
¦
400 Only)
¦
¦
¦ departure.
| ¦
¦
¦
¦
¦
¦
¦ 20-3 Fuel Transfer/
C ¦ 1 ¦ 0 ¦ (M)(O)May be inoperative provided
¦
¦
Crossfeed
¦
¦
¦ Transfer/Crossfeed valve(s) is
¦
¦
Indicator (Series
¦
¦
¦ verified to operate normally before
¦
¦
600 Through 800XP
¦
¦
¦ each departure.
| ¦
¦
Only)
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 20-4 Ventral Tank Fuel C ¦ 1 ¦ 0 ¦ (M)(O)May be inoperative provided:
¦
¦
Transfer Valve
¦
¦
¦
a) Tank remains empty,
¦
¦
(Series 3A/RA,
¦
¦
¦
b) Valve is secured closed, and | ¦
¦
3B/RA Through
¦
¦
¦
c) Dorsal tank remains empty.
| ¦
¦
800XP Only)
¦
¦
¦
| ¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
-------------------------------------------------------------------------------
------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION
¦
¦
¦
¦
MASTER MINIMUM EQUIPMENT LIST
¦
¦ FEDERAL AVIATION ADMINISTRATION
¦
¦ --------------------------------------------------------------------------- ¦
¦ AIRCRAFT:
¦ REVISION NO: 5
¦ PAGE:
¦
¦
HAWKER SIDDELEY HS-125
¦
¦
¦
¦
(SERIES 1 THROUGH 800XP)
¦ DATE: 05/30/2002
¦ 28-2
¦
¦ --------------------------------------------------------------------------- ¦
¦
1. ¦ 2. NUMBER INSTALLED
¦
¦ SYSTEM &
¦
-------------------------------------------- ¦
¦ SEQUENCE
ITEM
¦
¦ 3. NUMBER REQUIRED FOR DISPATCH
¦
¦ NUMBERS
¦
¦
--------------------------------------- ¦
¦ ------------------------- ¦
¦
¦ 4. REMARKS OR EXCEPTIONS
¦
¦ 28 FUEL
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 20-5 Ventral Tank
C ¦ 1 ¦ 0 ¦ (M)(O)May be inoperative provided:
¦
¦
Transfer Light/
¦
¦
¦
a) Associated valve is verified
¦
¦
Annunciator
¦
¦
¦
to operate normally, and
¦
¦
(Series 3A/RA,
¦
¦
¦
b) Valve position is verified
| ¦
¦
3B/RA Through
¦
¦
¦
after each refueling.
| ¦
¦
800XP Only)
¦
¦
¦
OR
| ¦
¦
C ¦
¦
¦
c) Tank remains empty, and
¦
¦
¦
¦
¦
d) Dorsal tank remains empty.
¦
¦
¦
¦
¦
¦
¦ 20-6 Fuel Filter
¦
¦
¦
¦
¦
De-Icing Systems
¦
¦
¦
¦
¦
(Series 1 Through
¦
¦
¦
| ¦
¦
600 With Viper
¦
¦
¦
| ¦
¦
Engines Only)
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
1) Automatic
C ¦ 1 ¦ 0 ¦ May be inoperative provided fuel
¦
¦
System
¦
¦
¦ temperature indicator, fuel low
¦
¦
¦
¦
¦ pressure warning, fuel filter ice
¦
¦
¦
¦
¦ warning, and manual system operate
¦
¦
¦
¦
¦ normally.
¦
¦
¦
¦
¦
¦
¦
2) Manual System
C ¦ 1 ¦ 0 ¦ May be inoperative provided:
¦
¦
¦
¦
¦
a) Fuel temperature indicator,
¦
¦
¦
¦
¦
fuel low pressure warning,
¦
¦
¦
¦
¦
fuel filter ice warning, and
¦
¦
¦
¦
¦
automatic system operate
¦
¦
¦
¦
¦
normally, and
¦
¦
¦
¦
¦
b) Automatic fuel pump filter
¦
¦
¦
¦
¦
ice warning Press-to-Test
¦
¦
¦
¦
¦
function operates normally.
¦
¦
¦
¦
¦
¦
¦
3) Manual and
C ¦ 2 ¦ 0 ¦ (O)May be inoperative provided:
¦
¦
Automatic
¦
¦
¦
a) Fuel temperature indicator
¦
¦
Systems
¦
¦
¦
operates normally, and
¦
¦
¦
¦
¦
b) Fuel temperature remains at
¦
¦
¦
¦
¦
or above 5 degrees C.
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
-------------------------------------------------------------------------------
------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION
¦
¦
¦
¦
MASTER MINIMUM EQUIPMENT LIST
¦
¦ FEDERAL AVIATION ADMINISTRATION
¦
¦ --------------------------------------------------------------------------- ¦
¦ AIRCRAFT:
¦ REVISION NO: 5
¦ PAGE:
¦
¦
HAWKER SIDDELEY HS-125
¦
¦
¦
¦
(SERIES 1 THROUGH 800XP)
¦ DATE: 05/30/2002
¦ 28-3
¦
¦ --------------------------------------------------------------------------- ¦
¦
1. ¦ 2. NUMBER INSTALLED
¦
¦ SYSTEM &
¦
-------------------------------------------- ¦
¦ SEQUENCE
ITEM
¦
¦ 3. NUMBER REQUIRED FOR DISPATCH
¦
¦ NUMBERS
¦
¦
--------------------------------------- ¦
¦ ------------------------- ¦
¦
¦ 4. REMARKS OR EXCEPTIONS
¦
¦ 28 FUEL
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 20-7 Fuel Filter
C ¦ 2 ¦ 1 ¦ (O)One may be inoperative provided
¦
¦
Warning Lights
¦
¦
¦ automatic fuel filter de-icing
¦
¦
(Viper Engine
¦
¦
¦ system operates normally, and is
¦
¦
Only)
¦
¦
¦ used during flight.
¦
¦
¦
¦
¦
¦
¦ 22-1 Pressure Fueling
¦
¦
¦
¦
¦
System
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
1) Series 700
C ¦ 1 ¦ 0 ¦ (M)(O)May be inoperative provided: | ¦
¦
Only
¦
¦
¦
a) Both refueling vent valves,
¦
¦
¦
¦
¦
master refuel valve and tank
¦
¦
¦
¦
¦
refueling valves are closed,
¦
¦
¦
¦
¦
b) Overwing refueling procedure
¦
¦
¦
¦
¦
is established and used, and
¦
¦
¦
¦
¦
c) Failure of the fueling
¦
¦
¦
¦
¦
system is not due to fuel
¦
¦
¦
¦
¦
pipe leakage.
¦
¦
¦
¦
¦
¦
¦
2) Series 800
C ¦ 1 ¦ 0 ¦ (M)(O)May be inoperative provided: | ¦
¦
and 800XP Only)
¦
¦
¦
a) Master refueling valve and
¦
¦
¦
¦
¦
all tank refueling valves
¦
¦
¦
¦
¦
are closed,
¦
¦
¦
¦
¦
b) Overwing refueling procedure
¦
¦
¦
¦
¦
is established and used, and
¦
¦
¦
¦
¦
c) Failure of the fueling
¦
¦
¦
¦
¦
system is not due to fuel
¦
¦
¦
¦
¦
pipe leakage.
¦
¦
¦
¦
¦
¦
¦ 22-2 Pressure Refuel
C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided
| ¦
¦
Blanking Cap
¦
¦
¦ master refuel valve is closed.
| ¦
¦
¦
¦
¦
¦
¦ 42-1 Fuel Content
B ¦ 2 ¦ 1 ¦ (M)(O)One may be inoperative
¦
¦
Indicators (Wing
¦
¦
¦ provided:
¦
¦
Tanks)
¦
¦
¦
a) Fuel in associated tank is
¦
¦
¦
¦
¦
verfied by an alternate
¦
¦
¦
¦
¦
means,
¦
¦
¦
¦
¦
b) All remaining fuel system
¦
¦
¦
¦
¦
components operate normally,
¦
¦
¦
¦
¦
and
¦
¦
¦
¦
¦
c) Fuel flow/fuel used indica¦
¦
¦
¦
¦
tors operate normally.
¦
-------------------------------------------------------------------------------
------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION
¦
¦
¦
¦
MASTER MINIMUM EQUIPMENT LIST
¦
¦ FEDERAL AVIATION ADMINISTRATION
¦
¦ --------------------------------------------------------------------------- ¦
¦ AIRCRAFT:
¦ REVISION NO: 5
¦ PAGE:
¦
¦
HAWKER SIDDELEY HS-125
¦
¦
¦
¦
(SERIES 1 THROUGH 800XP)
¦ DATE: 05/30/2002
¦ 28-4
¦
¦ --------------------------------------------------------------------------- ¦
¦
1. ¦ 2. NUMBER INSTALLED
¦
¦ SYSTEM &
¦
-------------------------------------------- ¦
¦ SEQUENCE
ITEM
¦
¦ 3. NUMBER REQUIRED FOR DISPATCH
¦
¦ NUMBERS
¦
¦
--------------------------------------- ¦
¦ ------------------------- ¦
¦
¦ 4. REMARKS OR EXCEPTIONS
¦
¦ 28 FUEL
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 42-2 Fuel Used
C ¦ - ¦ 0 ¦ (O)May be inoperative provided:
¦
¦
Counter/Fuel
¦
¦
¦
a) Associated wing tank
¦
¦
Totalizer
¦
¦
¦
quantity indicating
¦
¦
¦
¦
¦
system(s) operates normally,
¦
¦
¦
¦
¦
and
¦
¦
¦
¦
¦
b) Flight crew periodically
¦
¦
¦
¦
¦
computes fuel remaining, or
¦
¦
¦
¦
¦
verifies fuel remaining
¦
¦
¦
¦
¦
against a precomputed burn
¦
¦
¦
¦
¦
chart.
¦
¦
¦
¦
¦
¦
¦ 43-1 Ventral Tank
C ¦ 1 ¦ 0 ¦ (M)(O)May be inoperative provided
¦
¦
"EMPTY/FULL"
¦
¦
¦ tank is verified empty before each
¦
¦
Indicator
¦
¦
¦ departure
¦
¦
¦
¦
¦
¦
¦ 43-2 Dorsal Tank
C ¦ 1 ¦ 0 ¦ (M)(O)May be inoperative provided
¦
¦
"Empty/Full"
¦
¦
¦ tank is verified empty before each
¦
¦
Indicator (Series
¦
¦
¦ departure.
¦
¦
600 and 700
¦
¦
¦
| ¦
¦
Only)
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 43-3 Low VMO Audible
¦
¦
¦
¦
¦
Warning System
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
1) Series 3A/RA,
C ¦ 1 ¦ 0 ¦ (M)(O)May be inoperative provided
| ¦
¦
3B/RA Through
¦
¦
¦ ventral tank is verified empty
| ¦
¦
400, 800 and
¦
¦
¦ before each departure.
| ¦
¦
800XP Only
¦
¦
¦
| ¦
¦
¦
¦
¦
¦
¦
2) Series 600 and C ¦ 1 ¦ 0 ¦ (M)(O)May be inoperative provided
| ¦
¦
700 Only
¦
¦
¦ ventral and dorsal tanks are
| ¦
¦
¦
¦
¦ verified empty before each
¦
¦
¦
¦
¦ departure.
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
-------------------------------------------------------------------------------
------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION
¦
¦
¦
¦
MASTER MINIMUM EQUIPMENT LIST
¦
¦ FEDERAL AVIATION ADMINISTRATION
¦
¦ --------------------------------------------------------------------------- ¦
¦ AIRCRAFT:
¦ REVISION NO: 5
¦ PAGE:
¦
¦
HAWKER SIDDELEY HS-125
¦
¦
¦
¦
(SERIES 1 THROUGH 800XP)
¦ DATE: 05/30/2002
¦ 28-5
¦
¦ --------------------------------------------------------------------------- ¦
¦
1. ¦ 2. NUMBER INSTALLED
¦
¦ SYSTEM &
¦
-------------------------------------------- ¦
¦ SEQUENCE
ITEM
¦
¦ 3. NUMBER REQUIRED FOR DISPATCH
¦
¦ NUMBERS
¦
¦
--------------------------------------- ¦
¦ ------------------------- ¦
¦
¦ 4. REMARKS OR EXCEPTIONS
¦
¦ 28 FUEL
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 43-4 Fuel Vent Surge
C ¦ 2 ¦ 0 ¦ (M)(O)May be inoperative provided:
¦
¦
Tank Indicators
¦
¦
¦
a) Both fuel content indicators
¦
¦
(Series 3A/RA,
¦
¦
¦
operate normally, and
| ¦
¦
3B/RA Through
¦
¦
¦
b) Vent valves operate
| ¦
¦
600 Only)
¦
¦
¦
normally.
¦
¦
¦
¦
¦
¦
¦ 45-1 Fuel Temperature
¦
¦
¦
¦
¦
Indicator
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
1) Viper Engine
C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided:
¦
¦
Only
¦
¦
¦
a) Fuel filter ice warning
¦
¦
¦
¦
¦
system operates normally,
¦
¦
¦
¦
¦
b) Fuel filter de-icing system
¦
¦
¦
¦
¦
operates normally,
¦
¦
¦
¦
¦
c) OAT indicator operates
¦
¦
¦
¦
¦
normally, and
¦
¦
¦
¦
¦
d) Fuel temperature AFM
¦
¦
¦
¦
¦
Limitations are applied.
¦
¦
¦
¦
¦
¦
¦
2) TFE-731 Engines C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided:
¦
¦
Only
¦
¦
¦
a) OAT indicator operates
¦
¦
¦
¦
¦
normally, and
¦
¦
¦
¦
¦
b) Fuel temperature AFM
¦
¦
¦
¦
¦
Limitations are applied.
¦
¦
¦
¦
¦
¦
¦ 45-2 Fuel Management
C ¦ - ¦ 0 ¦
| ¦
¦ *** Computer System
¦
¦
¦
| ¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
-------------------------------------------------------------------------------
------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION
¦
¦
¦
¦
MASTER MINIMUM EQUIPMENT LIST
¦
¦ FEDERAL AVIATION ADMINISTRATION
¦
¦ --------------------------------------------------------------------------- ¦
¦ AIRCRAFT:
¦ REVISION NO: 5
¦ PAGE:
¦
¦
HAWKER SIDDELEY HS-125
¦
¦
¦
¦
(SERIES 1 THROUGH 800XP)
¦ DATE: 05/30/2002
¦ 29-1
¦
¦ --------------------------------------------------------------------------- ¦
¦
1. ¦ 2. NUMBER INSTALLED
¦
¦ SYSTEM &
¦
-------------------------------------------- ¦
¦ SEQUENCE
ITEM
¦
¦ 3. NUMBER REQUIRED FOR DISPATCH
¦
¦ NUMBERS
¦
¦
--------------------------------------- ¦
¦ ------------------------- ¦
¦
¦ 4. REMARKS OR EXCEPTIONS
¦
¦ 29 HYDRAULIC POWER
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 30-1 Hydraulic Flow
C ¦ 2 ¦ 1 ¦ (O)One may be inoperative provided:
¦
¦
Indicators (Viper
¦
¦
¦
a) Associated pump operates
¦
¦
Engines Only)
¦
¦
¦
normally,
¦
¦
¦
¦
¦
b) Main supply pressure indi¦
¦
¦
¦
¦
cator operates normally, and
¦
¦
¦
¦
¦
c) Associated engine is started
¦
¦
¦
¦
¦
first to verify pressure
¦
¦
¦
¦
¦
buildup before each
¦
¦
¦
¦
¦
departure.
¦
¦
¦
¦
¦
¦
¦ 30-2 HYD LO PRESS 1 and C ¦ 2 ¦ 1 ¦ (O)One may be inoperative provided:
¦
¦
2 Annunciators
¦
¦
¦
a) Associated pump operates
¦
¦
(TFE-731 Engines
¦
¦
¦
normally,
¦
¦
Only)
¦
¦
¦
b) Main supply pressure indi¦
¦
¦
¦
¦
cator operates normally, and
¦
¦
¦
¦
¦
c) Associated engine is started
¦
¦
¦
¦
¦
first to verify pressure
¦
¦
¦
¦
¦
buildup before each
¦
¦
¦
¦
¦
departure.
¦
¦
¦
¦
¦
¦
¦ 30-3 Combined Brakes
¦
¦
¦
¦
¦
and Supply
¦
¦
¦
¦
¦
Pressure Gauge
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
1) Brake Pressure C ¦ 2 ¦ 1 ¦ (O)One may be inoperative provided:
¦
¦
Indicators
¦
¦
¦
a) Main hydraulic system
¦
¦
¦
¦
¦
indication operates
¦
¦
¦
¦
¦
normally,
¦
¦
¦
¦
¦
b) Emergency brake pressure
¦
¦
¦
¦
¦
indicators/annunciators
¦
¦
¦
¦
¦
operate normally.
¦
¦
¦
¦
¦
c) Before each departure,
¦
¦
¦
¦
¦
normal braking is verified
¦
¦
¦
¦
¦
independently for left and
¦
¦
¦
¦
¦
right brakes.
¦
¦
¦
¦
¦
¦
¦ 4. Accummulator
¦
¦
¦ Deleted, Rev. 3.
¦
¦
Pressure Indicators
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
-------------------------------------------------------------------------------
------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION
¦
¦
¦
¦
MASTER MINIMUM EQUIPMENT LIST
¦
¦ FEDERAL AVIATION ADMINISTRATION
¦
¦ --------------------------------------------------------------------------- ¦
¦ AIRCRAFT:
¦ REVISION NO: 5
¦ PAGE:
¦
¦
HAWKER SIDDELEY HS-125
¦
¦
¦
¦
(SERIES 1 THROUGH 800XP)
¦ DATE: 05/30/2002
¦ 29-2
¦
¦ --------------------------------------------------------------------------- ¦
¦
1. ¦ 2. NUMBER INSTALLED
¦
¦ SYSTEM &
¦
-------------------------------------------- ¦
¦ SEQUENCE
ITEM
¦
¦ 3. NUMBER REQUIRED FOR DISPATCH
¦
¦ NUMBERS
¦
¦
--------------------------------------- ¦
¦ ------------------------- ¦
¦
¦ 4. REMARKS OR EXCEPTIONS
¦
¦ 29 HYDRAULIC POWER
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 30-5 Aux. Hyd. Low
C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided
¦
¦
Level Annunciator
¦
¦
¦ fluid quantity is confirmed
¦
¦
(Series 3 Through
¦
¦
¦ visually and is verified to be
| ¦
¦
800XP Only)
¦
¦
¦ adequate before each departure.
| ¦
¦
¦
¦
¦
¦
¦ 30-6 Accumulator
B ¦ 2 ¦ 0 ¦ (M)May be inoperative provided it
| ¦
¦
Pressure Indicators ¦
¦
¦ is verified that the gas charge
| ¦
¦
(Main and Emergency ¦
¦
¦ pressure is correct and that the
| ¦
¦
Only)
¦
¦
¦ accumulator is operating normally. | ¦
¦
¦
¦
¦
¦
¦ 30-7 Thrust Reverser
¦
¦
¦
| ¦
¦
Accumulator
¦
¦
¦
| ¦
¦
Pressure Indicator
¦
¦
¦
| ¦
¦
¦
¦
¦
¦
¦ *** 1) Series 800
C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided T/R | ¦
¦
¦
¦
¦ operation is checked before each
| ¦
¦
¦
¦
¦ departure.
| ¦
¦
¦
¦
¦
¦
¦
2) Series 800XP
C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided T/R | ¦
¦
¦
¦
¦ operation is checked before each
| ¦
¦
¦
¦
¦ departure.
| ¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
-------------------------------------------------------------------------------
------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION
¦
¦
¦
¦
MASTER MINIMUM EQUIPMENT LIST
¦
¦ FEDERAL AVIATION ADMINISTRATION
¦
¦ --------------------------------------------------------------------------- ¦
¦ AIRCRAFT:
¦ REVISION NO: 5
¦ PAGE:
¦
¦
HAWKER SIDDELEY HS-125
¦
¦
¦
¦
(SERIES 1 THROUGH 800XP)
¦ DATE: 05/30/2002
¦ 30-1
¦
¦ --------------------------------------------------------------------------- ¦
¦
1. ¦ 2. NUMBER INSTALLED
¦
¦ SYSTEM &
¦
-------------------------------------------- ¦
¦ SEQUENCE
ITEM
¦
¦ 3. NUMBER REQUIRED FOR DISPATCH
¦
¦ NUMBERS
¦
¦
--------------------------------------- ¦
¦ ------------------------- ¦
¦
¦ 4. REMARKS OR EXCEPTIONS
¦
¦ 30 ICE AND RAIN
¦
¦
¦
¦
¦
PROTECTION
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 10-1 TKS Airframe
C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided the
¦
¦
De-icing System
¦
¦
¦ airplane is not operated in known
¦
¦
¦
¦
¦ or forecast icing conditions.
¦
¦
¦
¦
¦
¦
¦ 10-2 Wing/Tail Anti-ice
¦
¦
¦
¦
¦
Control Switches
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
1) Time Switch
C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided:
¦
¦
¦
¦
¦
a) System is verified OFF when
¦
¦
¦
¦
¦
not in use,
¦
¦
¦
¦
¦
b) Priming can be accomplished, | ¦
¦
¦
¦
¦
and
| ¦
¦
¦
¦
¦
c) An alternate timing method
¦
¦
¦
¦
¦
is established and used.
¦
¦
¦
¦
¦
OR
¦
¦
C ¦
¦
¦
d) Airplane is not operated in
¦
¦
¦
¦
¦
known or forecast icing
¦
¦
¦
¦
¦
conditions.
¦
¦
¦
¦
¦
¦
¦
2) WING AND TAIL
C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided:
¦
¦
ON/OFF Switch
¦
¦
¦
a) System is verified OFF when
¦
¦
(Series 1
¦
¦
¦
not in use, and
| ¦
¦
Through 400
¦
¦
¦
b) Time switch is verified to
| ¦
¦
Only)
¦
¦
¦
operate normally and is used
¦
¦
¦
¦
¦
for anti-icing.
¦
¦
¦
¦
¦
¦
¦ 10-3 T.K.S. Quantity
C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided:
¦
¦
Indication System
¦
¦
¦
a) Fluid quantity is confirmed
¦
¦
¦
¦
¦
visually and is verified
¦
¦
¦
¦
¦
adequate before each
¦
¦
¦
¦
¦
departure.
¦
¦
¦
¦
¦
OR
¦
¦
C ¦
¦
¦
b) Airplane is not operated in
¦
¦
¦
¦
¦
known or forecast icing
¦
¦
¦
¦
¦
conditions.
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
-------------------------------------------------------------------------------
------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION
¦
¦
¦
¦
MASTER MINIMUM EQUIPMENT LIST
¦
¦ FEDERAL AVIATION ADMINISTRATION
¦
¦ --------------------------------------------------------------------------- ¦
¦ AIRCRAFT:
¦ REVISION NO: 5
¦ PAGE:
¦
¦
HAWKER SIDDELEY HS-125
¦
¦
¦
¦
(SERIES 1 THROUGH 800XP)
¦ DATE: 05/30/2002
¦ 30-2
¦
¦ --------------------------------------------------------------------------- ¦
¦
1. ¦ 2. NUMBER INSTALLED
¦
¦ SYSTEM &
¦
-------------------------------------------- ¦
¦ SEQUENCE
ITEM
¦
¦ 3. NUMBER REQUIRED FOR DISPATCH
¦
¦ NUMBERS
¦
¦
--------------------------------------- ¦
¦ ------------------------- ¦
¦
¦ 4. REMARKS OR EXCEPTIONS
¦
¦ 30 ICE AND RAIN
¦
¦
¦
¦
¦
PROTECTION
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 10-4 ANTI-ICE LO PRESS C ¦ 1 ¦ 0 ¦ (M)(O)May be inoperative provided:
¦
¦
Annunciator
¦
¦
¦
a) Fluid delivery system and
¦
¦
(Series 800 and
¦
¦
¦
quantity indication system
| ¦
¦
800XP Only)
¦
¦
¦
operate normally.
| ¦
¦
¦
¦
¦
OR
¦
¦
C ¦
¦
¦
b) Airplane is not operated in
¦
¦
¦
¦
¦
known or forecast icing
¦
¦
¦
¦
¦
conditions.
¦
¦
¦
¦
¦
¦
¦ 10-5 ANTI-ICE LO QTY
C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided:
¦
¦
Annunciator
¦
¦
¦
a) Fluid quantity is visually
¦
¦
(Series 800 and
¦
¦
¦
verified adequate before
¦
¦
800XP Only)
¦
¦
¦
each departure.
| ¦
¦
¦
¦
¦
OR
¦
¦
C ¦
¦
¦
b) Airplane is not operated in
¦
¦
¦
¦
¦
known or forecast icing
¦
¦
¦
¦
¦
conditions.
¦
¦
¦
¦
¦
¦
¦ 10-6 Auxiliary TKS
D ¦ 1 ¦ 0 ¦ (O)May be inoperative provided
¦
¦ *** System
¦
¦
¦ alternate procedures are
| ¦
¦
¦
¦
¦ established and used.
¦
¦
¦
¦
¦
¦
¦ 20-1 Engine Inlet
C ¦ 2 ¦ 1 ¦ (M)(O)One may be inoperative
¦
¦
Anti-icing Systems
¦
¦
¦ provided:
¦
¦
(TFE-731 Engine
¦
¦
¦
a) Associated anti-ice valve is
¦
¦
Aircraft Only)
¦
¦
¦
verified closed, and
¦
¦
¦
¦
¦
b) Airplane is not operated in
¦
¦
¦
¦
¦
visible moisture or in known
¦
¦
¦
¦
¦
or forecast icing
¦
¦
¦
¦
¦
conditions.
¦
¦
¦
¦
¦
¦
¦ 20-2 Engine Inlet
C ¦ 2 ¦ 1 ¦ (O)One may be inoperative provided:
¦
¦
Anti-Ice
¦
¦
¦
a) All power indicating
¦
¦
Indicators/
¦
¦
¦
instruments for associated
¦
¦
Annunciators
¦
¦
¦
engine operate normally, and
¦
¦
¦
¦
¦
b) Associated valve operates
¦
¦
¦
¦
¦
normally.
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
-------------------------------------------------------------------------------
------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION
¦
¦
¦
¦
MASTER MINIMUM EQUIPMENT LIST
¦
¦ FEDERAL AVIATION ADMINISTRATION
¦
¦ --------------------------------------------------------------------------- ¦
¦ AIRCRAFT:
¦ REVISION NO: 5
¦ PAGE:
¦
¦
HAWKER SIDDELEY HS-125
¦
¦
¦
¦
(SERIES 1 THROUGH 800XP)
¦ DATE: 05/30/2002
¦ 30-3
¦
¦ --------------------------------------------------------------------------- ¦
¦
1. ¦ 2. NUMBER INSTALLED
¦
¦ SYSTEM &
¦
-------------------------------------------- ¦
¦ SEQUENCE
ITEM
¦
¦ 3. NUMBER REQUIRED FOR DISPATCH
¦
¦ NUMBERS
¦
¦
--------------------------------------- ¦
¦ ------------------------- ¦
¦
¦ 4. REMARKS OR EXCEPTIONS
¦
¦ 30 ICE AND RAIN
¦
¦
¦
¦
¦
PROTECTION
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 20-3 MWS "ENG ICE PROT C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided "ENG
¦
¦
ON" White
¦
¦
¦ A/ICE" white annunciators on
¦
¦
Annunciator
¦
¦
¦ overhead panel are verified to
¦
¦
(Series 600 and
¦
¦
¦ operate normally.
| ¦
¦
700 Only)
¦
¦
¦
| ¦
¦
¦
¦
¦
¦
¦ 20-4 MWS "ICE PROT
C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided "ENG
¦
¦
SELECTED" White
¦
¦
¦ A/ICE" amber annunciators are
¦
¦
Annunciator
¦
¦
¦ verified to operate normally.
¦
¦
(Series 800 and
¦
¦
¦
| ¦
¦
800XP Only)
¦
¦
¦
| ¦
¦
¦
¦
¦
¦
¦ 30-1 Pitot Probe/
B ¦ 2 ¦ 1 ¦ (O)One may be inoperative provided: | ¦
¦
Pitot Mast
¦
¦
¦
a) Flight is conducted in day
| ¦
¦
Heaters
¦
¦
¦
VMC flight conditions only,
¦
¦
¦
¦
¦
and
¦
¦
¦
¦
¦
b) Airplane is not operated in
¦
¦
¦
¦
¦
visible moisture, or in
¦
¦
¦
¦
¦
known or forecast icing
¦
¦
¦
¦
¦
conditions.
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ NOTE: Both heaters are required for | ¦
¦
¦
¦
¦
RVSM operations.
| ¦
¦
¦
¦
¦
¦
¦ 30-2 Pitot Ammeters
C ¦ 2 ¦ 0 ¦ (O)May be inoperative provided
| ¦
¦
(Series 1 Through
¦
¦
¦ pitot heaters are verified to
| ¦
¦
400 Only)
¦
¦
¦ operate normally before each
| ¦
¦
¦
¦
¦ departure.
| ¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
-------------------------------------------------------------------------------
------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION
¦
¦
¦
¦
MASTER MINIMUM EQUIPMENT LIST
¦
¦ FEDERAL AVIATION ADMINISTRATION
¦
¦ --------------------------------------------------------------------------- ¦
¦ AIRCRAFT:
¦ REVISION NO: 5
¦ PAGE:
¦
¦
HAWKER SIDDELEY HS-125
¦
¦
¦
¦
(SERIES 1 THROUGH 800XP)
¦ DATE: 05/30/2002
¦ 30-4
¦
¦ --------------------------------------------------------------------------- ¦
¦
1. ¦ 2. NUMBER INSTALLED
¦
¦ SYSTEM &
¦
-------------------------------------------- ¦
¦ SEQUENCE
ITEM
¦
¦ 3. NUMBER REQUIRED FOR DISPATCH
¦
¦ NUMBERS
¦
¦
--------------------------------------- ¦
¦ ------------------------- ¦
¦
¦ 4. REMARKS OR EXCEPTIONS
¦
¦ 30 ICE AND RAIN
¦
¦
¦
¦
¦
PROTECTION
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 30-3 Pitot Ammeter &
C ¦ - ¦ 0 ¦ (M)(O)May be inoperative provided
¦
¦
Selector (Series
¦
¦
¦ pitot heaters are verified to
¦
¦
600 Through 800XP
¦
¦
¦ operate normally before each
| ¦
¦
Only)
¦
¦
¦ departure.
¦
¦
¦
¦
¦
¦
¦ 30-4 Pitot/Mast Heater B ¦ - ¦ 0 ¦ (O)May be inoperative provided:
| ¦
¦
Fail Light(s)
¦
¦
¦
a) Associated heating system is | ¦
¦
Annunciator(s)
¦
¦
¦
verified to operate normally
¦
¦
¦
¦
¦
before each departure, and
¦
¦
¦
¦
¦
b) Associated ammeter is
¦
¦
¦
¦
¦
installed and operates
¦
¦
¦
¦
¦
normally.
¦
¦
¦
¦
¦
¦
¦ 30-5 Static Plate
B ¦ 2 ¦ 1 ¦ (O)One may be inoperative provided: | ¦
¦
Heaters (Series
¦
¦
¦
a) Flight is conducted in day
| ¦
¦
*** 700, 800 and
¦
¦
¦
VMC flight conditions only
| ¦
¦
800XP Only)
¦
¦
¦
and
| ¦
¦
¦
¦
¦
b) Airplane is not operated in | ¦
¦
¦
¦
¦
visible moisture, or in
| ¦
¦
¦
¦
¦
known or forecast icing
| ¦
¦
¦
¦
¦
conditions.
| ¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ NOTE: Both heaters are required for | ¦
¦
¦
¦
¦
RVSM operations.
| ¦
¦
¦
¦
¦
¦
¦ 30-6 Stall Vane Heaters B ¦ 2 ¦ 1 ¦ (O)One may be inoperative provided: | ¦
¦
(Series 800 and
¦
¦
¦
a) Flight is conducted in day
| ¦
¦
800XP Only)
¦
¦
¦
VMC flight conditions only, | ¦
¦
¦
¦
¦
and
| ¦
¦
¦
¦
¦
b) Airplane is not operated in | ¦
¦
¦
¦
¦
visible moisture, or in
| ¦
¦
¦
¦
¦
known or forecast icing
| ¦
¦
¦
¦
¦
conditions.
| ¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
-------------------------------------------------------------------------------
------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION
¦
¦
¦
¦
MASTER MINIMUM EQUIPMENT LIST
¦
¦ FEDERAL AVIATION ADMINISTRATION
¦
¦ --------------------------------------------------------------------------- ¦
¦ AIRCRAFT:
¦ REVISION NO: 5
¦ PAGE:
¦
¦
HAWKER SIDDELEY HS-125
¦
¦
¦
¦
(SERIES 1 THROUGH 800XP)
¦ DATE: 05/30/2002
¦ 30-5
¦
¦ --------------------------------------------------------------------------- ¦
¦
1. ¦ 2. NUMBER INSTALLED
¦
¦ SYSTEM &
¦
-------------------------------------------- ¦
¦ SEQUENCE
ITEM
¦
¦ 3. NUMBER REQUIRED FOR DISPATCH
¦
¦ NUMBERS
¦
¦
--------------------------------------- ¦
¦ ------------------------- ¦
¦
¦ 4. REMARKS OR EXCEPTIONS
¦
¦ 30 ICE AND RAIN
¦
¦
¦
¦
¦
PROTECTION
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 40-1 Windscreen Heating
¦
¦
¦
¦
¦
System
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
1) 1 Through 700
C ¦ 2 ¦ 0 ¦ (O)May be inoperative provided:
| ¦
¦
Series Only
¦
¦
¦
a) Airplane is operated in
¦
¦
¦
¦
¦
accordance with AFM
¦
¦
¦
¦
¦
Limitations, and
¦
¦
¦
¦
¦
b) Windscreen fluid de-icing
¦
¦
¦
¦
¦
system is installed and
¦
¦
¦
¦
¦
operates normally.
¦
¦
¦
¦
¦
OR
¦
¦
C ¦
¦
¦
c) Airplane is operated in
¦
¦
¦
¦
¦
accordance with AFM
¦
¦
¦
¦
¦
Limitations, and
¦
¦
¦
¦
¦
d) Airplane is not operated in
¦
¦
¦
¦
¦
known or forecast icing
¦
¦
¦
¦
¦
conditions.
¦
¦
¦
¦
¦
¦
¦
2) Series 800 and C ¦ 4 ¦ 3 ¦ (O)Heating to one side screen "B"
| ¦
¦
800XP Only
¦
¦
¦ only may be inoperative.
| ¦
¦
¦
¦
¦
¦
¦
C ¦ 4 ¦ 0 ¦ (O)May be inoperative provided:
¦
¦
¦
¦
¦
a) Airplane is operated in
¦
¦
¦
¦
¦
accordance with AFM
¦
¦
¦
¦
¦
Limitations, and
¦
¦
¦
¦
¦
b) Airplane is not operated in
¦
¦
¦
¦
¦
known or forecast icing
¦
¦
¦
¦
¦
conditions.
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
-------------------------------------------------------------------------------
------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION
¦
¦
¦
¦
MASTER MINIMUM EQUIPMENT LIST
¦
¦ FEDERAL AVIATION ADMINISTRATION
¦
¦ --------------------------------------------------------------------------- ¦
¦ AIRCRAFT:
¦ REVISION NO: 5
¦ PAGE:
¦
¦
HAWKER SIDDELEY HS-125
¦
¦
¦
¦
(SERIES 1 THROUGH 800XP)
¦ DATE: 05/30/2002
¦ 30-6
¦
¦ --------------------------------------------------------------------------- ¦
¦
1. ¦ 2. NUMBER INSTALLED
¦
¦ SYSTEM &
¦
-------------------------------------------- ¦
¦ SEQUENCE
ITEM
¦
¦ 3. NUMBER REQUIRED FOR DISPATCH
¦
¦ NUMBERS
¦
¦
--------------------------------------- ¦
¦ ------------------------- ¦
¦
¦ 4. REMARKS OR EXCEPTIONS
¦
¦ 30 ICE AND RAIN
¦
¦
¦
¦
¦
PROTECTION
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 40-2 Windscreen
C ¦ - ¦ 0 ¦ (M)(O)May be inoperative provided: | ¦
¦
Overheat Lights/
¦
¦
¦
a) Affected windscreen heat
| ¦
¦
Annunciators
¦
¦
¦
system is not used,
| ¦
¦
¦
¦
¦
b) Airplane is not operated
| ¦
¦
¦
¦
¦
in known or forecast icing
| ¦
¦
¦
¦
¦
conditions, and
| ¦
¦
¦
¦
¦
c) AFM take-off temperature
| ¦
¦
¦
¦
¦
and airspeed limitations
| ¦
¦
¦
¦
¦
are observed.
| ¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ NOTE 1: Not required for an inoper- | ¦
¦
¦
¦
¦
ative windscreen heat
¦
¦
¦
¦
¦
system.
¦
¦
¦
¦
¦
¦
¦ 40-3 Windscreen Wiper
C ¦ 2 ¦ 0 ¦ May be inoperative provided
¦
¦
Systems (Series
¦
¦
¦ airplane is not operated in
| ¦
¦
1 Through 700
¦
¦
¦ precipitation within 5 nautical
| ¦
¦
Only)
¦
¦
¦ miles of the airport of takeoff or
¦
¦
¦
¦
¦ intended landing.
¦
¦
¦
¦
¦
¦
¦
1) Park and Slow
C ¦ - ¦ 0 ¦ May be inoperative without an an
¦
¦
Speed Function
¦
¦
¦ operational restriction provided
¦
¦
¦
¦
¦ blade(s) can be positioned in a
¦
¦
¦
¦
¦ location that will not obstruct
¦
¦
¦
¦
¦ forward vision.
¦
¦
¦
¦
¦
¦
¦ 80-1 Ice Detection
C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided:
| ¦
¦
System
¦
¦
¦
a) Flight is conducted in day
| ¦
¦
¦
¦
¦
VMC flight conditions only, | ¦
¦
¦
¦
¦
and
| ¦
¦
¦
¦
¦
b) Airplane is not operated in | ¦
¦
¦
¦
¦
visible moisture, or in
| ¦
¦
¦
¦
¦
known or forecast icing
| ¦
¦
¦
¦
¦
conditions.
| ¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
-------------------------------------------------------------------------------
------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION
¦
¦
¦
¦
MASTER MINIMUM EQUIPMENT LIST
¦
¦ FEDERAL AVIATION ADMINISTRATION
¦
¦ --------------------------------------------------------------------------- ¦
¦ AIRCRAFT:
¦ REVISION NO: 5
¦ PAGE:
¦
¦
HAWKER SIDDELEY HS-125
¦
¦
¦
¦
(SERIES 1 THROUGH 800XP)
¦ DATE: 05/30/2002
¦ 31-1
¦
¦ --------------------------------------------------------------------------- ¦
¦
1. ¦ 2. NUMBER INSTALLED
¦
¦ SYSTEM &
¦
-------------------------------------------- ¦
¦ SEQUENCE
ITEM
¦
¦ 3. NUMBER REQUIRED FOR DISPATCH
¦
¦ NUMBERS
¦
¦
--------------------------------------- ¦
¦ ------------------------- ¦
¦
¦ 4. REMARKS OR EXCEPTIONS
¦
¦ 31 INDICATING/RECORDING ¦
¦
¦
¦
¦
SYSTEMS
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 20-1 Clocks
C ¦ - ¦ 1 ¦ One may be inoperative at either
¦
¦
¦
¦
¦ pilot's or copilot's stations.
¦
¦
¦
¦
¦
¦
¦ 30-1 Flight Data
D ¦ - ¦ 1 ¦ Any in excess of those required by | ¦
¦ *** Recorder (FDR)
¦
¦
¦ FAR may be inoperative.
| ¦
¦
System
¦
¦
¦
¦
¦
¦
¦
¦
| ¦
¦
A ¦ - ¦ 0 ¦ May be inoperative provided:
| ¦
¦
¦
¦
¦
a) Cockpit Voice Recorder
| ¦
¦
¦
¦
¦
(CVR) operates normally,
| ¦
¦
¦
¦
¦
b) Airplane is not dispatched
| ¦
¦
¦
¦
¦
from a designated airport as | ¦
¦
¦
¦
¦
listed in the operator's MEL | ¦
¦
¦
¦
¦
unless:
| ¦
¦
¦
¦
¦
1. The FDR failure occurs
| ¦
¦
¦
¦
¦
after pushback but before | ¦
¦
¦
¦
¦
takeoff, or
| ¦
¦
¦
¦
¦
2. FDR repair was attempted | ¦
¦
¦
¦
¦
but was not sucessful.
| ¦
¦
¦
¦
¦
c) In those cases where repair | ¦
¦
¦
¦
¦
is attempted but not sucess- | ¦
¦
¦
¦
¦
ful, the aircraft may be
| ¦
¦
¦
¦
¦
dipatched on a flight or
| ¦
¦
¦
¦
¦
series of flights until the | ¦
¦
¦
¦
¦
next designated airport
| ¦
¦
¦
¦
¦
where repair must be accom- | ¦
¦
¦
¦
¦
plished before dispatch, and | ¦
¦
¦
¦
¦
d) Repairs are made within
| ¦
¦
¦
¦
¦
three flight days.
| ¦
¦
¦
¦
¦
¦
¦
1) FDR Recording
A ¦ - ¦ - ¦ May be inoperative provided:
| ¦
¦
Parameters
¦
¦
¦
a) Cockpit Voice Recorder
| ¦
¦
Required by FAR
¦
¦
¦
operates normally, and
| ¦
¦
¦
¦
¦
b) Repairs are made within 20
| ¦
¦
¦
¦
¦
calendar days.
| ¦
¦
¦
¦
¦
¦
¦
2) FDR Recording
A ¦ - ¦ - ¦ May be inoperative provided repairs | ¦
¦
Parameters
¦
¦
¦ are made prior to the completion of | ¦
¦
Not required
¦
¦
¦ the next heavy maintenance visit.
| ¦
¦
by FAR
¦
¦
¦
| ¦
-------------------------------------------------------------------------------
------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION
¦
¦
¦
¦
MASTER MINIMUM EQUIPMENT LIST
¦
¦ FEDERAL AVIATION ADMINISTRATION
¦
¦ --------------------------------------------------------------------------- ¦
¦ AIRCRAFT:
¦ REVISION NO: 5
¦ PAGE:
¦
¦
HAWKER SIDDELEY HS-125
¦
¦
¦
¦
(SERIES 1 THROUGH 800XP)
¦ DATE: 05/30/2002
¦ 31-2
¦
¦ --------------------------------------------------------------------------- ¦
¦
1. ¦ 2. NUMBER INSTALLED
¦
¦ SYSTEM &
¦
-------------------------------------------- ¦
¦ SEQUENCE
ITEM
¦
¦ 3. NUMBER REQUIRED FOR DISPATCH
¦
¦ NUMBERS
¦
¦
--------------------------------------- ¦
¦ ------------------------- ¦
¦
¦ 4. REMARKS OR EXCEPTIONS
¦
¦ 31 INDICATING/RECORDING ¦
¦
¦
¦
¦
SYSTEMS
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 40-1 Flight Hour Meter C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided
¦
¦ ***
¦
¦
¦ alternate procedures are
| ¦
¦
¦
¦
¦ established and used.
¦
¦
¦
¦
¦
¦
¦ 50-1 Dual Filament
¦
¦
¦
| ¦
¦
Annunciator(s)
¦
¦
¦
| ¦
¦
¦
¦
¦
¦
¦
1) Filament
C ¦ - ¦ - ¦ One filament in each annunciator
| ¦
¦
¦
¦
¦ may be inoperative.
| ¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
-------------------------------------------------------------------------------
------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION
¦
¦
¦
¦
MASTER MINIMUM EQUIPMENT LIST
¦
¦ FEDERAL AVIATION ADMINISTRATION
¦
¦ --------------------------------------------------------------------------- ¦
¦ AIRCRAFT:
¦ REVISION NO: 5
¦ PAGE:
¦
¦
HAWKER SIDDELEY HS-125
¦
¦
¦
¦
(SERIES 1 THROUGH 800XP)
¦ DATE: 05/30/2002
¦ 32-1
¦
¦ --------------------------------------------------------------------------- ¦
¦
1. ¦ 2. NUMBER INSTALLED
¦
¦ SYSTEM &
¦
-------------------------------------------- ¦
¦ SEQUENCE
ITEM
¦
¦ 3. NUMBER REQUIRED FOR DISPATCH
¦
¦ NUMBERS
¦
¦
--------------------------------------- ¦
¦ ------------------------- ¦
¦
¦ 4. REMARKS OR EXCEPTIONS
¦
¦ 32 LANDING GEAR
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 32-1 MLG Door Latch
D ¦ 2 ¦ 0 ¦
¦
¦
Springs
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 40-1 Maxaret Unit
¦
¦
¦ Deleted, Rev. 3.
¦
¦
(Anti-Skid System)
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 60-1 Gear Down and
¦
¦
¦
¦
¦
Locked Indicators
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
1) Primary
B ¦ 3 ¦ 2 ¦ (O)One indicator may be inoperative
¦
¦
Indicators
¦
¦
¦ provided all standby indicators
¦
¦
¦
¦
¦ operate normally.
¦
¦
¦
¦
¦
¦
¦
2) Standby
B ¦ 3 ¦ 2 ¦ (O)One indicator may be inoperative
¦
¦
Indicators
¦
¦
¦ provided all primary indicators
¦
¦
¦
¦
¦ operate normally.
¦
¦
¦
¦
¦
¦
¦ 60-2 Gear Unlocked
C ¦ 3 ¦ 3 ¦ One filament in each light may be
¦
¦
Indications
¦
¦
¦ inoperative.
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
-------------------------------------------------------------------------------
------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION
¦
¦
¦
¦
MASTER MINIMUM EQUIPMENT LIST
¦
¦ FEDERAL AVIATION ADMINISTRATION
¦
¦ --------------------------------------------------------------------------- ¦
¦ AIRCRAFT:
¦ REVISION NO: 5
¦ PAGE:
¦
¦
HAWKER SIDDELEY HS-125
¦
¦
¦
¦
(SERIES 1 THROUGH 800XP)
¦ DATE: 05/30/2002
¦ 33-1
¦
¦ --------------------------------------------------------------------------- ¦
¦
1. ¦ 2. NUMBER INSTALLED
¦
¦ SYSTEM &
¦
-------------------------------------------- ¦
¦ SEQUENCE
ITEM
¦
¦ 3. NUMBER REQUIRED FOR DISPATCH
¦
¦ NUMBERS
¦
¦
--------------------------------------- ¦
¦ ------------------------- ¦
¦
¦ 4. REMARKS OR EXCEPTIONS
¦
¦ 33 LIGHTS
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 10-1 Cockpit/Flight
C ¦ - ¦ - ¦ Individual lights may be
| ¦
¦
Deck/Flight
¦
¦
¦ inoperative provided remaining
| ¦
¦
Compartment and
¦
¦
¦ lights are:
| ¦
¦
Instrument Light¦
¦
¦
a) Sufficient to clearly
| ¦
¦
ing System
¦
¦
¦
illuminate all required
| ¦
¦
¦
¦
¦
instruments, controls, and
¦
¦
¦
¦
¦
devices for which they
¦
¦
¦
¦
¦
are intended,
¦
¦
¦
¦
¦
b) Positioned so that direct
¦
¦
¦
¦
¦
rays are shielded from
¦
¦
¦
¦
¦
flight crewmembers' eyes,
¦
¦
¦
¦
¦
and
| ¦
¦
¦
¦
¦
c) Lighting configuration and
¦
¦
¦
¦
¦
intensity is acceptable to
¦
¦
¦
¦
¦
the flightcrew.
¦
¦
¦
¦
¦
¦
¦ 10-2 CAGS Warning Light C ¦ 2 ¦ 1 ¦ One flasher may be inoperative
¦
¦
Systems (Series 1
¦
¦
¦ provided all remaining system
| ¦
¦
Through 400 Only)
¦
¦
¦ warning lights operate normally.
| ¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ NOTE: Not required for inoperative
¦
¦
¦
¦
¦
systems.
¦
¦
¦
¦
¦
¦
¦ 10-3 Master Warning
C ¦ 2 ¦ 1 ¦ One flasher may be inoperative
¦
¦
Light Systems
¦
¦
¦ provided all remaining system
¦
¦
(Series 600
¦
¦
¦ warning lights operate normally.
| ¦
¦
Through 800XP
¦
¦
¦
| ¦
¦
Only)
¦
¦
¦ NOTE: Not required for inoperative
¦
¦
¦
¦
¦
systems.
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
-------------------------------------------------------------------------------
------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION
¦
¦
¦
¦
MASTER MINIMUM EQUIPMENT LIST
¦
¦ FEDERAL AVIATION ADMINISTRATION
¦
¦ --------------------------------------------------------------------------- ¦
¦ AIRCRAFT:
¦ REVISION NO: 5
¦ PAGE:
¦
¦
HAWKER SIDDELEY HS-125
¦
¦
¦
¦
(SERIES 1 THROUGH 800XP)
¦ DATE: 05/30/2002
¦ 33-2
¦
¦ --------------------------------------------------------------------------- ¦
¦
1. ¦ 2. NUMBER INSTALLED
¦
¦ SYSTEM &
¦
-------------------------------------------- ¦
¦ SEQUENCE
ITEM
¦
¦ 3. NUMBER REQUIRED FOR DISPATCH
¦
¦ NUMBERS
¦
¦
--------------------------------------- ¦
¦ ------------------------- ¦
¦
¦ 4. REMARKS OR EXCEPTIONS
¦
¦ 33 LIGHTS
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 20-1 Cabin Interior
C ¦ - ¦ - ¦ (O)Individual lights may be
¦
¦
Light System
¦
¦
¦ inoperative provided:
¦
¦
¦
¦
¦
a) Remaining lighting is
¦
¦
¦
¦
¦
sufficient for cabin
¦
¦
¦
¦
¦
attendants to perform their
¦
¦
¦
¦
¦
duties, and
¦
¦
¦
¦
¦
b) Cabin emergency lighting is
¦
¦
¦
¦
¦
verified to operate
¦
¦
¦
¦
¦
normally.
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ NOTE 1: Not required for all cargo
¦
¦
¦
¦
¦
operations.
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ NOTE 2: Cabin emergency lighting
¦
¦
¦
¦
¦
does not include floor
¦
¦
¦
¦
¦
proximity lights.
¦
¦
¦
¦
¦
¦
¦ 20-2 Passenger Notice
C ¦ - ¦ 0 ¦ (O)If one or more "No Smoking/
¦
¦
System ("No
¦
¦
¦ Fasten Seat Belt" signs are inoper¦
¦
Smoking Fasten
¦
¦
¦ ative, the associated passenger
¦
¦
Seat Belt/ Return
¦
¦
¦ seat(s) may be occupied provided:
¦
¦
to Cabin") Signs
¦
¦
¦
a) PA System operates normally,
¦
¦
¦
¦
¦
and
¦
¦
¦
¦
¦
b) PA System is used to notify
¦
¦
¦
¦
¦
passengers when seat belts
¦
¦
¦
¦
¦
should be fastened, and
¦
¦
¦
¦
¦
smoking is prohibited.
¦
¦
¦
¦
¦
OR
¦
¦
C ¦
¦
¦
c) Alternate procedures are
¦
¦
¦
¦
¦
established and used to
¦
¦
¦
¦
¦
notify passengers when seat
¦
¦
¦
¦
¦
belts should be fastened,
¦
¦
¦
¦
¦
and smoking is prohibited.
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
-------------------------------------------------------------------------------
------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION
¦
¦
¦
¦
MASTER MINIMUM EQUIPMENT LIST
¦
¦ FEDERAL AVIATION ADMINISTRATION
¦
¦ --------------------------------------------------------------------------- ¦
¦ AIRCRAFT:
¦ REVISION NO: 4
¦ PAGE:
¦
¦
HAWKER SIDDELEY HS-125
¦
¦
¦
¦
(SERIES 1 THROUGH 800XP)
¦ DATE: 03/10/1998
¦ 33-3
¦
¦ --------------------------------------------------------------------------- ¦
¦
1. ¦ 2. NUMBER INSTALLED
¦
¦ SYSTEM &
¦
-------------------------------------------- ¦
¦ SEQUENCE
ITEM
¦
¦ 3. NUMBER REQUIRED FOR DISPATCH
¦
¦ NUMBERS
¦
¦
--------------------------------------- ¦
¦ ------------------------- ¦
¦
¦ 4. REMARKS OR EXCEPTIONS
¦
¦ 33 LIGHTS
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 20-5 EMERGENCY LTS SEL D ¦ 1 ¦ 0 ¦ (O)May be inoperative provided:
¦
¦ *** OFF Annunciation
¦
¦
¦
a) Passenger cabin emergency
¦
¦
¦
¦
¦
lighting system is verified
¦
¦
¦
¦
¦
to operate normally, and
¦
¦
¦
¦
¦
b) Flightcrew ensures the
¦
¦
¦
¦
¦
INTERIOR LIGHTS EMERG switch
¦
¦
¦
¦
¦
is ARMED before each
¦
¦
¦
¦
¦
departure.
¦
¦
¦
¦
¦
¦
¦ 30-1 Wheel Well
C ¦ - ¦ 0 ¦
¦
¦ *** Lighting System
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 30-2 Rear Equipment
C ¦ - ¦ 0 ¦
¦
¦ *** Bay Lighting
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 30-3 Pannier Lighting
D ¦ 1 ¦ 0 ¦
¦
¦ *** System
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 40-1 Anti-Collision
¦
¦
¦
¦
¦
Beacons
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
1) Fuselage/
C ¦ 2 ¦ 0 ¦ May be inoperative for night
¦
¦
Vertical Fin
¦
¦
¦ operations provided Wing/Tail white
¦
¦
¦
¦
¦ strobe lights operate normally.
¦
¦
¦
¦
¦
¦
¦
C ¦ 2 ¦ 0 ¦ May be inoperative for day
¦
¦
¦
¦
¦ operations.
¦
¦
¦
¦
¦
¦
¦
2) Wing/Tail White C ¦ 3 ¦ 0 ¦ May be inoperative for night
¦
¦
Strobe Lights
¦
¦
¦ operations provided anti-collision
¦
¦
¦
¦
¦ beacons operate normally.
¦
¦
¦
¦
¦
¦
¦
C ¦ 3 ¦ 0 ¦ May be inoperative for day
¦
¦
¦
¦
¦ operations.
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
-------------------------------------------------------------------------------
------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION
¦
¦
¦
¦
MASTER MINIMUM EQUIPMENT LIST
¦
¦ FEDERAL AVIATION ADMINISTRATION
¦
¦ --------------------------------------------------------------------------- ¦
¦ AIRCRAFT:
¦ REVISION NO: 5
¦ PAGE:
¦
¦
HAWKER SIDDELEY HS-125
¦
¦
¦
¦
(SERIES 1 THROUGH 800XP)
¦ DATE: 05/30/2002
¦ 33-4
¦
¦ --------------------------------------------------------------------------- ¦
¦
1. ¦ 2. NUMBER INSTALLED
¦
¦ SYSTEM &
¦
-------------------------------------------- ¦
¦ SEQUENCE
ITEM
¦
¦ 3. NUMBER REQUIRED FOR DISPATCH
¦
¦ NUMBERS
¦
¦
--------------------------------------- ¦
¦ ------------------------- ¦
¦
¦ 4. REMARKS OR EXCEPTIONS
¦
¦ 33 LIGHTS
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 40-2 Landing Lights
C ¦ 2 ¦ 1 ¦ One may be inoperative for night
¦
¦
¦
¦
¦ operations provided adjacent taxi
¦
¦
¦
¦
¦ light operates normally.
¦
¦
¦
¦
¦
¦
¦
C ¦ 2 ¦ 0 ¦ May be inoperative for day
¦
¦
¦
¦
¦ operations.
¦
¦
¦
¦
¦
¦
¦ 40-3 Taxi Lights (Wing C ¦ 2 ¦ 0 ¦ (O)May be inoperative provided both
¦
¦
Mounted)
¦
¦
¦ landing lights operate normally.
¦
¦
¦
¦
¦
OR
¦
¦
C ¦
¦
¦ May be inoperative for day
¦
¦
¦
¦
¦ operations only.
¦
¦
¦
¦
¦
OR
¦
¦
C ¦
¦
¦ (O)May be inoperative provided nose
¦
¦
¦
¦
¦ taxi lights operate normally.
¦
¦
¦
¦
¦
¦
¦ 40-4 Position
C ¦ - ¦ 3 ¦ For night operations, all except
¦
¦
(Navigation)
¦
¦
¦ the following minimum may be
¦
¦
Lights
¦
¦
¦ inoperative:
¦
¦
¦
¦
¦
a) One stationary red wing tip
¦
¦
¦
¦
¦
light,
¦
¦
¦
¦
¦
b) One stationary green wing
¦
¦
¦
¦
¦
tip light, and
¦
¦
¦
¦
¦
c) One stationary white tail
¦
¦
¦
¦
¦
light.
¦
¦
¦
¦
¦
¦
¦
C ¦ - ¦ 0 ¦ May be inoperative for day
¦
¦
¦
¦
¦ operations.
¦
¦
¦
¦
¦
¦
¦
1) Stationary
C ¦ - ¦ 0 ¦ May be inoperative for night
| ¦
¦
White Tail
¦
¦
¦ operations provied Tail white
| ¦
¦
Light
¦
¦
¦ strobe light operates normally.
| ¦
¦
¦
¦
¦
¦
¦ 40-5 Wing Illumination/ C ¦ - ¦ 0 ¦ May be inoperative for day
| ¦
¦
Ice Light(s)
¦
¦
¦ operations.
| ¦
¦
¦
¦
¦
¦
¦
C ¦ - ¦ 1 ¦
| ¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
-------------------------------------------------------------------------------
------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION
¦
¦
¦
¦
MASTER MINIMUM EQUIPMENT LIST
¦
¦ FEDERAL AVIATION ADMINISTRATION
¦
¦ --------------------------------------------------------------------------- ¦
¦ AIRCRAFT:
¦ REVISION NO: 5
¦ PAGE:
¦
¦
HAWKER SIDDELEY HS-125
¦
¦
¦
¦
(SERIES 1 THROUGH 800XP)
¦ DATE: 05/30/2002
¦ 33-5
¦
¦ --------------------------------------------------------------------------- ¦
¦
1. ¦ 2. NUMBER INSTALLED
¦
¦ SYSTEM &
¦
-------------------------------------------- ¦
¦ SEQUENCE
ITEM
¦
¦ 3. NUMBER REQUIRED FOR DISPATCH
¦
¦ NUMBERS
¦
¦
--------------------------------------- ¦
¦ ------------------------- ¦
¦
¦ 4. REMARKS OR EXCEPTIONS
¦
¦ 33 LIGHTS
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 40-6 Logo Lights
C ¦ - ¦ 0 ¦
¦
¦ ***
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 40-7 Nose Taxi Lights
C ¦ - ¦ 0 ¦
¦
¦ ***
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 40-8 Pulselite System
D ¦ 1 ¦ 0 ¦ (M)May be inoperative.
¦
¦ ***
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 40-9 Wing Tip Taxi
D ¦ 1 ¦ 0 ¦
¦
¦ *** Lighting System
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 40-10 Weight On Wheels C ¦ 1 ¦ 0 ¦ May be inoperative.
¦
¦ ***
Switch
¦
¦
¦
¦
¦
(Automatic Dim
¦
¦
¦
¦
¦
Function On
¦
¦
¦
¦
¦
Landing)
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 50-1 Cabin Emergency
C ¦ 1 ¦ 0 ¦ May be inoperative for all-cargo
¦
¦
Exit Lighting
¦
¦
¦ operations and flight without
| ¦
¦
System
¦
¦
¦ passengers.
| ¦
¦
¦
¦
¦
¦
¦ 50-2 Floor Proximity
C ¦ - ¦ 0 ¦
¦
¦ *** Lighting System
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
-------------------------------------------------------------------------------
------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION
¦
¦
¦
¦
MASTER MINIMUM EQUIPMENT LIST
¦
¦ FEDERAL AVIATION ADMINISTRATION
¦
¦ --------------------------------------------------------------------------- ¦
¦ AIRCRAFT:
¦ REVISION NO: 5
¦ PAGE:
¦
¦
HAWKER SIDDELEY HS-125
¦
¦
¦
¦
(SERIES 1 THROUGH 800XP)
¦ DATE: 05/30/2002
¦ 34-1
¦
¦ --------------------------------------------------------------------------- ¦
¦
1. ¦ 2. NUMBER INSTALLED
¦
¦ SYSTEM &
¦
-------------------------------------------- ¦
¦ SEQUENCE
ITEM
¦
¦ 3. NUMBER REQUIRED FOR DISPATCH
¦
¦ NUMBERS
¦
¦
--------------------------------------- ¦
¦ ------------------------- ¦
¦
¦ 4. REMARKS OR EXCEPTIONS
¦
¦ 34 NAVIGATION
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 9-1 Mach/Indications
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
1) Series 1
C ¦ 2 ¦ 1 ¦ One Mach indicator may be inopera- | ¦
¦
Through 700
¦
¦
¦ tive provided VMO/MMO aural warning | ¦
¦
Only
¦
¦
¦ operates normally.
¦
¦
¦
¦
¦
¦
¦
C ¦ 2 ¦ 0 ¦ (O)May be inoperative provided:
¦
¦
¦
¦
¦
a) Flight remains at or below
¦
¦
¦
¦
¦
FL 295, and
| ¦
¦
¦
¦
¦
b) A placard which sets forth
¦
¦
¦
¦
¦
this limitation is affixed
¦
¦
¦
¦
¦
to the instrument panel.
¦
¦
¦
¦
¦
¦
¦
2) EFIS Equipped
C ¦ 2 ¦ 1 ¦ One may be inoperative provided:
| ¦
¦
Aircraft
¦
¦
¦
a) EFIS Airspeed Tape displays | ¦
¦
¦
¦
¦
are installed at each pilot
¦
¦
¦
¦
¦
station and operate
¦
¦
¦
¦
¦
normally,
¦
¦
¦
¦
¦
b) One Mach/Airspeed warning
¦
¦
¦
¦
¦
system operates normally,
¦
¦
¦
¦
¦
and
¦
¦
¦
¦
¦
c) VMO/MMO aural warning system
¦
¦
¦
¦
¦
operates normally.
¦
¦
¦
¦
¦
¦
¦
C ¦ 2 ¦ 0 ¦ (O)May be inoperative provided:
¦
¦
¦
¦
¦
a) Flight remains at or below
¦
¦
¦
¦
¦
FL 295, and
| ¦
¦
¦
¦
¦
b) A placard which sets forth
¦
¦
¦
¦
¦
this limitation is affixed
¦
¦
¦
¦
¦
to the instrument panel.
¦
¦
¦
¦
¦
¦
¦ 9-2 SAT/TAT Indicating C ¦ - ¦ 0 ¦ (O)May be inoperative provided:
¦
¦ *** System
¦
¦
¦
a) Outside air temperature
¦
¦
¦
¦
¦
(OAT) indicator operates
¦
¦
¦
¦
¦
normally, and
¦
¦
¦
¦
¦
b) Flight management system
¦
¦
¦
¦
¦
(if installed) operates
| ¦
¦
¦
¦
¦
normally.
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
-------------------------------------------------------------------------------
------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION
¦
¦
¦
¦
MASTER MINIMUM EQUIPMENT LIST
¦
¦ FEDERAL AVIATION ADMINISTRATION
¦
¦ --------------------------------------------------------------------------- ¦
¦ AIRCRAFT:
¦ REVISION NO: 5
¦ PAGE:
¦
¦
HAWKER SIDDELEY HS-125
¦
¦
¦
¦
(SERIES 1 THROUGH 800XP)
¦ DATE: 05/30/2002
¦ 34-2
¦
¦ --------------------------------------------------------------------------- ¦
¦
1. ¦ 2. NUMBER INSTALLED
¦
¦ SYSTEM &
¦
-------------------------------------------- ¦
¦ SEQUENCE
ITEM
¦
¦ 3. NUMBER REQUIRED FOR DISPATCH
¦
¦ NUMBERS
¦
¦
--------------------------------------- ¦
¦ ------------------------- ¦
¦
¦ 4. REMARKS OR EXCEPTIONS
¦
¦ 34 NAVIGATION
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 9-3 TAS/Indicating
C ¦ - ¦ 0 ¦
¦
¦ *** System
¦
¦
¦
| ¦
¦
¦
¦
¦
¦
¦ 9-4 RMI/BDI Indicators C ¦ - ¦ 1 ¦ One indicating system may be
¦
¦ ***
¦
¦
¦ inoperative provided one indepen| ¦
¦
¦
¦
¦ dent compass heading indicator is
¦
¦
¦
¦
¦ available at each pilot's station.
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 9-5 Non-Stabilized
B ¦ 1 ¦ 0 ¦ May be inoperative provided any
¦
¦
Magnetic Compass
¦
¦
¦ combination of three gyro or INS
¦
¦
(Standby)
¦
¦
¦ (IRU) stabilized compass systems
¦
¦
¦
¦
¦ operate normally.
¦
¦
¦
¦
¦
¦
¦
B ¦ 1 ¦ 0 ¦ (O)May be inoperative provided:
¦
¦
¦
¦
¦
a) Any combination of two gyro
¦
¦
¦
¦
¦
OR INS (IRU) stabilized
¦
¦
¦
¦
¦
compass systems are
¦
¦
¦
¦
¦
operative, and
¦
¦
¦
¦
¦
b) Airplane is operated with
¦
¦
¦
¦
¦
dual independent navigation
¦
¦
¦
¦
¦
capability, and under
¦
¦
¦
¦
¦
positive radar control by
¦
¦
¦
¦
¦
ATC on the enroute portion
¦
¦
C ¦
¦
¦
of the flight.
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ (O)May be inoperative for flights
¦
¦
¦
¦
¦ that are entirely within areas of
¦
¦
¦
¦
¦ magnetic unreliability provided at
¦
¦
¦
¦
¦ least two stabilized directional
¦
¦
¦
¦
¦ gyro systems operate normally and
¦
¦
¦
¦
¦ are used in conjunction with
¦
¦
¦
¦
¦ approved free gyro navigation
¦
¦
¦
¦
¦ techniques.
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
-------------------------------------------------------------------------------
------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION
¦
¦
¦
¦
MASTER MINIMUM EQUIPMENT LIST
¦
¦ FEDERAL AVIATION ADMINISTRATION
¦
¦ --------------------------------------------------------------------------- ¦
¦ AIRCRAFT:
¦ REVISION NO: 5
¦ PAGE:
¦
¦
HAWKER SIDDELEY HS-125
¦
¦
¦
¦
(SERIES 1 THROUGH 800XP)
¦ DATE: 05/30/2002
¦ 34-3
¦
¦ --------------------------------------------------------------------------- ¦
¦
1. ¦ 2. NUMBER INSTALLED
¦
¦ SYSTEM &
¦
-------------------------------------------- ¦
¦ SEQUENCE
ITEM
¦
¦ 3. NUMBER REQUIRED FOR DISPATCH
¦
¦ NUMBERS
¦
¦
--------------------------------------- ¦
¦ ------------------------- ¦
¦
¦ 4. REMARKS OR EXCEPTIONS
¦
¦ 34 NAVIGATION
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 10-1 Mach/Airspeed
B ¦ 2 ¦ 1 ¦
¦
¦
Aural Warning
¦
¦
¦
¦
¦
Channels
¦
¦
¦
¦
¦
B ¦ 2 ¦ 0 ¦ (O)May be inoperative provided:
¦
¦
¦
¦
¦
a) Both Mach/Airspeed
¦
¦
¦
¦
¦
indicators at both pilot
¦
¦
¦
¦
¦
positions are verified to
¦
¦
¦
¦
¦
operate normally, and
¦
¦
¦
¦
¦
b) VMO/MMO AFM limitations are
¦
¦
¦
¦
¦
observed.
¦
¦
¦
¦
¦
¦
¦ 10-2 Altitude Alerting A ¦ - ¦ 0 ¦ (O)May be inoperative provided:
| ¦
¦
System
¦
¦
¦
a) Autopilot with altitude hold | ¦
¦
¦
¦
¦
is operative,
| ¦
¦
¦
¦
¦
b) Enroute operations do not
| ¦
¦
¦
¦
¦
require its use, and
| ¦
¦
¦
¦
¦
c) Repairs are made within
| ¦
¦
¦
¦
¦
three flight days.
| ¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ NOTE: One system must be
| ¦
¦
¦
¦
¦
operational for operations
| ¦
¦
¦
¦
¦
in RVSM airspace.
| ¦
¦
¦
¦
¦
¦
¦
C ¦ - ¦ 0 ¦ May be inoperative provided system | ¦
¦
¦
¦
¦ is not required by FAR.
| ¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
-------------------------------------------------------------------------------
------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION
¦
¦
¦
¦
MASTER MINIMUM EQUIPMENT LIST
¦
¦ FEDERAL AVIATION ADMINISTRATION
¦
¦ --------------------------------------------------------------------------- ¦
¦ AIRCRAFT:
¦ REVISION NO: 5
¦ PAGE:
¦
¦
HAWKER SIDDELEY HS-125
¦
¦
¦
¦
(SERIES 1 THROUGH 800XP)
¦ DATE: 05/30/2002
¦ 34-4
¦
¦ --------------------------------------------------------------------------- ¦
¦
1. ¦ 2. NUMBER INSTALLED
¦
¦ SYSTEM &
¦
-------------------------------------------- ¦
¦ SEQUENCE
ITEM
¦
¦ 3. NUMBER REQUIRED FOR DISPATCH
¦
¦ NUMBERS
¦
¦
--------------------------------------- ¦
¦ ------------------------- ¦
¦
¦ 4. REMARKS OR EXCEPTIONS
¦
¦ 34 NAVIGATION
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 10-3 Altimeter
¦
¦
¦
¦
¦
Vibrators
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
1) Servo
C ¦ 2 ¦ 1 ¦ One may be inoperative provided
¦
¦
Pneumatic
¦
¦
¦ associated air data computer is
¦
¦
¦
¦
¦ installed and operates normally.
¦
¦
¦
¦
¦
¦
¦
2) Pneumatic
C ¦ 2 ¦ 1 ¦ One may be inoperative provided VMC
¦
¦
¦
¦
¦ exists at departure and arrival
¦
¦
¦
¦
¦ airports.
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
3) One Pneumatic
C ¦ 2 ¦ 1 ¦ Servo Pneumatic may be inoperative
¦
¦
and One Servo
¦
¦
¦ provided:
¦
¦
Pneumatic
¦
¦
¦
a) Associated air data computer
¦
¦
¦
¦
¦
is installed and operates
¦
¦
¦
¦
¦
normally, and
¦
¦
¦
¦
¦
b) VMC exists at departure and
¦
¦
¦
¦
¦
arrival airports.
¦
¦
¦
¦
¦
¦
¦
4) Standby
C ¦ 1 ¦ 0 ¦ May be inoperative provided VMC
¦
¦
Altimeter
¦
¦
¦ exist at both departure and arrival | ¦
¦
Vibrator (With
¦
¦
¦ airports.
¦
¦
Electric
¦
¦
¦
¦
¦
Altimeters
¦
¦
¦
¦
¦
Installed)
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 10-4 Standby Altimeter B ¦ - ¦ 0 ¦ May be inoperative for day VMC
¦
¦
¦
¦
¦ flight only.
¦
¦
¦
¦
¦
¦
¦ 10-5 Altimeter Static
C ¦ - ¦ 0 ¦ (O)May be inoperative provided:
¦
¦
Error Correction
¦
¦
¦
a) Altimeter is switched to
¦
¦
Module
¦
¦
¦
STANDBY (BAROMETRIC), and
¦
¦
¦
¦
¦
b) AFM altitude correction
¦
¦
¦
¦
¦
information is used.
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
-------------------------------------------------------------------------------
------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION
¦
¦
¦
¦
MASTER MINIMUM EQUIPMENT LIST
¦
¦ FEDERAL AVIATION ADMINISTRATION
¦
¦ --------------------------------------------------------------------------- ¦
¦ AIRCRAFT:
¦ REVISION NO: 5
¦ PAGE:
¦
¦
HAWKER SIDDELEY HS-125
¦
¦
¦
¦
(SERIES 1 THROUGH 800XP)
¦ DATE: 05/30/2002
¦ 34-5
¦
¦ --------------------------------------------------------------------------- ¦
¦
1. ¦ 2. NUMBER INSTALLED
¦
¦ SYSTEM &
¦
-------------------------------------------- ¦
¦ SEQUENCE
ITEM
¦
¦ 3. NUMBER REQUIRED FOR DISPATCH
¦
¦ NUMBERS
¦
¦
--------------------------------------- ¦
¦ ------------------------- ¦
¦
¦ 4. REMARKS OR EXCEPTIONS
¦
¦ 34 NAVIGATION
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 10-6 Outside Air
C ¦ - ¦ 0 ¦ (O)May be inoperative provided
¦
¦
Temperature (OAT)
¦
¦
¦ alternate temperature indicating
¦
¦
Indicator
¦
¦
¦ system (TAT OR SAT) is available
¦
¦
¦
¦
¦ and used.
¦
¦
¦
¦
¦
¦
¦ 10-8 Air Data Computer C ¦ 2 ¦ 0 ¦ (O)May be inoperative provided:
¦
¦
Changeover/
¦
¦
¦
a) Associated instruments
¦
¦
Reversion
¦
¦
¦
operate normally from
| ¦
¦
Switches
¦
¦
¦
independent sources, and
| ¦
¦
¦
¦
¦
b) Inoperative switches are not
¦
¦
¦
¦
¦
moved during flight.
¦
¦
¦
¦
¦
¦
¦ 10-9 Vertical Speed
B ¦ 2 ¦ 1 ¦ One may be inoperative for day VMC
¦
¦
Indicator
¦
¦
¦ flight only.
¦
¦
¦
¦
¦
¦
¦ 20. Altimeter Vibrators
¦
¦
¦ Incorporated into item 10-3, Rev.
¦
¦
¦
¦
¦ #3.
¦
¦
¦
¦
¦
¦
¦ 20-1 Flight Director
C ¦ - ¦ 0 ¦ May be inoperative provided
¦
¦
System
¦
¦
¦ approach minimums do not require
¦
¦
¦
¦
¦ its use.
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ NOTE: One system must be
| ¦
¦
¦
¦
¦
operational to operate in
| ¦
¦
¦
¦
¦
RVSM airspace.
| ¦
¦
¦
¦
¦
¦
¦ 20-2 Turn and Bank
¦
¦
¦
¦
¦
Indication
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
1) Rate of Turn
C ¦ - ¦ 1 ¦ Turn function of one instrument may
¦
¦
Indication
¦
¦
¦ be inoperative provided flight is
| ¦
¦
¦
¦
¦ conducted in VMC conditions only.
| ¦
¦
¦
¦
¦
¦
¦
C ¦ - ¦ 0 ¦ May be inoperative provided
| ¦
¦
¦
¦
¦ standby attitude indicator operates | ¦
¦
¦
¦
¦ normally.
| ¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
-------------------------------------------------------------------------------
------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION
¦
¦
¦
¦
MASTER MINIMUM EQUIPMENT LIST
¦
¦ FEDERAL AVIATION ADMINISTRATION
¦
¦ --------------------------------------------------------------------------- ¦
¦ AIRCRAFT:
¦ REVISION NO: 5
¦ PAGE:
¦
¦
HAWKER SIDDELEY HS-125
¦
¦
¦
¦
(SERIES 1 THROUGH 800XP)
¦ DATE: 05/30/2002
¦ 34-6
¦
¦ --------------------------------------------------------------------------- ¦
¦
1. ¦ 2. NUMBER INSTALLED
¦
¦ SYSTEM &
¦
-------------------------------------------- ¦
¦ SEQUENCE
ITEM
¦
¦ 3. NUMBER REQUIRED FOR DISPATCH
¦
¦ NUMBERS
¦
¦
--------------------------------------- ¦
¦ ------------------------- ¦
¦
¦ 4. REMARKS OR EXCEPTIONS
¦
¦ 34 NAVIGATION
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 20-3 Attitude Heading
¦
¦
¦
¦
¦
Reference System
¦
¦
¦
¦
¦
(AHRS)/Inertial
¦
¦
¦
¦
¦
Reference System
¦
¦
¦
¦
¦
(IRS)
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
1) Primary AHRS/
C ¦ 2 ¦ 1 ¦ (O)One may be inoperative provided:
¦
¦
IRS
¦
¦
¦
a) Standby attitude reference
¦
¦
¦
¦
¦
system is selected and veri¦
¦
¦
¦
¦
fied to operate normally,
¦
¦
¦
¦
¦
b) AFM limitations are
¦
¦
¦
¦
¦
observed, and
¦
¦
¦
¦
¦
c) Autopilot is not used.
¦
¦
¦
¦
¦
¦
¦
2) Standby AHRS/
C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided both
¦
¦
IRS
¦
¦
¦ primary AHRS/IRS systems are veri¦
¦
¦
¦
¦ fied to operate normally.
¦
¦
¦
¦
¦
¦
¦ 20-4 Compass and
C ¦ 2 ¦ 0 ¦ (O)May be inoperative provided:
¦
¦
Attitude/AHRS
¦
¦
¦
a) Associated instruments
¦
¦
Changeover/
¦
¦
¦
operate normally from
¦
¦
Reversion
¦
¦
¦
independent sources, and
| ¦
¦
Switches
¦
¦
¦
b) Inoperative switches are not | ¦
¦
¦
¦
¦
moved during flight.
¦
¦
¦
¦
¦
¦
¦ 20-5 Angle of Attack
C ¦ - ¦ 0 ¦
¦
¦ *** System
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 20-6 Standby Attitude
B ¦ - ¦ 0 ¦ May be inoperative for day VMC
¦
¦
Indicator
¦
¦
¦ operations only.
¦
¦
¦
¦
¦
¦
¦ 20-7 Symbol Generator
C ¦ 2 ¦ 0 ¦ (O)May be inoperative provided:
¦
¦
Reversion Switches
¦
¦
¦
a) Associated instruments
¦
¦
¦
¦
¦
operate normally from
¦
¦
¦
¦
¦
independent sources, and
¦
¦
¦
¦
¦
b) Inoperative switches are not
¦
¦
¦
¦
¦
moved during flight.
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
-------------------------------------------------------------------------------
------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION
¦
¦
¦
¦
MASTER MINIMUM EQUIPMENT LIST
¦
¦ FEDERAL AVIATION ADMINISTRATION
¦
¦ --------------------------------------------------------------------------- ¦
¦ AIRCRAFT:
¦ REVISION NO: 4
¦ PAGE:
¦
¦
HAWKER SIDDELEY HS-125
¦
¦
¦
¦
(SERIES 1 THROUGH 800XP)
¦ DATE: 03/10/1998
¦ 34-7
¦
¦ --------------------------------------------------------------------------- ¦
¦
1. ¦ 2. NUMBER INSTALLED
¦
¦ SYSTEM &
¦
-------------------------------------------- ¦
¦ SEQUENCE
ITEM
¦
¦ 3. NUMBER REQUIRED FOR DISPATCH
¦
¦ NUMBERS
¦
¦
--------------------------------------- ¦
¦ ------------------------- ¦
¦
¦ 4. REMARKS OR EXCEPTIONS
¦
¦ 34 NAVIGATION
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 20-8 Instrument
C ¦ - ¦ 0 ¦ (O)May be inoperative provided
¦
¦
Comparator
¦
¦
¦ approach minimums do not require
¦
¦
¦
¦
¦ their use.
¦
¦
¦
¦
¦
¦
¦ 30-2 Marker Beacons
C ¦ - ¦ 0 ¦ May be inoperative provided
¦
¦
¦
¦
¦ approach minimums do not require
¦
¦
¦
¦
¦ their use.
¦
¦
¦
¦
¦
¦
¦ 30-3 Microwave Landing C ¦ - ¦ 0 ¦ As required by FAR.
¦
¦ *** System
¦
¦
¦
¦
¦
¦
¦
¦ NOTE: Equipment not operationally
¦
¦
¦
¦
¦
approved for steep
¦
¦
¦
¦
¦
approaches in U.S.
¦
¦
¦
¦
¦
¦
¦ 30-4 Radio Compass
C ¦ - ¦ - ¦ As required by FAR.
¦
¦
(ADF) System
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 30-5 NAV/COM Preselect C ¦ - ¦ 0 ¦ May be inoperative provided direct
¦
¦
Tuning Functions
¦
¦
¦ tuning mode is installed and
¦
¦
¦
¦
¦ operates normally for each
¦
¦
¦
¦
¦ associated unit.
¦
¦
¦
¦
¦
¦
¦ 30-6 NAV/COM/ADF/TDR
C ¦ - ¦ 0 ¦ May be inoperative provided manual
¦
¦
Memory Channels
¦
¦
¦ tuning operates normally.
¦
¦
¦
¦
¦
¦
¦ 30-7 NAV/COM/ADF/TDR
C ¦ - ¦ 1 ¦ One pilot side only may be
¦
¦
Digital Frequency
¦
¦
¦ inoperative provided:
¦
¦
Selector/LCD/LED
¦
¦
¦
a) Manual remote tune or dual
¦
¦
¦
¦
¦
FMS/CDU tune capability
¦
¦
¦
¦
¦
operates normally, and
¦
¦
¦
¦
¦
b) All Digital Frequency
¦
¦
¦
¦
¦
Selector/LCD/LED display
¦
¦
¦
¦
¦
units on opposite pilot side
¦
¦
¦
¦
¦
operate normally.
¦
¦
¦
¦
¦
¦
¦ 24. Air Data Computer
¦
¦
¦ Deleted, REV. 2.
¦
¦
System
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
-------------------------------------------------------------------------------
------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION
¦
¦
¦
¦
MASTER MINIMUM EQUIPMENT LIST
¦
¦ FEDERAL AVIATION ADMINISTRATION
¦
¦ --------------------------------------------------------------------------- ¦
¦ AIRCRAFT:
¦ REVISION NO: 4
¦ PAGE:
¦
¦
HAWKER SIDDELEY HS-125
¦
¦
¦
¦
(SERIES 1 THROUGH 800XP)
¦ DATE: 03/10/1998
¦ 34-8
¦
¦ --------------------------------------------------------------------------- ¦
¦
1. ¦ 2. NUMBER INSTALLED
¦
¦ SYSTEM &
¦
-------------------------------------------- ¦
¦ SEQUENCE
ITEM
¦
¦ 3. NUMBER REQUIRED FOR DISPATCH
¦
¦ NUMBERS
¦
¦
--------------------------------------- ¦
¦ ------------------------- ¦
¦
¦ 4. REMARKS OR EXCEPTIONS
¦
¦ 34 NAVIGATION
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 32-1 ILS Offset System C ¦ 1 ¦ 0 ¦ May be inoperative provided pro¦
¦
(FAA Flight
¦
¦
¦ cedures are not dependent upon its
¦
¦
Inspection
¦
¦
¦ use.
¦
¦
Aircraft Only)
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 40-1 Radio Altimeter
A ¦ - ¦ 0 ¦ May be inoperative provided:
¦
¦
System
¦
¦
¦
a) Dispatch deviation for
¦
¦
¦
¦
¦
ground proximity warning
¦
¦
¦
¦
¦
system (if inoperative) is
¦
¦
¦
¦
¦
observed,
¦
¦
¦
¦
¦
b) Approach minimums or opera¦
¦
¦
¦
¦
ting procedures do not
¦
¦
¦
¦
¦
require its use, and
¦
¦
¦
¦
¦
c) Repairs are made within
¦
¦
¦
¦
¦
three flight days.
¦
¦
¦
¦
¦
¦
¦ 40-2 Weather Radar
C ¦ - ¦ - ¦ As required by FAR.
¦
¦
System
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 40-3 VTA (Voice
C ¦ - ¦ 0 ¦ (M)May be inoperative provided
¦
¦ *** Terrain Advisory)
¦
¦
¦ system is deactivated.
¦
¦
System or
¦
¦
¦
¦
¦
Equivalent
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
-------------------------------------------------------------------------------
------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION
¦
¦
¦
¦
MASTER MINIMUM EQUIPMENT LIST
¦
¦ FEDERAL AVIATION ADMINISTRATION
¦
¦ --------------------------------------------------------------------------- ¦
¦ AIRCRAFT:
¦ REVISION NO: 5
¦ PAGE:
¦
¦
HAWKER SIDDELEY HS-125
¦
¦
¦
¦
(SERIES 1 THROUGH 800XP)
¦ DATE: 05/30/2002
¦ 34-9
¦
¦ --------------------------------------------------------------------------- ¦
¦
1. ¦ 2. NUMBER INSTALLED
¦
¦ SYSTEM &
¦
-------------------------------------------- ¦
¦ SEQUENCE
ITEM
¦
¦ 3. NUMBER REQUIRED FOR DISPATCH
¦
¦ NUMBERS
¦
¦
--------------------------------------- ¦
¦ ------------------------- ¦
¦
¦ 4. REMARKS OR EXCEPTIONS
¦
¦ 34 NAVIGATION
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 40-4 Ground Proximity
A ¦ - ¦ 0 ¦ (O)May be inoperative provided:
| ¦
¦
Warning System
¦
¦
¦
a) Alternate procedures are
| ¦
¦
(GPWS)/Terrain
¦
¦
¦
established and used, and
| ¦
¦
Awareness Warning
¦
¦
¦
b) Repairs are made within
| ¦
¦
System (TAWS)
¦
¦
¦
two flight days.
| ¦
¦
¦
¦
¦
¦
¦
C ¦ - ¦ 0 ¦ (O)May be inoperative provided:
| ¦
¦
¦
¦
¦
a) System(s) not required by
| ¦
¦
¦
¦
¦
FAR, and
| ¦
¦
¦
¦
¦
b) Alternate procedures are
| ¦
¦
¦
¦
¦
established and used.
| ¦
¦
¦
¦
¦
¦
¦
1) Modes 1-4
A ¦ - ¦ 0 ¦ (O)May be inoperative provided:
¦
¦
¦
¦
¦
a) Alternate procedures are
¦
¦
¦
¦
¦
established used, and
¦
¦
¦
¦
¦
b) Repairs are made within two
¦
¦
¦
¦
¦
flight days.
¦
¦
¦
¦
¦
¦
¦
2) Test Mode
A ¦ 1 ¦ 0 ¦ (O)May be inoperative provided:
¦
¦
¦
¦
¦
a) GPWS is considered
¦
¦
¦
¦
¦
inoperative, and
¦
¦
¦
¦
¦
b) Repairs are made within two
¦
¦
¦
¦
¦
flight days.
¦
¦
¦
¦
¦
¦
¦
3) Glideslope
B ¦ 2 ¦ 0 ¦
¦
¦
Deviation
¦
¦
¦
¦
¦
(Mode 5)
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ *** 4) Advisory Call
C ¦ - ¦ 0 ¦ (O)May be inoperative provided
¦
¦
outs
¦
¦
¦ alternate procedures are
¦
¦
¦
¦
¦ established and used.
¦
¦
¦
¦
¦
¦
¦ *** 5) Windshear Mode C ¦ - ¦ 0 ¦ (O)May be inoperative provided
¦
¦
¦
¦
¦ alternate procedures are
¦
¦
¦
¦
¦ established and used.
¦
¦
¦
¦
¦
¦
¦ *** 6) Enhanced GPWS
C ¦ - ¦ 0 ¦
¦
¦
(EGPWS)
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
-------------------------------------------------------------------------------
------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION
¦
¦
¦
¦
MASTER MINIMUM EQUIPMENT LIST
¦
¦ FEDERAL AVIATION ADMINISTRATION
¦
¦ --------------------------------------------------------------------------- ¦
¦ AIRCRAFT:
¦ REVISION NO: 5
¦ PAGE:
¦
¦
HAWKER SIDDELEY HS-125
¦
¦
¦
¦
(SERIES 1 THROUGH 800XP)
¦ DATE: 05/30/2002
¦ 34-10
¦
¦ --------------------------------------------------------------------------- ¦
¦
1. ¦ 2. NUMBER INSTALLED
¦
¦ SYSTEM &
¦
-------------------------------------------- ¦
¦ SEQUENCE
ITEM
¦
¦ 3. NUMBER REQUIRED FOR DISPATCH
¦
¦ NUMBERS
¦
¦
--------------------------------------- ¦
¦ ------------------------- ¦
¦
¦ 4. REMARKS OR EXCEPTIONS
¦
¦ 34 NAVIGATION
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 40-5 Lightning Sensor
C ¦ - ¦ 0 ¦
¦
¦ *** System
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 40-6 Radarnav/Datanav
C ¦ - ¦ 0 ¦
¦
¦ *** System
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 40-7 Storm Scope
D ¦ - ¦ 0 ¦
¦
¦ ***
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 42-1 TACAN Number 2
C ¦ 1 ¦ 0 ¦ May be inoperative provided pro¦
¦
Tuning System (FAA
¦
¦
¦ cedures are not dependent upon its
¦
¦
Flight Inspection
¦
¦
¦ use.
¦
¦
Aircraft Only)
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 43-1 ATC Transponder
C ¦ 1 ¦ 0 ¦ May be inoperative provided pro¦
¦
Attenuation System
¦
¦
¦ cedures are not dependent upon its
¦
¦
(FAA Flight
¦
¦
¦ use.
¦
¦
Inspection
¦
¦
¦
¦
¦
Aircraft Only)
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 50-1 LNAV or RNAV
C ¦ - ¦ - ¦ As required by FAR.
¦
¦
Systems
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 50-2 Flight Management C ¦ - ¦ - ¦
| ¦
¦ *** Systems (FMS)
¦
¦
¦
| ¦
¦
¦
¦
¦
| ¦
¦
1) NAV Data
C ¦ - ¦ 0 ¦ (O)May be out of currency provided: | ¦
¦
Base
¦
¦
¦
a) Current Aeronautical Charts | ¦
¦
¦
¦
¦
are use to verify
| ¦
¦
¦
¦
¦
Navigation Fixes before
| ¦
¦
¦
¦
¦
dispatch,
| ¦
¦
¦
¦
¦
b) Procedures are established
| ¦
¦
¦
¦
¦
and used to verify status
| ¦
¦
¦
¦
¦
and suitability of Naviga| ¦
¦
¦
¦
¦
tion Facilities used to
| ¦
¦
¦
¦
¦
define route of flight, and | ¦
¦
¦
¦
¦
c) Approach Navigation Radios
| ¦
¦
¦
¦
¦
are manually tuned and
| ¦
¦
¦
¦
¦
identified.
| ¦
¦
¦
¦
¦
¦
¦
C ¦ 2 ¦ 1 ¦ As required by FAR.
| ¦
-------------------------------------------------------------------------------
------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION
¦
¦
¦
¦
MASTER MINIMUM EQUIPMENT LIST
¦
¦ FEDERAL AVIATION ADMINISTRATION
¦
¦ --------------------------------------------------------------------------- ¦
¦ AIRCRAFT:
¦ REVISION NO: 5
¦ PAGE:
¦
¦
HAWKER SIDDELEY HS-125
¦
¦
¦
¦
(SERIES 1 THROUGH 800XP)
¦ DATE: 05/30/2002
¦ 34-11
¦
¦ --------------------------------------------------------------------------- ¦
¦
1. ¦ 2. NUMBER INSTALLED
¦
¦ SYSTEM &
¦
-------------------------------------------- ¦
¦ SEQUENCE
ITEM
¦
¦ 3. NUMBER REQUIRED FOR DISPATCH
¦
¦ NUMBERS
¦
¦
--------------------------------------- ¦
¦ ------------------------- ¦
¦
¦ 4. REMARKS OR EXCEPTIONS
¦
¦ 34 NAVIGATION
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 50-3 Distance Measuring D ¦ - ¦ - ¦ Any in excess of those required by | ¦
¦
Equipment (DME)
¦
¦
¦ FAR may be inoperative.
| ¦
¦
Systems
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 50-4 ATC Transponders
C ¦ - ¦ 0 ¦ May be inoperative provided:
| ¦
¦
and Automatic
¦
¦
¦
a) Enroute operations do not
| ¦
¦
Altitude Reporting
¦
¦
¦
require their use, and
| ¦
¦
Systems
¦
¦
¦
b) Before flight, approval is
| ¦
¦
¦
¦
¦
obtained from ATC facilities | ¦
¦
¦
¦
¦
having jurisdiction over the | ¦
¦
¦
¦
¦
planned route of flight.
| ¦
¦
¦
¦
¦
¦
¦
D ¦ - ¦ 1 ¦ Any in excess of those required by | ¦
¦
¦
¦
¦ FAR may be inoperative.
¦
¦
¦
¦
¦
¦
¦ 50-5 VHF Navigation
C ¦ - ¦ - ¦ As required by FAR.
¦
¦
(VOR/ILS) System
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 50-6 Global Positioning C ¦ - ¦ 0 ¦ As required by FAR.
¦
¦ *** System (GPS)
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 50-7 Traffic Advisory
D ¦ 1 ¦ 0 ¦
¦
¦ *** System
¦
¦
¦
¦
¦
(B.F. Goodrich
¦
¦
¦
¦
¦
Skywatch/SKY-497)
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 50-8 Transponder Ident C ¦ - ¦ 2 ¦ May be inoperative provided one is | ¦
¦
Switch
¦
¦
¦ operational on each side.
| ¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
-------------------------------------------------------------------------------
------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION
¦
¦
¦
¦
MASTER MINIMUM EQUIPMENT LIST
¦
¦ FEDERAL AVIATION ADMINISTRATION
¦
¦ --------------------------------------------------------------------------- ¦
¦ AIRCRAFT:
¦ REVISION NO: 5
¦ PAGE:
¦
¦
HAWKER SIDDELEY HS-125
¦
¦
¦
¦
(SERIES 1 THROUGH 800XP)
¦ DATE: 05/30/2002
¦ 34-12
¦
¦ --------------------------------------------------------------------------- ¦
¦
1. ¦ 2. NUMBER INSTALLED
¦
¦ SYSTEM &
¦
-------------------------------------------- ¦
¦ SEQUENCE
ITEM
¦
¦ 3. NUMBER REQUIRED FOR DISPATCH
¦
¦ NUMBERS
¦
¦
--------------------------------------- ¦
¦ ------------------------- ¦
¦
¦ 4. REMARKS OR EXCEPTIONS
¦
¦ 34 NAVIGATION
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 60-1 Traffic Collision B ¦ - ¦ 0 ¦ (M)(O)May be inoperative provided: | ¦
¦
and Avoidance
¦
¦
¦
a) System is deactivated and
| ¦
¦
System (TCAS I and
¦
¦
¦
secured, and
| ¦
¦
TCAS II)
¦
¦
¦
b) Enroute or approach
| ¦
¦
¦
¦
¦
procedures do not require
| ¦
¦
¦
¦
¦
its use.
| ¦
¦
¦
¦
¦
¦
¦
C ¦ - ¦ 0 ¦ (M)(O)May be inoperative provided: | ¦
¦
¦
¦
¦
a) System not required by FAR, | ¦
¦
¦
¦
¦
b) System is deactivated and
| ¦
¦
¦
¦
¦
secured, and
| ¦
¦
¦
¦
¦
c) Enroute or approach proced- | ¦
¦
¦
¦
¦
ures do not require its use. | ¦
¦
¦
¦
¦
¦
¦
1) Combined
C ¦ 2 ¦ 1 ¦ (O)One may be inoperative on the
¦
¦
Traffic Alert
¦
¦
¦ non-flying pilot side provided TA
¦
¦
(TA) and
¦
¦
¦ and RA elements and audio functions
¦
¦
Resolution
¦
¦
¦ are operative on the flying pilot
¦
¦
Advisory (RA)
¦
¦
¦ side.
¦
¦
Dual Display
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
2) Resolution
C ¦ 2 ¦ 1 ¦ (O)One may be inoperative on the
¦
¦
Advisory (RA)
¦
¦
¦ non-flying pilot side.
¦
¦
Display
¦
¦
¦
¦
¦
System(s)
C ¦ - ¦ 0 ¦ (O)May be inoperative provided:
¦
¦
¦
¦
¦
a) All Traffic Alert (TA)
¦
¦
¦
¦
¦
display elements and voice
¦
¦
¦
¦
¦
command audio functions are
¦
¦
¦
¦
¦
operative, and
¦
¦
¦
¦
¦
b) TA only mode is selected by
¦
¦
¦
¦
¦
the crew.
¦
¦
¦
¦
¦
¦
¦
3) Traffic Alert
C ¦ - ¦ 0 ¦ (O)May be inoperative provided all
¦
¦
(TA) Display
¦
¦
¦ installed RA display and audio
¦
¦
System(s)
¦
¦
¦ functions are operative.
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
-------------------------------------------------------------------------------
------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION
¦
¦
¦
¦
MASTER MINIMUM EQUIPMENT LIST
¦
¦ FEDERAL AVIATION ADMINISTRATION
¦
¦ --------------------------------------------------------------------------- ¦
¦ AIRCRAFT:
¦ REVISION NO: 5
¦ PAGE:
¦
¦
HAWKER SIDDELEY HS-125
¦
¦
¦
¦
(SERIES 1 THROUGH 800XP)
¦ DATE: 05/30/2002
¦ 34-13
¦
¦ --------------------------------------------------------------------------- ¦
¦
1. ¦ 2. NUMBER INSTALLED
¦
¦ SYSTEM &
¦
-------------------------------------------- ¦
¦ SEQUENCE
ITEM
¦
¦ 3. NUMBER REQUIRED FOR DISPATCH
¦
¦ NUMBERS
¦
¦
--------------------------------------- ¦
¦ ------------------------- ¦
¦
¦ 4. REMARKS OR EXCEPTIONS
¦
¦ 34 NAVIGATION
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 60-2 Windshear Detector C ¦ - ¦ 0 ¦
¦
¦ *** System
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 70-1 EFIS/MFD Cooling
A ¦ 5 ¦ 4 ¦ (O)One may be inoperative provided: | ¦
¦
Fans
¦
¦
¦
a) Standby attitude indicator
¦
¦
¦
¦
¦
operates normally,
¦
¦
¦
¦
¦
b) DBI and standby compass
¦
¦
¦
¦
¦
operate normally,
¦
¦
¦
¦
¦
c) Cabin temperature can be
¦
¦
¦
¦
¦
maintained below 35 degrees
¦
¦
¦
¦
¦
C, and
¦
¦
¦
¦
¦
d) Repairs are made within
¦
¦
¦
¦
¦
three flight days.
¦
¦
¦
¦
¦
¦
¦
A ¦ 3 ¦ 2 ¦ (O)One may be inoperative provided:
¦
¦
¦
¦
¦
a) Standby attitude indicator
| ¦
¦
¦
¦
¦
operates normally,
| ¦
¦
¦
¦
¦
b) DBI and standby compass
| ¦
¦
¦
¦
¦
operate normally,
| ¦
¦
¦
¦
¦
c) Cabin temperature can be
| ¦
¦
¦
¦
¦
maintained below 35 degrees | ¦
¦
¦
¦
¦
C, and
| ¦
¦
¦
¦
¦
d) Repairs are made within
| ¦
¦
¦
¦
¦
three flight days.
| ¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
-------------------------------------------------------------------------------
------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION
¦
¦
¦
¦
MASTER MINIMUM EQUIPMENT LIST
¦
¦ FEDERAL AVIATION ADMINISTRATION
¦
¦ --------------------------------------------------------------------------- ¦
¦ AIRCRAFT:
¦ REVISION NO: 5
¦ PAGE:
¦
¦
HAWKER SIDDELEY HS-125
¦
¦
¦
¦
(SERIES 1 THROUGH 800XP)
¦ DATE: 05/30/2002
¦ 34-14
¦
¦ --------------------------------------------------------------------------- ¦
¦
1. ¦ 2. NUMBER INSTALLED
¦
¦ SYSTEM &
¦
-------------------------------------------- ¦
¦ SEQUENCE
ITEM
¦
¦ 3. NUMBER REQUIRED FOR DISPATCH
¦
¦ NUMBERS
¦
¦
--------------------------------------- ¦
¦ ------------------------- ¦
¦
¦ 4. REMARKS OR EXCEPTIONS
¦
¦ 34 NAVIGATION
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 70-2 EFIS/MFD OVHT
C ¦ - ¦ 0 ¦ (M)May be inoperative provided:
¦
¦
Warning
¦
¦
¦
a) All EFIS cooling fans are
¦
¦
Annunciators
¦
¦
¦
verified to operate normally
¦
¦
(Except Proline 21
¦
¦
¦
before each departure, and
| ¦
¦
Equipped Aircraft)
¦
¦
¦
b) Associated EFIS fan fail
| ¦
¦
¦
¦
¦
warnings operate normally.
| ¦
¦
¦
¦
¦
¦
¦ 70-3 EFIS/MFD "FAN
C ¦ - ¦ 0 ¦ (O)May be inoperative provided all | ¦
¦
FAIL"
¦
¦
¦ EFIS/MFD cooling fans are verified
¦
¦
Annunciators
¦
¦
¦ to operate normally before each
¦
¦
¦
¦
¦ departure.
¦
¦
¦
¦
¦
¦
¦ 70-4 Electronic Flight C ¦ 4 ¦ 3 ¦ (O)One unit may be inoperative
¦
¦
Display (EFD)
¦
¦
¦ provided an independent PFD/EADI is
¦
¦
¦
¦
¦ available at each pilot's station.
¦
¦
¦
¦
¦
¦
¦
1) EFD Collins
C ¦ 4 ¦ 3 ¦ One unit may be inoperative
| ¦
¦
Proline 21
¦
¦
¦ provided inoperative unit is
| ¦
¦
Equipped
¦
¦
¦ positioned in Copilot MFD
| ¦
¦
Aircraft
¦
¦
¦ location.
| ¦
¦
¦
¦
¦
¦
¦ 70-5 EFIS Symbol
C ¦ - ¦ 2 ¦ (O)One may be inoperative provided
¦
¦
Generator Units
¦
¦
¦ each pilot's EFIS is driven by an
¦
¦
(SGU, DPU, and/or
¦
¦
¦ independent symbol generator unit
¦
¦
MPU)
¦
¦
¦ (SGU, DPU, or MPU) which operates
¦
¦
¦
¦
¦ normally.
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
-------------------------------------------------------------------------------
------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION
¦
¦
¦
¦
MASTER MINIMUM EQUIPMENT LIST
¦
¦ FEDERAL AVIATION ADMINISTRATION
¦
¦ --------------------------------------------------------------------------- ¦
¦ AIRCRAFT:
¦ REVISION NO: 5
¦ PAGE:
¦
¦
HAWKER SIDDELEY HS-125
¦
¦
¦
¦
(SERIES 1 THROUGH 800XP)
¦ DATE: 05/30/2002
¦ 34-15
¦
¦ --------------------------------------------------------------------------- ¦
¦
1. ¦ 2. NUMBER INSTALLED
¦
¦ SYSTEM &
¦
-------------------------------------------- ¦
¦ SEQUENCE
ITEM
¦
¦ 3. NUMBER REQUIRED FOR DISPATCH
¦
¦ NUMBERS
¦
¦
--------------------------------------- ¦
¦ ------------------------- ¦
¦
¦ 4. REMARKS OR EXCEPTIONS
¦
¦ 34 NAVIGATION
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 70-6 Multifunction
C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided:
¦
¦
Display (MFD)
¦
¦
¦
a) Procedures do not require
¦
¦
¦
¦
¦
its use, and
¦
¦
¦
¦
¦
b) When radar is required, at
¦
¦
¦
¦
¦
least one radar display
¦
¦
¦
¦
¦
operates normally.
¦
¦
¦
¦
¦
¦
¦ 70-7 EADI Annunciator/
¦
¦
¦
¦
¦ *** Displays
¦
¦
¦
| ¦
¦
¦
¦
¦
¦
¦
1) FAST/SLOW
C ¦ 2 ¦ 0 ¦
¦
¦
Indications
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 70-8 Laser Altimeter
¦
¦
¦ Deleted Rev. 4.
¦
¦
(FAA Flight
¦
¦
¦
¦
¦
Inspection
¦
¦
¦
¦
¦
Aircraft Only)
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 70-9 Multifunction
C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided:
¦
¦
Display Controller
¦
¦
¦
a) Procedures do not require
¦
¦
(Honeywell
¦
¦
¦
its use,
¦
¦
Aircraft Only)
¦
¦
¦
b) When radar is required, at
¦
¦
¦
¦
¦
least one radar display
¦
¦
¦
¦
¦
operates normally, and
¦
¦
¦
¦
¦
c) Both Symbol Generators (SG)
¦
¦
¦
¦
¦
and their reversionary
¦
¦
¦
¦
¦
switching are verified to
¦
¦
¦
¦
¦
operate normally.
¦
¦
¦
¦
¦
¦
¦ 70-10 Avionics Cooling C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided:
| ¦
¦ ***
Fan and/or Fan
¦
¦
¦
a) Door is in the closed
| ¦
¦
Door
¦
¦
¦
position, and
| ¦
¦
¦
¦
¦
b) AFM abnormal procedures are | ¦
¦
¦
¦
¦
followed.
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 70-11 Electronic
D ¦ - ¦ 0 ¦ (O)May be inoperative provided
| ¦
¦ ***
Checklist System
¦
¦
¦ alternate procedures are
| ¦
¦
¦
¦
¦ established and used.
| ¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
-------------------------------------------------------------------------------
------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION
¦
¦
¦
¦
MASTER MINIMUM EQUIPMENT LIST
¦
¦ FEDERAL AVIATION ADMINISTRATION
¦
¦ --------------------------------------------------------------------------- ¦
¦ AIRCRAFT:
¦ REVISION NO: 5
¦ PAGE:
¦
¦
HAWKER SIDDELEY HS-125
¦
¦
¦
¦
(SERIES 1 THROUGH 800XP)
¦ DATE: 05/30/2002
¦ 34-16
¦
¦ --------------------------------------------------------------------------- ¦
¦
1. ¦ 2. NUMBER INSTALLED
¦
¦ SYSTEM &
¦
-------------------------------------------- ¦
¦ SEQUENCE
ITEM
¦
¦ 3. NUMBER REQUIRED FOR DISPATCH
¦
¦ NUMBERS
¦
¦
--------------------------------------- ¦
¦ ------------------------- ¦
¦
¦ 4. REMARKS OR EXCEPTIONS
¦
¦ 34 NAVIGATION
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 70-12 Nose Compartment
¦
¦
¦
| ¦
¦ *** Ventilation System
¦
¦
¦
| ¦
¦
(Collins Equipped
¦
¦
¦
| ¦
¦
Aircraft Except
¦
¦
¦
| ¦
¦
Pro-Line 21)
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
1) Avionics
C ¦ 1 ¦ 0 ¦ (O)May be inoperative OFF provided
¦
¦
Cooling Fan Low
¦
¦
¦ Avionics Nose Cooling Fan is
¦
¦
Speed Warning
¦
¦
¦ verified to operate normally.
¦
¦
Detector
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
2) Avionics
C ¦ 1 ¦ 0 ¦ (O)May be inoperative OFF provided
¦
¦
Cooling Fan
¦
¦
¦ Avionics Nose Cooling Fan is
¦
¦
Nose Fail
¦
¦
¦ verified to operate normally.
¦
¦
Annunciator
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 80-1 Airborne Flight
D ¦ - ¦ 0 ¦ (O)May be inoperative provided
¦
¦ *** Information System
¦
¦
¦ alternate procedures are
¦
¦
(AFIS)
¦
¦
¦ established and used.
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
-------------------------------------------------------------------------------
------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION
¦
¦
¦
¦
MASTER MINIMUM EQUIPMENT LIST
¦
¦ FEDERAL AVIATION ADMINISTRATION
¦
¦ --------------------------------------------------------------------------- ¦
¦ AIRCRAFT:
¦ REVISION NO: 5
¦ PAGE:
¦
¦
HAWKER SIDDELEY HS-125
¦
¦
¦
¦
(SERIES 1 THROUGH 800XP)
¦ DATE: 05/30/2002
¦ 35-1
¦
¦ --------------------------------------------------------------------------- ¦
¦
1. ¦ 2. NUMBER INSTALLED
¦
¦ SYSTEM &
¦
-------------------------------------------- ¦
¦ SEQUENCE
ITEM
¦
¦ 3. NUMBER REQUIRED FOR DISPATCH
¦
¦ NUMBERS
¦
¦
--------------------------------------- ¦
¦ ------------------------- ¦
¦
¦ 4. REMARKS OR EXCEPTIONS
¦
¦ 35 OXYGEN
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 00-1 Oxygen Content
C ¦ 2 ¦ 1 ¦ (O)One may be inoperative
| ¦
¦
Indicators
¦
¦
¦ provided:
¦
¦
¦
¦
¦
a) An acceptable procedure is
¦
¦
¦
¦
¦
used to verify oxygen supply
¦
¦
¦
¦
¦
is above minimum required
¦
¦
¦
¦
¦
for the flight, and
¦
¦
¦
¦
¦
b) Fault is in the indicator
¦
¦
¦
¦
¦
only.
¦
¦
¦
¦
¦
¦
¦
C ¦ 2 ¦ 0 ¦ (O)May be inoperative provided
¦
¦
¦
¦
¦ flight remains at or below 10,000
¦
¦
¦
¦
¦ feet MSL.
¦
¦
¦
¦
¦
¦
¦ 00-2 Oxygen Cylinders
C ¦ - ¦ 1 ¦ (O)May be inoperative provided:
¦
¦
¦
¦
¦
a) Aircraft remains at or below
¦
¦
¦
¦
¦
10,000 feet MSL,
¦
¦
¦
¦
¦
b) Passenger oxygen supply
¦
¦
¦
¦
¦
valve is verified closed,
¦
¦
¦
¦
¦
c) Passengers are appropriately
¦
¦
¦
¦
¦
briefed, and
¦
¦
¦
¦
¦
d) Oxygen supply to the flight
¦
¦
¦
¦
¦
crew is verified sufficient
¦
¦
¦
¦
¦
to meet operations being
¦
¦
¦
¦
¦
conducted.
¦
¦
¦
¦
¦
¦
¦ 00-3 Barometric Valve
C ¦ 1 ¦ 1 ¦
¦
¦
¦
¦
¦
¦
¦
1) Auto Function
C ¦ 1 ¦ 0 ¦ (M)(O)May be inoperative provided: | ¦
¦
¦
¦
¦
a) Manual deployment system
¦
¦
¦
¦
¦
operates normally,
¦
¦
¦
¦
¦
b) Flight remains at or below
¦
¦
¦
¦
¦
FL 300, and
¦
¦
¦
¦
¦
c) Passenger supply valve
¦
¦
¦
¦
¦
operates normally.
¦
¦
¦
¦
¦
¦
¦ 10-1 Protective
D ¦ - ¦ - ¦ Any in excess of those required by
¦
¦
Breathing
¦
¦
¦ FAR may be inoperative or missing.
¦
¦
Equipment (PBE)
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
-------------------------------------------------------------------------------
------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION
¦
¦
¦
¦
MASTER MINIMUM EQUIPMENT LIST
¦
¦ FEDERAL AVIATION ADMINISTRATION
¦
¦ --------------------------------------------------------------------------- ¦
¦ AIRCRAFT:
¦ REVISION NO: 5
¦ PAGE:
¦
¦
HAWKER SIDDELEY HS-125
¦
¦
¦
¦
(SERIES 1 THROUGH 800XP)
¦ DATE: 05/30/2002
¦ 35-2
¦
¦ --------------------------------------------------------------------------- ¦
¦
1. ¦ 2. NUMBER INSTALLED
¦
¦ SYSTEM &
¦
-------------------------------------------- ¦
¦ SEQUENCE
ITEM
¦
¦ 3. NUMBER REQUIRED FOR DISPATCH
¦
¦ NUMBERS
¦
¦
--------------------------------------- ¦
¦ ------------------------- ¦
¦
¦ 4. REMARKS OR EXCEPTIONS
¦
¦ 35 OXYGEN
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 20-1 Passenger Oxygen
C ¦ - ¦ 0 ¦ (O)May be inoperative provided:
| ¦
¦
Masks and Stowages
¦
¦
¦
a) Associated seats are blocked
¦
¦
¦
¦
¦
and placarded to prevent
¦
¦
¦
¦
¦
occupancy.
¦
¦
¦
¦
¦
OR
¦
¦
C ¦
¦
¦
b) Flight is not conducted
¦
¦
¦
¦
¦
where the minimum enroute
¦
¦
¦
¦
¦
altitude is above 14,000
¦
¦
¦
¦
¦
feet MSL,
¦
¦
¦
¦
¦
c) Pressurization system
| ¦
¦
¦
¦
¦
operates normally,
| ¦
¦
¦
¦
¦
d) Flight remains at or below
¦
¦
¦
¦
¦
FL 250,
¦
¦
¦
¦
¦
e) Portable oxygen is provided
¦
¦
¦
¦
¦
to each passenger above
¦
¦
¦
¦
¦
15,000 feet MSL, and
¦
¦
¦
¦
¦
f) Passengers are appropriately
¦
¦
¦
¦
¦
briefed.
¦
¦
¦
¦
¦
¦
¦ 30-1 Portable Oxygen
C ¦ - ¦ - ¦ (M)Any in excess of those required
¦
¦
Dispensing Unit
¦
¦
¦ by FAR may be unserviceable or
¦
¦
¦
¦
¦ missing provided:
¦
¦
¦
¦
¦
a) Required distribution of
¦
¦
¦
¦
¦
serviceable bottles is
¦
¦
¦
¦
¦
maintained throughout the
¦
¦
¦
¦
¦
aircraft, and
¦
¦
¦
¦
¦
b) Bottles not properly ser¦
¦
¦
¦
¦
viced are replaced, serviced
¦
¦
¦
¦
¦
or removed at the next
¦
¦
¦
¦
¦
available maintenance
¦
¦
¦
¦
¦
facility.
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
-------------------------------------------------------------------------------
------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION
¦
¦
¦
¦
MASTER MINIMUM EQUIPMENT LIST
¦
¦ FEDERAL AVIATION ADMINISTRATION
¦
¦ --------------------------------------------------------------------------- ¦
¦ AIRCRAFT:
¦ REVISION NO: 5
¦ PAGE:
¦
¦
HAWKER SIDDELEY HS-125
¦
¦
¦
¦
(SERIES 1 THROUGH 800XP)
¦ DATE: 05/30/2002
¦ 49-1
¦
¦ --------------------------------------------------------------------------- ¦
¦
1. ¦ 2. NUMBER INSTALLED
¦
¦ SYSTEM &
¦
-------------------------------------------- ¦
¦ SEQUENCE
ITEM
¦
¦ 3. NUMBER REQUIRED FOR DISPATCH
¦
¦ NUMBERS
¦
¦
--------------------------------------- ¦
¦ ------------------------- ¦
¦
¦ 4. REMARKS OR EXCEPTIONS
¦
¦ 49 AIRBORNE AUXILIARY
¦
¦
¦
¦
¦
POWER
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 00-1 Auxiliary Power
C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided
¦
¦
Unit
¦
¦
¦ system is deactivated.
| ¦
¦
¦
¦
¦
¦
¦ 10-1 APU Air/Load
C ¦ - ¦ 0 ¦ (M)(O)May be inoperative provided: | ¦
¦
Control Valve
¦
¦
¦
a) Air valve is secured closed, | ¦
¦
¦
¦
¦
and
| ¦
¦
¦
¦
¦
b) APU air switch remains OFF.
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ NOTE: APU may be used to provide
¦
¦
¦
¦
¦
electric power.
¦
¦
¦
¦
¦
¦
¦ 10-2 APU
¦
¦
¦
¦
¦
Instrumentation
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
1) RPM/EGT
C ¦ 2 ¦ 0 ¦ (O)May be inoperative for ground
| ¦
¦
Indicators
¦
¦
¦ use only provided auto shutdown
¦
¦
(T62T¦
¦
¦ function of APU operates normally.
¦
¦
40C8D/T62T¦
¦
¦
¦
¦
40C8D1 And
¦
¦
¦
| ¦
¦
36-150/92/100/
¦
¦
¦
| ¦
¦
APU Only)
¦
¦
¦
| ¦
¦
¦
¦
¦
¦
¦
2) Amp Meter/
C ¦ 1 ¦ 0 ¦ (M)May be inoperative for ground
| ¦
¦
Load Meter
¦
¦
¦ use only provided PS2 bus voltage
| ¦
¦
¦
¦
¦ is monitored to remain within
| ¦
¦
¦
¦
¦ normal limits.
¦
¦
¦
¦
¦
¦
¦ 30-2 APU Operating
C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided an
¦
¦ *** Cycle Recorder
¦
¦
¦ alternate procedure for recording
¦
¦
¦
¦
¦ APU operating cycles is established
¦
¦
¦
¦
¦ and used.
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
-------------------------------------------------------------------------------
------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION
¦
¦
¦
¦
MASTER MINIMUM EQUIPMENT LIST
¦
¦ FEDERAL AVIATION ADMINISTRATION
¦
¦ --------------------------------------------------------------------------- ¦
¦ AIRCRAFT:
¦ REVISION NO: 4
¦ PAGE:
¦
¦
HAWKER SIDDELEY HS-125
¦
¦
¦
¦
(SERIES 1 THROUGH 800XP)
¦ DATE: 03/10/1998
¦ 52-1
¦
¦ --------------------------------------------------------------------------- ¦
¦
1. ¦ 2. NUMBER INSTALLED
¦
¦ SYSTEM &
¦
-------------------------------------------- ¦
¦ SEQUENCE
ITEM
¦
¦ 3. NUMBER REQUIRED FOR DISPATCH
¦
¦ NUMBERS
¦
¦
--------------------------------------- ¦
¦ ------------------------- ¦
¦
¦ 4. REMARKS OR EXCEPTIONS
¦
¦ 52 DOORS
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 11-1 Main Entry Door
C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided door
¦
¦
Unlock Indication
¦
¦
¦ is both visually and manually
¦
¦
System
¦
¦
¦ verified fully closed and locked
¦
¦
¦
¦
¦ before each departure.
¦
¦
¦
¦
¦
¦
¦ 25-1 Rear Baggage
C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided door
¦
¦ *** Pannier Door
¦
¦
¦ is both visually and manually
¦
¦
Unlock Indication
¦
¦
¦ verified fully closed and locked
¦
¦
¦
¦
¦ before each departure.
¦
¦
¦
¦
¦
¦
¦ 25-2 Rear Baggage
C ¦ 1 ¦ O ¦ (O)May be inoperative provided
¦
¦ *** Pannier Hatch
¦
¦
¦ hatch is both visually and manually
¦
¦
Unlock Indication
¦
¦
¦ verified fully closed and locked
¦
¦
¦
¦
¦ before each departure.
¦
¦
¦
¦
¦
¦
¦ 70-3 Optional Door or
C ¦ - ¦ 0 ¦ (O)May be inoperative provided
¦
¦ *** Hatch
¦
¦
¦ affected door or hatch is verified
¦
¦
Indications/Annun¦
¦
¦ closed and locked before each
¦
¦
ciators
¦
¦
¦ departure.
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ NOTE: Optional doors/hatches
¦
¦
¦
¦
¦
approved for relief under
¦
¦
¦
¦
¦
the above include the
¦
¦
¦
¦
¦
following:
¦
¦
¦
¦
¦
Remote Refuel Panel Door;
¦
¦
¦
¦
¦
Single Point Refuel Door;
¦
¦
¦
¦
¦
Ventral Tank Gravity
¦
¦
¦
¦
¦
Refuel Door; Rear
¦
¦
¦
¦
¦
Equipment Bay Door;
¦
¦
¦
¦
¦
Lavatory Service Panel
¦
¦
¦
¦
¦
Door.
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
-------------------------------------------------------------------------------
------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION
¦
¦
¦
¦
MASTER MINIMUM EQUIPMENT LIST
¦
¦ FEDERAL AVIATION ADMINISTRATION
¦
¦ --------------------------------------------------------------------------- ¦
¦ AIRCRAFT:
¦ REVISION NO: 5
¦ PAGE:
¦
¦
HAWKER SIDDELEY HS-125
¦
¦
¦
¦
(SERIES 1 THROUGH 800XP)
¦ DATE: 05/30/2002
¦ 52-2
¦
¦ --------------------------------------------------------------------------- ¦
¦
1. ¦ 2. NUMBER INSTALLED
¦
¦ SYSTEM &
¦
-------------------------------------------- ¦
¦ SEQUENCE
ITEM
¦
¦ 3. NUMBER REQUIRED FOR DISPATCH
¦
¦ NUMBERS
¦
¦
--------------------------------------- ¦
¦ ------------------------- ¦
¦
¦ 4. REMARKS OR EXCEPTIONS
¦
¦
¦
¦
¦
¦
¦ 70-4 Door Locks
D ¦ - ¦ 0 ¦ (O)May be inoperative provided
| ¦
¦ ***
¦
¦
¦ checks are made to ensure the lock | ¦
¦
¦
¦
¦ does not interfere with normal
| ¦
¦
¦
¦
¦ operation of the latch.
| ¦
¦
¦
¦
¦
¦
¦ 70-5 Ramp Guard System D ¦ - ¦ 0 ¦
| ¦
¦ ***
¦
¦
¦
| ¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
-------------------------------------------------------------------------------
------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION
¦
¦
¦
¦
MASTER MINIMUM EQUIPMENT LIST
¦
¦ FEDERAL AVIATION ADMINISTRATION
¦
¦ --------------------------------------------------------------------------- ¦
¦ AIRCRAFT:
¦ REVISION NO: 5
¦ PAGE:
¦
¦
HAWKER SIDDELEY HS-125
¦
¦
¦
¦
(SERIES 1 THROUGH 800XP)
¦ DATE: 05/30/2002
¦ 56-1
¦
¦ --------------------------------------------------------------------------- ¦
¦
1. ¦ 2. NUMBER INSTALLED
¦
¦ SYSTEM &
¦
-------------------------------------------- ¦
¦ SEQUENCE
ITEM
¦
¦ 3. NUMBER REQUIRED FOR DISPATCH
¦
¦ NUMBERS
¦
¦
--------------------------------------- ¦
¦ ------------------------- ¦
¦
¦ 4. REMARKS OR EXCEPTIONS
¦
¦ 56 WINDOWS
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 10-1 Windscreen
C ¦ - ¦ - ¦ (M)(O)May be delaminated provided: | ¦
¦
(Panel A)
¦
¦
¦
a) Visibility through the
| ¦
¦
(Series 1 Through
¦
¦
¦
affected windscreens is
| ¦
¦
700)
¦
¦
¦
acceptable to the crew,
| ¦
¦
¦
¦
¦
b) Airplane is not operated in | ¦
¦
¦
¦
¦
known or forecast icing
| ¦
¦
¦
¦
¦
conditions,
| ¦
¦
¦
¦
¦
c) Relevent SCREEN HEAT CTL
| ¦
¦
¦
¦
¦
circuit breaker is pulled
| ¦
¦
¦
¦
¦
and collared, and
| ¦
¦
¦
¦
¦
d) AFM limitations are
| ¦
¦
¦
¦
¦
observed.
| ¦
¦
¦
¦
¦
¦
¦ 10-2 Windscreens
c ¦ - ¦ - ¦ (M)(O)One "A" or "B" windscreen may | ¦
¦
"A"or"B"
¦
¦
¦ be delaminated provided:
| ¦
¦
(Series 800 and
¦
¦
¦
a) Visibility through the
| ¦
¦
800XP Only)
¦
¦
¦
affected windscreeen is
| ¦
¦
¦
¦
¦
acceptable to the crew,
| ¦
¦
¦
¦
¦
and vision is not impaired
| ¦
¦
¦
¦
¦
on the remaining windscreen, | ¦
¦
¦
¦
¦
b) Airplane is not operated in | ¦
¦
¦
¦
¦
known or forecast icing
| ¦
¦
¦
¦
¦
conditions,
| ¦
¦
¦
¦
¦
c) Revlevent SCREEN HEAT CTL
| ¦
¦
¦
¦
¦
circuit breaker is pulled
| ¦
¦
¦
¦
¦
and collard, and
| ¦
¦
¦
¦
¦
d) AFM limitations are
| ¦
¦
¦
¦
¦
observed.
| ¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
-------------------------------------------------------------------------------
------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION
¦
¦
¦
¦
MASTER MINIMUM EQUIPMENT LIST
¦
¦ FEDERAL AVIATION ADMINISTRATION
¦
¦ --------------------------------------------------------------------------- ¦
¦ AIRCRAFT:
¦ REVISION NO: 5
¦ PAGE:
¦
¦
HAWKER SIDDELEY HS-125
¦
¦
¦
¦
(SERIES 1 THROUGH 800XP)
¦ DATE: 05/30/2002
¦ 73-1
¦
¦ --------------------------------------------------------------------------- ¦
¦
1. ¦ 2. NUMBER INSTALLED
¦
¦ SYSTEM &
¦
-------------------------------------------- ¦
¦ SEQUENCE
ITEM
¦
¦ 3. NUMBER REQUIRED FOR DISPATCH
¦
¦ NUMBERS
¦
¦
--------------------------------------- ¦
¦ ------------------------- ¦
¦
¦ 4. REMARKS OR EXCEPTIONS
¦
¦ 73 ENGINE FUEL & CONTROL ¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 22-1 Engine SynchronC ¦ 1 ¦ 0 ¦ (O)May be inoperative provided:
¦
¦
izer System
¦
¦
¦
a) System is selected "OFF",
¦
¦
(Series 1 Through
¦
¦
¦
b) APR system is not armed, and | ¦
¦
800 With TFE-731
¦
¦
¦
c) AFM limitations are observed. | ¦
¦
Engines Only)
¦
¦
¦
| ¦
¦
¦
¦
¦
¦
¦ 22-2 Top Temperature
C ¦ 2 ¦ 1 ¦ (M)(O)One may be inoperative
¦
¦
Control System
¦
¦
¦ provided:
¦
¦
(Viper Engine Only) ¦
¦
¦
a) Associated switch remains
¦
¦
¦
¦
¦
OFF,
¦
¦
¦
¦
¦
b) Associated circuit breakers
¦
¦
¦
¦
¦
are pulled and collared, and
¦
¦
¦
¦
¦
c) Associated JPT indicator
¦
¦
¦
¦
¦
operates normally.
¦
¦
¦
¦
¦
¦
¦ 3. Engine Electronic
¦
¦
¦ Deleted, REV. 2.
¦
¦
Fuel Computer System
¦
¦
¦
¦
¦
(Series 1 Through
¦
¦
¦
| ¦
¦
800 With TFE-731
¦
¦
¦
¦
¦
Engines Only)
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 23-1 APR Computer
C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided:
¦
¦ *** System (Series
¦
¦
¦
a) AFM performance limitations
¦
¦
1 Through 800
¦
¦
¦
are observed,
¦
¦
With TFE-731
¦
¦
¦
b) APR system is selected OFF, | ¦
¦
¦
¦
¦
and
¦
¦
Engines Only)
¦
¦
¦
c) Procedures for monitoring
| ¦
¦
¦
¦
¦
engine limitations are
¦
¦
¦
¦
¦
established and used.
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
-------------------------------------------------------------------------------
------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION
¦
¦
¦
¦
MASTER MINIMUM EQUIPMENT LIST
¦
¦ FEDERAL AVIATION ADMINISTRATION
¦
¦ --------------------------------------------------------------------------- ¦
¦ AIRCRAFT:
¦ REVISION NO: 5
¦ PAGE:
¦
¦
HAWKER SIDDELEY HS-125
¦
¦
¦
¦
(SERIES 1 THROUGH 800XP)
¦ DATE: 05/30/2002
¦ 73-2
¦
¦ --------------------------------------------------------------------------- ¦
¦
1. ¦ 2. NUMBER INSTALLED
¦
¦ SYSTEM &
¦
-------------------------------------------- ¦
¦ SEQUENCE
ITEM
¦
¦ 3. NUMBER REQUIRED FOR DISPATCH
¦
¦ NUMBERS
¦
¦
--------------------------------------- ¦
¦ ------------------------- ¦
¦
¦ 4. REMARKS OR EXCEPTIONS
¦
¦ 73 ENGINE FUEL & CONTROL ¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 24-1 Automatic Thrust
C ¦ 2 ¦ 0 ¦ (O)May be inoperative provided
¦
¦
Limiter System
¦
¦
¦ RPM and JPT can be controlled
¦
¦
(Viper Engines Only) ¦
¦
¦ manually.
¦
¦
¦
¦
¦
¦
¦ 31-1 Fuel Flow
C ¦ 2 ¦ 1 ¦ (O)One may be inoperative
| ¦
¦
Indicators
¦
¦
¦ provided:
¦
¦
¦
¦
¦
a) Associated RPM and JPT/ITT
¦
¦
¦
¦
¦
indicators operate normally,
¦
¦
¦
¦
¦
b) All fuel quantity indicators
¦
¦
¦
¦
¦
operate normally, and
¦
¦
¦
¦
¦
c) A fuel monitoring procedure
¦
¦
¦
¦
¦
is established and used.
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
-------------------------------------------------------------------------------
------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION
¦
¦
¦
¦
MASTER MINIMUM EQUIPMENT LIST
¦
¦ FEDERAL AVIATION ADMINISTRATION
¦
¦ --------------------------------------------------------------------------- ¦
¦ AIRCRAFT:
¦ REVISION NO: 3
¦ PAGE:
¦
¦
HAWKER SIDDELEY HS-125
¦
¦
¦
¦
(SERIES 1 THROUGH 800XP)
¦ DATE: 09/07/1993
¦ 74-1
¦
¦ --------------------------------------------------------------------------- ¦
¦
1. ¦ 2. NUMBER INSTALLED
¦
¦ SYSTEM &
¦
-------------------------------------------- ¦
¦ SEQUENCE
ITEM
¦
¦ 3. NUMBER REQUIRED FOR DISPATCH
¦
¦ NUMBERS
¦
¦
--------------------------------------- ¦
¦ ------------------------- ¦
¦
¦ 4. REMARKS OR EXCEPTIONS
¦
¦ 74 IGNITION
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 10-1 Ignition systems
B ¦ 4 ¦ 3 ¦ (O)One ignitor on one engine may
¦
¦
¦
¦
¦ be inoperative provided:
¦
¦
¦
¦
¦
a) Aircraft is not operated
¦
¦
¦
¦
¦
in visible moisture or from
¦
¦
¦
¦
¦
contaminated runways, and
¦
¦
¦
¦
¦
b) Aircraft is not operated in
¦
¦
¦
¦
¦
known or forecast icing
¦
¦
¦
¦
¦
conditions.
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
-------------------------------------------------------------------------------
------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION
¦
¦
¦
¦
MASTER MINIMUM EQUIPMENT LIST
¦
¦ FEDERAL AVIATION ADMINISTRATION
¦
¦ --------------------------------------------------------------------------- ¦
¦ AIRCRAFT:
¦ REVISION NO: 5
¦ PAGE:
¦
¦
HAWKER SIDDELEY HS-125
¦
¦
¦
¦
(SERIES 1 THROUGH 800XP)
¦ DATE: 05/30/2002
¦ 77-1
¦
¦ --------------------------------------------------------------------------- ¦
¦
1. ¦ 2. NUMBER INSTALLED
¦
¦ SYSTEM &
¦
-------------------------------------------- ¦
¦ SEQUENCE
ITEM
¦
¦ 3. NUMBER REQUIRED FOR DISPATCH
¦
¦ NUMBERS
¦
¦
--------------------------------------- ¦
¦ ------------------------- ¦
¦
¦ 4. REMARKS OR EXCEPTIONS
¦
¦ 77 ENGINE INDICATING
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 10-2 Engine Indications
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
1) N1 Indicators
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
a) Digital
C ¦ 2 ¦ 0 ¦
| ¦
¦
Readout(s)
¦
¦
¦
| ¦
¦
¦
¦
¦
¦
¦
2) N2/RPM
C ¦ 2 ¦ 1 ¦ (O)One may be inoperative provided
¦
¦
Indicators
¦
¦
¦ N1 and Fuel Flow Indicators for the
¦
¦
¦
¦
¦ associated engine operate normally.
¦
¦
¦
¦
¦
¦
¦
3) ITT/EGT
¦
¦
¦
¦
¦
Indicators
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
a) Digital
C ¦ 2 ¦ 0 ¦
| ¦
¦
Readout(s)
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 32-1 Power Loss
C ¦ 2 ¦ 0 ¦ (O)May be inoperative provided all
¦
¦
Indicator Systems
¦
¦
¦ remaining engine indicating systems
¦
¦
(Viper Engine
¦
¦
¦ operate normally.
¦
¦
Only)
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 32-2 Above 92% Light
C ¦ 2 ¦ 0 ¦ (O)May be inoperative provided
¦
¦
Systems (Viper
¦
¦
¦ alternate procedures are
¦
¦
Engine Only)
¦
¦
¦ established and used.
¦
¦
¦
¦
¦
¦
¦ 32-3 Climb Power
C ¦ 2 ¦ 1 ¦ (O)One may be inoperative.
¦
¦
Annunciators
¦
¦
¦
¦
¦
(Series 1 Through
¦
¦
¦
¦
¦
800 With TFE-731
¦
¦
¦
¦
¦
Engines Only)
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
-------------------------------------------------------------------------------
------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION
¦
¦
¦
¦
MASTER MINIMUM EQUIPMENT LIST
¦
¦ FEDERAL AVIATION ADMINISTRATION
¦
¦ --------------------------------------------------------------------------- ¦
¦ AIRCRAFT:
¦ REVISION NO: 4
¦ PAGE:
¦
¦
HAWKER SIDDELEY HS-125
¦
¦
¦
¦
(SERIES 1 THROUGH 800XP)
¦ DATE: 03/10/1998
¦ 78-1
¦
¦ --------------------------------------------------------------------------- ¦
¦
1. ¦ 2. NUMBER INSTALLED
¦
¦ SYSTEM &
¦
-------------------------------------------- ¦
¦ SEQUENCE
ITEM
¦
¦ 3. NUMBER REQUIRED FOR DISPATCH
¦
¦ NUMBERS
¦
¦
--------------------------------------- ¦
¦ ------------------------- ¦
¦
¦ 4. REMARKS OR EXCEPTIONS
¦
¦ 78 ENGINE EXHAUST
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦ 30-1 Thrust Reversing
C ¦ 2 ¦ 0 ¦ (M)(O)May be inoperative provided:
¦
¦ *** System
¦
¦
¦
a) No damage to the thrust
¦
¦
¦
¦
¦
reverser system exists which
¦
¦
¦
¦
¦
would adversely affect
¦
¦
¦
¦
¦
operation of the airplane,
¦
¦
¦
¦
¦
and
¦
¦
¦
¦
¦
b) A procedure is established
¦
¦
¦
¦
¦
and used to ensure that the
¦
¦
¦
¦
¦
associated thrust
¦
¦
¦
¦
¦
reverser(s) is disabled and
¦
¦
¦
¦
¦
pinned in the stowed
¦
¦
¦
¦
¦
(forward thrust) position.
¦
¦
¦
¦
¦
¦
¦ 30-2 Thrust Reverser
C ¦ 4 ¦ 0 ¦ (M)(O)May be inoperative provided
¦
¦
Indicating
¦
¦
¦ procedures are established and used
¦
¦
Annunciators
¦
¦
¦ to ensure associated thrust
¦
¦
¦
¦
¦ reverser(s) is disabled and pinned
¦
¦
¦
¦
¦ in the stowed (forward thrust)
¦
¦
¦
¦
¦ position.
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
¦
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-------------------------------------------------------------------------------
------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION
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MASTER MINIMUM EQUIPMENT LIST
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¦ FEDERAL AVIATION ADMINISTRATION
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¦ --------------------------------------------------------------------------- ¦
¦ AIRCRAFT:
¦ REVISION NO: 3
¦ PAGE:
¦
¦
HAWKER SIDDELEY HS-125
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¦
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(SERIES 1 THROUGH 800XP)
¦ DATE: 09/07/1993
¦ 79-1
¦
¦ --------------------------------------------------------------------------- ¦
¦
1. ¦ 2. NUMBER INSTALLED
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¦ SYSTEM &
¦
-------------------------------------------- ¦
¦ SEQUENCE
ITEM
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¦ 3. NUMBER REQUIRED FOR DISPATCH
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¦ NUMBERS
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--------------------------------------- ¦
¦ ------------------------- ¦
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¦ 4. REMARKS OR EXCEPTIONS
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¦ 79 OIL
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¦ 30-1 Oil Pressure Low
C ¦ 2 ¦ 0 ¦ (O)May be inoperative provided:
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Warning Lights/
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a) Associated Oil Pressure and
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Annunciators
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Oil Temperature indicators
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operate normally,
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b) Associated oil tank is
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serviced to recommended
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capacity before each
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departure, and
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c) There is no evidence of
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above normal oil consumption
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or leakage.
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-------------------------------------------------------------------------------
------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION
¦
¦
¦
¦
MASTER MINIMUM EQUIPMENT LIST
¦
¦ FEDERAL AVIATION ADMINISTRATION
¦
¦ --------------------------------------------------------------------------- ¦
¦ AIRCRAFT:
¦ REVISION NO: 3
¦ PAGE:
¦
¦
HAWKER SIDDELEY HS-125
¦
¦
¦
¦
(SERIES 1 THROUGH 800XP)
¦ DATE: 09/07/1993
¦ 80-1
¦
¦ --------------------------------------------------------------------------- ¦
¦
1. ¦ 2. NUMBER INSTALLED
¦
¦ SYSTEM &
¦
-------------------------------------------- ¦
¦ SEQUENCE
ITEM
¦
¦ 3. NUMBER REQUIRED FOR DISPATCH
¦
¦ NUMBERS
¦
¦
--------------------------------------- ¦
¦ ------------------------- ¦
¦
¦ 4. REMARKS OR EXCEPTIONS
¦
¦ 80 STARTING
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¦ 00-1 Starter Power
C ¦ 1 ¦ 0 ¦
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Available
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Annunciator
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(TFE-731 Engines
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Only)
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¦ 00-2 Starter Select
C ¦ 1 ¦ 0 ¦
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Light (Viper
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Engines Only)
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¦ 00-3 Starter Operating C ¦ 2 ¦ 0 ¦ (O)May be inoperative provided:
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Annunciators
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a) Start power and EXT PWR
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(TFE-731 Engines
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switches are disengaged
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Only)
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when engine reaches self¦
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sustaining speed, and
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b) Generator is verified to be
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on line.
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