DEPARTMENT OF TRANSPORTATION Revision: 6 Date: 11/03/2004 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/ DENNIS OVERMAN, 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)917-6600 FAX: (425)917-6638

FEDERAL AVIATION ADMINISTRATION Page: I Revision: 6 MASTER MINIMUM EQUIPMENT LIST Date: 11/03/2004 HAWKER SIDDELEY HS-125 (SERIES 1 THROUGH 800XP) Table of Contents SYSTEM NO. SYSTEM PAGE -- Table of Contents I, II -- Log of Revisions III, IV -- Control Page V, VI, VII, VIII -- Control Page IX -- Highlights of Change X, XI, XII, XIII -- Highlights of Change XIV, XV, XVI, XVII -- Highlights of Change XVIII, XIX, XX, XXI -- Highlights of Change XXII, XXIII, XXIV, XXV -- Highlights of Change XXVI, XXVII, XXVIII, X -- Highlights of Change XXX, XXXI, XXXII, XXXI -- Highlights of Change XXXIV, XXXV, XXXVI, XX -- Highlights of Change -- Definitions Table, of Con, tents, -- Definitions TO, MMEL10, 000101, 80 -- Preamble 21 Air Conditioning 21-1, 2, 3, 4, 5 21 Air Conditioning 21-6 THRU 10 21 Air Conditioning 21-11 THRU 15 21 Air Conditioning 21-16 THRU 20 21 Air Conditioning 21-21 22 Auto Flight 22-1, 2, 3, 4, 5 22 Auto Flight 22-6 23 Communications 23-1, 2, 3, 4, 5 23 Communications 23-6, 7, 8, 9 24 Electrical Power 24-1, 2, 3, 4, 5 24 Electrical Power 24-6 25 Equipment/Furnishings 25-1, 2, 3, 4, 5 26 Fire Protection 26-1, 2, 3 27 Flight Controls 27-1, 2, 3, 4, 5 27 Flight Controls 27-6, 7 28 Fuel 28-1, 2, 3, 4, 5 28 Fuel 28-6 29 Hydraulic Power 29-1, 2, 3 30 Ice and Rain Protection 30-1, 2, 3, 4, 5 30 Ice and Rain Protection 30-6 THRU 10

FEDERAL AVIATION ADMINISTRATION Page: II Revision: 6 MASTER MINIMUM EQUIPMENT LIST Date: 11/03/2004 HAWKER SIDDELEY HS-125 (SERIES 1 THROUGH 800XP) Table of Contents SYSTEM NO. SYSTEM PAGE 30 Ice and Rain Protection 30-11 31 Indicating/Recording Systems 31-1, 2 32 Landing Gear 32-1 33 Lights 33-1, 2, 3, 4, 5 34 Navigation 34-1, 2, 3, 4, 5 34 Navigation 34-6 THRU 10 34 Navigation 34-11 THRU 15 34 Navigation 34-16 THRU 20 34 Navigation 34-21 THRU 25 34 Navigation 34-26 THRU 27 35 Oxygen 35-1, 2, 3, 4 38 Water/Waste 38-1, 2, 3 49 Airborne Auxiliary Power 49-1 52 Doors 52-1, 2 56 Windows 56-1 73 Engine Fuel & Control 73-1, 2 74 Ignition 74-1 77 Engine Indicating 77-1, 2 78 Engine Exhaust 78-1 79 Engine Oil 79-1 80 Starting 80-1

FEDERAL AVIATION ADMINISTRATION Page: III Revision: 6 MASTER MINIMUM EQUIPMENT LIST Date: 11/03/2004 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 ¦ ¦ ¦ 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 ¦ ¦ ¦ 3 ¦ 09/07/1993 ¦ 28-4,28-5,29-1,29-2,30-1 ¦ ¦ ¦ 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 ¦ ¦ ¦ 4 ¦ 03/10/1998 ¦ 22-3,22-4,23-1,23-2,23-3 ¦ ¦ ¦ 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 ¦ ¦ ¦ 4 ¦ 03/10/1998 ¦ 34-4,34-5,34-6,34-7,34-8 ¦ ¦ ¦ 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 Page: IV Revision: 6 MASTER MINIMUM EQUIPMENT LIST Date: 11/03/2004 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 ¦ ¦ ¦ 5 ¦ 05/30/2002 ¦ 25-1,25-2,25-3,25-4,26-1 ¦ ¦ ¦ 5 ¦ 05/30/2002 ¦ 26-2,27-2,27-3,27-4,27-5 ¦ ¦ ¦ 5 ¦ 05/30/2002 ¦ 28-1,28-2,28-3,28-4,28-5 ¦ ¦ ¦ 5 ¦ 05/30/2002 ¦ 29-1,29-2,30-1,30-2,30-3 ¦ ¦ ¦ 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 ¦ ¦ ¦ 5 ¦ 05/30/2002 ¦ 73-1,73-2,77-1 ¦ ¦ ¦ 6 ¦ 11/03/2004 ¦ HIGHLIGHTS OF REV.,DEFINITIONS ¦ ¦ ¦ 6 ¦ 11/03/2004 ¦ 21-1,21-2,21-3,21-4,21-5 ¦ ¦ ¦ 6 ¦ 11/03/2004 ¦ 21-6,21-7,21-8,21-9,21-10 ¦ ¦ ¦ 6 ¦ 11/03/2004 ¦ 21-11,21-12,21-13,21-14,21-15 ¦ ¦ ¦ 6 ¦ 11/03/2004 ¦ 21-16,21-17,21-18,21-19,21-20 ¦ ¦ ¦ 6 ¦ 11/03/2004 ¦ 21-21,22-1,22-2,22-3,22-4 ¦ ¦ ¦ 6 ¦ 11/03/2004 ¦ 22-5,22-6,23-1,23-2,23-3 ¦ ¦ ¦ 6 ¦ 11/03/2004 ¦ 23-4,23-5,23-6,23-7,23-8 ¦ ¦ ¦ 6 ¦ 11/03/2004 ¦ 23-9,24-1,24-2,24-3,24-4 ¦ ¦ ¦ 6 ¦ 11/03/2004 ¦ 24-5,24-6,25-1,25-2,25-3 ¦ ¦ ¦ 6 ¦ 11/03/2004 ¦ 25-4,25-5,26-1,26-2,26-3 ¦ ¦ ¦ 6 ¦ 11/03/2004 ¦ 27-1,27-2,27-3,27-4,27-5 ¦ ¦ ¦ 6 ¦ 11/03/2004 ¦ 27-6,27-7,28-1,28-2,28-3 ¦ ¦ ¦ 6 ¦ 11/03/2004 ¦ 28-4,28-5,28-6,29-1,29-2 ¦ ¦ ¦ 6 ¦ 11/03/2004 ¦ 29-3,30-1,30-2,30-3,30-4 ¦ ¦ ¦ 6 ¦ 11/03/2004 ¦ 30-5,30-6,30-7,30-8,30-9 ¦ ¦ ¦ 6 ¦ 11/03/2004 ¦ 30-10,30-11,31-1,31-2,32-1 ¦ ¦ ¦ 6 ¦ 11/03/2004 ¦ 33-1,33-2,33-3,33-4,33-5 ¦ ¦ ¦ 6 ¦ 11/03/2004 ¦ 34-1,34-2,34-3,34-4,34-5 ¦ ¦ ¦ 6 ¦ 11/03/2004 ¦ 34-6,34-7,34-8,34-9,34-10 ¦ ¦ ¦ 6 ¦ 11/03/2004 ¦ 34-11,34-12,34-13,34-14,34-15 ¦ ¦ ¦ 6 ¦ 11/03/2004 ¦ 34-16,34-17,34-18,34-19,34-20 ¦ ¦ ¦ 6 ¦ 11/03/2004 ¦ 34-21,34-22,34-23,34-24,34-25 ¦ ¦ ¦ 6 ¦ 11/03/2004 ¦ 34-26,34-27,35-1,35-2,35-3 ¦ ¦ ¦ 6 ¦ 11/03/2004 ¦ 35-4,38-1,38-2,38-3,49-1 ¦ ¦ ¦ 6 ¦ 11/03/2004 ¦ 52-1,52-2,56-1,73-1,73-2 ¦ ¦ ¦ 6 ¦ 11/03/2004 ¦ 74-1,77-1,77-2,78-1,79-1 ¦ ¦ ¦ 6 ¦ 11/03/2004 ¦ 80-1 ¦ ¦ ----------------------------------------------------------------------

FEDERAL AVIATION ADMINISTRATION Page: V Revision: 6 MASTER MINIMUM EQUIPMENT LIST Date: 11/03/2004 HAWKER SIDDELEY HS-125 (SERIES 1 THROUGH 800XP) Control Page SYSTEM PAGE REV NO. CURRENT DATE Cover Page - 6 11/03/2004 Table of Contents I 6 11/03/2004 II 6 11/03/2004 Log of Revisions III 6 11/03/2004 IV 6 11/03/2004 Control Page V 6 11/03/2004 VI 6 11/03/2004 VII 6 11/03/2004 VIII 6 11/03/2004 IX 6 11/03/2004 Highlights of Change X 6 11/03/2004 XI 6 11/03/2004 XII 6 11/03/2004 XIII 6 11/03/2004 XIV 6 11/03/2004 XV 6 11/03/2004 XVI 6 11/03/2004 XVII 6 11/03/2004 XVIII 6 11/03/2004 XIX 6 11/03/2004 XX 6 11/03/2004 XXI 6 11/03/2004 XXII 6 11/03/2004 XXIII 6 11/03/2004 XXIV 6 11/03/2004 XXV 6 11/03/2004 XXVI 6 11/03/2004 XXVII 6 11/03/2004 XXVIII 6 11/03/2004 XXIX 6 11/03/2004 XXX 6 11/03/2004 XXXI 6 11/03/2004 XXXII 6 11/03/2004 XXXIII 6 11/03/2004 XXXIV 6 11/03/2004 XXXV 6 11/03/2004 XXXVI 6 11/03/2004 XXXVII 6 11/03/2004 XXXVIII 6 11/03/2004 XXXIX 6 11/03/2004

FEDERAL AVIATION ADMINISTRATION Page: VI Revision: 6 MASTER MINIMUM EQUIPMENT LIST Date: 11/03/2004 HAWKER SIDDELEY HS-125 (SERIES 1 THROUGH 800XP) Control Page SYSTEM PAGE REV NO. CURRENT DATE XL 6 11/03/2004 XLI 6 11/03/2004 Definitions XLII 6 01/31/1995 XLIII 6 01/31/1995 XLIV 6 01/31/1995 XLV 6 01/31/1995 XLVI 6 01/31/1995 XLVII 6 01/31/1995 XLVIII 6 01/31/1995 XLVIX 6 01/31/1995 Preamble L 2 06/14/1989 LI 2 06/14/1989 21 21-1 6 11/03/2004 21-2 6 11/03/2004 21-3 6 11/03/2004 21-4 6 11/03/2004 21-5 6 11/03/2004 21-6 6 11/03/2004 21-7 6 11/03/2004 21-8 6 11/03/2004 21-9 6 11/03/2004 21-10 6 11/03/2004 21-11 6 11/03/2004 21-12 6 11/03/2004 21-13 6 11/03/2004 21-14 6 11/03/2004 21-15 6 11/03/2004 21-16 6 11/03/2004 21-17 6 11/03/2004 21-18 6 11/03/2004 21-19 6 11/03/2004 21-20 6 11/03/2004 21-21 6 11/03/2004 22 22-1 6 11/03/2004 22-2 6 11/03/2004 22-3 6 11/03/2004 22-4 6 11/03/2004 22-5 6 11/03/2004 22-6 6 11/03/2004 23 23-1 6 11/03/2004

FEDERAL AVIATION ADMINISTRATION Page: VII Revision: 6 MASTER MINIMUM EQUIPMENT LIST Date: 11/03/2004 HAWKER SIDDELEY HS-125 (SERIES 1 THROUGH 800XP) Control Page SYSTEM PAGE REV NO. CURRENT DATE 23-2 6 11/03/2004 23-3 6 11/03/2004 23-4 6 11/03/2004 23-5 6 11/03/2004 23-6 6 11/03/2004 23-7 6 11/03/2004 23-8 6 11/03/2004 23-9 6 11/03/2004 24 24-1 6 11/03/2004 24-2 6 11/03/2004 24-3 6 11/03/2004 24-4 6 11/03/2004 24-5 6 11/03/2004 24-6 6 11/03/2004 25 25-1 6 11/03/2004 25-2 6 11/03/2004 25-3 6 11/03/2004 25-4 6 11/03/2004 25-5 6 11/03/2004 26 26-1 6 11/03/2004 26-2 6 11/03/2004 26-3 6 11/03/2004 27 27-1 6 11/03/2004 27-2 6 11/03/2004 27-3 6 11/03/2004 27-4 6 11/03/2004 27-5 6 11/03/2004 27-6 6 11/03/2004 27-7 6 11/03/2004 28 28-1 6 11/03/2004 28-2 6 11/03/2004 28-3 6 11/03/2004 28-4 6 11/03/2004 28-5 6 11/03/2004 28-6 6 11/03/2004 29 29-1 6 11/03/2004 29-2 6 11/03/2004 29-3 6 11/03/2004 30 30-1 6 11/03/2004 30-2 6 11/03/2004

FEDERAL AVIATION ADMINISTRATION Page: VIII Revision: 6 MASTER MINIMUM EQUIPMENT LIST Date: 11/03/2004 HAWKER SIDDELEY HS-125 (SERIES 1 THROUGH 800XP) Control Page SYSTEM PAGE REV NO. CURRENT DATE 30-3 6 11/03/2004 30-4 6 11/03/2004 30-5 6 11/03/2004 30-6 6 11/03/2004 30-7 6 11/03/2004 30-8 6 11/03/2004 30-9 6 11/03/2004 30-10 6 11/03/2004 30-11 6 11/03/2004 31 31-1 6 11/03/2004 31-2 6 11/03/2004 32 32-1 6 11/03/2004 33 33-1 6 11/03/2004 33-2 6 11/03/2004 33-3 6 11/03/2004 33-4 6 11/03/2004 33-5 6 11/03/2004 34 34-1 6 11/03/2004 34-2 6 11/03/2004 34-3 6 11/03/2004 34-4 6 11/03/2004 34-5 6 11/03/2004 34-6 6 11/03/2004 34-7 6 11/03/2004 34-8 6 11/03/2004 34-9 6 11/03/2004 34-10 6 11/03/2004 34-11 6 11/03/2004 34-12 6 11/03/2004 34-13 6 11/03/2004 34-14 6 11/03/2004 34-15 6 11/03/2004 34-16 6 11/03/2004 34-17 6 11/03/2004 34-18 6 11/03/2004 34-19 6 11/03/2004 34-20 6 11/03/2004 34-21 6 11/03/2004 34-22 6 11/03/2004 34-23 6 11/03/2004

FEDERAL AVIATION ADMINISTRATION Page: IX Revision: 6 MASTER MINIMUM EQUIPMENT LIST Date: 11/03/2004 HAWKER SIDDELEY HS-125 (SERIES 1 THROUGH 800XP) Control Page SYSTEM PAGE REV NO. CURRENT DATE 34-24 6 11/03/2004 34-25 6 11/03/2004 34-26 6 11/03/2004 34-27 6 11/03/2004 35 35-1 6 11/03/2004 35-2 6 11/03/2004 35-3 6 11/03/2004 35-4 6 11/03/2004 38 38-1 6 11/03/2004 38-2 6 11/03/2004 38-3 6 11/03/2004 49 49-1 6 11/03/2004 52 52-1 6 11/03/2004 52-2 6 11/03/2004 56 56-1 6 11/03/2004 73 73-1 6 11/03/2004 73-2 6 11/03/2004 74 74-1 6 11/03/2004 77 77-1 6 11/03/2004 77-2 6 11/03/2004 78 78-1 6 11/03/2004 79 79-1 6 11/03/2004 80 80-1 6 11/03/2004

FEDERAL AVIATION ADMINISTRATION Page: X Revision: 6 MASTER MINIMUM EQUIPMENT LIST Date: 11/03/2004 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 of the previous list with revision 6 for a complete up to date MMEL. ATA 21 AIR CONDITIONING: 21-10-1 Engine Main Air Valves - Provisos of second relief statement expanded to detail procedures for configuring and operating in an unpressurized configuration. 21-10-2 Engine Main Air Valve Position Indicators - "OR" removed and proviso's reformatted IAW FOPB Policy Letter 31. Slight rewording of first and second relief statements for clarity. Provisos of third relief statement expanded to detail procedures for configuring and operating in an unpressurized configuration. 21-10-3 Refrigeration Unit System/Air Cycle Machine - Provisos relief statement expanded to detail procedures for configuring and operating in an unpressurized configuration. NOTE: This reflects a correction to the Highlights of Change for Rev. 5 (no change bars have been appended to Item in ATA Chapter 21). The Rev. 5 statement should have noted that the Item title was expanded to include "/Air Cycle Machine." (Previous statement in Highlights of Change to Rev. 5 denoting "Number of item changed" were erroneous.) 21-10-6 Cabin Flood Valve - Title simplified and parenthetical Series reference removed. Sub-Items added for "Two-Way Cabin Flood Valve (Aircraft without Cabin Floor Valves)," and "Cabin Flood Valve (Aircraft with Cabin Floor Valves)." NOTE: Reference from Highlights of Change for Rev. 5 neglected to mention that this Item had been relocated from Item 21-60-6 at manufacturer's request with a new item [Cabin/VIP Temperature Control Switch] placed under 21-60-6.

FEDERAL AVIATION ADMINISTRATION Page: XI Revision: 6 MASTER MINIMUM EQUIPMENT LIST Date: 11/03/2004 HAWKER SIDDELEY HS-125 (SERIES 1 THROUGH 800XP) Highlights of Change 21-10-6-2) Cabin Floor Valve-Cabin Flood Valve (Aircraft with Cabin Floor Valves) - IAW FOPB Policy Letter 31, "OR" removed from between relief statements. First relief statement amended to include wording, "is confirmed to operate normally." Provisos of second relief statement expanded to detail procedures for configuring and operating in an unpressurized configuration. 21-10-11 Cabin Floor Valves - An "s" appended to Title to indicate two Valves are installed. Parenthetical Series reference removed from Title. New "C/2/1" relief provided. IAW FOPB Policy Letter 31, "OR" removed from between "C/2/0" proviso statements. First relief statement amended to include wording, "is confirmed to operate normally." Provisos of second relief statement expanded to detail procedures for configuring and operating in an unpressurized configuration. 21-10-12 Cabin Flood Valve Indicator - Parenthetical Series references removed from Title. Two relief statements provided. 21-10-13 Cabin Floor Valve Indicator - Parenthetical Series references removed from Title. IAW FOPB Policy Letter 31, "OR" removed from between relief statements. First relief statement, proviso "a)" changed from "verified" to "confirmed;" and, proviso "b)" added requiring confirmation of normal operation of Flood Valve Indicator. Second relief statement expanded to detail procedures for configuring and operating in an unpressurized configuration.

FEDERAL AVIATION ADMINISTRATION Page: XII Revision: 6 MASTER MINIMUM EQUIPMENT LIST Date: 11/03/2004 HAWKER SIDDELEY HS-125 (SERIES 1 THROUGH 800XP) Highlights of Change 21-10-14 Flow Control Valve (Series 1 Through 800, and C-29A) - Provisos of relief statement expanded to detail procedures for configuring and operating in an unpressurized configuration. Title also revised for technical accuracy. NOTE: Rev. 5 Highlights of Change mentioned that this Item was moved from Item 21-30-9. 21-10-15 HP Air Valve (Series 1 Through 800XP) With TFE-731 Engines Only) - Proviso a) of first proviso set revised to change the word "secured" to "confirmed." Proviso c) added to first proviso set restricting altitude to FL250 or below. Second relief statement expanded to detail procedures for configuring and operating in an unpressurized configuration. 21-10-16 Pressure Regulating Shutoff Valve (PRSOV) (Series 800XP and C-29A) - New relief added to distinguish between Series 800 and 800XP aircraft. 21-20-1 Cabin Recirculating Fan - Relief for this Item is restored, and erroneous statement, "Moved to Item 34-10-10, Rev. 5" is deleted. 21-20-2 Flight Deck Heat Valve/Auxiliary Heating Valve - Second relief statement expanded to detail procedures for configuring and operating in an unpressurized configuration. 21-20-3 Flight Deck Recirculating Fan(s) - "(s)" added to Title to be consistent with variable ("-") number installed. 21-20-4 Mixing Valves (TFE 731 Engine Only) - Relief statement expanded to detail procedures for configuring and operating in an unpressurized configuration.

FEDERAL AVIATION ADMINISTRATION Page: XIII Revision: 6 MASTER MINIMUM EQUIPMENT LIST Date: 11/03/2004 HAWKER SIDDELEY HS-125 (SERIES 1 THROUGH 800XP) Highlights of Change 21-21-1 Nose Compartment Ventilation System - A notation has been added to the Remarks and Exception section to the effect that this Item was relocated to 34-70-12, in Revision 5. Previously, neither the Highlights of Change, nor ATA Chapter 21 documented this action. 21-30-1 Cabin Altitude Warning Light/Annunciator - "OR" removed and provisos reformatted IAW FOPB Policy Letter 31. Second relief statement expanded to detail procedures for configuring and operating in an unpressurized configuration. 21-30-2 Cabin Altitude Aural Warning - "OR" removed and provisos reformatted IAW FOPB Policy Letter 31. Second relief statement expanded to detail procedures for configuring and operating in an unpressurized configuration. 21-30-3 Automatic Cabin Pressure Controller - "OR" removed and provisos reformatted IAW FOPB Policy Letter 31. Second relief statement expanded to detail procedures for configuring and operating in an unpressurized configuration. 21-30-4 Fan Operated Venturi - New proviso b) added. 21-30-5 Outflow/Safety Valves - Relief statement expanded to detail procedures for configuring and operating in an unpressurized configuration. 21-30-6 Cabin Pressure Instruments (Triple Indicator or Separate Indicators) - "OR's" removed and provisos reformatted IAW FOPB Policy Letter 31. 21-30-6-1) Cabin Pressure Instruments (Triple Indicator or Separate Indicators)-Cabin Altimeter Indicator - Second relief statement expanded to detail procedures for configuring and operating in an unpressurized configuration. 21-30-6-2) Cabin Pressure Instruments (Triple Indicator or Separate Indicators)-Cabin Differential Pressure Indicator - Second relief statement expanded to detail procedures for configuring and operating in an unpressurized configuration.

FEDERAL AVIATION ADMINISTRATION Page: XIV Revision: 6 MASTER MINIMUM EQUIPMENT LIST Date: 11/03/2004 HAWKER SIDDELEY HS-125 (SERIES 1 THROUGH 800XP) Highlights of Change 21-30-6-3) Cabin Pressure Instruments (Triple Indicator or Separate Indicators)-Cabin Rate of Climb Indicator - Second relief statement expanded to detail procedures for configuring and operating in an unpressurized configuration. 21-30-9 Flow Control Valve - Superfluous "C/1/0" deleted. 21-30-10 Automatic Pressure Regulators - "s" added to Title to denote two(2) Regulators installed. Relief statement expanded to detail procedures for configuring and operating in an unpressurized configuration. 21-60-4 Turbine Unit Bypass Valve (Series 1 Through 800)/Low Limit Temp Control Valve (Series 800XP) - Relief statement expanded to detail procedures for configuring and operating in an unpressurized configuration. 21-60-5 Cabin/VIP Temperature Control Switch - Item number changed to conform with previous MMEL numbering system. NOTE: This was a New Item in Rev. 5, however Highlights of Change for Rev. 5 (apparently confusing Item number with previous Item 21-60-5, "Cabin Flood Control Valve/Flood Flow Valve"), erroneously indicated it had been, "moved to Item 21-10-15" (Item 21-60-5, was, in fact, renamed, reformatted, expanded and relocated to Item 21-10-6.) 21-60-6 Cabin Flood Control Valve/Flood Flow Valve - For historical accuracy, the Item number in effect prior to Rev. 5 has been restored. NOTE: IAW the manufacturer's request, this Item was renamed, reformatted, expanded and relocated to ATA 21-10-6, in Rev. 5. Possibly due to numbering confusion over then new Item 21-60-5, above, Highlights of Change for Rev. 5 erroneously described 21-60-6 as a "New Item."

FEDERAL AVIATION ADMINISTRATION Page: XV Revision: 6 MASTER MINIMUM EQUIPMENT LIST Date: 11/03/2004 HAWKER SIDDELEY HS-125 (SERIES 1 THROUGH 800XP) Highlights of Change 21-60-7 Refrigeration Unit Bypass Valve (RBV) (Series 1 Through 800)/Cabin Temperature Control Valve (Series 800XP) - Relief statement expanded to detail procedures for configuring and operating in an unpressurized configuration. ATA 22 AUTO FLIGHT: 22-10-1 Autopilot Systems - IAW FOPB Policy Letter 84 and Policy Letter 101, Revision 1, dated September 13, 2001, Item reformatted, Repair Interval for the "0 Required for Dispatch" case changed to Category "B." Previous "B/1/0" reference deleted, its relief statement relocated to the "B/-/0" position, and reference to "enroute operations" added. 22-10-2 Autopilot Control Yoke Disengage Switches - Item numbering scheme in effect prior to Rev. 5 has been restored. IAW manufacturer's established nomenclature, Title changed from "Control Wheel Disengage Switches," to "Control Yoke Disengage Switches." IAW FOPB Policy Letter 93, wording of first proviso changed to "not less than initial approach altitude." IAW Revision 1 of FOPB Policy Letter 101, dated September 13, 2001, Repair Interval for "Autopilot is not used" case changed to Category "B." Provisos expanded for consistency with other items. NOTE: "Yaw Damper/Autopilot Controller Disconnect Switch Bar, which was introduced in Rev. 5 as 22-10-2, has been relocated to 22-10-4.

FEDERAL AVIATION ADMINISTRATION Page: XVI Revision: 6 MASTER MINIMUM EQUIPMENT LIST Date: 11/03/2004 HAWKER SIDDELEY HS-125 (SERIES 1 THROUGH 800XP) Highlights of Change 22-10-3 Autopilot Disconnect Annunciator Lights - Item numbering scheme in effect prior to Rev. 5 has been restored. "OR" removed and provisos reformatted IAW FOPB Policy Letter 31. Wording of first proviso changed to "not less than initial approach altitude" IAW FOPB Policy Letter 93. IAW Revision 1 of FOPB Policy Letter 101, dated September 13, 2001, Repair Interval for "Autopilot is not used" case changed to Category "B." Provisos expanded for consistency with other items. NOTE: "Autopilot Control Wheel Disengage Switches," erroneously relocated to Item 22-10-3 in Revision 5, has been restored to its previous position of 22-10- 2. 22-10-4 Yaw Damp/Autopilot Controller Disconnect Switch Bar (Collins Avionics Equipped Aircraft Only) - Item renumbered to conform with numbering scheme in effect prior to Rev. 5. For consistency with FOPB Policy Letter 31, as well as conformity with Item 22-10-2, Proviso wording changed from "Control Wheel Disengage Switches," to "Autopilot Control Yoke Disengage Switches." NOTE: This Item was erroneously introduced in Rev. 5 as 22-10-2. 22-10-5 Touch Control Steering (TCS) - "C/2/0" relief statement expanded, and a "B/2/0 - Autopilot is considered inoperative and is not used" relief statement added. 22-10-7 Control Yoke Pitch/Roll Switches (Series 800 and 800XP with Collins A/P, only) - "Control Yoke" added to Title IAW manufacturer's original proposal. "Switches" pluralized to reflect two(2) installed. Word order of parenthetical model applicability reference changed for clarity and consistency. 22-10-8 A/P Flap Annunciator (Honeywell Equipped Aircraft Only) - In relief statement for "C/-/0" case,"is" replaced by "are" to reflect multiple items, and numbers in column 2 changed to [-] 22-20-1 Yaw Damper System - Because Autopilot cannot be engaged with an inoperative Yaw Damper System, Repair Interval to Category "B" IAW Revision 1 of FOPB Policy Letter 101, dated September 13, 2001.

FEDERAL AVIATION ADMINISTRATION Page: XVII Revision: 6 MASTER MINIMUM EQUIPMENT LIST Date: 11/03/2004 HAWKER SIDDELEY HS-125 (SERIES 1 THROUGH 800XP) Highlights of Change 22-20-2 Aileron Out-of-Trim Annunciators - Relief for this item, which had been deleted in Revision 5, has been amended for clarity and re-instituted. Title amended and parenthetical references added to title to reflect series applicability, and to clarify sub-components encompassed by this relief. 22-20-3 Elevator Out-of-Trim Annunciators - Relief for this item, which had been deleted in Revision 5, has been amended for clarity and re-instituted. Title amended and parenthetical references added to title to reflect series applicability, and to clarify sub-components encompassed by this relief. 22-20-4 Autopilot Trim Annunciators (Aircraft With Digital Avionics Only) - Repair Interval for the "Autopilot is not used" case changed to Category "B" IAW Revision 1 of FOPB Policy Letter 101, dated September 13, 2001. Provisos expanded for consistency with other items. 22-20-5 Autopilot Aileron Trim Indicator (Series 1 Through 700, Only) - For consistency, Series applicability has been relocated as a parenthetical reference to the title. Repair Interval for the "Autopilot is not used" case changed to Category "B" IAW Revision 1 of FOPB Policy Letter 101, dated September 13, 2001. Provisos expanded for consistency with other items. 22-20-6 Autopilot Elevator Trim Indicator (Series 1 Through 700, Only) - For consistency, Series applicability has been relocated as a parenthetical reference to the title. Repair Interval for the "Autopilot not used" case changed to Category "B" IAW Revision 1 of FOPB Policy Letter 101, dated September 13, 2001. Provisos expanded for consistency with other items. 22-20-7 Guidance Controller (Honeywell SPZ-8000 and Collins APS-85 and Collins Proline 21 Equipped Aircraft) - Failure of this Item renders the Autopilot Inoperative, therefore, Repair Interval has been changed to Category "B" IAW Revision 1 of FOPB Policy Letter 101, dated September 13, 2001. Proviso requiring autopilot to be considered inoperative added as "a)." Reference to "enroute operations" added to proviso "b)" IAW Revision 1 of FOPB Policy Letter 84. Reference to AFM limitations deleted in favor of proviso describing series 800XP applicability and requirement that Mach Trim operate normally, and be used, above 0.73 IMN.

FEDERAL AVIATION ADMINISTRATION Page: XVIII Revision: 6 MASTER MINIMUM EQUIPMENT LIST Date: 11/03/2004 HAWKER SIDDELEY HS-125 (SERIES 1 THROUGH 800XP) Highlights of Change 22-20-9 Mode Select Panel - Because an inoperative Mode Control Panel renders the autopilot unusable, Repair Interval changed to Category "B" IAW Revision 1 of FOPB Policy Letter 101, dated September 13. Provisos expanded for consistency with other items. ATA 23 COMMUNICATIONS: 23-05-1 Radio Management Units (RMU's)/ Radio Tuning Units (RTU's) - An "s" added to Titles to denote two(2) RMU's/RTU's installed. IAW FOPB Policy Letter 63, proviso added, restricting relief to Units not powered by Emergency Bus, or equivalent, and not required to accomplish Emergency Procedures NOTE: This Item was previously revised in Revision 5, however no change bars were included next to the Item. 23-10-1 Communications System (VHF, HF, UHF) - Revision 1 of FOPB Policy Letter 95 notwithstanding, "HF" has been restored to the Title of Communications Systems. HF provisions which comply with the intent of Revision 1 of FOPB Policy Letter 106, dated January 18, 2001, have been added. Minor spelling correction ("DC" instead of previous "TC"). Relief statement references to Emergency Buses revised to reflect HS-125 electrical system nomenclature. 23-10-1-1) VHF Communications Control Panels - IAW FOPB Policy Letter 95, Title expanded. For Sub-Item's "c)," Frequency Selector Knob, and "d)," Frequency Indicator, Number Required for Dispatch changed to two(2).

FEDERAL AVIATION ADMINISTRATION Page: XIX Revision: 6 MASTER MINIMUM EQUIPMENT LIST Date: 11/03/2004 HAWKER SIDDELEY HS-125 (SERIES 1 THROUGH 800XP) Highlights of Change 23-10-1-2) High Frequency (HF) Communication System(s) - IAW FOPB Policy Letter 106, Sub-Title expanded. Wording, "Long Range Communication Systems," added to relief proviso statement to clarify meaning of "LCRS." NOTE: Highlights of Change to Rev. 5 neglected to mention that additional relief provisos for HF System(s) was added IAW FOPB Policy Letter 106, dated October 18, 2000. The provisos have been further amended, as appropriate, to reflect changes implemented by Revision 1 to Policy Letter 106, which is dated January 18, 2001. 23-10-3 Standby Nav/Comm Controller (Clearance Delivery Unit) - Item has been deleted IAW the MMEL Preamble and FOPB Policy Letter 63, because its normal operation is required in order to perform Emergency Procedures. 23-20-2 ACARS System - "(O)" added to denote the requirement to develop and use alternate procedures. 23-20-3 AFIS (VHF/SAT - "(O)" added to denote the requirement to develop and use alternate procedures. 23-30-1 Passenger Address System - Provisos amended and NOTE added IAW FOPB Policy Letter 9, Revision 6, dated 02/05/03. NOTE: PA Systems not required by FAR Part 91. FAR 135.150 does not require PA Systems for aircraft with a passenger seating capacity of 19, or less. 23-30-2 Cabin Chimes - Reformatted and "OR" removed IAW FOPB Policy Letter 31. 23-30-5 Emergency Locator Transmitter (ELT) - Proviso wording changed for consistency of intent with FOPB Policy Letter 52. 23-40-1 Crewmember Interphone System - Title amended, Sub-Titling introduced, provisos altered, and NOTE added IAW FOPB Policy Letter 09, as it applies to the Operating Rules under which the HS-125 is currently known to operate.

FEDERAL AVIATION ADMINISTRATION Page: XX Revision: 6 MASTER MINIMUM EQUIPMENT LIST Date: 11/03/2004 HAWKER SIDDELEY HS-125 (SERIES 1 THROUGH 800XP) Highlights of Change NOTE: Crew Interphone System not required by FAR Part 91. FAR 135.150 does not require Crewmember Interphone Systems until an aircraft's passenger seating configuration exceeds 19. 23-50-1 Headsets - IAW FOPB Policy Letter 52, provisions for "Category D" Repair Interval added for Headsets in excess of those required by FAR. 23-50-2 Microphones - IAW FOPB Policy Letter 52, Repair Interval for Microphones in excess of those required by FAR changed to "Category D." 23-50-3 Boom Microphones - Slight addition to Titles for clarity. IAW FOPB Policy Letter 58, "if installed" added to first proviso set to reflect FAR applicability. 23-50-5 Flight Deck Pilot-to-Pilot "Hot Mic" Interphone System - Title and proviso wording added to clarify that this relief applies only to the optional Pilot-to-Pilot "Hot Mic" system. 23-60-1 Static Dischargers - Proviso revised for clarity. 23-60-2 Surface Bond Straps - New Item. 23-70-1 Cockpit Voice Recorder (CVR) - Title changed IAW Revision 3 of FOPB Policy Letter 29, dated August 15, 1997. Sub-Titles and provisos expanded for clarity, FAR applicability, and consistency with reciprocal provisions of Item 23-50-3. 23-70-3 Satellite Communications Systems (SATCOM) - IAW newly revised FOPB Policy Letter 106, provisos added to account for inoperative SATCOM during operations requiring Long Range Communications System (LCRS). "Category D" Repair Interval for first proviso set changed to "C" IAW FOPB PL 52. It is apparent that flight crews will rely on this Item through training or routine procedure, and/or, its absence may cause an adverse effect on crew workload. Proviso wording for "Category D" Repair Interval for second proviso set changed for consistency of intent with FOPB Policy Letter 52.

FEDERAL AVIATION ADMINISTRATION Page: XXI Revision: 6 MASTER MINIMUM EQUIPMENT LIST Date: 11/03/2004 HAWKER SIDDELEY HS-125 (SERIES 1 THROUGH 800XP) Highlights of Change ATA 24 ELECTRICAL POWER: 24-20-1 AC Main Inverters - Title changed to include parenthetical reference to applicability. Provisos reworded and expanded. 24-20-3 20-3 Standby Inverter - IAW FOPB Policy Letter 63, and the MMEL Preamble, this Item has been deleted because it is required to operate normally in order to perform Emergency Procedure(s). 24-20-5 Standby Inverter "ON" Light/ Annunciator - "Verified" changed to "confirmed" in relief statement. 24-20-8 AC Generator(s) - An "s" added to Title to account for two(2) AC Generator installations on some HS-125's. 24-21-1 115 VAC/60 Hz System - For consistency with other Items, reference to "FAA Flight Inspection Aircraft" replaced by "***" (if installed). Proviso reworded for consistency. 24-30-1 DC Voltmeter - For historical purposes, this Item's Title and pre-existent number have been restored in the MMEL. IAW FOPB Policy Letter 31, notation has been made that this Item was deleted in Revision 5. NOTE: Mention of the deletion was inadvertently omitted from the Revision 5 Remarks or Exceptions column, as well as from Revision 5 Highlights of Change. 24-30-7 Bus Tie Contactor System (Split Bus Tie Contactor Aircraft Only) - "(M)" replaced with "(O)." For clarity, provisos' re- ordered, and wording amended. 24-30-9 Battery Contactor Annunciators (Series 800 and 800XP Only) - "(M)" procedure deleted." "Confirmed to operate normally" added to both proviso sets, and item reformatted for clarity.

FEDERAL AVIATION ADMINISTRATION Page: XXII Revision: 6 MASTER MINIMUM EQUIPMENT LIST Date: 11/03/2004 HAWKER SIDDELEY HS-125 (SERIES 1 THROUGH 800XP) Highlights of Change 24-30-12 Battery Heater Muffs - Inappropriate asterisks removed. "A- three flight day" relief provisions removed. NOTE: Battery Heater Muffs are required equipment on certain models of the HS-125. When installed, their normal operation is essential to operation within certain temperature ranges. 24-30-15 FIS Power Recovery System - For consistency with other Items, reference to "FAA Flight Inspection Aircraft" replaced by "***" (if installed). Proviso reworded slightly for consistency. 24-30-17 External Power System - New Item. 24-50-1 AC Bus Fail Lights/ Annunciators - Parenthetical reference added to title to indicate that relief only applies to HS- 125's with Standby Inverter installed. Provisos "a)" and "b)" have been amended to require that named components are confirmed to operate normally before each departure. 24-50-2 26 VAC Bus Fail Annunciators - "Fail" changed to "FAIL" in both Sub-Titles. Titles in column 1 revised for accuracy. Relief provisos for both Sub-Item "-1)," and "-2" have been deleted. ATA 25 EQUIPMENT/FURNISHINGS: 25-1 Crewmember Shoulder Harness - IAW FOPB Policy Letter [PL] 31, this item and the notation of its deletion in Revision 2, have been restored to the MMEL for historical tracking. 25-10-3 Exterior Lavatory Door Ash Tray(s) - New Item added IAW Revision 2 of FOPB Policy Letter 85, dated February 7, 2000. 25-10-4 Galley Waste Receptacle(s)/Access Door(s)/Covers - New Item added IAW Revision 1 of FOPB Policy Letter 96, dated June 8, 2001. Relief Category and proviso wording modified as appropriate to present use in the HS-125.

FEDERAL AVIATION ADMINISTRATION Page: XXIII Revision: 6 MASTER MINIMUM EQUIPMENT LIST Date: 11/03/2004 HAWKER SIDDELEY HS-125 (SERIES 1 THROUGH 800XP) Highlights of Change 25-20-1 Passenger Seats (Including Seat Backs and Armrests) - An "(s)" added to Recline Mechanisms' Sub-Title to signify more than one may be installed. Proviso wording changed from "secured" to "locked" in the up-right position. "Restraining Bars," previously omitted from second Sub-Title, added. 25-20-2 Flight Inspection Panel System - For consistency with other Items, reference to "FAA Flight Inspection Aircraft" replaced by "***" (if installed). Proviso reworded for consistency. 25-4 Passenger Seat Ashtray - IAW FOPB Policy Letter 31, Item, and dispositional history, which were dropped from Revision 5, have been restored. 25-25-1 Cockpit Sun Visors - Relief Interval changed to "D" IAW FOPB Policy Letter 52. IAW FOPB Policy Letter 31, superfluous proviso wording dropped. 25-60-3 Passenger Convenience Items(s) - IAW FOPB Policy Letters 33 and 85, NOTE wording expanded to clarify that it refers to "Exterior" Lavatory Doors. 25-60-4 Observer Seat (Including Associated Equipment) - Provisos updated IAW Revision 3 of FOPB Policy Letter 56, dated January 16, 2001. 25-60-5 Emergency Vision Assurance System (EVAS) (STC # SA00892LA) - Number Installed changed to "-" (variable). ATA 26 FIRE PROTECTION: 26-15-1-1) APU Fire Detection System - Warning Bell - The "(M)" and "(O)" have been dropped and proviso "b)" wording expanded to clarify that a "qualified person" is required to continuously monitor operation of the APU from the Cockpit Control Panel.

FEDERAL AVIATION ADMINISTRATION Page: XXIV Revision: 6 MASTER MINIMUM EQUIPMENT LIST Date: 11/03/2004 HAWKER SIDDELEY HS-125 (SERIES 1 THROUGH 800XP) Highlights of Change 26-15-1-2) APU Fire Detection System - Warning Annunciator - The "(M)" and "(O)" have been dropped and proviso "b)" wording expanded to clarify that a "qualified person" is required to continuously monitor operation of the APU from the Cockpit Control Panel. 26-15-2 APU Fire Detection Test System - "OR" removed and provisos reformatted IAW FOPB Policy Letter 31. 26-20-2 APU Extinguisher Pressure Relief Discharge Indicator - "(O)" dropped from first proviso IAW MMEL Definition 15, which permits qualified and authorized personnel, other than maintenance personnel to perform (M) procedures which do not require specialized knowledge, or skill, and do not require the use of tools or test equipment. "OR" removed and provisos reformatted IAW FOPB Policy Letter 31. 26-30-1 Forward/Aft Baggage Smoke Detection Systems - Provisos revised IAW FOPB Policy Letter #108, dated October 10, 2001. 26-30-2 Lavatory Smoke Detection System - Title and provisos changed to reflect Revision 3 of FOPB Policy Letter 24, dated October 15, 2001. 26-30-3 Rear Baggage Panier Smoke Detection System - Wording of proviso "b)" amended for clarity and consistency with FOPB Policy Letter 31. ATA 27 FLIGHT CONTROLS: 27-10-1 Aileron Trim Position Indicator - "(M)" dropped. "Before each departure" added to lead statement. "Visually confirmed" added to proviso "a)." "Verified" replaced with "confirmed" in proviso "b)."

FEDERAL AVIATION ADMINISTRATION Page: XXV Revision: 6 MASTER MINIMUM EQUIPMENT LIST Date: 11/03/2004 HAWKER SIDDELEY HS-125 (SERIES 1 THROUGH 800XP) Highlights of Change 27-20-1 Rudder Trim Position Indicator - "(M)" dropped. "Before each departure" added to lead statement. "Visually confirmed" added to proviso "a)." "Verified" replaced with "confirmed" in proviso "b)." 27-20-2 Rudder Pedal Adjustment System - "(M)" added to reflect maintenance action to secure Rudder Pedals in position. Relief statement amended for clarity. 27-30-1 Electrical Elevator Trim System - IAW Revision 1 to FOPB Policy Letter 101, dated September 13, 2001, the Repair Interval has been changed to Category "B," and proviso c) has been added to reflect that failure of this system renders the autopilot inoperative. Existing provisos "a)" and "b)" reversed for clarity. For accuracy and consistency with Item 27-30-5, proviso b) changed to "Mechanical" Elevator Trim System. Since this system is not presently deferrable in the MMEL, a requirement to verify its normal operation before departure has been added. Proviso "d)" added to reflect that failure of this item will render the Mach Trim system of the Series 800XP inoperative, thus requiring adherence to 0.73 AFM maximum IMN speed limitation. For consistency, NOTE 1 wording changed to "operate normally." Inappropriate NOTE 3 has been deleted and incorporated as proviso d) of the relief statement. 27-30-2-1) Stall Warning/ Identification Systems-Series 1 Through 700, Only - "Before each departure" added to relief statement to clarify that both provisos must be accomplished at that interval. Proviso order reversed to reflect that maintenance procedure is accomplished prior to operational procedures. "Confirmed" added to proviso "b)."

FEDERAL AVIATION ADMINISTRATION Page: XXVI Revision: 6 MASTER MINIMUM EQUIPMENT LIST Date: 11/03/2004 HAWKER SIDDELEY HS-125 (SERIES 1 THROUGH 800XP) Highlights of Change 27-30-2-2) Stall Warning/Identification Systems (Series 800 and 800XP Only) - "(M)," which was erroneously removed in Revision 5, has been restored to reflect maintenance action to pull and collar circuit breakers, and deactivate warning lights which may remain ON. 27-30-4 Stall Warning Autopilot Disconnect System (Series 800 Without Mod. 253146 Installed, Only) - Parenthetical title reference amended to accurately reflect effectivity. "(O)" added and relief statement expanded to clarify that it is the stall warning disconnect function of each autopilot channel that must be confirmed to operate normally before each departure 27-30-5 Mach Trim System (Series 800XP) - In proviso "a)," the requirement to confirm its normal operation before each departure has been added. Proviso "b)" reference to AFM Speed Limitations has been expanded. 27-50-1 Flap Position Indicator (On Pilots' Instrument Panel) - Parenthetical reference added to title to clarify which cockpit-located indicator relief applies to. "Verified" replaced with "confirmed" in proviso "a)." Wording of proviso "c)" amended for clarity. 27-50-2 Flap Handle Select Position Indicator (On Control Pedestal) - Parenthetical reference added to title to clarify which cockpit-located indicator relief applies to. First relief statement permitting flaps to be used, expanded for clarity of intent. Second relief statement, covering case in which both the Flap Position Indicator and the Flap Handle Select Position Indicator are inoperative, has been expanded to conform with relief statement for Item 27-50-1, "Flap Position Indicator (On Pilots' Instrument Panel)." 27-60-1 Air Brake Position Indicator - "(s)" added to Title to coincide with variable number installed. "Before each departure" added to lead relief statement to indicate that all provisos are to be accomplished before each departure. Wording of all provisos expanded for clarity. 27-60-2 Control Column Lock System - Wording of provisos expanded for clarity of intent.

FEDERAL AVIATION ADMINISTRATION Page: XXVII Revision: 6 MASTER MINIMUM EQUIPMENT LIST Date: 11/03/2004 HAWKER SIDDELEY HS-125 (SERIES 1 THROUGH 800XP) Highlights of Change 27-60-3 Rudder Gust Lock Flapper Door - Proviso wording expanded to require that a cover be installed to protect against contamination by foreign material. ATA 28 FUEL: 28-20-1 Fuel Booster Pumps - Deleted due to current AFM requirements. 28-20-2 Wing Transfer Magnetic Indicator (Series 1 Through 400 Only) - Provisos re-written for clarity of intent, and (M) procedure deleted. 28-20-3 Fuel Transfer/Crossfeed Indicator (Series 600 Through 800XP Only) - Provisos re-written for clarity of intent, and (M) procedure deleted. 28-20-4 Ventral Tank Fuel Transfer Valve - Proviso c) revised for clarity. 28-20-5 Ventral Tank Transfer Light/Annunciator (Series 3A/RA, 3B/RA Through 800XP Only) - "OR" removed and provisos reformatted IAW FOPB Policy Letter 31. Proviso b) of second proviso set revised for clarity. 28-22-1-1) Pressure Fueling System-Series 400 Through 700, (If Installed) - Series applicability expanded for clarity. Proviso order reversed for consistency. Wording added to proviso "a)" to assure maintenance action is taken to verify that failure is not due to fuel line leakage. 28-22-1-2) Pressure Fueling System-Series 800 and 800XP, Only - Proviso order reversed for consistency. Wording added to proviso "a)" to assure maintenance action is taken to verify that failure is not due to fuel line leakage. 28-42-1 Wing Tank Fuel Content Indicators - "Wing Tank" removed as parenthetical reference and added to title. Provisos expanded and revised for clarity. [M] procedure deleted and new provisos d) and e) added. 28-42-2 Fuel Used Counter(s)/Fuel Totalizer(s) - "(s)" added to both Item titles to coincide with variable number installed ("-").

FEDERAL AVIATION ADMINISTRATION Page: XXVIII Revision: 6 MASTER MINIMUM EQUIPMENT LIST Date: 11/03/2004 HAWKER SIDDELEY HS-125 (SERIES 1 THROUGH 800XP) Highlights of Change Provisos reworded for clarity. 28-43-1 Ventral Tank "EMPTY/FULL" Indicator - "Ventral" added to proviso "a)" to indicate which fuel tank is intended. In accordance with manufacturer's procedural information, proviso "b)" added to clarify what the "(O)" procedures is intended to be. 28-43-2 Dorsal Tank "Empty/Full" Indicator (Series 600 and 700 Only) - "Dorsal" added to proviso "a)" to indicate which fuel tank is intended. In accordance with manufacturer's procedural information, proviso "b)" added to clarify what the "(O)" procedures is intended to be. 28-43-3-1) Low VMO Audible Warning System-Series 3A/RA, 3B/RA Through 400, 800 and 800XP Only - Proviso "b)" added to clarify what the "(O)" procedure is intended to be. 28-43-3-2) Low VMO Audible Warning System-Series 600 and 700, Only - Proviso "b)" added to clarify what the "(O)" procedure is intended to be. ATA 29 HYDRAULIC POWER: 29-30-1 L/R HYD LO FLOW Annunciators (Viper Engines Only) - Title amended for clarity. "Hydraulic" added to proviso "a)" to indicate which pump is intended. "Hydraulic" added to proviso "b)" to indicate which main supply indicator is intended. New proviso c) added. 29-30-2 HYD LO PRESS 1 and 2 Annunciators (TFE-731 Engines Only) - "Hydraulic" added to proviso "a)" to indicate which pump is intended. "Hydraulic" added to proviso "b)" to indicate which main supply indicator is intended. New proviso c) added. 29-30-3-1) Combined BRAKES and SUPPLY Pressure Gauge-BRAKE Pressure Indicators - BRAKES and SUPPLY capitalized in title. Provisos expanded and revised for clarity of intent. 29-30-5 AUX HYD LO LEVEL Annunciator (Series 3 Through 800XP Only) - Proviso revised slightly for clarity/consistency.

FEDERAL AVIATION ADMINISTRATION Page: XXIX Revision: 6 MASTER MINIMUM EQUIPMENT LIST Date: 11/03/2004 HAWKER SIDDELEY HS-125 (SERIES 1 THROUGH 800XP) Highlights of Change 29-30-6 Accumulator Pressure Indicators (Main and Emergency Only) - Provisos reworded for clarity of intent, and new proviso a) requirements added. (M) procedure changed to (O). 29-30-7 Thrust Reverser Accumulator Pressure Indicator - Sub-Items incorporated as parenthetical reference in title. Relief now revised to include new provisos a) and b) with proviso b) a new pre dispatch requirement. ATA 30 ICE AND RAIN PROTECTION: 30-10-2 WING/TAIL ANIT-ICE Control Switches - This Item has been substantially amended to reflect differences in system architecture between HS-125's of Series 1 through 400, which have both an ON/OFF Switch and a TIME Switch, and those of Series 600 through 800XP which have only a TIME Switch. 30-10-3 T.K.S. Quantity Indication System - "OR" removed and provisos reformatted IAW FOPB Policy Letter 31. Wording of first proviso set changed for clarity. 30-10-4 ANTI-ICE LO PRESS Annunciator (Series 800 and 800XP Only) - Superfluous "(M)" removed from first proviso set. An "s" has been added to "operates" in "b)" of first proviso set. "OR" removed and provisos reformatted IAW FOPB Policy Letter 31. 30-10-5 ANTI-ICE LO QTY Annunciator (Series 800 and 800XP Only) - "OR" removed and provisos reformatted IAW FOPB Policy Letter 31. Wording of first proviso set changed for clarity. 30-20-1 Engine Inlet Anti-icing Systems (TFE-731 Engine Aircraft Only) - Relief substantially expanded and clarified. Additional provisions granted for operating in icing conditions provided the Engine Anti-Icing Valve can be confirmed to be failed "ON"

FEDERAL AVIATION ADMINISTRATION Page: XXX Revision: 6 MASTER MINIMUM EQUIPMENT LIST Date: 11/03/2004 HAWKER SIDDELEY HS-125 (SERIES 1 THROUGH 800XP) Highlights of Change 30-20-3 MWS "ENG ICE PROT ON" White Annunciator (Series 600 and 700 Only) - "Verified" changed to "confirmed" in proviso "a)." Proviso "b)" added requiring alternate procedures for determining Engine Ant-Ice operation be established and used. 20-20-4 MWS "ICE PROT SELECTED" White Annunciator (Series 800 and 800XP Only) - "Verified" changed to "confirmed" in proviso. 30-30-2 Pitot Ammeters (Series 1 Through 400 With SB 34-140, Or Mod. 252733 Installed, Only) - Title amended by addition of parenthetical reference to appropriate Service Bulletin/ Modification effectivity. Provisos now require Pitot/Mast Heater FAIL Lights be "confirmed" to operate normally before each departure, and new proviso b) added. 30-30-3 Pitot Ammeter & Selector (Series 600 and 700 With SB 34-140, Or Mod. 252733 Installed, Or 800 and 800XP Only). Title ammended by addition of parenthetical reference to appropriate SB/Modification effectivity. Proviso now requires Pitot/Mast Heater FAIL Lights be "confirmed" to operate normally before each departure. (M) procedure deleted. 30-30-4 Pitot/Mast Heater FAIL Light(s)/ Annunciator(s) (Series 1 Through 700 With SB 34-140, Or Mod. 252733 Installed, and 800 and 800XP, Only) - Title amended to by addition of parenthetical reference to appropriate Series and Service Bulletin/Modification effectivity. Provisos now require Pitot/Mast Heater FAIL Lights be "confirmed" to operate normally before each departure. Requirement to establish and use alternate procedures for monitoring Pitot Heater function in icing conditions has also been added. 30-30-5 Static Plate Heaters (Series 700, if installed, 800 and 800XP Only) - For accuracy, parenthetical Series reference expanded by addition of "if installed" added following "700." IAW FOPB Policy Letter 84, reference, Except where enroute operations require that both operate normally," has been added to lead relief statement.

FEDERAL AVIATION ADMINISTRATION Page: XXXI Revision: 6 MASTER MINIMUM EQUIPMENT LIST Date: 11/03/2004 HAWKER SIDDELEY HS-125 (SERIES 1 THROUGH 800XP) Highlights of Change 30-30-6 Stall Vane Heaters (Series 800 and 800XP Only) - IAW FOPB Policy Letter 84, reference, "Except where enroute operations require that both operate normally," has been added to lead relief statement. New proviso "a)" added to require FAIL Annunciator of remaining normally operating Stall Vane Heater to operate normally. 30-30-7 L and R VANE HTR FAIL Annunciators (Series 800 and 800XP Only) - New Item. 30-40-1-1) Windscreen Heating System-1 Through 700 Series Only - Sub-Title wording changed for consistency. "OR" removed and provisos reformatted IAW FOPB Policy Letter 31. 30-40-1-2) Windscreen Heating System-Series 800 and 800XP Only - Superfluous "(O)" removed from first relief statement. Second "C/4/2" relief statement added for inoperative "B" Screens. 30-40-2 Windscreen Overheat Lights/Annunciators - "(M)/(O)" procedures deleted. Unnecessary numeral "1" deleted from NOTE.

FEDERAL AVIATION ADMINISTRATION Page: XXXII Revision: 6 MASTER MINIMUM EQUIPMENT LIST Date: 11/03/2004 HAWKER SIDDELEY HS-125 (SERIES 1 THROUGH 800XP) Highlights of Change ATA 31 INDICATING/RECORDING SYSTEMS: 31-30-1 Flight Data Recorder (FDR) System - Amended IAW Revision 6 to FOPB Policy Letter 87, dated July 23, 2001. Optional equipment designation [***] deleted, and proviso a) of second proviso set modified to add the words, "if installed." ATA 32 LANDING GEAR: 32-60-2 Gear Unlocked Indications - Deleted, Revision 6. Relief already provided for in item 31-50-1. ATA 33 LIGHTS: 33-20-1 Cabin Interior Light System - "Verified" replaced with "confirmed" in proviso "b)." 33-20-2 Passenger Notice System ("No Smoking Fasten Seat Belt/Return to Cabin") Signs - "OR" removed and provisos reformatted IAW FOPB Policy Letter 31. 33-20-5 EMERG LTS NOT SEL/ EMRG LTS NOT SLCT Annunciator - Title expanded to reflect nomenclature in various models of HS-125. Asterisks ("***") removed. "D" Repair Interval changed to "C" because this Item becomes part of the certification basis when aircraft interiors are added, therefore the "optional" provisions of FOPB P/L 52 are not met. Before each departure added to lead relief statement. "Verified" replaced with "confirmed" in proviso "a)." 33-40-1-2 Number in column two [2] for both proviso sets changed from a [3] to a [-] for technical accuracy. 33-40-3 Taxi Lights (Wing Mounted) - "OR's" removed and provisos reformatted IAW FOPB Policy Letter 31. 33-40-4-1) Position (Navigation) Lights-Stationary White Tail Light Amended IAW Revision 1 of FOPB Policy Letter 91, dated November 14, 2003.

FEDERAL AVIATION ADMINISTRATION Page: XXXIII Revision: 6 MASTER MINIMUM EQUIPMENT LIST Date: 11/03/2004 HAWKER SIDDELEY HS-125 (SERIES 1 THROUGH 800XP) Highlights of Change 33-40-5 Wing Illumination/Ice Light(s) - Amended IAW Revision 2 of FOPB Policy Letter 72, dated August 15, 1997. New proviso against "C" -/1 relief added to address current AFM severe icing Limitations. 33-40-8 Pulselite System - Proviso wording expanded to clarify intent of maintenance action. 33-40-10 Weight On Wheels Switch (Automatic Dim Function On Landing) - Superfluous relief statement deleted IAW FOPB Policy Letter 31. 33-50-2 Floor Proximity Lighting System - Provisos added for clarity of intent, and number in column three changed to a dash [-]. ATA 34 NAVIGATION: 34-9-1 Mach Indications - Superfluous "/" removed from Item title. 34-9-1-1) Mach Indications - Non-EFIS Equipped Aircraft - Sub-Title changed for clarity and consistency. 34-9-5 Non-Stabilized Magnetic Compass (Standby) - Repair Interval for third proviso changed to "Category B" IAW Revision 1 of FOPB Policy Letter 10, dated August 15, 1997, and number installed and required added to correct a previous editing error. 34-10-1 Mach/Airspeed Aural Warning Channels - Title revised for clarity and "B" 2/0 relief statement revised to delete the word "verified." A new proviso b) also added to address Ventral Tank conditions.

FEDERAL AVIATION ADMINISTRATION Page: XXXIV Revision: 6 MASTER MINIMUM EQUIPMENT LIST Date: 11/03/2004 HAWKER SIDDELEY HS-125 (SERIES 1 THROUGH 800XP) Highlights of Change 34-10-2 Altitude Alerting System - Wording of NOTE changed for consistency. NOTE added to second proviso set. 34-10-4 Standby Altimeter - This Item has been incorporated into new Item 34-20-9, this Revision. 34-20-1 Flight Director System(s) - "(s)" added to title to denote multiple number installed. Separate Sub-Items provided for Honeywell-equipped and Collins-equipped aircraft. 34-20-3-1) Attitude Heading Reference System (AHRS)/Inertial Reference System (IRS)-Primary AHRS/IRS - Because relief calls for not using the Autopilot, Repair Interval has been changed to "Category B" IAW Revision 1 to FOPB Policy Letter 101, dated September 13, 2001. 34-20-6 Standby Attitude Indicator - This Item has been incorporated into new Item 34-20-9, this Revision. 34-20-9 Standby Flight Instruments/ Displays - New Item. Incorporates Items 34-10-4, "Standby Altimeter," and 34-20-6, "Standby Attitude Indicator." The references to Standby Attitude Indicator have been amended IAW FOPB P/L 111. This item has also been expanded to include relief for Meggitt Secondary Flight Display Units [SFD's].

FEDERAL AVIATION ADMINISTRATION Page: XXXV Revision: 6 MASTER MINIMUM EQUIPMENT LIST Date: 11/03/2004 HAWKER SIDDELEY HS-125 (SERIES 1 THROUGH 800XP) Highlights of Change 34-32-1 ILS Offset System - For consistency, reference to "FAA Flight Inspection Aircraft" deleted, and "***" (if installed) added. Proviso wording amended for consistency. 34-40-1 Radio Altimeter System - Inoperative Radio Altimeter renders GPWS inoperative, therefore, therefore, IAW provisions of Revision 7 of FOPB Policy Letter 54, dated October 15, 2001, Relief Interval reduced to two(2) flight days, which conforms with relief for Item 34-40-4, "GPWS." 34-40-4 Ground Proximity Warning System (GPWS)/Terrain Awareness Warning System (TAWS) - Relief amended IAW Revision 7 of FOPB Policy Letter 54, dated October 15, 2001. 34-42-1 TACAN Number 2 Tuning System - For consistency, reference to "FAA Flight Inspection Aircraft" deleted, and "***" (if installed) added. Proviso wording amended for consistency. 34-43-1 ATC Transponder Attenuation System - For consistency, reference to "FAA Flight Inspection Aircraft" deleted, and "***" (if installed) added. Proviso wording amended for consistency. 34-50-2 Flight Management Systems (FMS) - "C/-/-" revised to"C/-/0" in first proviso set and new relief provisos a) and b) added. Subitem 1) NAV Data Base amended IAW FOPB Policy Letter 98, dated January 20, 1999. 34-50-8 Transponder Ident Switch - Proviso revised for clarity. 34-60-1 Traffic Collision and Avoidance System (TCAS I and TCAS II) - Amended IAW Revision 6 of FOPB Policy Letter 32, dated October 16, 2002. 34-70-1 EFIS/MFD Cooling Fans (Except Collins ProLine 21-Equipped A/C) - Sub-Title added to clarify that relief does not apply to Collins Proline 21-equipped A/C. Item reformatted for clarity. Reference to "Bearing Distance Indicator [BDI] corrects previous erroneous "DBI" reference.

FEDERAL AVIATION ADMINISTRATION Page: XXXVI Revision: 6 MASTER MINIMUM EQUIPMENT LIST Date: 11/03/2004 HAWKER SIDDELEY HS-125 (SERIES 1 THROUGH 800XP) Highlights of Change 34-70-2 EFIS/MFD OVHT Annunciators (Series 700, 800, 800XP Except Proline 21-Equipped Aircraft) - Title revised for clarity. Both provisos revised for clarity as well. 34-70-3 EFIS/MFD FAN FAIL Annunciators (Series 700, 800, 800XP Except Proline 21-Equipped aircraft) - New first proviso set added. Proviso b) of second proviso set revised for clarity and new proviso c) added. 34-70-4 Electronic Flight Displays (EFD) - "s" added to Title and parenthetical "(EFD's)" reference to signify multiple number installed. Sub-Items added and numbering scheme amended to clarify avionics suite applicability. 34-70-9 Multifunction Display Controller (Honeywell Aircraft Only) - "-Equipped" added to parenthetical Title reference for clarity and consistency. In proviso "b)," "confirmed," and "before each departure" added. In proviso "c)," "before each departure" added, and "verified' replaced with "confirmed." New proviso "d)" added requiring alternate Normal and Emergency Procedures to be established and used.

FEDERAL AVIATION ADMINISTRATION Page: XXXVII Revision: 6 MASTER MINIMUM EQUIPMENT LIST Date: 11/03/2004 HAWKER SIDDELEY HS-125 (SERIES 1 THROUGH 800XP) Highlights of Change 34-70-10 Nose Compartment Avionics Cooling System (Honeywell-Equipped Aircraft, Only) - Title expanded and parenthetical effectivity reference added for clarity. Separate relief statements for Avionics Cooling Fan, and Avionics Cooling Fan Door Implemented. 34-70-11 Electronic Checklist System - Relief already covered in item 34-70-9. 34-70-12 Nose Compartment Ventilation System (Collins Equipped Aircraft Except Pro-Line 21) - "(O)'s" replaced with "(M)'s" to reflect maintenance action required to verify normal operation of Avionics Nose Cooling Fans. NOTE: This Item was previously designated as Item 21-21-1. It was relocated from ATA Chapter 21, to ATA Chapter 34 in Revision 5. ATA 35 OXYGEN: 35-00-1 Oxygen Content Indicators - Item divided into Sub-Titles for clarity. Relief statements completely revised. 35-00-2 Oxygen Cylinders - Item divided into Sub-Titles for clarity. Separate relief now addressing both 750 and 1,400 liter bottles. 35-00-3 Barometric Valve Automatic Function - For clarity, Item retitled to incorporate previous Sub-Item. 35-10-1 Protective Breathing Equipment (PBE) - IAW Revision 1 of FOPB Policy Letter 43, dated August 15, 1997, the phrase, "or missing" has been deleted. 35-20-1 Passenger Oxygen Masks and Stowages - "OR" removed and provisos reformatted IAW FOPB Policy Letter 31.

FEDERAL AVIATION ADMINISTRATION Page: XXXVIII Revision: 6 MASTER MINIMUM EQUIPMENT LIST Date: 11/03/2004 HAWKER SIDDELEY HS-125 (SERIES 1 THROUGH 800XP) Highlights of Change ATA 38 WATER/WASTE: NOTE: This ATA Chapter, inadvertently deleted from Revision 5, has been restored. 38-10-1 Potable Water System - Relief amended IAW Revision 4 of FOPB Policy Letter 83, dated October 15, 2001. 38-10-2 Lavatory Waste System(s) - New relief added IAW Revision 4 of FOPB Policy Letter 83, dated October 15, 2001. 38-10-3 Lavatory Plug Assembly (Lavatory Doughnut) - New relief item. ATA 49 AIRBORNE AUXILIARY POWER: 49-00-1 Auxiliary Power Unit - "(O)" deleted, and proviso changed to require that inoperative APU not be used. 49-10-1 APU Air/Load Control Valve - Number Installed changed to "1." NOTE expanded for clarity of intent. Second "C/1/0" relief statement added providing that inoperative APU not be used. 49-10-2 APU Instrumentation - Relief statements for both Sub-Items changed to require that inoperative APU not be used. ATA 52 DOORS: 52-11-1 Main Entry Door Unlock Indication System - "Verified" replaced with "confirmed" in relief statement. 52-25-1 Rear Baggage Pannier Door Unlock Indications - Optional equipment designation [***] deleted. Number in column two changed to a dash [-] and first proviso set revised for clarity. New second proviso set relief added. 52-25-2 Rear Baggage Pannier Hatch Unlock Indication - Optional equipment designation [***] deleted. First proviso set revised for clarity/technical consistency. New second proviso set relief added.

FEDERAL AVIATION ADMINISTRATION Page: XXXIX Revision: 6 MASTER MINIMUM EQUIPMENT LIST Date: 11/03/2004 HAWKER SIDDELEY HS-125 (SERIES 1 THROUGH 800XP) Highlights of Change 52-70-3 Optional Door or Hatch Unlocked Annunciator - Number in column two changed to a one [1] and proviso revised for clarity/ technical accuracy. 52-70-4 Right and Left Avionics Nose Access Doors - IAW FOPB Policy Letter 31, the Item title, which was deleted in Revision 5, has been restored for historical purposes. Associated references in Remarks and Exceptions, and Highlights of Change, which were inadvertently omitted, have been added. 52-70-5 Door Locks - Item renumbered sequentially following restored Item 52-70-4 reference. 52-70-6 Ramp Guard System - Item renumbered sequentially following restored Item 52-70-4 reference. ATA 56 WINDOWS: 56-10-1 Windscreen (Panel A) (Series 1 Through 700) - An "(s)" is added to "windscreen(s)" in proviso "a)." "Relevant" (sic) in proviso "c)" replaced with more appropriate term, "Associated." NOTE: Highlights of Change for Revision 5 may have unintentionally given the impression that this entire Item had been deleted. In point of fact, the only change which occurred was dropping the word "cracked." The second half of the Highlights comment was inadvertently cut off, and should have read, "FOEB does not allow relief for cracked windows."

FEDERAL AVIATION ADMINISTRATION Page: XL Revision: 6 MASTER MINIMUM EQUIPMENT LIST Date: 11/03/2004 HAWKER SIDDELEY HS-125 (SERIES 1 THROUGH 800XP) Highlights of Change 56-10-2 Windscreens "A"or"B" (Series 800 and 800XP Only) - Letter "C" representing Relief Interval changed from lower case ("c") to upper case ("C"). An "s" is added to "windscreens" in proviso "a)." "Relevant" (sic) in sub-proviso "c)" replaced with more appropriate term, "Associated." In proviso "c)," the term "collared" (as in, "circuit breaker is pulled and collared") is substituted for "collard." NOTE: Highlights of Change for Revision 5 may have unintentionally given the impression that this entire Item had been deleted. In point of fact, the only change which occurred was dropping the word "cracked." The second half of the Highlights comment was inadvertently cut off, and should have read, "FOEB does not allow relief for cracked windows." ATA 77 ENGINE INDICATING: 77-10-2-1)-a) Engine Indications - N1 Indicators - Digital Readout(s) (Except ProLine-21-Equipped Aircraft) - Parenthetical Sub-Title added for clarity. Number Installed changed to "-" (variable). 77-10-2-2)-a) Engine Indications - N2/RPM Indicators - Digital Readout(s) - New Sub-Sub-Item added. 77-10-2-3)-a) Engine Indications - ITT/EGT Indicators - Digital Readout(s) (Except ProLine 21-Equipped Aircraft) - Parenthetical Sub-Title added for clarity. Number Installed changed to "-" (variable). 77-32-3 Climb Power Annunciators (Series 1 Through 800 With TFE-731 Engines Only) - "XP" added to 800 in Sub-Title to clarify effectivity. Number Required for Dispatch changed to "0." Proviso to establish and use of alternate procedures added IAW MMEL Definition 16.

FEDERAL AVIATION ADMINISTRATION Page: XLI Revision: 6 MASTER MINIMUM EQUIPMENT LIST Date: 11/03/2004 HAWKER SIDDELEY HS-125 (SERIES 1 THROUGH 800XP) Highlights of Change ATA 78 ENGINE EXHAUST: 78-30-1 Thrust Reversing Systems - Title revised for clarity. ATA 80 STARTING: 80-00-3 Starter Operating Annunciators (TFE-731 Engines Only) - IAW MMEL Definition 16, operational procedural references added to clarify intent of relief provisos.

FEDERAL AVIATION ADMINISTRATION Page: XLII Revision: 6 MASTER MINIMUM EQUIPMENT LIST 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 Page: XLIII Revision: 6 MASTER MINIMUM EQUIPMENT LIST 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 Page: XLIV Revision: 6 MASTER MINIMUM EQUIPMENT LIST 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 Page: XLV Revision: 6 MASTER MINIMUM EQUIPMENT LIST 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 Page: XLVI Revision: 6 MASTER MINIMUM EQUIPMENT LIST 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 Page: XLVII Revision: 6 MASTER MINIMUM EQUIPMENT LIST 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 Page: XLVIII Revision: 6 MASTER MINIMUM EQUIPMENT LIST Date: 01/31/1995 HAWKER SIDDELEY HS-125 (SERIES 1 THROUGH 800XP) Definitions Fokker aircraft are equipped with Multi Function Display System ¦ (MFDS) which provides electronic message referring to the ¦ different priority levels of system information (WARNING (red), ¦ CAUTION (amber), AWARENESS (cyan) AND STATUS (white). Any ¦ messages that affects aircraft dispatch will be at the WARNING, ¦ CAUTION or AWARENESS level. In these cases the MEL must be ¦ verified for dispatch capability and maintenance may be ¦ required. ¦ System conditions that only require maintenance are not ¦ presented on the flight deck. These maintenance ¦ indications/messages may be presented on the Maintenance & Test ¦ Panel (MAP) or the Centralized Fault Display Unit (CFDU) and by ¦ dedicated Built In Test Evaluation (BITE) of systems. ¦ 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 Page: XLVIX Revision: 6 MASTER MINIMUM EQUIPMENT LIST 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 Page: L Revision: 2 MASTER MINIMUM EQUIPMENT LIST 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 Page:LI Revision:2 MASTER MINIMUM EQUIPMENT LIST 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: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 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) Both valves are secured ¦¦ ¦ ¦ ¦ closed, ¦¦ ¦ ¦ ¦ b) Ram Air and Dump Valves are | ¦¦ ¦ ¦ ¦ confirmed to operate | ¦¦ ¦ ¦ ¦ normally before the first | ¦¦ ¦ ¦ ¦ flight of the day, | ¦¦ ¦ ¦ ¦ c) Before each departure, DUMP | ¦¦ ¦ ¦ ¦ VLV is selected OPEN, | ¦¦ ¦ ¦ ¦ d) Flight is conducted in an | ¦¦ ¦ ¦ ¦ unpressurized configuration, | ¦¦ ¦ ¦ ¦ and | ¦¦ ¦ ¦ ¦ e) Altitude limitations in | ¦¦ ¦ ¦ ¦ accordance with FAR | ¦¦ ¦ ¦ ¦ operating rules are | ¦¦ ¦ ¦ ¦ observed. | ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 21-2 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 21 AIR CONDITIONING ¦ ¦ ¦ ¦ ¦ 10-2 Engine Main Air C ¦ 2 ¦ 1 ¦ (O)One may be inoperative provided ¦¦ Valve Position ¦ ¦ ¦ both engine main air valves operate | ¦¦ Indicators ¦ ¦ ¦ normally. ¦¦ ¦ ¦ ¦ | ¦¦ C ¦ 2 ¦ 1 ¦ (O)One may be inoperative provided | ¦¦ ¦ ¦ ¦ indicator associated with the | ¦¦ ¦ ¦ ¦ operative main engine air valve | ¦¦ ¦ ¦ ¦ operates normally. ¦ ¦ C ¦ 2 ¦ 0 ¦ (M)(O)May be inoperative provided: ¦¦ ¦ ¦ ¦ a) Both valves are secured ¦¦ ¦ ¦ ¦ closed, ¦¦ ¦ ¦ ¦ b) Ram Air and Dump Valves are | ¦¦ ¦ ¦ ¦ confirmed to operate | ¦¦ ¦ ¦ ¦ normally before the first | ¦¦ ¦ ¦ ¦ flight of the day, | ¦¦ ¦ ¦ ¦ c) Before each departure, DUMP | ¦¦ ¦ ¦ ¦ VLV is selected OPEN, | ¦¦ ¦ ¦ ¦ d) Flight is conducted in an | ¦¦ ¦ ¦ ¦ unpressurized configuration, | ¦¦ ¦ ¦ ¦ and | ¦¦ ¦ ¦ ¦ e) Altitude limitations in | ¦¦ ¦ ¦ ¦ accordance with FAR | ¦¦ ¦ ¦ ¦ operating rules are | ¦¦ ¦ ¦ ¦ observed. | ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 21-3 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 21 AIR CONDITIONING ¦ ¦ ¦ ¦ ¦ 10-3 Refrigeration Unit C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided: ¦¦ System/Air Cycle ¦ ¦ ¦ a) Ram Air and Dump Valves are | ¦¦ Machine ¦ ¦ ¦ confirmed to operate | ¦¦ ¦ ¦ ¦ normally before the first | ¦¦ ¦ ¦ ¦ flight of the day, | ¦¦ ¦ ¦ ¦ b) Before each departure, both | ¦¦ ¦ ¦ ¦ MAIN AIR VALVES are selected | ¦¦ ¦ ¦ ¦ CLOSED, | ¦¦ ¦ ¦ ¦ c) Before each departure, DUMP | ¦¦ ¦ ¦ ¦ VLV is selected OPEN, | ¦¦ ¦ ¦ ¦ d) Flight is conducted in an | ¦¦ ¦ ¦ ¦ unpressurized configuration, | ¦¦ ¦ ¦ ¦ and | ¦¦ ¦ ¦ ¦ e) Altitude limitations in | ¦¦ ¦ ¦ ¦ accordance with FAR | ¦¦ ¦ ¦ ¦ operating rules are | ¦¦ ¦ ¦ ¦ observed. | ¦ ¦ 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) ¦ ¦ ¦ ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 21-4 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 21 AIR CONDITIONING ¦ ¦ ¦ ¦ ¦ 10-6 Cabin Flood Valve ¦ ¦ ¦ | ¦ ¦ 1) Two-Way Cabin C ¦ 1 ¦ 0 ¦ ¦¦ Flood Valve ¦ ¦ ¦ ¦¦ (Aircraft with- ¦ ¦ ¦ | ¦¦ out Cabin Floor ¦ ¦ ¦ | ¦¦ Valves) ¦ ¦ ¦ | ¦ ¦ 2) Cabin Flood C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided LH | ¦¦ Valve (Aircraft ¦ ¦ ¦ or RH Cabin Floor Valve is | ¦¦ with Cabin ¦ ¦ ¦ confirmed to operate normally. | ¦¦ Floor Valves) ¦ ¦ ¦ | ¦¦ C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided: | ¦¦ ¦ ¦ ¦ a) Ram Air and Dump Valves are | ¦¦ ¦ ¦ ¦ confirmed to operate | ¦¦ ¦ ¦ ¦ normally before the first | ¦¦ ¦ ¦ ¦ flight of the day, | ¦¦ ¦ ¦ ¦ b) Before each departure, DUMP | ¦¦ ¦ ¦ ¦ VLV is selected OPEN, | ¦¦ ¦ ¦ ¦ c) Flight is conducted in an | ¦¦ ¦ ¦ ¦ unpressurized configuration, | ¦¦ ¦ ¦ ¦ and | ¦¦ ¦ ¦ ¦ d) Altitude limitations in | ¦¦ ¦ ¦ ¦ accordance with FAR | ¦¦ ¦ ¦ ¦ operating rules are | ¦¦ ¦ ¦ ¦ observed. | ¦ ¦ 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: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 21-5 ¦¦ --------------------------------------------------------------------------- ¦¦ 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 21-60-7, Revision 5. ¦¦ Bypass Valve (RBV) ¦ ¦ ¦ ¦ ¦ 10-10 Overhead Air D ¦ - ¦ 0 ¦ ¦¦ Flow ¦ ¦ ¦ ¦¦ Distribution ¦ ¦ ¦ ¦¦ Vents (Punkah ¦ ¦ ¦ ¦¦ Louvers) ¦ ¦ ¦ ¦ ¦ 10-11 Cabin Floor C ¦ 2 ¦ 1 ¦ | ¦¦ Valves ¦ ¦ ¦ | ¦¦ C ¦ 2 ¦ 0 ¦ (O)May be inoperative provided | ¦¦ ¦ ¦ ¦ Cabin Flood Valve is confirmed to | ¦¦ ¦ ¦ ¦ operate normally. | ¦¦ ¦ ¦ ¦ | ¦¦ C ¦ 2 ¦ 0 ¦ (O)May be inoperative provided: | ¦¦ ¦ ¦ ¦ a) Ram Air and Dump Valves are | ¦¦ ¦ ¦ ¦ confirmed to operate | ¦¦ ¦ ¦ ¦ normally before the first | ¦¦ ¦ ¦ ¦ flight of the day, | ¦¦ ¦ ¦ ¦ b) Before each departure, DUMP | ¦¦ ¦ ¦ ¦ VLV is selected OPEN, | ¦¦ ¦ ¦ ¦ c) Flight is conducted in an | ¦¦ ¦ ¦ ¦ unpressurized configuration, | ¦¦ ¦ ¦ ¦ and | ¦¦ ¦ ¦ ¦ d) Altitude limitations in | ¦¦ ¦ ¦ ¦ accordance with FAR | ¦¦ ¦ ¦ ¦ operating rules are | ¦¦ ¦ ¦ ¦ observed. | ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 21-6 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 21 AIR CONDITIONING ¦ ¦ ¦ ¦ ¦ 10-12 Cabin Flood C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided: | ¦¦ Valve Indicator ¦ ¦ ¦ a) Cabin Flood Valve is | ¦¦ (Series 800A ¦ ¦ ¦ confirmed to operate | ¦¦ and 800XP) ¦ ¦ ¦ normally, and | ¦¦ ¦ ¦ ¦ b) Cabin Floor Valve Indicator | ¦¦ ¦ ¦ ¦ is confirmed to operate | ¦¦ ¦ ¦ ¦ normally. | ¦¦ ¦ ¦ ¦ | ¦¦ C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided: | ¦¦ ¦ ¦ ¦ a) Ram Air and Dump Valves are | ¦¦ ¦ ¦ ¦ confirmed to operate | ¦¦ ¦ ¦ ¦ normally before the first | ¦¦ ¦ ¦ ¦ flight of the day, | ¦¦ ¦ ¦ ¦ b) Before each departure, DUMP | ¦¦ ¦ ¦ ¦ VLV is selected OPEN, | ¦¦ ¦ ¦ ¦ c) Flight is conducted in an | ¦¦ ¦ ¦ ¦ unpressurized configuration, | ¦¦ ¦ ¦ ¦ and | ¦¦ ¦ ¦ ¦ d) Altitude limitations in | ¦¦ ¦ ¦ ¦ accordance with FAR | ¦¦ ¦ ¦ ¦ operating rules are | ¦¦ ¦ ¦ ¦ observed. | ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 21-7 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 21 AIR CONDITIONING ¦ ¦ ¦ ¦ ¦ 10-13 Cabin Floor C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided: | ¦¦ Valve Indicator ¦ ¦ ¦ a) Cabin Floor Valve is | ¦¦ ¦ ¦ ¦ confirmed to operate | ¦¦ ¦ ¦ ¦ normally, and | ¦¦ ¦ ¦ ¦ b) Cabin Flood Valve Indicator | ¦¦ ¦ ¦ ¦ is confirmed to operate | ¦¦ ¦ ¦ ¦ normally. | ¦¦ ¦ ¦ ¦ | ¦¦ C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided: | ¦¦ ¦ ¦ ¦ a) Ram Air and Dump Valves are | ¦¦ ¦ ¦ ¦ confirmed to operate | ¦¦ ¦ ¦ ¦ normally before the first | ¦¦ ¦ ¦ ¦ flight of the day, | ¦¦ ¦ ¦ ¦ b) Before each departure, DUMP | ¦¦ ¦ ¦ ¦ VLV is selected OPEN, | ¦¦ ¦ ¦ ¦ c) Flight is conducted in an | ¦¦ ¦ ¦ ¦ unpressurized configuration, | ¦¦ ¦ ¦ ¦ and | ¦¦ ¦ ¦ ¦ d) Altitude limitations in | ¦¦ ¦ ¦ ¦ accordance with FAR | ¦¦ ¦ ¦ ¦ operating rules are | ¦¦ ¦ ¦ ¦ observed. ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 21-8 ¦¦ --------------------------------------------------------------------------- ¦¦ 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 1 ¦ ¦ ¦ a) Prior to each departure, | ¦¦ Through 800 and ¦ ¦ ¦ Ram Air Valve is confirmed | ¦¦ C-29A) ¦ ¦ ¦ to operate normally, | ¦¦ ¦ ¦ ¦ b) Dump Valve is selected OPEN, | ¦¦ ¦ ¦ ¦ c) Flight is conducted in an | ¦¦ ¦ ¦ ¦ unpressurized configuration, | ¦¦ ¦ ¦ ¦ and | ¦¦ ¦ ¦ ¦ d) Altitude limitations in | ¦¦ ¦ ¦ ¦ accordance with FAR | ¦¦ ¦ ¦ ¦ operating rules are | ¦¦ ¦ ¦ ¦ observed. | ¦ ¦ 10-15 HP Air Valve C ¦ 2 ¦ 1 ¦ O)One may be inoperative ¦¦ (Series 1 ¦ ¦ ¦ provided: ¦¦ Through 800XP) ¦ ¦ ¦ a) Main air valve on the ¦¦ (With TFE-731 ¦ ¦ ¦ affected side is confirmed | ¦¦ Engines, Only) ¦ ¦ ¦ in the closed position, | ¦¦ ¦ ¦ ¦ b) Cockpit auxiliary heating ¦¦ ¦ ¦ ¦ system operates normally, ¦¦ ¦ ¦ ¦ and ¦¦ ¦ ¦ ¦ c) Flight is conducted at or | ¦¦ ¦ ¦ ¦ below FL 250. | ¦ ¦ C ¦ 2 ¦ 0 ¦ (O)May be inoperative provided: | ¦¦ ¦ ¦ ¦ a) Both Main Air Valves are | ¦¦ ¦ ¦ ¦ confirmed in the closed | ¦¦ ¦ ¦ ¦ position, | ¦¦ ¦ ¦ ¦ b) Ram Air and Dump Valves are | ¦¦ ¦ ¦ ¦ confirmed to operate | ¦¦ ¦ ¦ ¦ normally before the first | ¦¦ ¦ ¦ ¦ flight of the day, | ¦¦ ¦ ¦ ¦ c) Before each departure, DUMP | ¦¦ ¦ ¦ ¦ VLV is selected OPEN, | ¦¦ ¦ ¦ ¦ d) Flight is conducted in an | ¦¦ ¦ ¦ ¦ unpressurized configuration, | ¦¦ ¦ ¦ ¦ and | ¦¦ ¦ ¦ ¦ e) Altitude limitations in | ¦¦ ¦ ¦ ¦ accordance with FAR | ¦¦ ¦ ¦ ¦ operating rules are | ¦¦ ¦ ¦ ¦ observed. | ¦-------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 21-9 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 21 AIR CONDITIONING ¦ ¦ ¦ ¦ ¦ 10-16 Pressure C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided: | ¦¦ Regulating ¦ ¦ ¦ a) Prior to each departure, Ram | ¦¦ Shutoff Valve ¦ ¦ ¦ Air Valve is confirmed to | ¦¦ (PRSOV)(Series ¦ ¦ ¦ operate normally, | ¦¦ 800XP and C-29A) ¦ ¦ ¦ b) Dump Valve is selected OPEN, | ¦¦ ¦ ¦ ¦ c) RH Main Air Valve is | ¦¦ ¦ ¦ ¦ selected CLOSED, | ¦¦ ¦ ¦ ¦ d) Flight is conducted in an | ¦¦ ¦ ¦ ¦ unpressurized configuration, | ¦¦ ¦ ¦ ¦ and | ¦¦ ¦ ¦ ¦ e) Altitude limitations in | ¦¦ ¦ ¦ ¦ accordance with FAR | ¦¦ ¦ ¦ ¦ operating rules are | ¦¦ ¦ ¦ ¦ observed. | ¦ ¦ 20-1 Cabin C ¦ 1 ¦ 0 ¦ | ¦¦ Recirculating Fan ¦ ¦ ¦ | ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 21-10 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 21 AIR CONDITIONING ¦ ¦ ¦ ¦ ¦ 20-2 Flight Deck Heat C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided ¦¦ Valve/Auxiliary ¦ ¦ ¦ flight is conducted at or below FL ¦¦ Heating Valve ¦ ¦ ¦ 250. ¦ ¦ ¦ ¦ ¦ (O)May be inoperative closed ¦¦ ¦ ¦ ¦ provided: ¦¦ ¦ ¦ ¦ a) Ram Air and Dump Valves are | ¦¦ ¦ ¦ ¦ confirmed to operate | ¦¦ ¦ ¦ ¦ normally before the first | ¦¦ ¦ ¦ ¦ flight of the day, | ¦¦ ¦ ¦ ¦ b) Before each departure, DUMP | ¦¦ ¦ ¦ ¦ VLV is selected OPEN, | ¦¦ ¦ ¦ ¦ c) Flight is conducted in an | ¦¦ ¦ ¦ ¦ unpressurized configuration, | ¦¦ ¦ ¦ ¦ and | ¦¦ ¦ ¦ ¦ d) Altitude limitations in | ¦¦ ¦ ¦ ¦ accordance with FAR | ¦¦ ¦ ¦ ¦ operating rules are | ¦¦ ¦ ¦ ¦ observed. | ¦ ¦ 20-3 Flight Deck C ¦ - ¦ 0 ¦ ¦¦ Recirculating ¦ ¦ ¦ ¦¦ Fan(s) ¦ ¦ ¦ | ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 21-11 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 21 AIR CONDITIONING ¦ ¦ ¦ ¦ ¦ 20-4 Mixing Valves (TFE C ¦ 2 ¦ 1 ¦ ¦¦ 731 Engine Only) ¦ ¦ ¦ ¦¦ C ¦ 2 ¦ 0 ¦ (O)May be inoperative provided: ¦¦ ¦ ¦ ¦ a) Ram Air and Dump Valves are | ¦¦ ¦ ¦ ¦ confirmed to operate | ¦¦ ¦ ¦ ¦ normally before the first | ¦¦ ¦ ¦ ¦ flight of the day, | ¦¦ ¦ ¦ ¦ b) Before each departure, DUMP | ¦¦ ¦ ¦ ¦ VLV is selected OPEN, | ¦¦ ¦ ¦ ¦ c) Flight is conducted in an | ¦¦ ¦ ¦ ¦ unpressurized configuration, | ¦¦ ¦ ¦ ¦ and | ¦¦ ¦ ¦ ¦ d) Altitude limitations in | ¦¦ ¦ ¦ ¦ accordance with FAR | ¦¦ ¦ ¦ ¦ operating rules are | ¦¦ ¦ ¦ ¦ observed. | ¦ ¦ 21-1 Nose Compartment ¦ ¦ ¦ Relocated to 34-70-12, Revision 5. | ¦¦ Ventilation System ¦ ¦ ¦ | ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 21-12 ¦¦ --------------------------------------------------------------------------- ¦¦ 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. ¦¦ ¦ ¦ ¦ | ¦¦ C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided: | ¦¦ ¦ ¦ ¦ a) Ram Air and Dump Valves are | ¦¦ ¦ ¦ ¦ confirmed to operate | ¦¦ ¦ ¦ ¦ normally before the first | ¦¦ ¦ ¦ ¦ flight of the day, | ¦¦ ¦ ¦ ¦ b) Before each departure, DUMP | ¦¦ ¦ ¦ ¦ VLV is selected OPEN, | ¦¦ ¦ ¦ ¦ c) Flight is conducted in an | ¦¦ ¦ ¦ ¦ unpressurized configuration, | ¦¦ ¦ ¦ ¦ and | ¦¦ ¦ ¦ ¦ d) Altitude limitations in | ¦¦ ¦ ¦ ¦ accordance with FAR | ¦¦ ¦ ¦ ¦ operating rules are | ¦¦ ¦ ¦ ¦ observed. | ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 21-13 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 21 AIR CONDITIONING ¦ ¦ ¦ ¦ ¦ 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. ¦¦ ¦ ¦ ¦ | ¦¦ C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided: | ¦¦ ¦ ¦ ¦ a) Ram Air and Dump Valves are | ¦¦ ¦ ¦ ¦ confirmed to operate | ¦¦ ¦ ¦ ¦ normally before the first | ¦¦ ¦ ¦ ¦ flight of the day, | ¦¦ ¦ ¦ ¦ b) Before each departure, DUMP | ¦¦ ¦ ¦ ¦ VLV is selected OPEN, | ¦¦ ¦ ¦ ¦ c) Flight is conducted in an | ¦¦ ¦ ¦ ¦ unpressurized configuration, | ¦¦ ¦ ¦ ¦ and | ¦¦ ¦ ¦ ¦ d) Altitude limitations in | ¦¦ ¦ ¦ ¦ accordance with FAR | ¦¦ ¦ ¦ ¦ operating rules are | ¦¦ ¦ ¦ ¦ observed. | ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 21-14 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 21 AIR CONDITIONING ¦ ¦ ¦ ¦ ¦ 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. ¦¦ ¦ ¦ ¦ | ¦¦ C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided: | ¦¦ ¦ ¦ ¦ a) Ram Air and Dump Valves are | ¦¦ ¦ ¦ ¦ confirmed to operate | ¦¦ ¦ ¦ ¦ normally before the first | ¦¦ ¦ ¦ ¦ flight of the day, | ¦¦ ¦ ¦ ¦ b) Before each departure, DUMP | ¦¦ ¦ ¦ ¦ VLV is selected OPEN, | ¦¦ ¦ ¦ ¦ c) Flight is conducted in an | ¦¦ ¦ ¦ ¦ unpressurized configuration, | ¦¦ ¦ ¦ ¦ and | ¦¦ ¦ ¦ ¦ d) Altitude limitations in | ¦¦ ¦ ¦ ¦ accordance with FAR | ¦¦ ¦ ¦ ¦ operating rules are | ¦¦ ¦ ¦ ¦ observed. | ¦ ¦ 30-4 Fan Operated C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided: | ¦¦ Venturi ¦ ¦ ¦ a) Dump valve operates | ¦¦ ¦ ¦ ¦ normally, and | ¦¦ ¦ ¦ ¦ b) Cabin is confirmed | ¦¦ ¦ ¦ ¦ depressurized before the | ¦¦ ¦ ¦ ¦ Main Entry Door is opened. | ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 21-15 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 21 AIR CONDITIONING ¦ ¦ ¦ ¦ ¦ 30-5 Outflow/Safety C ¦ 2 ¦ 0 ¦ (O)May be inoperative provided: ¦¦ Valves ¦ ¦ ¦ a) Ram Air and Dump Valves are | ¦¦ ¦ ¦ ¦ confirmed to operate | ¦¦ ¦ ¦ ¦ normally before the first | ¦¦ ¦ ¦ ¦ flight of the day, | ¦¦ ¦ ¦ ¦ b) Before each departure, DUMP | ¦¦ ¦ ¦ ¦ VLV is selected OPEN, | ¦¦ ¦ ¦ ¦ c) Flight is conducted in an | ¦¦ ¦ ¦ ¦ unpressurized configuration, | ¦¦ ¦ ¦ ¦ and | ¦¦ ¦ ¦ ¦ d) Altitude limitations in | ¦¦ ¦ ¦ ¦ accordance with FAR | ¦¦ ¦ ¦ ¦ operating rules are | ¦¦ ¦ ¦ ¦ observed. | ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 21-16 ¦¦ --------------------------------------------------------------------------- ¦¦ 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) ¦ ¦ ¦ ¦ ¦ 1) Cabin Altimeter C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided: ¦¦ Indicator ¦ ¦ ¦ a) Cabin differential pressure ¦¦ ¦ ¦ ¦ indicator operates normally, ¦¦ ¦ ¦ ¦ and ¦¦ ¦ ¦ ¦ b) A chart is provided to the ¦¦ ¦ ¦ ¦ flight crew to convert cabin ¦¦ ¦ ¦ ¦ differential pressure to ¦¦ ¦ ¦ ¦ cabin altitude. ¦¦ ¦ ¦ ¦ | ¦¦ C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided: | ¦¦ ¦ ¦ ¦ a) Ram Air and Dump Valves are | ¦¦ ¦ ¦ ¦ confirmed to operate | ¦¦ ¦ ¦ ¦ normally before the first | ¦¦ ¦ ¦ ¦ flight of the day, | ¦¦ ¦ ¦ ¦ b) Before each departure, DUMP | ¦¦ ¦ ¦ ¦ VLV is selected OPEN, | ¦¦ ¦ ¦ ¦ c) Flight is conducted in an | ¦¦ ¦ ¦ ¦ unpressurized configuration, | ¦¦ ¦ ¦ ¦ and | ¦¦ ¦ ¦ ¦ d) Altitude limitations in | ¦¦ ¦ ¦ ¦ accordance with FAR | ¦¦ ¦ ¦ ¦ operating rules are | ¦¦ ¦ ¦ ¦ observed. | ¦ ¦ ¦ ¦ ¦ (Continued) ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 21-17 ¦¦ --------------------------------------------------------------------------- ¦¦ 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. ¦¦ ¦ ¦ ¦ | ¦¦ C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided: | ¦¦ ¦ ¦ ¦ a) Ram Air and Dump Valves are | ¦¦ ¦ ¦ ¦ confirmed to operate | ¦¦ ¦ ¦ ¦ normally before the first | ¦¦ ¦ ¦ ¦ flight of the day, | ¦¦ ¦ ¦ ¦ b) Before each departure, DUMP | ¦¦ ¦ ¦ ¦ VLV is selected OPEN, | ¦¦ ¦ ¦ ¦ c) Flight is conducted in an | ¦¦ ¦ ¦ ¦ unpressurized configuration, | ¦¦ ¦ ¦ ¦ and | ¦¦ ¦ ¦ ¦ d) Altitude limitations in | ¦¦ ¦ ¦ ¦ accordance with FAR | ¦¦ ¦ ¦ ¦ operating rules are | ¦¦ ¦ ¦ ¦ observed. | ¦ ¦ ¦ ¦ ¦ (Continued) ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 21-18 ¦¦ --------------------------------------------------------------------------- ¦¦ 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) ¦ ¦ ¦ ¦ ¦ 3) Cabin Rate of C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided: ¦¦ Climb Indicator ¦ ¦ ¦ a) All remaining cabin | ¦¦ ¦ ¦ ¦ pressure instruments and | ¦¦ ¦ ¦ ¦ functions of the pressuriza- | ¦¦ ¦ ¦ ¦ tion system operate | ¦¦ ¦ ¦ ¦ normally. | ¦ ¦ C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided: | ¦¦ ¦ ¦ ¦ a) Ram Air and Dump Valves are | ¦¦ ¦ ¦ ¦ confirmed to operate | ¦¦ ¦ ¦ ¦ normally before the first | ¦¦ ¦ ¦ ¦ flight of the day, | ¦¦ ¦ ¦ ¦ b) Before each departure, DUMP | ¦¦ ¦ ¦ ¦ VLV is selected OPEN, | ¦¦ ¦ ¦ ¦ c) Flight is conducted in an | ¦¦ ¦ ¦ ¦ unpressurized configuration, | ¦¦ ¦ ¦ ¦ and | ¦¦ ¦ ¦ ¦ d) Altitude limitations in | ¦¦ ¦ ¦ ¦ accordance with FAR | ¦¦ ¦ ¦ ¦ operating rules are | ¦¦ ¦ ¦ ¦ observed. | ¦ ¦ 30-9 Flow Control Valve ¦ ¦ ¦ Moved to 21-10-14, Revision 5. | ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 21-19 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 21 AIR CONDITIONING ¦ ¦ ¦ ¦ ¦ 30-10 Automatic C ¦ 2 ¦ 0 ¦ (O)May be inoperative provided: ¦¦ Pressure ¦ ¦ ¦ a) Ram Air and Dump Valves are ¦¦ Regulators ¦ ¦ ¦ confirmed to operate | ¦¦ ¦ ¦ ¦ normally before the first | ¦¦ ¦ ¦ ¦ flight of the day, | ¦¦ ¦ ¦ ¦ b) Before each departure, DUMP | ¦¦ ¦ ¦ ¦ VLV is selected OPEN, | ¦¦ ¦ ¦ ¦ c) Flight is conducted in an | ¦¦ ¦ ¦ ¦ unpressurized configuration, | ¦¦ ¦ ¦ ¦ and | ¦¦ ¦ ¦ ¦ d) Altitude limitations in | ¦¦ ¦ ¦ ¦ accordance with FAR | ¦¦ ¦ ¦ ¦ operating rules are | ¦¦ ¦ ¦ ¦ observed. | ¦ ¦ 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: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 21-20 ¦¦ --------------------------------------------------------------------------- ¦¦ 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) Ram Air and Dump Valves are | ¦¦ (Series 1 Through ¦ ¦ ¦ confirmed to operate | ¦¦ 800)/Low Limit ¦ ¦ ¦ normally before the first | ¦¦ Temp Control Valve ¦ ¦ ¦ flight of the day, | ¦¦ (Series 800XP) ¦ ¦ ¦ b) Before each departure, DUMP | ¦¦ ¦ ¦ ¦ VLV is selected OPEN, | ¦¦ ¦ ¦ ¦ c) Flight is conducted in an | ¦¦ ¦ ¦ ¦ unpressurized configuration, | ¦¦ ¦ ¦ ¦ and | ¦¦ ¦ ¦ ¦ d) Altitude limitations in | ¦¦ ¦ ¦ ¦ accordance with FAR | ¦¦ ¦ ¦ ¦ operating rules are | ¦¦ ¦ ¦ ¦ observed. | ¦ ¦ 60-5 Cabin/VIP D ¦ - ¦ 0 ¦ (O)May be inoperative provided | ¦¦ Temperature ¦ ¦ ¦ temperature control system operates ¦¦ Control Switch ¦ ¦ ¦ normally from the cockpit. ¦ ¦ 60-6 Cabin Flood ¦ ¦ ¦ Renamed, reformatted, and moved to | ¦¦ Control ¦ ¦ ¦ 21-10-6, Revision 5. | ¦¦ Valve/Flood Flow ¦ ¦ ¦ ¦¦ Valve ¦ ¦ ¦ ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 21-21 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 21 AIR CONDITIONING ¦ ¦ ¦ ¦ ¦ 60-7 Refrigeration Unit C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided: ¦¦ Bypass Valve (RBV) ¦ ¦ ¦ a) Ram Air and Dump Valves are | ¦¦ (Series 1 Through ¦ ¦ ¦ confirmed to operate | ¦¦ 800)/Cabin ¦ ¦ ¦ normally before the first | ¦¦ Temperature ¦ ¦ ¦ flight of the day, | ¦¦ Control Valve ¦ ¦ ¦ b) Before each departure, DUMP | ¦¦ (Series 800XP) ¦ ¦ ¦ VLV is selected OPEN, | ¦¦ ¦ ¦ ¦ c) Flight is conducted in an | ¦¦ ¦ ¦ ¦ unpressurized configuration, | ¦¦ ¦ ¦ ¦ and | ¦¦ ¦ ¦ ¦ d) Altitude limitations in | ¦¦ ¦ ¦ ¦ accordance with FAR | ¦¦ ¦ ¦ ¦ operating rules are | ¦¦ ¦ ¦ ¦ observed. | ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 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 C ¦ - ¦ 1 ¦ May be inoperative provided enroute | ¦¦ System(s) ¦ ¦ ¦ operations and approach minimums do | ¦¦ ¦ ¦ ¦ not require its use. | ¦ ¦ B ¦ - ¦ 0 ¦ May be inoperative provided enroute | ¦¦ ¦ ¦ ¦ operations and/or approach minimums | ¦¦ ¦ ¦ ¦ do not require autopilot use. | ¦ ¦ ¦ ¦ ¦ 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, ¦¦ ¦ ¦ ¦ d) 1 Altitude Alerter. ¦ ¦ ¦ ¦ ¦ NOTE 3: Flying below, above or ¦¦ ¦ ¦ ¦ crossing RVSM airspace ¦¦ ¦ ¦ ¦ does not require the above ¦¦ ¦ ¦ ¦ items to be operating. ¦ ¦ 10-2 Autopilot Control C ¦ 2 ¦ 1 ¦ (O)One may be inoperative provided | ¦¦ Yoke Disengage ¦ ¦ ¦ autopilot is not used at less than | ¦¦ Switches ¦ ¦ ¦ initial approach altitude. | ¦ ¦ B ¦ 2 ¦ 0 ¦ May be inoperative provided: | ¦¦ ¦ ¦ ¦ a) Autopilot is not used, and | ¦¦ ¦ ¦ ¦ b) Enroute operations and/or | ¦¦ ¦ ¦ ¦ approach minimums do not | ¦¦ ¦ ¦ ¦ require autopilot use. | ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 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 C ¦ - ¦ 0 ¦ May be inoperative provided: | ¦¦ Disconnect ¦ ¦ ¦ a) Autopilot is not used at | ¦¦ Annunciator Lights ¦ ¦ ¦ less than initial approach | ¦¦ ¦ ¦ ¦ altitude, and | ¦¦ ¦ ¦ ¦ b) All remaining A/P disengage- ¦¦ ¦ ¦ ¦ ment alerts operate ¦¦ ¦ ¦ ¦ normally. ¦ ¦ B ¦ - ¦ 0 ¦ May be inoperative provided: | ¦¦ ¦ ¦ ¦ a) Autopilot is not used, and | ¦¦ ¦ ¦ ¦ b) Enroute operations and/or | ¦¦ ¦ ¦ ¦ approach minimums do not | ¦¦ ¦ ¦ ¦ require autopilot use. | ¦ ¦ 10-4 Yaw Damper/Auto- C ¦ 1 ¦ 0 ¦ May be inoperative provided both | ¦¦ pilot Disconnect ¦ ¦ ¦ Autopilot Control Yoke Disengage | ¦¦ Switch on ¦ ¦ ¦ Switches operate normally. | ¦¦ Autopilot ¦ ¦ ¦ | ¦¦ Controller Panel ¦ ¦ ¦ | ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 22-3 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 22 AUTO FLIGHT ¦ ¦ ¦ ¦ ¦ 10-5 Touch Control C ¦ 2 ¦ 0 ¦ (O)May be inoperative provided: | ¦¦ *** Steering (TCS) ¦ ¦ ¦ a) Before each departure, TCS | ¦¦ (Honeywell Equipped ¦ ¦ ¦ is confirmed to be OFF, and | ¦¦ Aircraft Only) ¦ ¦ ¦ b) TCS is not used. | ¦¦ ¦ ¦ ¦ | ¦¦ B ¦ 2 ¦ 0 ¦ May be inoperative provided: | ¦¦ ¦ ¦ ¦ a) Autopilot is considered | ¦¦ ¦ ¦ ¦ inoperative and not used, | ¦¦ ¦ ¦ ¦ and | ¦¦ ¦ ¦ ¦ b) Enroute operations and/or | ¦¦ ¦ ¦ ¦ approach minimums do not | ¦¦ ¦ ¦ ¦ require autopilot use. | ¦ ¦ 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. ¦ ¦ 10-7 Control Yoke C ¦ 2 ¦ 1 ¦ (O) One may be inoperative provided | ¦¦ Pitch/Roll ¦ ¦ ¦ Autopilot Controller operates ¦¦ Switches (Series ¦ ¦ ¦ normally. | ¦¦ 800 and 800XP with ¦ ¦ ¦ | ¦¦ Collins A/P, only) ¦ ¦ ¦ | ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 22-4 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 22 AUTO FLIGHT ¦ ¦ ¦ ¦ ¦ 10-8 A/P Flap C ¦ - ¦ 1 ¦ | ¦¦ Annunciator(s) ¦ ¦ ¦ | ¦¦ (Honeywell C ¦ - ¦ 0 ¦ May be inoperative provided | ¦¦ Equipped Aircraft ¦ ¦ ¦ autopilot and flight director are | ¦¦ Only) ¦ ¦ ¦ not used with flaps extended. ¦ ¦ 20-1 Yaw Damper System B ¦ 1 ¦ 0 ¦ (O)May be inoperative provided the | ¦¦ ¦ ¦ ¦ airplane is operated in accordance ¦¦ ¦ ¦ ¦ with AFM Limitations. ¦ ¦ 20-2 Aileron Out-of- C ¦ 2 ¦ 1 ¦ | ¦¦ Trim Annunciators ¦ ¦ ¦ | ¦¦ (Honeywell- B ¦ 2 ¦ 0 ¦ May be inoperative provided: | ¦¦ Equipped Series ¦ ¦ ¦ a) Autopilot is not used, and | ¦¦ 800 And 800XP ¦ ¦ ¦ b) Enroute operations and/or | ¦¦ Aircraft Only) ¦ ¦ ¦ approach minimums do not | ¦¦ ¦ ¦ ¦ require autopilot use. | ¦ ¦ 20-3 Elevator Out-of- C ¦ 2 ¦ 1 ¦ | ¦¦ Trim Annunciators ¦ ¦ ¦ | ¦¦ (Honeywell- B ¦ 2 ¦ 0 ¦ May be inoperative provided: | ¦¦ Equipped Series ¦ ¦ ¦ a) Autopilot is not used, and | ¦¦ 800 And 800XP ¦ ¦ ¦ b) Enroute operations and/or | ¦¦ Aircraft Only) ¦ ¦ ¦ approach minimums do not | ¦¦ ¦ ¦ ¦ require autopilot use. | ¦ ¦ 20-4 Autopilot Trim B ¦ 2 ¦ 0 ¦ (O)May be inoperative provided: | ¦¦ Annunciators ¦ ¦ ¦ a) Autopilot is not used, and | ¦¦ (Aircraft With ¦ ¦ ¦ b) Enroute operations and/or | ¦¦ Digital Avionics ¦ ¦ ¦ approach minimums do not | ¦¦ Only) ¦ ¦ ¦ require autopilot use. | ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 22-5 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 22 AUTO FLIGHT ¦ ¦ ¦ ¦ ¦ 20-5 Autopilot Aileron B ¦ 1 ¦ 0 ¦ May be inoperative provided: | ¦¦ Trim Indicator ¦ ¦ ¦ a) Autopilot is not used, and | ¦¦ (Series 1 Through ¦ ¦ ¦ b) Enroute operations and/or | ¦¦ 700, Only) ¦ ¦ ¦ approach minimums do not | ¦¦ ¦ ¦ ¦ require autopilot use. | ¦ ¦ 20-6 Autopilot Elevator B ¦ 1 ¦ 0 ¦ May be inoperative provided: | ¦¦ Trim Indicator ¦ ¦ ¦ a) Autopilot is not used, and | ¦¦ (Series 1 Through ¦ ¦ ¦ b) Enroute operations and/or | ¦¦ 700, Only) ¦ ¦ ¦ approach minimums do not | ¦¦ ¦ ¦ ¦ require autopilot use. | ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 22-6 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 22 AUTO FLIGHT ¦ ¦ ¦ ¦ ¦ 20-7 Guidance B ¦ 1 ¦ 0 ¦ (O)May be inoperative provided: | ¦¦ Controller ¦ ¦ ¦ a) Autopilot is considered | ¦¦ (Honeywell ¦ ¦ ¦ inoperative, | ¦¦ SPZ-8000 and ¦ ¦ ¦ b) Enroute operations and/or | ¦¦ Collins APS-85 and ¦ ¦ ¦ approach minimums do not | ¦¦ Collins Proline 21 ¦ ¦ ¦ require autopilot/Guidance | ¦¦ Equipped Aircraft) ¦ ¦ ¦ Controller use, and | ¦¦ ¦ ¦ ¦ c) For 800XP aircraft, 0.73 IMN | ¦¦ ¦ ¦ ¦ is not exceeded unless Mach | ¦¦ ¦ ¦ ¦ Trim operates normally and | ¦¦ ¦ ¦ ¦ is used. | ¦ ¦ ¦ ¦ ¦ NOTE 1: Autopilot and yaw damper ¦¦ ¦ ¦ ¦ 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, ¦¦ ¦ ¦ ¦ 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 ¦ ¦ ¦ This Item moved to ATA 27-30-5, ¦¦ ¦ ¦ ¦ Revision 5. ¦ ¦ 20-9 Mode Select Panel B ¦ - ¦ 0 ¦ May be inoperative provided: | ¦¦ ¦ ¦ ¦ a) Autopilot is not used, and | ¦¦ ¦ ¦ ¦ b) Enroute operations and/or | ¦¦ ¦ ¦ ¦ approach minimums do not | ¦¦ ¦ ¦ ¦ require autopilot use. | ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 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: ¦¦ Units (RMU's)/ ¦ ¦ ¦ a) Inoperative Unit is not | ¦¦ Radio Tuning Units ¦ ¦ ¦ powered by an Emergency Bus, | ¦¦ (RTU's) ¦ ¦ ¦ or equivalent, and is not | ¦¦ ¦ ¦ ¦ required to accomplish | ¦¦ ¦ ¦ ¦ Emergency Procedures, | ¦¦ ¦ ¦ ¦ b) Remaining RMU/RTU operates ¦¦ ¦ ¦ ¦ normally, and ¦¦ ¦ ¦ ¦ b) Alternate procedures are ¦¦ ¦ ¦ ¦ established and used. ¦ ¦ 10-1 Communications D ¦ - ¦ - ¦ Any in excess of those required by ¦¦ System (VHF, HF, ¦ ¦ ¦ FAR may be inoperative provided | ¦¦ UHF) ¦ ¦ ¦ they are not powered by the ¦¦ ¦ ¦ ¦ Emergency AC Bus (XE), or Emergency | ¦¦ ¦ ¦ ¦ DC Bus (PE), and are not required | ¦¦ ¦ ¦ ¦ for emergency procedures. ¦ ¦ 1) VHF Comm ¦ ¦ ¦ | ¦¦ Control Panels ¦ ¦ ¦ | ¦ ¦ a) Frequency C ¦ - ¦ 0 ¦ ¦¦ Transfer ¦ ¦ ¦ ¦¦ Light ¦ ¦ ¦ ¦ ¦ b) Frequency C ¦ - ¦ 0 ¦ ¦¦ Transfer ¦ ¦ ¦ ¦¦ Switch ¦ ¦ ¦ ¦ ¦ c) Frequency C ¦ - ¦ 2 ¦ | ¦¦ Selector Knob ¦ ¦ ¦ ¦ ¦ d) Frequency C ¦ - ¦ 2 ¦ | ¦¦ Indication ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ (Continued) ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 23-2 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 23 COMMUNICATIONS ¦ ¦ ¦ ¦ ¦ 10-1 Communications ¦ ¦ ¦ ¦¦ System (VHF, HF, ¦ ¦ ¦ ¦¦ UHF) (Cont'd) ¦ ¦ ¦ ¦ ¦ 2) High Frequency C ¦ - ¦ 1 ¦ (O)May be inoperative while con- ¦¦ (HF) Communica- ¦ ¦ ¦ ducting operations that require two ¦¦ tion System(s) ¦ ¦ ¦ Long Range Communication Systems | ¦¦ ¦ ¦ ¦ (LRCS) provided: | ¦¦ ¦ ¦ ¦ a) SATCOM (High or Low Gain) ¦¦ ¦ ¦ ¦ Data Link system operates ¦¦ ¦ ¦ ¦ normally, and ¦¦ ¦ ¦ ¦ b) SATCOM Data Link communica- ¦¦ ¦ ¦ ¦ tion operates normally over ¦¦ ¦ ¦ ¦ the intended route of ¦¦ ¦ ¦ ¦ flight. ¦ ¦ D ¦ - ¦ - ¦ Any in excess of those required by ¦¦ ¦ ¦ ¦ FAR may be inoperative. ¦ ¦ 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 ¦ ¦ ¦ Deleted, Revision 6. | ¦¦ Controller ¦ ¦ ¦ ¦¦ (Clearance ¦ ¦ ¦ ¦¦ Delivery Unit) ¦ ¦ ¦ ¦ ¦ 20-1 Selective Call C ¦ - ¦ 0 ¦ ¦¦ *** System (SELCAL) ¦ ¦ ¦ ¦ ¦ 20-2 ACARS System C ¦ 1 ¦ 0 ¦ (O)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: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 23-3 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 23 COMMUNICATIONS ¦ ¦ ¦ ¦ ¦ 20-3 AFIS (VHF/SAT) C ¦ - ¦ 0 ¦ (O)May be inoperative provided | ¦¦ *** ¦ ¦ ¦ alternate procedures are ¦¦ ¦ ¦ ¦ established and used. ¦ ¦ 30-1 Passenger Address ¦ ¦ ¦ ¦¦ System ¦ ¦ ¦ ¦ ¦ 1) Passenger C ¦ 1 ¦ 0 ¦ (0)May be inoperative provided: ¦¦ Configuration ¦ ¦ ¦ a) Passenger Address System is | ¦¦ ¦ ¦ ¦ not required by FAR, and | ¦¦ ¦ ¦ ¦ b) Alternate normal and emer- ¦¦ ¦ ¦ ¦ gency procedures, and/or ¦¦ ¦ ¦ ¦ operating restrictions are ¦¦ ¦ ¦ ¦ established and used. ¦ ¦ ¦ ¦ ¦ NOTE: Any station function(s) that | ¦¦ ¦ ¦ ¦ operates normally may be | ¦¦ ¦ ¦ ¦ used. | ¦ ¦ 2) Cargo C ¦ 1 ¦ 0 ¦ May be inoperative provided ¦¦ Configuration ¦ ¦ ¦ alternate normal and emergency ¦¦ ¦ ¦ ¦ procedures, and/or operating ¦¦ ¦ ¦ ¦ restrictions are established and ¦¦ ¦ ¦ ¦ used. ¦ ¦ 30-2 Cabin Chimes C ¦ - ¦ 0 ¦ (O)May be inoperative provided ¦¦ ¦ ¦ ¦ Passenger Address system operates ¦¦ ¦ ¦ ¦ normally. ¦¦ ¦ ¦ ¦ | ¦¦ C ¦ - ¦ 0 ¦ (O)May be inoperative provided | ¦¦ ¦ ¦ ¦ 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 ¦ ¦ ¦ ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 23-4 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 23 COMMUNICATIONS ¦ ¦ ¦ ¦ ¦ 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 ¦ - ¦ - ¦ Any in excess of those required by | ¦¦ *** Transmitter (ELT) ¦ ¦ ¦ FAR may be inoperative. | ¦ ¦ 40-1 Crewmember ¦ ¦ ¦ | ¦¦ Interphone System ¦ ¦ ¦ | ¦¦ ¦ ¦ ¦ | ¦¦ 1) Flight Deck to C ¦ - ¦ 0 ¦ (0)May be inoperative provided: | ¦¦ Cabin, Cabin to ¦ ¦ ¦ a) Crewmember Interphone System | ¦¦ Flight Deck ¦ ¦ ¦ is not required by FAR, and | ¦¦ Function(s) ¦ ¦ ¦ b) Alternate normal and emer- | ¦¦ ¦ ¦ ¦ gency procedures, and/or | ¦¦ ¦ ¦ ¦ operating restrictions are | ¦¦ ¦ ¦ ¦ established and used. | ¦¦ ¦ ¦ ¦ | ¦¦ ¦ ¦ ¦ NOTE: Any station function(s) that | ¦¦ ¦ ¦ ¦ operates normally may be | ¦¦ ¦ ¦ ¦ used. | ¦¦ ¦ ¦ ¦ | ¦¦ 2) Flight Deck to C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided | ¦¦ Ground Function ¦ ¦ ¦ alternate normal and emergency | ¦¦ ¦ ¦ ¦ procedures are established and | ¦¦ ¦ ¦ ¦ used. | ¦¦ ¦ ¦ ¦ | ¦¦ D ¦ 1 ¦ 0 ¦ May be inoperative provided | ¦¦ ¦ ¦ ¦ procedures do not require its use. | ¦ ¦ 50-1 Headsets C ¦ - ¦ 1 ¦ One may be inoperative at either ¦¦ ¦ ¦ ¦ pilot's station provided speaker ¦¦ ¦ ¦ ¦ system operates normally. ¦ ¦ D ¦ - ¦ - ¦ Any in excess of those required by | ¦¦ ¦ ¦ ¦ FAR may be inoperative. | ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 23-5 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 23 COMMUNICATIONS ¦ ¦ ¦ ¦ ¦ 50-2 Microphones D ¦ - ¦ - ¦ Any in excess of those required by | ¦¦ ¦ ¦ ¦ FAR may be inoperative. ¦ ¦ 50-3 Boom Microphones ¦ ¦ ¦ ¦ ¦ 1) Airplanes with A ¦ - ¦ 0 ¦ May be inoperative provided: | ¦¦ Cockpit Voice ¦ ¦ ¦ a) Flight Data Recorder (FDR), ¦¦ Recorder ¦ ¦ ¦ if installed, operates | ¦¦ Equipped To ¦ ¦ ¦ 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) Airplanes with D ¦ - ¦ 0 ¦ Any in excess of those required by | ¦¦ Cockpit Voice ¦ ¦ ¦ FAR may be inoperative. ¦¦ Recorder Not ¦ ¦ ¦ ¦¦ 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 Pilot- C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided | ¦¦ *** to-Pilot "Hot Mic" ¦ ¦ ¦ alternate pilot to pilot | ¦¦ Interphone System ¦ ¦ ¦ communication procedures are | ¦¦ ¦ ¦ ¦ established and used. | ¦ ¦ 60-1 Static Dischargers C ¦ - ¦ - ¦ One discharger from each control | ¦¦ ¦ ¦ ¦ surface or structural area may be | ¦¦ ¦ ¦ ¦ damaged or missing. | ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 23-6 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 23 COMMUNICATIONS ¦ ¦ ¦ ¦ ¦ 60-2 Surface Bond ¦ ¦ ¦ | ¦¦ Straps ¦ ¦ ¦ | ¦ ¦ 1) Ailerons and C ¦ 12 ¦ 4 ¦ (O)Two may be broken or missing per | ¦¦ Aileron Tabs ¦ ¦ ¦ surface provided: | ¦¦ ¦ ¦ ¦ a) Condition of the remaining | ¦¦ ¦ ¦ ¦ straps is confirmed to be | ¦¦ ¦ ¦ ¦ satisfactory prior to each | ¦¦ ¦ ¦ ¦ departure, | ¦¦ ¦ ¦ ¦ b) Aircraft is not flown in | ¦¦ ¦ ¦ ¦ precipitation, and | ¦¦ ¦ ¦ ¦ c) Aircraft is not flown within | ¦¦ ¦ ¦ ¦ 50 nautical miles of active | ¦¦ ¦ ¦ ¦ or potential lightning | ¦¦ ¦ ¦ ¦ activity. | ¦ ¦ 2) Airbrakes C ¦ 8 ¦ 4 ¦ (O)One may be broken or missing per | ¦¦ (Upper and ¦ ¦ ¦ surface provided: | ¦¦ Lower) ¦ ¦ ¦ a) Condition of the remaining | ¦¦ ¦ ¦ ¦ strap is confirmed to be | ¦¦ ¦ ¦ ¦ satisfactory prior to each | ¦¦ ¦ ¦ ¦ departure, | ¦¦ ¦ ¦ ¦ b) Aircraft is not flown in | ¦¦ ¦ ¦ ¦ precipitation, and | ¦¦ ¦ ¦ ¦ c) Aircraft is not flown within | ¦¦ ¦ ¦ ¦ 50 nautical miles of active | ¦¦ ¦ ¦ ¦ or potential lightning | ¦¦ ¦ ¦ ¦ activity. | ¦ ¦ ¦ ¦ ¦ (Continued) | ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 23-7 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 23 COMMUNICATIONS ¦ ¦ ¦ ¦ ¦ 60-2 Surface Bond ¦ ¦ ¦ | ¦¦ Straps (Cont'd) ¦ ¦ ¦ | ¦ ¦ 3) Flaps C ¦ 4 ¦ 2 ¦ (O)One may be broken or missing per | ¦¦ ¦ ¦ ¦ surface provided: | ¦¦ ¦ ¦ ¦ a) Condition of the remaining | ¦¦ ¦ ¦ ¦ strap is confirmed to be | ¦¦ ¦ ¦ ¦ satisfactory prior to each | ¦¦ ¦ ¦ ¦ departure, | ¦¦ ¦ ¦ ¦ b) Aircraft is not flown in | ¦¦ ¦ ¦ ¦ precipitation, and | ¦¦ ¦ ¦ ¦ c) Aircraft is not flown within | ¦¦ ¦ ¦ ¦ 50 nautical miles of active | ¦¦ ¦ ¦ ¦ or potential lightning | ¦¦ ¦ ¦ ¦ activity. | ¦ ¦ 4) Nose and Main C ¦ 4 ¦ 0 ¦ (O)May be broken or missing | ¦¦ Gear Doors ¦ ¦ ¦ provided aircraft is not flown | ¦¦ ¦ ¦ ¦ within 50 nautical miles of active | ¦¦ ¦ ¦ ¦ or potential lightning activity. | ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 23-8 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 23 COMMUNICATIONS ¦ ¦ ¦ ¦ ¦ 70-1 Cockpit Voice C ¦ - ¦ 0 ¦ As required by FAR ¦¦ Recorder (CVR) ¦ ¦ ¦ | ¦ ¦ 1) Airplanes with A ¦ - ¦ 0 ¦ May be inoperative provided: | ¦¦ Cockpit Voice ¦ ¦ ¦ a) Flight Data Recorder (FDR), | ¦¦ Recorder ¦ ¦ ¦ if installed, operates | ¦¦ Equipped To ¦ ¦ ¦ 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) Airplanes with D ¦ - ¦ 0 ¦ Any in excess of those required by | ¦¦ Cockpit Voice ¦ ¦ ¦ FAR may be inoperative. | ¦¦ Recorder Not ¦ ¦ ¦ ¦¦ Equipped To ¦ ¦ ¦ ¦¦ Record Boom ¦ ¦ ¦ ¦¦ Microphone ¦ ¦ ¦ ¦ ¦ 70-2 Flight Phone ¦ ¦ ¦ ¦¦ *** ¦ ¦ ¦ ¦¦ 1) Cockpit D ¦ - ¦ 0 ¦ ¦ ¦ 2) Cabin D ¦ - ¦ 0 ¦ ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 23-9 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 23 COMMUNICATIONS ¦ ¦ ¦ ¦ ¦ 70-3 Satellite C ¦ - ¦ 0 ¦ (O)May be inoperative for | ¦¦ *** Communications ¦ ¦ ¦ operations requiring Long Range | ¦¦ Systems (SATCOM) ¦ ¦ ¦ Communications Systems (LCRS) | ¦¦ ¦ ¦ ¦ provided: | ¦¦ ¦ ¦ ¦ a) Two High Frequency (HF) | ¦¦ ¦ ¦ ¦ radio systems are installed | ¦¦ ¦ ¦ ¦ and operate normally, and | ¦¦ ¦ ¦ ¦ b) Alternate procedures are | ¦¦ ¦ ¦ ¦ established and used. | ¦¦ ¦ ¦ ¦ | ¦¦ D ¦ - ¦ 0 ¦ Any in excess of those required by | ¦¦ ¦ ¦ ¦ FAR may be inoperative. | ¦ ¦ 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: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 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: | ¦¦ (Aircraft Equipped ¦ ¦ ¦ a) Standby inverter is | ¦¦ with Dual AC ¦ ¦ ¦ confirmed to operate | ¦¦ Generators and a ¦ ¦ ¦ normally before each | ¦¦ Standby Inverter, ¦ ¦ ¦ departure, | ¦¦ Only) ¦ ¦ ¦ b) Both AC Generators operate | ¦¦ ¦ ¦ ¦ normally, and | ¦¦ ¦ ¦ ¦ c) Flight is not conducted in | ¦¦ ¦ ¦ ¦ known or forecast icing | ¦¦ ¦ ¦ ¦ conditions. | ¦ ¦ 20-3 Standby Inverter ¦ ¦ ¦ Deleted, Revision 6. | ¦ ¦ 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 confirmed 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: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 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(s) ¦ ¦ ¦ | ¦ ¦ 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: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 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 ¦ ¦ ¦ cedures do not require its use. | ¦¦ ¦ ¦ ¦ | ¦ ¦ 30-1 DC Voltmeter ¦ ¦ ¦ Deleted, Revision 5. | ¦ ¦ 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 Only) ¦ ¦ ¦ normally. ¦ ¦ 30-7 Bus Tie Contactor C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided: | ¦¦ System (Split Bus ¦ ¦ ¦ a) Both engine driven DC gener- | ¦¦ Tie Contactor ¦ ¦ ¦ ators operate normally, ¦¦ Aircraft Only) ¦ ¦ ¦ b) Bus Tie contactor is | ¦¦ ¦ ¦ ¦ confirmed to be open before | ¦¦ ¦ ¦ ¦ each departure, and ¦¦ ¦ ¦ ¦ c) PS1 and PS2 voltage is | ¦¦ ¦ ¦ ¦ confirmed to be normal | ¦¦ ¦ ¦ ¦ before each departure. | ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 24-4 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 24 ELECTRICAL POWER ¦ ¦ ¦ ¦ ¦ 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 ¦ (O)One may be inoperative provided | ¦¦ Annunciators ¦ ¦ ¦ before each departure: | ¦¦ Series 800 and ¦ ¦ ¦ a) Emergency contactor is | ¦¦ 800XP Only) ¦ ¦ ¦ confirmed to operate | ¦¦ ¦ ¦ ¦ normally, and | ¦¦ ¦ ¦ ¦ b) Battery contactor is | ¦¦ ¦ ¦ ¦ confirmed to operate | ¦¦ ¦ ¦ ¦ normally. | ¦ ¦ 30-10 Emergency Power ¦ ¦ ¦ Deleted Revision 5. ¦¦ Packs ¦ ¦ ¦ ¦ ¦ 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. ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 24-5 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 24 ELECTRICAL POWER ¦ ¦ ¦ ¦ ¦ 30-12 Battery Heater C ¦ 2 ¦ 0 ¦ (O)May be inoperative provided: | ¦¦ Muffs ¦ ¦ ¦ a) Battery temperature gauge ¦¦ ¦ ¦ ¦ operates normally, and ¦¦ ¦ ¦ ¦ b) Battery temperature is ¦¦ ¦ ¦ ¦ monitored by the flightcrew ¦¦ ¦ ¦ ¦ to ensure temperature ¦¦ ¦ ¦ ¦ remains above -10 degrees C ¦¦ ¦ ¦ ¦ at all times. | ¦ ¦ 30-15 FIS Power C ¦ 1 ¦ 0 ¦ May be inoperative provided pro- ¦¦ *** Recovery System ¦ ¦ ¦ cedures do not require its use. | ¦ ¦ 30-17 External Power D ¦ 1 ¦ 0 ¦ | ¦¦ System ¦ ¦ ¦ | ¦ ¦ 50-1 AC Bus Fail C ¦ 3 ¦ 2 ¦ (O)One may be inoperative provided: ¦¦ Lights/ ¦ ¦ ¦ a) Standby inverter is ¦¦ Annunciators ¦ ¦ ¦ confirmed to operate | ¦¦ (Standby Inverter- ¦ ¦ ¦ normally before each | ¦¦ Equipped Aircraft, ¦ ¦ ¦ departure, | ¦¦ Only) ¦ ¦ ¦ b) Inverter associated with the | ¦¦ ¦ ¦ ¦ inoperative light/annun- ¦¦ ¦ ¦ ¦ ciator is confirmed to | ¦¦ ¦ ¦ ¦ operate normally before each | ¦¦ ¦ ¦ ¦ departure, and ¦¦ ¦ ¦ ¦ c) Voltmeter operates normally. ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 24-6 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 24 ELECTRICAL POWER ¦ ¦ ¦ ¦ ¦ 50-2 26 VAC Bus Fail ¦ ¦ ¦ ¦¦ *** Annunciators ¦ ¦ ¦ ¦ ¦ 1) INST 1 FAIL C ¦ 1 ¦ 0 ¦ | ¦¦ ¦ ¦ ¦ | ¦ ¦ 2) INST 2 FAIL C ¦ 1 ¦ 0 ¦ | ¦¦ ¦ ¦ ¦ | ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 25-1 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 25 EQUIPMENT/FURNISHINGS ¦ ¦ ¦ ¦ ¦ 1. Crewmember Shoulder ¦ ¦ ¦ Deleted, Revision 2. | ¦¦ Harness ¦ ¦ ¦ ¦ ¦ 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. ¦ ¦ 10-3 Exterior Lavatory A ¦ 1 ¦ 0 ¦ May be missing provided it is | ¦¦ Door Ash Tray(s) ¦ ¦ ¦ replaced within 3 calendar days. | ¦ ¦ 10-4 Galley Waste D ¦ - ¦ - ¦ May be inoperative provided: | ¦¦ Receptacle(s)/ ¦ ¦ ¦ a) Container is empty and | ¦¦ Access Door(s)/ ¦ ¦ ¦ access is secured to prevent | ¦¦ Covers ¦ ¦ ¦ waste introduction into | ¦¦ ¦ ¦ ¦ compartment, and | ¦¦ ¦ ¦ ¦ b) Sufficient galley waste | ¦¦ ¦ ¦ ¦ receptacles are available to | ¦¦ ¦ ¦ ¦ accommodate all waste that | ¦¦ ¦ ¦ ¦ may be generated on a | ¦¦ ¦ ¦ ¦ flight. | ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 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 ¦ ¦ ¦ Emergency Exit, ¦¦ Armrests) ¦ ¦ ¦ b) Seat does not restrict any ¦¦ ¦ ¦ ¦ passenger from access to the ¦¦ ¦ ¦ ¦ main aircraft aisle, and ¦¦ ¦ ¦ ¦ c) Affected seat(s) are blocked ¦¦ ¦ ¦ ¦ and placarded "DO NOT ¦¦ ¦ ¦ ¦ OCCUPY" ¦ ¦ ¦ ¦ ¦ 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(s) ¦ ¦ ¦ occupied provided seat is locked in | ¦¦ ¦ ¦ ¦ the up-right position. ¦ ¦ 2) Underseat C ¦ - ¦ - ¦ (O)May be inoperative provided: ¦¦ Baggage ¦ ¦ ¦ a) Baggage is not stowed under ¦¦ Restraining ¦ ¦ ¦ seat with inoperative | ¦¦ Bars ¦ ¦ ¦ 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: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 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 ¦ ¦ ¦ cedures do not require its use. | ¦ ¦ 4. Passenger Seat ¦ ¦ ¦ Moved to 25-7, Rev. 2. Incorporated | ¦¦ Ashtray ¦ ¦ ¦ into 25-60-3, Passenger Convenience | ¦¦ ¦ ¦ ¦ Items, Rev.4. | ¦ ¦ 25-1 Cockpit Sun Visors D ¦ - ¦ 0 ¦ | ¦ ¦ 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: Exterior Lavatory Door Ash | ¦¦ ¦ ¦ ¦ Trays are not considered ¦¦ ¦ ¦ ¦ convenience items. ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 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, and ¦¦ ¦ ¦ ¦ b) Repairs are made within two | ¦¦ ¦ ¦ ¦ flight days. | ¦¦ ¦ ¦ ¦ | ¦¦ A ¦ - ¦ - ¦ May be inoperative provided: | ¦¦ ¦ ¦ ¦ a) Required minimum safety | ¦¦ ¦ ¦ ¦ equipment (safety belt and | ¦¦ ¦ ¦ ¦ oxygen) is available, | ¦¦ ¦ ¦ ¦ b) Seat is acceptable to the | ¦¦ ¦ ¦ ¦ FAA Inspector for | ¦¦ ¦ ¦ ¦ performance of official | ¦¦ ¦ ¦ ¦ duties, and | ¦¦ ¦ ¦ ¦ c) Repairs are made within two | ¦¦ ¦ ¦ ¦ flight days. | ¦¦ ¦ ¦ ¦ | ¦¦ ¦ ¦ ¦ NOTE 1: These provisos are | ¦¦ ¦ ¦ ¦ intended to provide for | ¦¦ ¦ ¦ ¦ occupancy of the above | ¦¦ ¦ ¦ ¦ seat by an FAA Inspector | ¦¦ ¦ ¦ ¦ when the minimum safety | ¦¦ ¦ ¦ ¦ equipment (oxygen and | ¦¦ ¦ ¦ ¦ safety belt) is functional | ¦¦ ¦ ¦ ¦ and the Inspector | ¦¦ ¦ ¦ ¦ determines the conditions | ¦¦ ¦ ¦ ¦ to be acceptable. | ¦ ¦ ¦ ¦ ¦ NOTE 2: The Pilot-in-Command will | ¦¦ ¦ ¦ ¦ determine if the minimum | ¦¦ ¦ ¦ ¦ safety equipment is | ¦¦ ¦ ¦ ¦ functional for other | ¦¦ ¦ ¦ ¦ person(s) authorized to | ¦¦ ¦ ¦ ¦ occupy an observer seat. | ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 25-5 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 25 EQUIPMENT/FURNISHINGS ¦ ¦ ¦ ¦ ¦ 60-5 Emergency Vision C ¦ - ¦ 0 ¦ | ¦¦ *** Assurance System ¦ ¦ ¦ ¦¦ (EVAS) (STC ¦ ¦ ¦ ¦¦ #SA00892LA) ¦ ¦ ¦ ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 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 HP cock ¦¦ Through 700 ¦ ¦ ¦ lights operate normally. ¦¦ Only ¦ ¦ ¦ ¦ ¦ 2) Series 800 and C ¦ - ¦ 0 ¦ May be inoperative provided HP cock ¦¦ 800XP Only ¦ ¦ ¦ lights operate normally. ¦ ¦ 10-2 HP Cock Fire C ¦ 2 ¦ 0 ¦ May be inoperative provided engine ¦¦ Warning Lights ¦ ¦ ¦ fire warning system operates ¦¦ ¦ ¦ ¦ normally. ¦ ¦ 15-1 APU Fire Detection C ¦ 1 ¦ 0 ¦ May be inoperative provided APU is ¦¦ System ¦ ¦ ¦ not used. ¦ ¦ 1) Warning Bell C ¦ 1 ¦ 0 ¦ May be inoperative for ground | ¦¦ ¦ ¦ ¦ operations provided: ¦¦ ¦ ¦ ¦ a) APU Fire warning annunciator ¦¦ ¦ ¦ ¦ operates normally, and ¦¦ ¦ ¦ ¦ b) System is continuously ¦¦ ¦ ¦ ¦ monitored by a qualified | ¦¦ ¦ ¦ ¦ person from the cockpit | ¦¦ ¦ ¦ ¦ control panel. ¦ ¦ 2) Warning C ¦ 1 ¦ 0 ¦ May be inoperative for ground | ¦¦ Annunciator ¦ ¦ ¦ operations provided: ¦¦ ¦ ¦ ¦ a) APU Fire warning bell ¦¦ ¦ ¦ ¦ operates normally, and ¦¦ ¦ ¦ ¦ b) System is continuously ¦¦ ¦ ¦ ¦ monitored by a qualified | ¦¦ ¦ ¦ ¦ person from the cockpit | ¦¦ ¦ ¦ ¦ control panel. ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 26-2 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 26 FIRE PROTECTION ¦ ¦ ¦ ¦ ¦ 15-2 APU Fire Detection C ¦ 1 ¦ 0 ¦ (M)May be inoperative provided: ¦¦ Test System ¦ ¦ ¦ a) Failure is verified to be in ¦¦ ¦ ¦ ¦ the light circuit, and ¦¦ ¦ ¦ ¦ b) System operation is verified ¦¦ ¦ ¦ ¦ once each flight day. ¦¦ ¦ ¦ ¦ | ¦¦ C ¦ 1 ¦ 0 ¦ May be inoperative provide APU is | ¦¦ ¦ ¦ ¦ not used. ¦ ¦ 20-1 APU Fire C ¦ 1 ¦ 0 ¦ May be inoperative provided APU is ¦¦ Extinguisher ¦ ¦ ¦ not used. ¦¦ System ¦ ¦ ¦ ¦ ¦ 20-2 APU Extinguisher C ¦ 1 ¦ 0 ¦ (M)May be missing provided | ¦¦ Pressure Relief ¦ ¦ ¦ Indicator readings or other | ¦¦ Discharge ¦ ¦ ¦ acceptable means are used to verify ¦¦ Indicator ¦ ¦ ¦ adequate charge. ¦¦ ¦ ¦ ¦ | ¦¦ C ¦ 1 ¦ 0 ¦ May be inoperative provided APU is | ¦¦ ¦ ¦ ¦ not used. ¦ ¦ 20-3 Engine Fire C ¦ 2 ¦ 0 ¦ (M)May be inoperative provided an ¦¦ Extinguisher ¦ ¦ ¦ acceptable procedure is used to ¦¦ Relief Discharge ¦ ¦ ¦ verify bottle charge is adequate ¦¦ Indicators ¦ ¦ ¦ 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 functional ¦¦ ¦ ¦ ¦ unit, and ¦¦ ¦ ¦ ¦ b) Required distribution is ¦¦ ¦ ¦ ¦ maintained. ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 26-3 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 26 FIRE PROTECTION ¦ ¦ ¦ ¦ ¦ 30-1 Forward/Aft C ¦ - ¦ 0 ¦ (O)May be inoperative provided | ¦¦ Baggage Smoke ¦ ¦ ¦ procedures are established and used | ¦¦ Detection Systems ¦ ¦ ¦ to ensure the associated | ¦¦ ¦ ¦ ¦ compartment remains empty, or is | ¦¦ ¦ ¦ ¦ confirmed to contain only cargo | ¦¦ ¦ ¦ ¦ handling equipment, ballast, which | ¦¦ ¦ ¦ ¦ may be loaded in ULD's, and/or Fly | ¦¦ ¦ ¦ ¦ Away Kits. | ¦¦ ¦ ¦ ¦ | ¦¦ ¦ ¦ ¦ NOTE: Operator MEL's must define | ¦¦ ¦ ¦ ¦ which items are approved for | ¦¦ ¦ ¦ ¦ inclusion in Fly Away Kits, | ¦¦ ¦ ¦ ¦ and which materials can be | ¦¦ ¦ ¦ ¦ used as ballast. | ¦ ¦ 30-2 Lavatory Smoke C ¦ - ¦ - ¦ May be inoperative provided: | ¦¦ *** Detection System ¦ ¦ ¦ a) Lavatory waste receptacle is | ¦¦ ¦ ¦ ¦ empty, ¦¦ ¦ ¦ ¦ b) Lavatory door is locked | ¦¦ ¦ ¦ ¦ closed and placarded ¦¦ ¦ ¦ ¦ "INOPERATIVE - DO NOT ¦¦ ¦ ¦ ¦ ENTER," and ¦¦ ¦ ¦ ¦ c) Lavatory is used only by | ¦¦ ¦ ¦ ¦ crewmembers. | ¦¦ ¦ ¦ ¦ | ¦¦ ¦ ¦ ¦ NOTE 1: These provisos are not in- ¦¦ ¦ ¦ ¦ tended to prohibit ¦¦ ¦ ¦ ¦ Lavatory use or inspec- | ¦¦ ¦ ¦ ¦ tions by crewmembers. ¦ ¦ ¦ ¦ ¦ NOTE 2: A Lavatory 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 Selector | ¦¦ ¦ ¦ ¦ remains OFF. | ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 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 ¦ (O)May be inoperative provided, | ¦¦ Position Indicator ¦ ¦ ¦ before each departure: | ¦¦ ¦ ¦ ¦ a) Aileron trim system is ¦¦ ¦ ¦ ¦ visually confirmed to | ¦¦ ¦ ¦ ¦ operate normally, and ¦¦ ¦ ¦ ¦ b) Aileron trim is visually ¦¦ ¦ ¦ ¦ confirmed to be centered. | ¦ ¦ 20-1 Rudder Trim B ¦ 1 ¦ 0 ¦ (O)May be inoperative provided, | ¦¦ Position Indicator ¦ ¦ ¦ before each departure: | ¦¦ ¦ ¦ ¦ a) Rudder trim system is ¦¦ ¦ ¦ ¦ visually confirmed to | ¦¦ ¦ ¦ ¦ operate normally, and ¦¦ ¦ ¦ ¦ b) Rudder trim is visually ¦¦ ¦ ¦ ¦ confirmed to be centered. | ¦ ¦ 20-2 Rudder Pedal C ¦ 2 ¦ 0 ¦ (M)May be inoperative provided | ¦¦ Adjustment Systems ¦ ¦ ¦ affected adjustment system(s) can | ¦¦ ¦ ¦ ¦ be secured in a position which | ¦¦ ¦ ¦ ¦ suits affected pilots' | ¦¦ ¦ ¦ ¦ requirements. | ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 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 B ¦ 1 ¦ 0 ¦ (M)(O)May be inoperative provided: ¦¦ Elevator Trim ¦ ¦ ¦ a) Associated circuit breakers ¦¦ System ¦ ¦ ¦ are pulled and collared, ¦¦ ¦ ¦ ¦ b) Mechanical Elevator Trim | ¦¦ ¦ ¦ ¦ System is confirmed to | ¦¦ ¦ ¦ ¦ operate normally before | ¦¦ ¦ ¦ ¦ departure, | ¦¦ ¦ ¦ ¦ c) Autopilot is considered | ¦¦ ¦ ¦ ¦ inoperative, and | ¦¦ ¦ ¦ ¦ d) For 800XP aircraft, the Mach | ¦¦ ¦ ¦ ¦ Trim system is considered | ¦¦ ¦ ¦ ¦ inoperative and appropriate | ¦¦ ¦ ¦ ¦ AFM speed limitations | ¦¦ ¦ ¦ ¦ observed. | ¦ ¦ ¦ ¦ ¦ NOTE 1: For operations within RVSM ¦¦ ¦ ¦ ¦ airspace, the following ¦¦ ¦ ¦ ¦ items must operate | ¦¦ ¦ ¦ ¦ normally: | ¦ ¦ ¦ ¦ ¦ a) 2 ADC's ¦¦ ¦ ¦ ¦ b) 1 ATC Transponder ¦¦ ¦ ¦ ¦ c) 1 A/P altitude hold ¦¦ ¦ ¦ ¦ Function, and ¦¦ ¦ ¦ ¦ d) Altitude Alerter ¦ ¦ ¦ ¦ ¦ NOTE 2: Flying below, above or ¦¦ ¦ ¦ ¦ crossing RVSM airspace ¦¦ ¦ ¦ ¦ does not require the above ¦¦ ¦ ¦ ¦ items to be operating. | ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 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 ¦ ¦ ¦ ¦ ¦ 1) (Series 1 B ¦ 2 ¦ 1 ¦ (M)(O)One may be inoperative ¦¦ Through 700, ¦ ¦ ¦ provided, before each departure: | ¦¦ Only) ¦ ¦ ¦ a) Remaining stall detector | ¦¦ ¦ ¦ ¦ pneumatic system is verified ¦¦ ¦ ¦ ¦ to operate normally, and | ¦¦ ¦ ¦ ¦ b) Remaining stall test channel | ¦¦ ¦ ¦ ¦ is confirmed to operate | ¦¦ ¦ ¦ ¦ normally. ¦ ¦ ¦ ¦ ¦ (Continued) ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 27-4 ¦¦ --------------------------------------------------------------------------- ¦¦ 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 and B ¦ 3 ¦ 2 ¦ (M)(O)One stall warning and/or | ¦¦ 800XP, Only) ¦ ¦ ¦ identification channel may be ¦¦ ¦ ¦ ¦ inoperative provided: ¦¦ ¦ ¦ ¦ a) Inoperative channel is ¦¦ ¦ ¦ ¦ inhibited by pulling and ¦¦ ¦ ¦ ¦ collaring the associated ¦¦ ¦ ¦ ¦ STALL IDENT 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 800 ¦ ¦ ¦ a) Both stall warning channels ¦¦ and 800XP Only) ¦ ¦ ¦ operate normally, and ¦¦ ¦ ¦ ¦ b) Remaining stick shaker ¦¦ ¦ ¦ ¦ system operates normally. ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 27-5 ¦¦ --------------------------------------------------------------------------- ¦¦ 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 | ¦¦ Autopilot ¦ ¦ ¦ Stick Shaker Autopilot Disconnect | ¦¦ Disconnect System ¦ ¦ ¦ functions of both Stall Warning | ¦¦ (Series 800 ¦ ¦ ¦ Channels 1 and 2 are confirmed to | ¦¦ Without Mod. ¦ ¦ ¦ operate normally before each | ¦¦ 253146 Installed, ¦ ¦ ¦ departure. | ¦¦ Only) ¦ ¦ ¦ ¦ ¦ 30-5 Mach Trim System C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided: ¦¦ (Series 800XP) ¦ ¦ ¦ a) Mechanical Elevator Trim ¦¦ ¦ ¦ ¦ System is confirmed to | ¦¦ ¦ ¦ ¦ operate normally before each | ¦¦ ¦ ¦ ¦ departure, and | ¦¦ ¦ ¦ ¦ b) AFM Speed Limitation of 0.73 | ¦¦ ¦ ¦ ¦ IMN is not exceeded unless | ¦¦ ¦ ¦ ¦ Auto Pilot operates normally | ¦¦ ¦ ¦ ¦ and is used. | ¦ ¦ 50-1 Flap Position C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided: | ¦¦ Indicator (On ¦ ¦ ¦ a) Flap position is visually | ¦¦ Center Instrument ¦ ¦ ¦ confirmed to be at 0 degrees | ¦¦ Panel) ¦ ¦ ¦ before each departure, | ¦¦ ¦ ¦ ¦ b) AFM procedures for flap 0 ¦¦ ¦ ¦ ¦ degree take-off and landing ¦¦ ¦ ¦ ¦ are observed, and ¦¦ ¦ ¦ ¦ c) Flaps remain in the | ¦¦ ¦ ¦ ¦ retracted position for the | ¦¦ ¦ ¦ ¦ entire flight. | ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 27-6 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 27 FLIGHT CONTROLS ¦ ¦ ¦ ¦ ¦ 50-2 Flap Handle Select C ¦ 1 ¦ 0 ¦ (O)May be inoperative, and flaps | ¦¦ Position Indicator ¦ ¦ ¦ used, provided: | ¦¦ (On Control ¦ ¦ ¦ a) Flap Position Indicator (On | ¦¦ Pedestal) ¦ ¦ ¦ Center Instrument Panel | ¦¦ ¦ ¦ ¦ operates normally, and | ¦¦ ¦ ¦ ¦ b) Before each departure, flap | ¦¦ ¦ ¦ ¦ position indication is | ¦¦ ¦ ¦ ¦ visually confirmed for each | ¦¦ ¦ ¦ ¦ flap selection. | ¦ ¦ C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided: | ¦¦ ¦ ¦ ¦ a) Flap position is visually | ¦¦ ¦ ¦ ¦ confirmed to be at 0 degrees | ¦¦ ¦ ¦ ¦ before each departure, | ¦¦ ¦ ¦ ¦ b) AFM procedures for flap 0 ¦¦ ¦ ¦ ¦ degree take-off and landing ¦¦ ¦ ¦ ¦ are observed, and ¦¦ ¦ ¦ ¦ c) Flaps remain in the | ¦¦ ¦ ¦ ¦ retracted position for the | ¦¦ ¦ ¦ ¦ entire flight. | ¦ ¦ 60-1 Air Brake Position C ¦ - ¦ 0 ¦ (O)May be inoperative provided, ¦¦ Indicator(s) ¦ ¦ ¦ before each departure: | ¦¦ ¦ ¦ ¦ a) Airbrakes are visually | ¦¦ ¦ ¦ ¦ confirmed to operate ¦¦ ¦ ¦ ¦ normally, ¦¦ ¦ ¦ ¦ b) Takeoff warning system is | ¦¦ ¦ ¦ ¦ confirmed to operate | ¦¦ ¦ ¦ ¦ normally with Air Brake | ¦¦ ¦ ¦ ¦ deployment, and | ¦¦ ¦ ¦ ¦ c) Airbrakes are visually | ¦¦ ¦ ¦ ¦ confirmed to be retracted. | ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 27-7 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 27 FLIGHT CONTROLS ¦ ¦ ¦ ¦ ¦ 60-2 Control Column C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided: ¦¦ Lock System ¦ ¦ ¦ a) Procedures are established | ¦¦ ¦ ¦ ¦ and used to prevent damage | ¦¦ ¦ ¦ ¦ from gusts while aircraft is | ¦¦ ¦ ¦ ¦ on the ground, and | ¦¦ ¦ ¦ ¦ b) Throttle Lever Baulks are | ¦¦ ¦ ¦ ¦ confirmed to be disengaged | ¦¦ ¦ ¦ ¦ prior to each departure. | ¦ ¦ 60-3 Rudder Gust Lock D ¦ 1 ¦ 0 ¦ (O)May be inoperative provided a | ¦¦ Flapper Door ¦ ¦ ¦ cover is installed to protect | ¦¦ ¦ ¦ ¦ against contamination by foreign | ¦¦ ¦ ¦ ¦ material. | ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 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 ¦ ¦ ¦ Deleted, Revision 6. | ¦ ¦ 20-2 Wing Transfer C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided: | ¦¦ Magnetic Indicator ¦ ¦ ¦ a) Both Fuel Booster Pumps | ¦¦ (Series 1 Through ¦ ¦ ¦ operate normally, | ¦¦ 400 Only) ¦ ¦ ¦ b) Wing Fuel Content Indicators | ¦¦ ¦ ¦ ¦ operate normally, and | ¦¦ ¦ ¦ ¦ c) Before each departure, | ¦¦ ¦ ¦ ¦ TRANSFER and CROSSFEED | ¦¦ ¦ ¦ ¦ Valves are confirmed to | ¦¦ ¦ ¦ ¦ operate normally. | ¦ ¦ 20-3 Fuel Transfer/ C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided: | ¦¦ Crossfeed ¦ ¦ ¦ a) Both Fuel Booster Pumps | ¦¦ Indicator (Series ¦ ¦ ¦ operate normally, | ¦¦ 600 Through 800XP ¦ ¦ ¦ b) Wing Fuel Content Indicators | ¦¦ Only) ¦ ¦ ¦ operate normally, and | ¦¦ ¦ ¦ ¦ c) Before each departure, | ¦¦ ¦ ¦ ¦ TRANSFER and CROSSFEED | ¦¦ ¦ ¦ ¦ Valves are confirmed to | ¦¦ ¦ ¦ ¦ operate normally. | ¦ ¦ 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) ¦ ¦ ¦ (Series 600 and 700, ONLY) | ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 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)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) ¦ ¦ ¦ ¦¦ C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided: | ¦¦ ¦ ¦ ¦ a) Tank remains empty, and ¦¦ ¦ ¦ ¦ b) Dorsal tank remains empty. ¦¦ ¦ ¦ ¦ (Series 600 and 700, ONLY) | ¦ ¦ 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: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 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 400 C ¦ 1 ¦ 0 ¦ (M)(O)May be inoperative provided: | ¦¦ through 700, ¦ ¦ ¦ a) Failure of the fueling | ¦¦ Only (If ¦ ¦ ¦ system is verified not to be | ¦¦ Installed) ¦ ¦ ¦ due to fuel pipe leakage, | ¦¦ ¦ ¦ ¦ b) Both refueling vent valves, ¦¦ ¦ ¦ ¦ master refuel valve, and ¦¦ ¦ ¦ ¦ refueling valves are closed, ¦¦ ¦ ¦ ¦ and ¦¦ ¦ ¦ ¦ c) Overwing refueling procedure ¦¦ ¦ ¦ ¦ is established and used. ¦ ¦ 2) Series 800 and C ¦ 1 ¦ 0 ¦ (M)(O)May be inoperative provided: ¦¦ 800XP, Only ¦ ¦ ¦ a) Failure of the fueling ¦¦ ¦ ¦ ¦ system is verified not to be | ¦¦ ¦ ¦ ¦ due to fuel pipe leakage. | ¦¦ ¦ ¦ ¦ b) Master refueling valve and ¦¦ ¦ ¦ ¦ all tank refueling valves ¦¦ ¦ ¦ ¦ are closed, and ¦¦ ¦ ¦ ¦ c) Overwing refueling procedure ¦¦ ¦ ¦ ¦ is established and used. ¦ ¦ 22-2 Pressure Refuel C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided ¦¦ Blanking Cap ¦ ¦ ¦ master refuel valve is closed. ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 28-4 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 28 FUEL ¦ ¦ ¦ ¦ ¦ 42-1 Wing Tank Fuel B ¦ 2 ¦ 1 ¦ (O)One may be inoperative | ¦¦ Content Indicators ¦ ¦ ¦ provided: | ¦¦ ¦ ¦ ¦ a) Before departure, fuel | ¦¦ ¦ ¦ ¦ quantity in associated tank | ¦¦ ¦ ¦ ¦ is confirmed by an alternate | ¦¦ ¦ ¦ ¦ means, | ¦¦ ¦ ¦ ¦ b) All remaining fuel system | ¦¦ ¦ ¦ ¦ components operate normally, | ¦¦ ¦ ¦ ¦ c) FUEL FLOW/FUEL USED COUNTER/ | ¦¦ ¦ ¦ ¦ FUEL TOTALIZER indicators | ¦¦ ¦ ¦ ¦ operate normally, | ¦¦ ¦ ¦ ¦ d) Aircraft remains within One | ¦¦ ¦ ¦ ¦ [1] hour flying time from a | ¦¦ ¦ ¦ ¦ suitable airport, and | ¦¦ ¦ ¦ ¦ e) Alternate procedures for | ¦¦ ¦ ¦ ¦ monitoring enroute fuel | ¦¦ ¦ ¦ ¦ consumption are established | ¦¦ ¦ ¦ ¦ and used. | ¦ ¦ 42-2 Fuel Used C ¦ - ¦ 0 ¦ (O)May be inoperative provided: ¦¦ Counter(s)/Fuel ¦ ¦ ¦ a) Wing Tank Content Indicators | ¦¦ Totalizer(s) ¦ ¦ ¦ operate normally, and | ¦¦ ¦ ¦ ¦ b) Alternate procedures for | ¦¦ ¦ ¦ ¦ monitoring enroute fuel | ¦¦ ¦ ¦ ¦ consumption are established | ¦¦ ¦ ¦ ¦ and used. | ¦ ¦ 43-1 Ventral Tank C ¦ 1 ¦ 0 ¦ (M)(O)May be inoperative provided: ¦¦ "EMPTY/FULL" ¦ ¦ ¦ a) Ventral Tank is verified to | ¦¦ Indicator ¦ ¦ ¦ be empty before each ¦¦ ¦ ¦ ¦ departure, and ¦¦ ¦ ¦ ¦ b) Procedures are established | ¦¦ ¦ ¦ ¦ and used to assure that fuel | ¦¦ ¦ ¦ ¦ is not transferred into | ¦¦ ¦ ¦ ¦ Ventral Tank during flight. | ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 28-5 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 28 FUEL ¦ ¦ ¦ ¦ ¦ 43-2 Dorsal Tank C ¦ 1 ¦ 0 ¦ (M)(O)May be inoperative provided: ¦¦ "Empty/Full" ¦ ¦ ¦ a) Dorsal Tank is verified | ¦¦ Indicator (Series ¦ ¦ ¦ empty before each departure ¦¦ 600 and 700, Only) ¦ ¦ ¦ departure, and ¦¦ ¦ ¦ ¦ b) Procedures are established | ¦¦ ¦ ¦ ¦ and used to assure that fuel | ¦¦ ¦ ¦ ¦ is not transferred into | ¦¦ ¦ ¦ ¦ Dorsal Tank during flight. | ¦ ¦ 43-3 Low VMO Audible ¦ ¦ ¦ ¦¦ Warning System ¦ ¦ ¦ ¦ ¦ 1) Series 3A/RA, C ¦ 1 ¦ 0 ¦ (M)(O)May be inoperative provided: ¦¦ 3B/RA Through ¦ ¦ ¦ a) Ventral tank is verified to ¦¦ 400, 800 and ¦ ¦ ¦ be empty before each ¦¦ 800XP, Only ¦ ¦ ¦ departure, and ¦¦ ¦ ¦ ¦ b) Procedures are established | ¦¦ ¦ ¦ ¦ and used to assure that fuel | ¦¦ ¦ ¦ ¦ is not transferred into | ¦¦ ¦ ¦ ¦ Ventral Tank during flight. | ¦ ¦ 2) Series 600 and C ¦ 1 ¦ 0 ¦ (M)(O)May be inoperative provided: ¦¦ 700, Only ¦ ¦ ¦ a) Ventral and Dorsal Tanks are ¦¦ ¦ ¦ ¦ verified empty before each ¦¦ ¦ ¦ ¦ departure, and ¦¦ ¦ ¦ ¦ b) Procedures are established | ¦¦ ¦ ¦ ¦ and used to assure that fuel | ¦¦ ¦ ¦ ¦ is not transferred into | ¦¦ ¦ ¦ ¦ Ventral Tank or Dorsal Tank | ¦¦ ¦ ¦ ¦ during flight. | ¦ ¦ 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 600 ¦ ¦ ¦ b) Vent valves operate ¦¦ Only) ¦ ¦ ¦ normally. ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 28-6 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 28 FUEL ¦ ¦ ¦ ¦ ¦ 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: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 29-1 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 29 HYDRAULIC POWER ¦ ¦ ¦ ¦ ¦ 30-1 L/R HYD LO FLOW C ¦ 2 ¦ 1 ¦ (O)One may be inoperative provided: ¦¦ Annunciators ¦ ¦ ¦ a) Associated hydraulic pump | ¦¦ (Viper Engines, ¦ ¦ ¦ operates normally, ¦¦ Only) ¦ ¦ ¦ b) Main hydraulic supply | ¦¦ ¦ ¦ ¦ pressure indicator operates ¦¦ ¦ ¦ ¦ normally, ¦¦ ¦ ¦ ¦ c) EMRG HYD LO PRESS | ¦¦ ¦ ¦ ¦ annunciator operates | ¦¦ ¦ ¦ ¦ normally, ¦¦ ¦ ¦ ¦ d) 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 hydraulic pump | ¦¦ (TFE-731 Engines, ¦ ¦ ¦ operates normally, ¦¦ Only) ¦ ¦ ¦ b) Main hydraulic supply | ¦¦ ¦ ¦ ¦ pressure indicator operates ¦¦ ¦ ¦ ¦ normally, | ¦¦ ¦ ¦ ¦ c) EMRG BRK LO PRESS | ¦¦ ¦ ¦ ¦ annunciator operates | ¦¦ ¦ ¦ ¦ normally, and | ¦¦ ¦ ¦ ¦ d) Associated engine is started ¦¦ ¦ ¦ ¦ first to verify pressure ¦¦ ¦ ¦ ¦ buildup before each ¦¦ ¦ ¦ ¦ departure. ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 29-2 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 29 HYDRAULIC POWER ¦ ¦ ¦ ¦ ¦ 30-3 Combined BRAKES ¦ ¦ ¦ ¦¦ and SUPPLY ¦ ¦ ¦ ¦¦ Pressure Gauge ¦ ¦ ¦ ¦ ¦ 1) BRAKE Pressure C ¦ 2 ¦ 1 ¦ (O)One may be inoperative provided | ¦¦ Indicators ¦ ¦ ¦ before each departue: | ¦¦ ¦ ¦ ¦ a) Main hydraulic SUPPLY | ¦¦ ¦ ¦ ¦ indication is within normal | ¦¦ ¦ ¦ ¦ limits, | ¦¦ ¦ ¦ ¦ b) Emergency Brake Pressure ¦¦ ¦ ¦ ¦ Indicators/Annunciators are | ¦¦ ¦ ¦ ¦ confirmed to operate | ¦¦ ¦ ¦ ¦ normally, and ¦¦ ¦ ¦ ¦ c) Normal braking is confirmed | ¦¦ ¦ ¦ ¦ independently for left and ¦¦ ¦ ¦ ¦ right brakes. ¦ ¦ 4. Accumulator ¦ ¦ ¦ Deleted, Rev. 3. ¦¦ Pressure Indicators ¦ ¦ ¦ ¦ ¦ 30-5 AUX HYD LO LEVEL C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided | ¦¦ Annunciator ¦ ¦ ¦ fluid quantity is visually | ¦¦ (Series 3 Through ¦ ¦ ¦ confirmed to be adequate before | ¦¦ 800XP, Only) ¦ ¦ ¦ each departure. | ¦ ¦ 30-6 Accumulator C ¦ 2 ¦ 1 ¦ (O)One may be inoperative provided | ¦¦ Pressure ¦ ¦ ¦ before each departure: | ¦¦ Indicators (Main ¦ ¦ ¦ a) Combined BRAKES and SUPPLY | ¦¦ and Emergency Only) ¦ ¦ ¦ Pressure Gauge operates | ¦¦ ¦ ¦ ¦ normally, | ¦¦ ¦ ¦ ¦ b) Gas pre-charge on associated | ¦¦ ¦ ¦ ¦ accumulator is confirmed to | ¦¦ ¦ ¦ ¦ be adequate, and | ¦¦ ¦ ¦ ¦ b) Normal operation of the | ¦¦ ¦ ¦ ¦ associated accumulator is | ¦¦ ¦ ¦ ¦ confirmed. | ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 29-3 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 29 HYDRAULIC POWER ¦ ¦ ¦ ¦ ¦ 30-7 Thrust Reverser C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided | ¦¦ Accumulator ¦ ¦ ¦ before each departure: | ¦¦ Pressure Indicator ¦ ¦ ¦ a) Normal thrust reverser | ¦¦ (Series 800, if ¦ ¦ ¦ operation is checked, and | ¦¦ installed, and ¦ ¦ ¦ b) Normal accumulator pressure, | ¦¦ 800XP) ¦ ¦ ¦ is checked. | ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 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) WING/TAIL TIME ¦ ¦ ¦ | ¦¦ Switch ¦ ¦ ¦ | ¦¦ ¦ ¦ ¦ | ¦¦ a) Series 1 C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided: | ¦¦ Through 400, ¦ ¦ ¦ a) WING/TAIL ON/OFF Switch is | ¦¦ Only ¦ ¦ ¦ confirmed to operate | ¦¦ ¦ ¦ ¦ normally, | ¦¦ ¦ ¦ ¦ b) WING/TAIL ON/OFF Switch is | ¦¦ ¦ ¦ ¦ confirmed to be OFF when not | ¦¦ ¦ ¦ ¦ in use (no audible sound | ¦¦ ¦ ¦ ¦ from Anti-Icing Pump), and | ¦¦ ¦ ¦ ¦ c) Alternate procedures for | ¦¦ ¦ ¦ ¦ accomplishing timing are | ¦¦ ¦ ¦ ¦ established and used. | ¦¦ ¦ ¦ ¦ | ¦¦ C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided: | ¦¦ ¦ ¦ ¦ a) WING/TAIL ANTI-ICE System is | ¦¦ ¦ ¦ ¦ confirmed to be OFF (no | ¦¦ ¦ ¦ ¦ audible sound from Anti- | ¦¦ ¦ ¦ ¦ Icing Pump), and | ¦¦ ¦ ¦ ¦ b) Airplane is not operated in | ¦¦ ¦ ¦ ¦ visible moisture or known or | ¦¦ ¦ ¦ ¦ forecast icing conditions. | ¦ ¦ ¦ ¦ ¦ (Continued) ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 30-2 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 30 ICE AND RAIN ¦ ¦ ¦ ¦¦ PROTECTION ¦ ¦ ¦ ¦ ¦ 10-2 WING/TAIL ANTI-ICE ¦ ¦ ¦ ¦¦ Control Switches ¦ ¦ ¦ ¦ ¦ 1) WING/TAIL TIME ¦ ¦ ¦ ¦¦ Switch (Cont'd) ¦ ¦ ¦ ¦ ¦ b) Time C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided: | ¦¦ Function ¦ ¦ ¦ a) System is confirmed OFF when | ¦¦ (Series 600 ¦ ¦ ¦ not in use, | ¦¦ Through 800XP ¦ ¦ ¦ b) Priming can be accomplished, | ¦¦ Only) ¦ ¦ ¦ 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/TAIL C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided: | ¦¦ ON/OFF Switch ¦ ¦ ¦ a) WING/TAIL ANTI-ICE System is | ¦¦ (Series 1 ¦ ¦ ¦ confirmed to be OFF when not | ¦¦ Through 400, ¦ ¦ ¦ in use (no audible sound | ¦¦ Only) ¦ ¦ ¦ from Anti-Icing Pump), and | ¦¦ ¦ ¦ ¦ b) WING/TAIL TIME Switch is | ¦¦ ¦ ¦ ¦ confirmed to operate | ¦¦ ¦ ¦ ¦ normally, and is used for | ¦¦ ¦ ¦ ¦ Anti-Icing. | ¦¦ ¦ ¦ ¦ | ¦¦ ¦ ¦ ¦ (O)May be inoperative provided: | ¦¦ ¦ ¦ ¦ a) WING/TAIL ANTI-ICE System is | ¦¦ ¦ ¦ ¦ confirmed to be OFF (no | ¦¦ ¦ ¦ ¦ audible sound from Anti- | ¦¦ ¦ ¦ ¦ Icing Pump), and | ¦¦ ¦ ¦ ¦ b) Airplane is not operated in | ¦¦ ¦ ¦ ¦ visible moisture or known or | ¦¦ ¦ ¦ ¦ forecast icing conditions. | ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 30-3 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 30 ICE AND RAIN ¦ ¦ ¦ ¦¦ PROTECTION ¦ ¦ ¦ ¦ ¦ 10-3 T.K.S. Quantity C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided ¦¦ Indication System ¦ ¦ ¦ fluid quantity is confirmed | ¦¦ ¦ ¦ ¦ adequate before each departure. | ¦¦ ¦ ¦ ¦ | ¦¦ C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided | ¦¦ ¦ ¦ ¦ airplane is not operated in known ¦¦ ¦ ¦ ¦ or forecast icing conditions. ¦ ¦ 10-4 ANTI-ICE LO PRESS C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided: | ¦¦ Annunciator ¦ ¦ ¦ a) Fluid delivery system ¦¦ (Series 800 and ¦ ¦ ¦ operates normally, and ¦¦ 800XP, Only) ¦ ¦ ¦ b) Quantity indication system ¦¦ ¦ ¦ ¦ operates normally. | ¦¦ ¦ ¦ ¦ | ¦¦ C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided | ¦¦ ¦ ¦ ¦ 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 ¦ ¦ ¦ fluid quantity is confirmed | ¦¦ (Series 800 and ¦ ¦ ¦ adequate before each departure. | ¦¦ 800XP, Only) ¦ ¦ ¦ | ¦¦ C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided | ¦¦ ¦ ¦ ¦ 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. ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 30-4 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 30 ICE AND RAIN ¦ ¦ ¦ ¦¦ PROTECTION ¦ ¦ ¦ ¦ ¦ 20-1 Engine Inlet C ¦ 2 ¦ 1 ¦ (O)One may be inoperative ON | ¦¦ Anti-icing ¦ ¦ ¦ provided: | ¦¦ Systems ¦ ¦ ¦ a) Associated Engine Inlet | ¦¦ (TFE-731 Engined ¦ ¦ ¦ Anti-Ice (ENG A/ICE) | ¦¦ Aircraft, Only) ¦ ¦ ¦ Annunciator operates | ¦¦ ¦ ¦ ¦ normally, | ¦¦ ¦ ¦ ¦ b) Associated Engine Inlet | ¦¦ ¦ ¦ ¦ Anti-Ice (ENG A/ICE) | ¦¦ ¦ ¦ ¦ Annunciator extinguishes | ¦¦ ¦ ¦ ¦ when ENG ANTICE for that | ¦¦ ¦ ¦ ¦ engine is selected, | ¦¦ ¦ ¦ ¦ c) Takeoff and Landing field | ¦¦ ¦ ¦ ¦ temperatures do not exceed | ¦¦ ¦ ¦ ¦ +10 degrees C, and | ¦¦ ¦ ¦ ¦ d) AFM Engine Anti-Ice ON | ¦¦ ¦ ¦ ¦ Performance and Limitations | ¦¦ ¦ ¦ ¦ are observed. | ¦¦ ¦ ¦ ¦ | ¦¦ C ¦ 2 ¦ 1 ¦ (O)One may be inoperative provided: | ¦¦ ¦ ¦ ¦ a) Airplane is not operated in | ¦¦ ¦ ¦ ¦ visible moisture or in known | ¦¦ ¦ ¦ ¦ or forecast icing | ¦¦ ¦ ¦ ¦ conditions, | ¦¦ ¦ ¦ ¦ b) Takeoff and Landing field | ¦¦ ¦ ¦ ¦ temperatures do not exceed | ¦¦ ¦ ¦ ¦ +10 degrees C, and | ¦¦ ¦ ¦ ¦ c) AFM Engine Anti-Ice ON | ¦¦ ¦ ¦ ¦ Performance and Limitations | ¦¦ ¦ ¦ ¦ are observed. | ¦ ¦ 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: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 30-5 ¦¦ --------------------------------------------------------------------------- ¦¦ 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: ¦¦ ON" White ¦ ¦ ¦ a) "ENG A/ICE" white | ¦¦ Annunciator ¦ ¦ ¦ annunciators on overhead ¦¦ (Series 600 and ¦ ¦ ¦ panel are confirmed to | ¦¦ 700, Only) ¦ ¦ ¦ operate normally, and ¦¦ ¦ ¦ ¦ b) Alternate procedures for | ¦¦ ¦ ¦ ¦ determining operation of | ¦¦ ¦ ¦ ¦ Engine Anti-Ice are | ¦¦ ¦ ¦ ¦ established and used. | ¦ ¦ 20-4 MWS "ICE PROT C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided "ENG ¦¦ SELECTED" White ¦ ¦ ¦ A/ICE" amber annunciators are ¦¦ Annunciator ¦ ¦ ¦ confirmed to operate normally. | ¦¦ (Series 800 and ¦ ¦ ¦ ¦¦ 800XP, Only) ¦ ¦ ¦ ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 30-6 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 30 ICE AND RAIN ¦ ¦ ¦ ¦¦ PROTECTION ¦ ¦ ¦ ¦ ¦ 30-1 Pitot Probe/ Pitot B ¦ 2 ¦ 1 ¦ (O)One may be inoperative provided: ¦¦ Mast Heaters ¦ ¦ ¦ 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. ¦ ¦ ¦ ¦ ¦ NOTE: Both heaters are required ¦¦ ¦ ¦ ¦ for RVSM operations. ¦ ¦ 30-2 Pitot Ammeters C ¦ 2 ¦ 0 ¦ (O)May be inoperative provided: | ¦¦ (Series 1 Through ¦ ¦ ¦ a) Pitot/Mast Heater Fail | ¦¦ 400 With SB 34- ¦ ¦ ¦ annunciators are confirmed | ¦¦ 140, Or Mod. ¦ ¦ ¦ to operate normally before | ¦¦ 252733 Installed, ¦ ¦ ¦ each departure, and | ¦¦ Only) ¦ ¦ ¦ b) Alternate procedures are | ¦¦ ¦ ¦ ¦ established and used. | ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 30-7 ¦¦ --------------------------------------------------------------------------- ¦¦ 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 ¦ (O)May be inoperative provided | ¦¦ Selector (Series ¦ ¦ ¦ Pitot/Mast Heater Fail Lights are | ¦¦ 600 and 700 With ¦ ¦ ¦ confirmed to operate normally | ¦¦ SB 34-140, Or ¦ ¦ ¦ before each departure. | ¦¦ Mod. 252733 ¦ ¦ ¦ | ¦¦ Installed, Or 800 ¦ ¦ ¦ | ¦¦ and 800XP Only) ¦ ¦ ¦ | ¦ ¦ 30-4 Pitot/Mast Heater B ¦ - ¦ 0 ¦ (O)May be inoperative provided: | ¦¦ FAIL Light(s)/ ¦ ¦ ¦ a) Associated Pitot Heating | ¦¦ Annunciator(s) ¦ ¦ ¦ System is confirmed to | ¦¦ (Series 1 Through ¦ ¦ ¦ operate normally before each | ¦¦ 700 With SB 34- ¦ ¦ ¦ departure, | ¦¦ 140, Or Mod. ¦ ¦ ¦ b) Associated Pitot Heat | ¦¦ 252733 Installed, ¦ ¦ ¦ Ammeter operates normally, | ¦¦ and 800 and 800XP, ¦ ¦ ¦ and | ¦¦ Only) ¦ ¦ ¦ c) Alternate procedures for | ¦¦ ¦ ¦ ¦ monitoring Pitot Heater | ¦¦ ¦ ¦ ¦ function in icing conditions | ¦¦ ¦ ¦ ¦ are established and used. | ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 30-8 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 30 ICE AND RAIN ¦ ¦ ¦ ¦¦ PROTECTION ¦ ¦ ¦ ¦ ¦ 30-5 Static Plate B ¦ 2 ¦ 1 ¦ (O)Except where enroute operations | ¦¦ Heaters (Series ¦ ¦ ¦ require that both operate normally, | ¦¦ 700, if installed, ¦ ¦ ¦ one may be inoperative provided: | ¦¦ 800 and 800XP ¦ ¦ ¦ a) Flight is conducted in day ¦¦ Only) ¦ ¦ ¦ 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. ¦ ¦ 30-6 Stall Vane Heaters B ¦ 2 ¦ 1 ¦ (O)Except where enroute operations | ¦¦ (Series 800 and ¦ ¦ ¦ require that both operate normally, | ¦¦ 800XP Only) ¦ ¦ ¦ one may be inoperative provided: ¦¦ ¦ ¦ ¦ a) VANE HTR FAIL Annunciator | ¦¦ ¦ ¦ ¦ for normally operating Stall | ¦¦ ¦ ¦ ¦ Vane Heater operates | ¦¦ ¦ ¦ ¦ normally, | ¦¦ ¦ ¦ ¦ b) Flight is conducted in day ¦¦ ¦ ¦ ¦ VMC flight conditions only, ¦¦ ¦ ¦ ¦ and ¦¦ ¦ ¦ ¦ c) 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: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 30-9 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 30 ICE AND RAIN ¦ ¦ ¦ ¦¦ PROTECTION ¦ ¦ ¦ ¦ ¦ 30-7 L and R VANE HTR B ¦ 2 ¦ 1 ¦ (O)One may be inoperative provided: | ¦¦ FAIL Annunciators ¦ ¦ ¦ a) Both Stall Vane Heaters are | ¦¦ (Series 800 and ¦ ¦ ¦ confirmed to operate | ¦¦ 800XP Only) ¦ ¦ ¦ normally before each | ¦¦ ¦ ¦ ¦ departure, | ¦¦ ¦ ¦ ¦ b) Flight is conducted in day | ¦¦ ¦ ¦ ¦ VMC conditions, only, and | ¦¦ ¦ ¦ ¦ c) 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: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 30-10 ¦¦ --------------------------------------------------------------------------- ¦¦ 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) Series 1 C ¦ 2 ¦ 0 ¦ (O)May be inoperative provided: | ¦¦ Through 700 ¦ ¦ ¦ a) Airplane is operated in | ¦¦ Series Only ¦ ¦ ¦ accordance with AFM ¦¦ ¦ ¦ ¦ Limitations, and ¦¦ ¦ ¦ ¦ b) Windscreen fluid de-icing ¦¦ ¦ ¦ ¦ system is installed and ¦¦ ¦ ¦ ¦ operates normally. ¦¦ ¦ ¦ ¦ | ¦¦ C ¦ 2 ¦ 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. ¦ ¦ 2) Series 800 and C ¦ 4 ¦ 3 ¦ Heating to one side screen "B" only | ¦¦ 800XP Only ¦ ¦ ¦ may be inoperative. ¦ ¦ C ¦ 4 ¦ 2 ¦ (O)Both "B" screens may be | ¦¦ ¦ ¦ ¦ inoperative provided airplane is | ¦¦ ¦ ¦ ¦ not operated in known or forecast | ¦¦ ¦ ¦ ¦ icing conditions. | ¦ ¦ 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: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 30-11 ¦¦ --------------------------------------------------------------------------- ¦¦ 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 ¦ 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: Not required for an inoper- | ¦¦ ¦ ¦ ¦ ative windscreen heat ¦¦ ¦ ¦ ¦ system. ¦ ¦ 40-3 Windscreen Wiper C ¦ 2 ¦ 0 ¦ May be inoperative provided ¦¦ Systems (Series 1 ¦ ¦ ¦ airplane is not operated in ¦¦ Through 700 Only) ¦ ¦ ¦ precipitation within 5 nautical ¦¦ ¦ ¦ ¦ miles of the airport of takeoff or ¦¦ ¦ ¦ ¦ intended landing. ¦ ¦ 1) Park and Slow C ¦ - ¦ 0 ¦ May be inoperative without 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: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 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 ¦ - ¦ - ¦ 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), if installed, | ¦¦ ¦ ¦ ¦ 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 successful. ¦¦ ¦ ¦ ¦ c) In those cases where repair ¦¦ ¦ ¦ ¦ is attempted but not ¦¦ ¦ ¦ ¦ successful, the aircraft may ¦¦ ¦ ¦ ¦ be dispatched 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 Not ¦ ¦ ¦ are made prior to the completion of ¦¦ required by FAR ¦ ¦ ¦ the next heavy maintenance visit. ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 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: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 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 ¦ ¦ ¦ Deleted, Revision 6. Relief | ¦¦ Indications ¦ ¦ ¦ already provided for in item | ¦¦ ¦ ¦ ¦ 31-50-1. | ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 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: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 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 ¦¦ ¦ ¦ ¦ confirmed 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. ¦¦ ¦ ¦ ¦ | ¦¦ C ¦ - ¦ 0 ¦ (O)May be inoperative provided | ¦¦ ¦ ¦ ¦ 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: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 33-3 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 33 LIGHTS ¦ ¦ ¦ ¦ ¦ 20-5 EMERG LTS NOT SEL/ C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided, | ¦¦ EMRG LTS NOT SLCT ¦ ¦ ¦ before each departure: | ¦¦ Annunciator ¦ ¦ ¦ a) Passenger cabin emergency ¦¦ ¦ ¦ ¦ lighting system is confirmed | ¦¦ ¦ ¦ ¦ to operate normally, and ¦¦ ¦ ¦ ¦ b) Flightcrew ensures the ¦¦ ¦ ¦ ¦ INTERIOR LIGHTS EMERG switch ¦¦ ¦ ¦ ¦ is ARMED. | ¦ ¦ 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 ¦ - ¦ 0 ¦ May be inoperative for night | ¦¦ Strobe Lights ¦ ¦ ¦ operations provided anti-collision ¦¦ ¦ ¦ ¦ beacons operate normally. ¦ ¦ C ¦ - ¦ 0 ¦ May be inoperative for day | ¦¦ ¦ ¦ ¦ operations. ¦ ¦ 40-2 Landing Lights C ¦ 2 ¦ 1 ¦ One may be inoperative for night ¦¦ ¦ ¦ ¦ operations provided adjacent taxi ¦¦ ¦ ¦ ¦ light operates normally. ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 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 ¦ 0 ¦ May be inoperative for day ¦¦ (Cont'd) ¦ ¦ ¦ operations. ¦ ¦ 40-3 Taxi Lights (Wing C ¦ 2 ¦ 0 ¦ (O)May be inoperative provided both ¦¦ Mounted) ¦ ¦ ¦ landing lights operate normally. ¦¦ ¦ ¦ ¦ | ¦¦ C ¦ 2 ¦ 0 ¦ (O)May be inoperative for day | ¦¦ ¦ ¦ ¦ operations only. ¦¦ ¦ ¦ ¦ | ¦¦ C ¦ 2 ¦ 0 ¦ (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 provided a normally | ¦¦ Light(s) ¦ ¦ ¦ operating white strobe light is | ¦¦ ¦ ¦ ¦ located in close proximity to the | ¦¦ ¦ ¦ ¦ inoperative white position light. | ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 33-5 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 33 LIGHTS ¦ ¦ ¦ ¦ ¦ 40-5 Wing Illumination/ C ¦ - ¦ 0 ¦ May be inoperative for day | ¦¦ Ice Light(s) ¦ ¦ ¦ operations. ¦ ¦ C ¦ - ¦ 1 ¦ May be inoperative provided AFM | ¦¦ ¦ ¦ ¦ severe icing limitations are | ¦¦ ¦ ¦ ¦ observed. | ¦ ¦ 40-6 Logo Lights C ¦ - ¦ 0 ¦ ¦¦ *** ¦ ¦ ¦ ¦ ¦ 40-7 Nose Taxi Lights C ¦ - ¦ 0 ¦ ¦¦ *** ¦ ¦ ¦ ¦ ¦ 40-8 Pulselite System D ¦ 1 ¦ 0 ¦ (M)May be inoperative provided | ¦¦ *** ¦ ¦ ¦ system is deactivated. | ¦ ¦ 40-9 Wing Tip Taxi D ¦ 1 ¦ 0 ¦ ¦¦ *** Lighting System ¦ ¦ ¦ ¦ ¦ 40-10 Weight On Wheels C ¦ 1 ¦ 0 ¦ | ¦¦ *** 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 ¦ - ¦ - ¦ Any in excess of those required by | ¦¦ *** Lighting System ¦ ¦ ¦ FAR may be inoperative. | ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 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) Non-EFIS C ¦ 2 ¦ 1 ¦ One Mach indicator may be inopera- | ¦¦ Equipped ¦ ¦ ¦ tive provided VMO/MMO aural warning | ¦¦ Aircraft ¦ ¦ ¦ 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: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 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 ¦¦ ¦ ¦ ¦ of the flight. ¦ ¦ B ¦ 1 ¦ 0 ¦ (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: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 34-3 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 34 NAVIGATION ¦ ¦ ¦ ¦ ¦ 10-1 VMO/MMO Aural B ¦ 2 ¦ 1 ¦ | ¦¦ Warnings ¦ ¦ ¦ | ¦ ¦ B ¦ 2 ¦ 0 ¦ (O)May be inoperative provided: ¦¦ ¦ ¦ ¦ a) Both Mach/Airspeed ¦¦ ¦ ¦ ¦ indicators at both pilot ¦¦ ¦ ¦ ¦ positions operate normally, | ¦¦ ¦ ¦ ¦ b) If installed, Ventral Tank | ¦¦ ¦ ¦ ¦ is either empty or EMPTY/ | ¦¦ ¦ ¦ ¦ FULL indicator operates | ¦¦ ¦ ¦ ¦ normally, and | ¦¦ ¦ ¦ ¦ c) VMO/MMO AFM limitations are ¦¦ ¦ ¦ ¦ observed. ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 34-4 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 34 NAVIGATION ¦ ¦ ¦ ¦ ¦ 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 operate | ¦¦ ¦ ¦ ¦ normally for operations in | ¦¦ ¦ ¦ ¦ RVSM airspace. ¦ ¦ C ¦ - ¦ 0 ¦ May be inoperative provided system ¦¦ ¦ ¦ ¦ is not required by FAR. ¦ ¦ ¦ ¦ ¦ NOTE: One system must operate | ¦¦ ¦ ¦ ¦ normally for operations in | ¦¦ ¦ ¦ ¦ RVSM airspace. | ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 34-5 ¦¦ --------------------------------------------------------------------------- ¦¦ 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 Pneumatic C ¦ 2 ¦ 1 ¦ One may be inoperative provided ¦¦ ¦ ¦ ¦ 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 ¦ ¦ ¦ Incorporated into Item 34-20-9, | ¦¦ ¦ ¦ ¦ Revision 6. | ¦ ¦ 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: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 34-6 ¦¦ --------------------------------------------------------------------------- ¦¦ 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 Switches ¦ ¦ ¦ operate normally from ¦¦ ¦ ¦ ¦ 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, ¦¦ ¦ ¦ ¦ Revision 3. ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 34-7 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 34 NAVIGATION ¦ ¦ ¦ ¦ ¦ 20-1 Flight Director ¦ ¦ ¦ ¦¦ System(s) ¦ ¦ ¦ | ¦ ¦ 1) A/C Equipped C ¦ 2 ¦ 1 ¦ One may be inoperative provided | ¦¦ With Honeywell ¦ ¦ ¦ approach minimums do not require | ¦¦ Avionics ¦ ¦ ¦ its use. | ¦¦ ¦ ¦ ¦ | ¦¦ B ¦ 2 ¦ 0 ¦ Except for RVSM operations, may be | ¦¦ ¦ ¦ ¦ inoperative provided: | ¦¦ ¦ ¦ ¦ a) Auto Pilot is considered | ¦¦ ¦ ¦ ¦ inoperative, and | ¦¦ ¦ ¦ ¦ b) Approach minimums do not | ¦¦ ¦ ¦ ¦ require their use. | ¦¦ ¦ ¦ ¦ | ¦¦ 2) A/C Equipped B ¦ 2 ¦ 0 ¦ Except for RVSM operations, may be | ¦¦ With Collins ¦ ¦ ¦ inoperative provided: | ¦¦ Avionics ¦ ¦ ¦ a) Auto Pilot is considered | ¦¦ ¦ ¦ ¦ inoperative, and | ¦¦ ¦ ¦ ¦ b) Approach minimums do not | ¦¦ ¦ ¦ ¦ require their use. | ¦¦ ¦ ¦ ¦ | ¦¦ ¦ ¦ ¦ NOTE: With Collins Proline- | ¦¦ ¦ ¦ ¦ equipped aircraft, the A/P | ¦¦ ¦ ¦ ¦ cannot be engaged unless | ¦¦ ¦ ¦ ¦ both Flight Director Systems | ¦¦ ¦ ¦ ¦ operate normally. | ¦ ¦ 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: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 34-8 ¦¦ --------------------------------------------------------------------------- ¦¦ 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/ B ¦ 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 Switches ¦ ¦ ¦ independent sources, and ¦¦ ¦ ¦ ¦ b) Inoperative switches are not ¦¦ ¦ ¦ ¦ moved during flight. ¦ ¦ 20-5 Angle of Attack C ¦ - ¦ 0 ¦ ¦¦ *** System ¦ ¦ ¦ ¦ ¦ 20-6 Standby Attitude ¦ ¦ ¦ Incorporated into Item 34-20-9, | ¦¦ Indicator ¦ ¦ ¦ Revision 6. | ¦ ¦ 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: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 34-9 ¦¦ --------------------------------------------------------------------------- ¦¦ 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. ¦ ¦ 20-9 Standby Flight ¦ ¦ ¦ | ¦¦ Instruments/ ¦ ¦ ¦ | ¦¦ Displays ¦ ¦ ¦ | ¦¦ ¦ ¦ ¦ | ¦¦ 1) Standby C ¦ - ¦ 0 ¦ May be inoperative provided not | ¦¦ Attitude ¦ ¦ ¦ required by FAR. | ¦¦ Indicator(s) ¦ ¦ ¦ | ¦¦ (Electro- B ¦ - ¦ 0 ¦ May be inoperative provided: | ¦¦ Mechanical Gyro ¦ ¦ ¦ a) Operations are conducted in | ¦¦ Horizons) ¦ ¦ ¦ day VMC, only, and | ¦¦ ¦ ¦ ¦ b) Operations are not conducted | ¦¦ ¦ ¦ ¦ into known or forecast VFR- | ¦¦ ¦ ¦ ¦ on-Top conditions. | ¦¦ ¦ ¦ ¦ | ¦¦ a) Glideslope/ C ¦ - ¦ 0 ¦ | ¦¦ Localizer ¦ ¦ ¦ | ¦¦ Indicator(s) ¦ ¦ ¦ | ¦ ¦ 2) Standby B ¦ - ¦ 0 ¦ May be inoperative provided | ¦¦ Altimeter(s) ¦ ¦ ¦ airplane is operated in day VMC, | ¦¦ (Stand-Alone ¦ ¦ ¦ only. | ¦¦ Unit) ¦ ¦ ¦ | ¦ ¦ ¦ ¦ ¦ (Continued) | ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 34-10 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 34 NAVIGATION ¦ ¦ ¦ ¦ ¦ 20-9 Standby Flight ¦ ¦ ¦ | ¦¦ Instruments/ ¦ ¦ ¦ | ¦¦ Displays (Cont'd) ¦ ¦ ¦ | ¦ ¦ 3) Secondary Flight ¦ ¦ ¦ | ¦¦ Display (3-In-1 ¦ ¦ ¦ | ¦¦ Color Graphic ¦ ¦ ¦ | ¦¦ Standby Attitude, ¦ ¦ ¦ | ¦¦ Altitude, and ¦ ¦ ¦ | ¦¦ Airspeed ¦ ¦ ¦ | ¦¦ Indicator OR ¦ ¦ ¦ | ¦¦ 4-In-1 Color ¦ ¦ ¦ | ¦¦ Graphic Standby ¦ ¦ ¦ | ¦¦ Attitude, ¦ ¦ ¦ | ¦¦ Altitude, ¦ ¦ ¦ | ¦¦ Heading and ¦ ¦ ¦ | ¦¦ Airspeed ¦ ¦ ¦ | ¦¦ Indicator (SFD's) ¦ ¦ ¦ | ¦¦ (Meggitt) ¦ ¦ ¦ | ¦ ¦ a) Standy C ¦ 1 ¦ 0 ¦ May be inoperative provided not | ¦¦ Attitude ¦ ¦ ¦ required by FAR. | ¦¦ Display ¦ ¦ ¦ | ¦ ¦ B ¦ 1 ¦ 0 ¦ May be inoperative provide: | ¦¦ ¦ ¦ ¦ a) Operations are conducted | ¦¦ ¦ ¦ ¦ in day VMC, only, and | ¦¦ ¦ ¦ ¦ b) Operations are not conducted | ¦¦ ¦ ¦ ¦ into known or forecast VFR- | ¦¦ ¦ ¦ ¦ On-Top conditions. | ¦ ¦ b) Standy C ¦ 1 ¦ 0 ¦ May be inoperative provided | ¦¦ Altimeter ¦ ¦ ¦ airplane is operated in day VMC | ¦¦ Display ¦ ¦ ¦ only. | ¦ ¦ c) Baroset C ¦ 1 ¦ 0 ¦ May be inoperative provided | ¦¦ Knob ¦ ¦ ¦ airplane is operated in day VMC | ¦¦ ¦ ¦ ¦ only. | ¦ ¦ ¦ ¦ ¦ (Continued) | ¦-------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 34-11 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 34 NAVIGATION ¦ ¦ ¦ ¦ ¦ 20-9 Standby Flight ¦ ¦ ¦ | ¦¦ Instruments/ ¦ ¦ ¦ | ¦¦ Displays (Cont'd) ¦ ¦ ¦ | ¦ ¦ 3) Secondary Flight ¦ ¦ ¦ | ¦¦ Display Units ¦ ¦ ¦ | ¦¦ (SFD's)(Meggitt) ¦ ¦ ¦ | ¦¦ (Cont'd) ¦ ¦ ¦ | ¦ ¦ d) Standby C ¦ - ¦ 0 ¦ May be inoperative provided: | ¦¦ Heading ¦ ¦ ¦ a) All installed Heading | ¦¦ Display(s) ¦ ¦ ¦ Reference Systems operate | ¦¦ ¦ ¦ ¦ normally, and | ¦¦ ¦ ¦ ¦ b) Magnetic compass operates | ¦¦ ¦ ¦ ¦ normally. | ¦¦ ¦ ¦ ¦ | ¦¦ e) Standby Mach C ¦ 1 ¦ 0 ¦ | ¦¦ Number ¦ ¦ ¦ | ¦¦ Indicator ¦ ¦ ¦ | ¦¦ ¦ ¦ ¦ | ¦¦ f) ILS Button C ¦ 1 ¦ 0 ¦ | ¦¦ ¦ ¦ ¦ | ¦¦ g) HP/IN C ¦ 1 ¦ 0 ¦ | ¦¦ Button ¦ ¦ ¦ | ¦¦ ¦ ¦ ¦ | ¦¦ h) Light C ¦ 1 ¦ 0 ¦ | ¦¦ Sensor ¦ ¦ ¦ | ¦ ¦ 24. Air Data Computer ¦ ¦ ¦ Deleted, Revision 2. ¦¦ System ¦ ¦ ¦ ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 34-12 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 34 NAVIGATION ¦ ¦ ¦ ¦ ¦ 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. ¦ ¦ 32-1 ILS Offset System C ¦ 1 ¦ 0 ¦ May be inoperative provided pro- | ¦¦ *** ¦ ¦ ¦ cedures do not require its use. | ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 34-13 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 34 NAVIGATION ¦ ¦ ¦ ¦ ¦ 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 two | ¦¦ ¦ ¦ ¦ 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: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 34-14 ¦¦ --------------------------------------------------------------------------- ¦¦ 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 two ¦¦ System (TAWS) ¦ ¦ ¦ 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. ¦ ¦ C ¦ - ¦ 0 ¦ (O)May be inoperative provided: | ¦¦ ¦ ¦ ¦ a) System(s) not required by | ¦¦ ¦ ¦ ¦ FAR, and | ¦¦ ¦ ¦ ¦ b) Alternate procedures are | ¦¦ ¦ ¦ ¦ established and used. | ¦ ¦ 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. ¦ ¦ C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided: | ¦¦ ¦ ¦ ¦ a) System(s) not required by | ¦¦ ¦ ¦ ¦ FAR, and | ¦¦ ¦ ¦ ¦ b) Alternate procedures are | ¦¦ ¦ ¦ ¦ established and used. | ¦ ¦ ¦ ¦ ¦ (Continued) ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 34-15 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 34 NAVIGATION ¦ ¦ ¦ ¦ ¦ 40-4 Ground Proximity ¦ ¦ ¦ ¦¦ Warning System ¦ ¦ ¦ ¦¦ (GPWS)/Terrain ¦ ¦ ¦ ¦¦ Awareness Warning ¦ ¦ ¦ ¦¦ System (TAWS) ¦ ¦ ¦ ¦¦ (Cont'd) ¦ ¦ ¦ ¦ ¦ 3) Glideslope B ¦ 2 ¦ 0 ¦ ¦¦ Deviation ¦ ¦ ¦ ¦¦ (Mode 5) C ¦ 2 ¦ 0 ¦ May be inoperative provided: ¦¦ ¦ ¦ ¦ a) System is not required by ¦¦ ¦ ¦ ¦ FAR, and ¦¦ ¦ ¦ ¦ b) GPWS is considered ¦¦ ¦ ¦ ¦ inoperative. ¦ ¦ *** 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: ¦¦ ¦ ¦ ¦ a) Alternate procedures are ¦¦ ¦ ¦ ¦ established and used, and ¦¦ ¦ ¦ ¦ b) Windshear Detection and | ¦¦ ¦ ¦ ¦ Avoidance System operates | ¦¦ ¦ ¦ ¦ normally. | ¦ ¦ C ¦ - ¦ 0 ¦ (O)May be inoperative provided: | ¦¦ ¦ ¦ ¦ a) Alternate procedures are | ¦¦ ¦ ¦ ¦ established and used, and | ¦¦ ¦ ¦ ¦ b) Takeoffs and landings are | ¦¦ ¦ ¦ ¦ not conducted in known or | ¦¦ ¦ ¦ ¦ forecast windshear | ¦¦ ¦ ¦ ¦ conditions. | ¦ ¦ *** 6) Enhanced GPWS C ¦ - ¦ 0 ¦ ¦¦ (EGPWS) ¦ ¦ ¦ ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 34-16 ¦¦ --------------------------------------------------------------------------- ¦¦ 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 ¦ ¦ ¦ cedures do not require its use. | ¦ ¦ 43-1 ATC Transponder C ¦ 1 ¦ 0 ¦ May be inoperative provided pro- | ¦¦ *** Attenuation System ¦ ¦ ¦ cedures do not require its use. | ¦ ¦ 50-1 LNAV or RNAV C ¦ - ¦ - ¦ As required by FAR. ¦¦ Systems ¦ ¦ ¦ ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 34-17 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 34 NAVIGATION ¦ ¦ ¦ ¦ ¦ 50-2 Flight Management C ¦ - ¦ 0 ¦ (O)Except as required by FAR, may | ¦¦ *** Systems (FMS) ¦ ¦ ¦ be inoperative provided: | ¦¦ ¦ ¦ ¦ a) Enroute operations and | ¦¦ ¦ ¦ ¦ approach procedures do not | ¦¦ ¦ ¦ ¦ require its use, and | ¦¦ ¦ ¦ ¦ b) Alternate procedures are | ¦¦ ¦ ¦ ¦ established and used. | ¦ ¦ 1) NAV Data Base C ¦ - ¦ - ¦ (O)May be out of currency provided: | ¦¦ ¦ ¦ ¦ a) Current Aeronautical Charts ¦¦ ¦ ¦ ¦ are used 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. ¦¦ ¦ ¦ ¦ | ¦ ¦ 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. ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 34-18 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 34 NAVIGATION ¦ ¦ ¦ ¦ ¦ 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 at each pilot position. | ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 34-19 ¦¦ --------------------------------------------------------------------------- ¦¦ 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 ¦ ¦ ¦ secured, and ¦¦ and/or 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 ¦ May be inoperative on the | ¦¦ Traffic Alert ¦ ¦ ¦ non-flying pilot side provided: | ¦¦ (TA) and ¦ ¦ ¦ a) TA and RA visual display | ¦¦ Resolution ¦ ¦ ¦ is operative on the flying | ¦¦ Advisory (RA) ¦ ¦ ¦ pilot's side, and | ¦¦ Dual Display ¦ ¦ ¦ b) TA and RA audio function | ¦¦ System(s) ¦ ¦ ¦ is operative on the flying | ¦¦ ¦ ¦ ¦ pilot's side. | ¦ ¦ 2) Resolution C ¦ 2 ¦ 1 ¦ May be inoperative on non-flying | ¦¦ Advisory (RA) ¦ ¦ ¦ pilot's side. ¦¦ Display ¦ ¦ ¦ ¦¦ System(s) C ¦ - ¦ 0 ¦ (O)May be inoperative provided: | ¦¦ ¦ ¦ ¦ a) Traffic Alert (TA) visual | ¦¦ ¦ ¦ ¦ display and audio functions | ¦¦ ¦ ¦ ¦ are operative, | ¦¦ ¦ ¦ ¦ b) TA only mode is selected by ¦¦ ¦ ¦ ¦ the crew, and ¦¦ ¦ ¦ ¦ c) Enroute and/or approach | ¦¦ ¦ ¦ ¦ procedures do not require | ¦¦ ¦ ¦ ¦ their use. | ¦ ¦ ¦ ¦ ¦ (Continued) ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 34-20 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 34 NAVIGATION ¦ ¦ ¦ ¦ ¦ 60-1 Traffic Collision ¦ ¦ ¦ ¦¦ and Avoidance ¦ ¦ ¦ ¦¦ System (TCAS I ¦ ¦ ¦ ¦¦ and/or TCAS II) ¦ ¦ ¦ ¦¦ (Cont'd) ¦ ¦ ¦ ¦ ¦ 3) Traffic Alert C ¦ - ¦ 0 ¦ (O)May be inoperative provided: | ¦¦ (TA) Display ¦ ¦ ¦ a) RA visual display and audio | ¦¦ System(s) ¦ ¦ ¦ functions are operative, and | ¦¦ ¦ ¦ ¦ b) Enroute and/or approach | ¦¦ ¦ ¦ ¦ procedures do not require | ¦¦ ¦ ¦ ¦ its use. | ¦ ¦ 60-2 Windshear Detector C ¦ - ¦ 0 ¦ ¦¦ *** System ¦ ¦ ¦ ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 34-21 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 34 NAVIGATION ¦ ¦ ¦ ¦ ¦ 70-1 EFIS/MFD Cooling ¦ ¦ ¦ ¦¦ Fans (Except ¦ ¦ ¦ | ¦¦ Collins ProLine ¦ ¦ ¦ | ¦¦ 21-Equipped A/C) ¦ ¦ ¦ | ¦ ¦ 1) Aircraft with 5 A ¦ 5 ¦ 4 ¦ (O)One may be inoperative provided: | ¦¦ Fans Installed ¦ ¦ ¦ a) Standby attitude indicator | ¦¦ ¦ ¦ ¦ operates normally, ¦¦ ¦ ¦ ¦ b) Bearing Distance Indicator | ¦¦ ¦ ¦ ¦ (BDI) and standby compass | ¦¦ ¦ ¦ ¦ operate normally, ¦¦ ¦ ¦ ¦ c) Cabin temperature can be ¦¦ ¦ ¦ ¦ maintained below 35 degrees ¦¦ ¦ ¦ ¦ C, and ¦¦ ¦ ¦ ¦ d) Repairs are made within ¦¦ ¦ ¦ ¦ three flight days. ¦ ¦ 2) Aircraft with 3 A ¦ 3 ¦ 2 ¦ (O)One may be inoperative provided: | ¦¦ Fans Installed ¦ ¦ ¦ a) Standby attitude indicator | ¦¦ ¦ ¦ ¦ operates normally, ¦¦ ¦ ¦ ¦ b) Distance Bearing Indicator | ¦¦ ¦ ¦ ¦ (BDI) 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: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 34-22 ¦¦ --------------------------------------------------------------------------- ¦¦ 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: | ¦¦ Annunciators ¦ ¦ ¦ a) All EFIS/MFD cooling fans | ¦¦ (Series 700, 800 ¦ ¦ ¦ are verified to operate ¦¦ and 800XP, Except ¦ ¦ ¦ normally before each ¦¦ Proline 21 ¦ ¦ ¦ departure, and ¦¦ Equipped Aircraft) ¦ ¦ ¦ b) Associated EFIS/MFD FAN FAIL | ¦¦ ¦ ¦ ¦ annunciators operate | ¦¦ ¦ ¦ ¦ normally. ¦ ¦ C ¦ - ¦ - ¦ (O)One may be inoperative provided: | ¦¦ ¦ ¦ ¦ a) Nose Cooling Fan and Fan | ¦¦ ¦ ¦ ¦ Door are confirmed to | ¦¦ ¦ ¦ ¦ operate normally, | ¦¦ ¦ ¦ ¦ b) Associated EFIS/MFD FAN FAIL | ¦¦ ¦ ¦ ¦ Annunciators operate | ¦¦ ¦ ¦ ¦ normally, and | ¦¦ ¦ ¦ ¦ c) Ground use of EFIS is | ¦¦ ¦ ¦ ¦ limited to not more than 30 | ¦¦ ¦ ¦ ¦ minutes. | ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 34-23 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 34 NAVIGATION ¦ ¦ ¦ ¦ ¦ 70-3 EFIS/MFD FAN FAIL C ¦ - ¦ - ¦ (O)One may be inoperative provided: | ¦¦ Annunciators ¦ ¦ ¦ a) Nose Cooling Fan and Fan | ¦¦ (Series 700, 800, ¦ ¦ ¦ Door are confirmed to | ¦¦ 800XP Only Except ¦ ¦ ¦ operate normally before each | ¦¦ Proline 21 ¦ ¦ ¦ departure, | ¦¦ Equipped Aircraft) ¦ ¦ ¦ b) Associated EFIS/MFD OVHT | ¦¦ ¦ ¦ ¦ Annunciators operate | ¦¦ ¦ ¦ ¦ normally, and | ¦¦ ¦ ¦ ¦ c) Ground use of EFIS is | ¦¦ ¦ ¦ ¦ limited to not more than | ¦¦ ¦ ¦ ¦ 30 minutes. | ¦¦ ¦ ¦ ¦ | ¦¦ C ¦ - ¦ 0 ¦ (M)May be inoperative provided: | ¦¦ ¦ ¦ ¦ a) All EFIS/MFD cooling fans | ¦¦ ¦ ¦ ¦ are verified to operate | ¦¦ ¦ ¦ ¦ normally before each | ¦¦ ¦ ¦ ¦ departure, | ¦¦ ¦ ¦ ¦ b) Associated EFIS/MFD overheat | ¦¦ ¦ ¦ ¦ system operates normally, | ¦¦ ¦ ¦ ¦ and ¦¦ ¦ ¦ ¦ c) Ground use of EFIS is | ¦¦ ¦ ¦ ¦ limited to not more than | ¦¦ ¦ ¦ ¦ 30 minutes. | ¦ ¦ 70-4 Electronic Flight ¦ ¦ ¦ | ¦¦ Displays (EFD's) ¦ ¦ ¦ | ¦ ¦ 1) Non-Collins C ¦ 4 ¦ 3 ¦ (O)One unit may be inoperative | ¦¦ Proline 21 ¦ ¦ ¦ provided an independent PFD/EADI is | ¦¦ Equipped ¦ ¦ ¦ available at each pilot's station. | ¦¦ Aircraft, Only ¦ ¦ ¦ | ¦ ¦ 2) Collins Proline C ¦ 4 ¦ 3 ¦ One unit may be inoperative | ¦¦ 21 Equipped ¦ ¦ ¦ provided inoperative unit is ¦¦ Aircraft, Only ¦ ¦ ¦ positioned in Copilot MFD location. ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 34-24 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 34 NAVIGATION ¦ ¦ ¦ ¦ ¦ 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. ¦ ¦ 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 Revision 4. ¦¦ (FAA Flight ¦ ¦ ¦ ¦¦ Inspection ¦ ¦ ¦ ¦¦ Aircraft only) ¦ ¦ ¦ ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 34-25 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 34 NAVIGATION ¦ ¦ ¦ ¦ ¦ 70-9 Multifunction C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided: ¦¦ Display Controller ¦ ¦ ¦ a) Procedures do not require ¦¦ (Honeywell ¦ ¦ ¦ its use, ¦¦ Equipped Aircraft, ¦ ¦ ¦ b) When Radar is required, at | ¦¦ Only) ¦ ¦ ¦ least one Radar Display is ¦¦ ¦ ¦ ¦ confirmed to operate | ¦¦ ¦ ¦ ¦ normally before each | ¦¦ ¦ ¦ ¦ departure, and | ¦¦ ¦ ¦ ¦ c) Before each departure, both | ¦¦ ¦ ¦ ¦ Symbol Generators (SG) and ¦¦ ¦ ¦ ¦ their reversionary switching ¦¦ ¦ ¦ ¦ are confirmed to operate | ¦¦ ¦ ¦ ¦ normally, and ¦¦ ¦ ¦ ¦ d) Alternate Normal and | ¦¦ ¦ ¦ ¦ Emergency Procedures are | ¦¦ ¦ ¦ ¦ established and used. | ¦ ¦ 70-10 Nose Compartment ¦ ¦ ¦ | ¦¦ Avionics Cooling ¦ ¦ ¦ | ¦¦ System ¦ ¦ ¦ | ¦¦ ¦ ¦ ¦ | ¦¦ ¦ ¦ ¦ | ¦¦ ¦ ¦ ¦ | ¦¦ ¦ ¦ ¦ | ¦¦ 1) Avionics C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided: | ¦¦ Cooling Fan ¦ ¦ ¦ a) Avionics Cooling Fan Door | ¦¦ ¦ ¦ ¦ remains closed, and | ¦¦ ¦ ¦ ¦ b) Ground operation of the EFIS | ¦¦ ¦ ¦ ¦ and MFD is limited to not | ¦¦ ¦ ¦ ¦ more than 30 minutes. | ¦¦ ¦ ¦ ¦ | ¦¦ 2) Avionics C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided: | ¦¦ Cooling Fan ¦ ¦ ¦ a) Avionics Cooling Fan Door | ¦¦ Door ¦ ¦ ¦ remains closed, and | ¦¦ ¦ ¦ ¦ b) Ground operation of the EFIS | ¦¦ ¦ ¦ ¦ and MFD is limited to not | ¦¦ ¦ ¦ ¦ more than 30 minutes. | ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 34-26 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 34 NAVIGATION ¦ ¦ ¦ ¦ ¦ 70-11 Electronic ¦ ¦ ¦ Relief incorporated into item | ¦¦ Checklist System ¦ ¦ ¦ 34.70-9. | ¦¦ (Aircraft with ¦ ¦ ¦ ¦¦ MC-800 MFD ¦ ¦ ¦ ¦¦ Controller ¦ ¦ ¦ ¦¦ Installed) ¦ ¦ ¦ ¦ ¦ 70-12 Nose Compartment ¦ ¦ ¦ ¦¦ Ventilation ¦ ¦ ¦ ¦¦ System (Collins ¦ ¦ ¦ ¦¦ Equipped ¦ ¦ ¦ ¦¦ Aircraft Except ¦ ¦ ¦ ¦¦ Pro-Line 21) ¦ ¦ ¦ ¦ ¦ 1) Avionics C ¦ 1 ¦ 0 ¦ (M)May be inoperative OFF provided | ¦¦ Cooling Fan ¦ ¦ ¦ Avionics Nose Cooling Fan is ¦¦ Low Speed ¦ ¦ ¦ verified to operate normally. ¦¦ Warning ¦ ¦ ¦ ¦¦ Detector ¦ ¦ ¦ ¦ ¦ 2) Avionics C ¦ 1 ¦ 0 ¦ (M)May be inoperative OFF provided | ¦¦ Cooling Fan ¦ ¦ ¦ Avionics Nose Cooling Fan is ¦¦ Nose FAIL ¦ ¦ ¦ verified to operate normally. ¦¦ Annunciator ¦ ¦ ¦ ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 34-27 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 34 NAVIGATION ¦ ¦ ¦ ¦ ¦ 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: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 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 ¦ ¦ ¦ | ¦¦ Indicator(s) ¦ ¦ ¦ | ¦¦ ¦ ¦ ¦ | ¦¦ 1) Servicing D ¦ - ¦ 0 ¦ (O)May be inoperative provided: | ¦¦ Gauge ¦ ¦ ¦ a) Cockpit gauge is confirmed | ¦¦ ¦ ¦ ¦ to operate normally, and | ¦¦ ¦ ¦ ¦ b) Contents are confirmed full | ¦¦ ¦ ¦ ¦ following servicing of the | ¦¦ ¦ ¦ ¦ oxygen system. | ¦ ¦ 2) Cockpit Gauge C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided: | ¦¦ ¦ ¦ ¦ a) Flight remains at or below | ¦¦ ¦ ¦ ¦ 10,000 feet MSL, | ¦¦ ¦ ¦ ¦ b) An acceptable procedure is | ¦¦ ¦ ¦ ¦ used to confirm oxygen | ¦¦ ¦ ¦ ¦ supply is above minimum | ¦¦ ¦ ¦ ¦ required to complete the | ¦¦ ¦ ¦ ¦ AFM smoke evacuation | ¦¦ ¦ ¦ ¦ procedures, and | ¦¦ ¦ ¦ ¦ c) Passengers, if carried, are | ¦¦ ¦ ¦ ¦ appropriately briefed. | ¦ ¦ C ¦ 1 ¦ 0 ¦ (O)Except where required by FAR, | ¦¦ ¦ ¦ ¦ may be inoperative provided: | ¦¦ ¦ ¦ ¦ a) Before each departure, an | ¦¦ ¦ ¦ ¦ acceptable procedure is used | ¦¦ ¦ ¦ ¦ to confirm oxygen supply is | ¦¦ ¦ ¦ ¦ above minimum required for | ¦¦ ¦ ¦ ¦ the flight, and | ¦¦ ¦ ¦ ¦ b) It is confirmed that the | ¦¦ ¦ ¦ ¦ fault is in the indicator | ¦¦ ¦ ¦ ¦ only. | ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 35-2 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 35 OXYGEN ¦ ¦ ¦ ¦ ¦ 00-2 Oxygen Cylinders ¦ ¦ ¦ ¦ ¦ 1) Aircraft A ¦ - ¦ 1 ¦ (O)May be inoperative provided: | ¦¦ Fitted With ¦ ¦ ¦ a) Aircraft remains at or below | ¦¦ 750 Liter ¦ ¦ ¦ 10,000 feet MSL, | ¦¦ Bottles ¦ ¦ ¦ b) Passenger oxygen supply | ¦¦ ¦ ¦ ¦ valve is confirmed closed, | ¦¦ ¦ ¦ ¦ c) Passengers are appropriately ¦¦ ¦ ¦ ¦ briefed, ¦¦ ¦ ¦ ¦ d) Oxygen supply to the flight ¦¦ ¦ ¦ ¦ crew is confirmed adequate | ¦¦ ¦ ¦ ¦ to meet operations being ¦¦ ¦ ¦ ¦ conducted, ¦¦ ¦ ¦ ¦ e) Cockpit oxygen quantity | ¦¦ ¦ ¦ ¦ indicator is confirmed to | ¦¦ ¦ ¦ ¦ operate normally, and | ¦¦ ¦ ¦ ¦ f) Repairs are made within | ¦¦ ¦ ¦ ¦ three flight days. | ¦ ¦ C ¦ - ¦ 2 ¦ (O)Any bottles in excess of | ¦¦ ¦ ¦ ¦ minimum may be inoperative provided | ¦¦ ¦ ¦ ¦ oxygen supply to the flight crew | ¦¦ ¦ ¦ ¦ and passengers is confirmed | ¦¦ ¦ ¦ ¦ adequate to meet operations being | ¦¦ ¦ ¦ ¦ conducted. | ¦ ¦ 2) Aircraft C ¦ - ¦ 1 ¦ (O)Any bottles in excess of | ¦¦ Fitted With ¦ ¦ ¦ minimum may be inoperative provided | ¦¦ 1,400 Liter ¦ ¦ ¦ oxygen supply to the flight crew | ¦¦ Bottles ¦ ¦ ¦ and passengers is confirmed | ¦¦ ¦ ¦ ¦ adequate to meet operations being | ¦¦ ¦ ¦ ¦ conducted. | ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 35-3 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 35 OXYGEN ¦ ¦ ¦ ¦ ¦ 00-3 Barometric Valve C ¦ 1 ¦ 0 ¦ (M)(O)May be inoperative provided: | ¦¦ Automatic Function ¦ ¦ ¦ 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. | ¦¦ Equipment (PBE) ¦ ¦ ¦ ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 35-4 ¦¦ --------------------------------------------------------------------------- ¦¦ 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 ¦ ¦ ¦ Associated seats are blocked and ¦¦ ¦ ¦ ¦ placarded to prevent occupancy. ¦¦ ¦ ¦ ¦ | ¦¦ C ¦ - ¦ 0 ¦ (O)May be inoperative provided: | ¦¦ ¦ ¦ ¦ a) Flight is not conducted ¦¦ ¦ ¦ ¦ where the minimum enroute ¦¦ ¦ ¦ ¦ altitude is above 14,000 ¦¦ ¦ ¦ ¦ feet MSL, ¦¦ ¦ ¦ ¦ b) Pressurization system ¦¦ ¦ ¦ ¦ operates normally, ¦¦ ¦ ¦ ¦ c) Flight remains at or below ¦¦ ¦ ¦ ¦ FL 250, ¦¦ ¦ ¦ ¦ d) Portable oxygen is provided ¦¦ ¦ ¦ ¦ to each passenger above ¦¦ ¦ ¦ ¦ 15,000 feet MSL, and ¦¦ ¦ ¦ ¦ e) 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: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 38-1 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 38 WATER/WASTE ¦ ¦ ¦ ¦ ¦ 10-1 Potable Water C ¦ - ¦ - ¦ (M)Individual components may be | ¦¦ System ¦ ¦ ¦ inoperative provided: | ¦¦ ¦ ¦ ¦ a) Associated components are | ¦¦ ¦ ¦ ¦ deactivated or isolated, and | ¦¦ ¦ ¦ ¦ b) Associated system components | ¦¦ ¦ ¦ ¦ are verified not to have | ¦¦ ¦ ¦ ¦ leaks. | ¦¦ ¦ ¦ ¦ | ¦¦ ¦ ¦ ¦ NOTE: Any portion of the system | ¦¦ ¦ ¦ ¦ which operates normally may | ¦¦ ¦ ¦ ¦ be used. | ¦¦ ¦ ¦ ¦ | ¦¦ D ¦ - ¦ - ¦ (O)May be inoperative provided: | ¦¦ ¦ ¦ ¦ a) System is drained, and | ¦¦ ¦ ¦ ¦ b) Procedures are established | ¦¦ ¦ ¦ ¦ to ensure that the system is | ¦¦ ¦ ¦ ¦ not serviced. | ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 38-2 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 38 WATER/WASTE ¦ ¦ ¦ ¦ ¦ 10-2 Lavatory Waste C ¦ - ¦ - ¦ (M)Individual components may be | ¦¦ System(s) ¦ ¦ ¦ inoperative provided: | ¦¦ ¦ ¦ ¦ a) Affected component (Lavatory | ¦¦ ¦ ¦ ¦ Sink Water Supply, or | ¦¦ ¦ ¦ ¦ Lavatory Toilet Water | ¦¦ ¦ ¦ ¦ Supply) are deactivated and | ¦¦ ¦ ¦ ¦ isolated, and | ¦¦ ¦ ¦ ¦ b) Affected system component is | ¦¦ ¦ ¦ ¦ verified not to have leaks. | ¦¦ ¦ ¦ ¦ | ¦¦ ¦ ¦ ¦ NOTE: Any portion of the system | ¦¦ ¦ ¦ ¦ which operates normally may | ¦¦ ¦ ¦ ¦ be used. | ¦¦ ¦ ¦ ¦ | ¦¦ C ¦ - ¦ - ¦ (M)Associated lavatory system(s) | ¦¦ ¦ ¦ ¦ may be inoperative provided: | ¦¦ ¦ ¦ ¦ a) Associated components | ¦¦ ¦ ¦ ¦ (Lavatory Sink Water Supply, | ¦¦ ¦ ¦ ¦ and Lavatory Toilet Water | ¦¦ ¦ ¦ ¦ Supply) are deactivated, | ¦¦ ¦ ¦ ¦ drained, and removed to | ¦¦ ¦ ¦ ¦ prevent leaks, | ¦¦ ¦ ¦ ¦ b) Pilot-in-Command determines | ¦¦ ¦ ¦ ¦ that flight duration is | ¦¦ ¦ ¦ ¦ acceptable with lavatory(s) | ¦¦ ¦ ¦ ¦ unusable, and | ¦¦ ¦ ¦ ¦ c) Associated lavatory door(s) | ¦¦ ¦ ¦ ¦ is secured closed and | ¦¦ ¦ ¦ ¦ placarded, "INOPERATIVE - DO | ¦¦ ¦ ¦ ¦ NOT ENTER." | ¦¦ ¦ ¦ ¦ | ¦¦ ¦ ¦ ¦ NOTE: These provisions are not | ¦¦ ¦ ¦ ¦ intended to prohibit | ¦¦ ¦ ¦ ¦ inspections by crewmembers. | ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 38-3 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 38 WATER/WASTE ¦ ¦ ¦ ¦ ¦ 10-3 Lavatory Plug C ¦ - ¦ 0 ¦ (O)May be inoperative, or missing, | ¦¦ Assembly (Lavatory ¦ ¦ ¦ provided: | ¦¦ Doughnut) ¦ ¦ ¦ a) Associated Lavatory Waste | ¦¦ ¦ ¦ ¦ Tank is drained, | ¦¦ ¦ ¦ ¦ b) Pilot in Command determines | ¦¦ ¦ ¦ ¦ that flight duration is | ¦¦ ¦ ¦ ¦ acceptable with lavatory(s) | ¦¦ ¦ ¦ ¦ unusable, | ¦¦ ¦ ¦ ¦ c) Associated lavatory door(s) | ¦¦ ¦ ¦ ¦ is secured closed and | ¦¦ ¦ ¦ ¦ placarded, "INOPERATIVE - DO | ¦¦ ¦ ¦ ¦ NOT ENTER," | ¦¦ ¦ ¦ ¦ d) Ram Air and Dump Valves are | ¦¦ ¦ ¦ ¦ confirmed to operate | ¦¦ ¦ ¦ ¦ normally before the first | ¦¦ ¦ ¦ ¦ flight of the day, | ¦¦ ¦ ¦ ¦ e) Before each departure, DUMP | ¦¦ ¦ ¦ ¦ VLV is selected OPEN, | ¦¦ ¦ ¦ ¦ f) Flight is conducted in an | ¦¦ ¦ ¦ ¦ unpressurized configuration, | ¦¦ ¦ ¦ ¦ and | ¦¦ ¦ ¦ ¦ g) Altitude limitations in | ¦¦ ¦ ¦ ¦ accordance with FAR | ¦¦ ¦ ¦ ¦ operating rules are | ¦¦ ¦ ¦ ¦ observed. | ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 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 ¦ May be inoperative provided APU is | ¦¦ Unit ¦ ¦ ¦ not used. | ¦ ¦ 10-1 APU Air/Load C ¦ 1 ¦ 0 ¦ (M)(O)May be inoperative provided: | ¦¦ Control Valve ¦ ¦ ¦ a) Air valve is secured closed, ¦¦ ¦ ¦ ¦ and ¦¦ ¦ ¦ ¦ b) APU air switch remains OFF. ¦ ¦ ¦ ¦ ¦ NOTE: If APU and APU Generator | ¦¦ ¦ ¦ ¦ operate normally, APU may be | ¦¦ ¦ ¦ ¦ used to provide electric | ¦¦ ¦ ¦ ¦ power. ¦ ¦ C ¦ 1 ¦ 0 ¦ May be inoperative provided APU is | ¦¦ ¦ ¦ ¦ not used. | ¦ ¦ 10-2 APU ¦ ¦ ¦ ¦¦ Instrumentation ¦ ¦ ¦ ¦ ¦ 1) RPM/EGT C ¦ 2 ¦ 0 ¦ May be inoperative provided APU is | ¦¦ Indicators ¦ ¦ ¦ not used. | ¦¦ (T62T- ¦ ¦ ¦ ¦¦ 40C8D/T62T- ¦ ¦ ¦ ¦¦ 40C8D1 And ¦ ¦ ¦ ¦¦ 36-150/92/100/ ¦ ¦ ¦ ¦¦ APU Only) ¦ ¦ ¦ ¦ ¦ 2) Amp Meter/Load C ¦ 1 ¦ 0 ¦ May be inoperative provided APU is | ¦¦ Meter ¦ ¦ ¦ not used. | ¦ ¦ 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: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 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 ¦ ¦ ¦ confirmed to be fully closed and | ¦¦ ¦ ¦ ¦ locked before each departure. ¦ ¦ 25-1 Rear Baggage C ¦ - ¦ 0 ¦ (O)May be inoperative OFF provided | ¦¦ Pannier Door ¦ ¦ ¦ door(s) is visually and manually | ¦¦ Unlock Indications ¦ ¦ ¦ confirmed fully closed and locked | ¦¦ ¦ ¦ ¦ before each departure. ¦ ¦ C ¦ - ¦ 0 ¦ (M)(O)May be inoperative ON | ¦¦ ¦ ¦ ¦ provided: | ¦¦ ¦ ¦ ¦ a) System is deactivated, and | ¦¦ ¦ ¦ ¦ b) Door(s) is visually and | ¦¦ ¦ ¦ ¦ manually confirmed fully | ¦¦ ¦ ¦ ¦ closed and locked before | ¦¦ ¦ ¦ ¦ each departure. | ¦ ¦ 25-2 Rear Baggage C ¦ 1 ¦ O ¦ (O)May be inoperative OFF provided | ¦¦ Pannier Hatch ¦ ¦ ¦ associated hatch is both visually | ¦¦ Unlock Indication ¦ ¦ ¦ and manually confirmed fully closed | ¦¦ ¦ ¦ ¦ and locked before each departure. | ¦ ¦ C ¦ 1 ¦ 0 ¦ (M)(O)May be inoperative ON | ¦¦ ¦ ¦ ¦ provided: | ¦¦ ¦ ¦ ¦ a) System is deactivated, and | ¦¦ ¦ ¦ ¦ b) Hatch is both visually and | ¦¦ ¦ ¦ ¦ manually confirmed fully | ¦¦ ¦ ¦ ¦ closed and locked before | ¦¦ ¦ ¦ ¦ each departure. | ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 52-2 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 52 DOORS ¦ ¦ ¦ ¦ ¦ 70-3 Optional Door or C ¦ 1 ¦ 0 ¦ (O)May be inoperative OFF provided | ¦¦ *** Hatch Unlocked ¦ ¦ ¦ associated door(s) or hatch(es) is | ¦¦ Annunciator ¦ ¦ ¦ visually and manually confirmed | ¦¦ ¦ ¦ ¦ fully closed and locked before each | ¦¦ ¦ ¦ ¦ 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. ¦ ¦ 70-4 Right and Left ¦ ¦ ¦ Deleted Revision 5. | ¦¦ Avionics Access ¦ ¦ ¦ ¦¦ Doors ¦ ¦ ¦ ¦ ¦ 70-5 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. ¦ ¦ 70-6 Ramp Guard System D ¦ - ¦ 0 ¦ | ¦¦ *** ¦ ¦ ¦ ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 56-1 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 56 WINDOWS ¦ ¦ ¦ ¦ ¦ 10-1 Windscreen (Panel C ¦ - ¦ - ¦ (M)(O)May be delaminated provided: ¦¦ "A")(Series 1 ¦ ¦ ¦ a) Visibility through the ¦¦ Through 700) ¦ ¦ ¦ affected windscreen(s) is | ¦¦ ¦ ¦ ¦ acceptable to the crew, ¦¦ ¦ ¦ ¦ b) Airplane is not operated in ¦¦ ¦ ¦ ¦ known or forecast icing ¦¦ ¦ ¦ ¦ conditions, ¦¦ ¦ ¦ ¦ c) Associated 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" (Series ¦ ¦ ¦ be delaminated provided: ¦¦ 800 and 800XP ¦ ¦ ¦ a) Visibility through the ¦¦ Only) ¦ ¦ ¦ affected windscreen is ¦¦ ¦ ¦ ¦ acceptable to the crew, and ¦¦ ¦ ¦ ¦ vision is not impaired on ¦¦ ¦ ¦ ¦ the remaining windscreens, | ¦¦ ¦ ¦ ¦ b) Airplane is not operated in ¦¦ ¦ ¦ ¦ known or forecast icing ¦¦ ¦ ¦ ¦ conditions, ¦¦ ¦ ¦ ¦ c) Associated SCREEN HEAT CTL | ¦¦ ¦ ¦ ¦ circuit breaker is pulled ¦¦ ¦ ¦ ¦ and collared, and | ¦¦ ¦ ¦ ¦ d) AFM limitations are ¦¦ ¦ ¦ ¦ observed. ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 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 Synchron- C ¦ 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 ¦¦ Engines Only) ¦ ¦ ¦ observed. ¦ ¦ 22-2 Top Temperature C ¦ 2 ¦ 1 ¦ (M)(O)One may be inoperative ¦¦ Control System ¦ ¦ ¦ provided: ¦¦ (Viper Engine ¦ ¦ ¦ a) Associated switch remains ¦¦ Only) ¦ ¦ ¦ OFF, ¦¦ ¦ ¦ ¦ b) Associated circuit breakers ¦¦ ¦ ¦ ¦ are pulled and collared, and ¦¦ ¦ ¦ ¦ c) Associated JPT indicator ¦¦ ¦ ¦ ¦ operates normally. ¦ ¦ 3. Engine Electronic ¦ ¦ ¦ Deleted, Revision 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 1 ¦ ¦ ¦ a) AFM performance limitations ¦¦ Through 800 With ¦ ¦ ¦ are observed, ¦¦ TFE-731 Engines ¦ ¦ ¦ b) APR system is selected OFF, ¦¦ Only) ¦ ¦ ¦ and ¦¦ ¦ ¦ ¦ c) Procedures for monitoring ¦¦ ¦ ¦ ¦ engine limitations are ¦¦ ¦ ¦ ¦ established and used. ¦ ¦ 24-1 Automatic Thrust C ¦ 2 ¦ 0 ¦ (O)May be inoperative provided RPM ¦¦ Limiter System ¦ ¦ ¦ and JPT can be controlled manually. ¦¦ (Viper Engines ¦ ¦ ¦ ¦¦ Only) ¦ ¦ ¦ ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 73-2 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 73 ENGINE FUEL & CONTROL ¦ ¦ ¦ ¦ ¦ 31-1 Fuel Flow C ¦ 2 ¦ 1 ¦ (O)One may be inoperative provided: ¦¦ Indicators ¦ ¦ ¦ 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: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 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: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 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 Indicator ¦ ¦ ¦ ¦¦ Digital ¦ ¦ ¦ ¦¦ Readouts ¦ ¦ ¦ ¦ ¦ a) Digital C ¦ - ¦ 0 ¦ | ¦¦ Readout(s) ¦ ¦ ¦ | ¦¦ (Except ¦ ¦ ¦ | ¦¦ ProLine 21- ¦ ¦ ¦ | ¦¦ Equipped ¦ ¦ ¦ | ¦¦ Aircraft) ¦ ¦ ¦ | ¦ ¦ 2) N2/RPM C ¦ 2 ¦ 1 ¦ (O)One may be inoperative provided ¦¦ Indicators ¦ ¦ ¦ N1 and Fuel Flow Indicators for the ¦¦ ¦ ¦ ¦ associated engine operate normally. ¦ ¦ a) Digital C ¦ - ¦ 0 ¦ | ¦¦ Readout(s) ¦ ¦ ¦ | ¦ ¦ 3) ITT/EGT ¦ ¦ ¦ ¦¦ Indicators ¦ ¦ ¦ ¦ ¦ a) Digital C ¦ - ¦ 0 ¦ | ¦¦ Readout(s) ¦ ¦ ¦ | ¦¦ (Except ¦ ¦ ¦ | ¦¦ ProLine 21- ¦ ¦ ¦ | ¦¦ Equipped ¦ ¦ ¦ | ¦¦ Aircraft) ¦ ¦ ¦ | ¦ ¦ 32-1 Power Loss C ¦ 2 ¦ 0 ¦ (O)May be inoperative provided all ¦¦ Indicator Systems ¦ ¦ ¦ remaining engine indicating systems ¦¦ (Viper Engine ¦ ¦ ¦ operate normally. ¦¦ Only) ¦ ¦ ¦ ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 77-2 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 77 ENGINE INDICATING ¦ ¦ ¦ ¦ ¦ 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 ¦ 0 ¦ (O)May be inoperative provided | ¦¦ Annunciators ¦ ¦ ¦ alternate procedures are | ¦¦ (Series 1 Through ¦ ¦ ¦ established and used. | ¦¦ 800XP With TFE-731 ¦ ¦ ¦ | ¦¦ Engines Only) ¦ ¦ ¦ ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 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 (Series ¦ ¦ ¦ a) No damage to the thrust | ¦¦ 700 and 800, If ¦ ¦ ¦ reverser system exists which | ¦¦ Installed, and ¦ ¦ ¦ would adversely affect | ¦¦ 800XP) ¦ ¦ ¦ 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. ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 79-1 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 79 ENGINE OIL ¦ ¦ ¦ ¦ ¦ 30-1 Oil Pressure Low C ¦ 2 ¦ 0 ¦ (O)May be inoperative provided: ¦¦ Warning Lights/ ¦ ¦ ¦ a) Associated Oil Pressure and ¦¦ Annunciators ¦ ¦ ¦ Oil Temperature Indicators ¦¦ ¦ ¦ ¦ operate normally, ¦¦ ¦ ¦ ¦ b) Associated Oil Tank is ¦¦ ¦ ¦ ¦ serviced to recommended ¦¦ ¦ ¦ ¦ capacity before each ¦¦ ¦ ¦ ¦ departure, and ¦¦ ¦ ¦ ¦ c) There is no evidence of ¦¦ ¦ ¦ ¦ above normal oil consumption ¦¦ ¦ ¦ ¦ or leakage. ¦ -------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦¦ HAWKER SIDDELEY HS-125 ¦ ¦ ¦¦ (SERIES 1 THROUGH 800XP) ¦ DATE: 11/03/2004 ¦ 80-1 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 80 STARTING ¦ ¦ ¦ ¦ ¦ 00-1 Starter Power C ¦ 1 ¦ 0 ¦ ¦¦ Available ¦ ¦ ¦ ¦¦ Annunciator ¦ ¦ ¦ ¦¦ (TFE-731 Engines ¦ ¦ ¦ ¦¦ Only) ¦ ¦ ¦ ¦ ¦ 00-2 Starter Select C ¦ 1 ¦ 0 ¦ ¦¦ Light (Viper ¦ ¦ ¦ ¦¦ Engines Only) ¦ ¦ ¦ ¦ ¦ 00-3 Starter Operating C ¦ 2 ¦ 0 ¦ (O)May be inoperative provided: ¦¦ Annunciators ¦ ¦ ¦ a) Procedures are established | ¦¦ (TFE-731 Engines ¦ ¦ ¦ and used to assure that | ¦¦ Only) ¦ ¦ ¦ start power and EXT PWR ¦¦ ¦ ¦ ¦ switches are disengaged when ¦¦ ¦ ¦ ¦ engine reaches self- ¦¦ ¦ ¦ ¦ sustaining speed, and ¦¦ ¦ ¦ ¦ b) Procedures are established | ¦¦ ¦ ¦ ¦ and used to assure that | ¦¦ ¦ ¦ ¦ associated generator(s) is | ¦¦ ¦ ¦ ¦ on line after each start. | ¦ -------------------------------------------------------------------------------