DEPARTMENT OF TRANSPORTATION Revision: 5 Date: 08/12/2002 FEDERAL AVIATION ADMINISTRATION WASHINGTON, D.C. M A S T E R M I N I M U M E Q U I P M E N T L I S T MITSUBISHI MU-300 MITSUBISHI MU-300-10 BEECH 400 BEECH 400A FEDERAL AVIATION ADMINISTRATION AIRCRAFT EVALUATION GROUP, MKC-AEG 901 LOCUST STREET, ROOM 332 KANSAS CITY, MO 64106-2641 TELEPHONE: (816) 329-3233 FAX: (816) 329-3241

FEDERAL AVIATION ADMINISTRATION Page: I Revision: 5 MASTER MINIMUM EQUIPMENT LIST Date: 08/12/2002 MU-300, MU-300-10, BE-400, BE-400A Table of Contents SYSTEM NO. SYSTEM PAGE -- Table of Contents I -- Log of Revisions II -- Control Page III, IV -- Highlights of Change V, VI, VII, VIII -- Highlights of Change IX, X, XI, XII -- Highlights of Change XIII, XIV, XV -- Definitions XVI, XVII, XVIII, XIX -- Definitions XX, XXI, XXII, XXIII -- Preamble XXIV, XXV -- Guidelines for (O) & (M) Procedures XXVI, XXVII, XXVIII, X -- Guidelines for (O) & (M) Procedures XXX, XXXI 21 Air Conditioning 21-1, 2 22 Auto Flight 22-1, 2 23 Communications 23-1, 2, 3, 4 24 Electrical Power 24-1, 2 25 Equipment/Furnishings 25-1, 2, 3, 4, 5 26 Fire Protection 26-1, 2, 3 27 Flight Controls 27-1 28 Fuel 28-1, 2 29 Hydraulic Power 29-1 30 Ice and Rain Protection 30-1, 2 31 Indicating/Recording Systems 31-1, 2 32 Landing Gear 32-1 33 Lights 33-1, 2, 3 34 Navigation 34-1, 2, 3, 4, 5 34 Navigation 34-6 THRU 10 35 Oxygen 35-1, 2 52 Doors 52-1 73 Engine Fuel & Control 73-1 74 Ignition 74-1 77 Engine Indicating 77-1 78 Engine Exhaust 78-1

FEDERAL AVIATION ADMINISTRATION Page: II Revision: 5 MASTER MINIMUM EQUIPMENT LIST Date: 08/12/2002 MU-300, MU-300-10, BE-400, BE-400A Log of Revisions ---------------------------------------------------------------------- ¦ REV.NO. ¦ DATE ¦ PAGE NUMBERS ¦ INITIALS ¦ ---------------------------------------------------------------------- ¦ ORIGINAL ¦ 03/11/1982 ¦ Original Issue ¦ ¦ ¦ 1 ¦ 07/14/1983 ¦ 28-1 ¦ ¦ ¦ 2 ¦ 11/16/1984 ¦ Complete ¦ ¦ ¦ 3 ¦ 07/09/1991 ¦ ALL PAGES ¦ ¦ ¦ 3a ¦ 06/12/1996 ¦ HIGHLIGHTS OF REV.,DEFINITIONS ¦ ¦ ¦ 3a ¦ 06/12/1996 ¦ GUIDELINES ¦ ¦ ¦ 3a ¦ 06/12/1996 ¦ 21-1,21-2,22-1,23-1,23-2 ¦ ¦ ¦ 3a ¦ 06/12/1996 ¦ 24-1,24-2,25-1,25-2,25-3 ¦ ¦ ¦ 3a ¦ 06/12/1996 ¦ 26-1,26-2,26-3,27-1,28-1 ¦ ¦ ¦ 3a ¦ 06/12/1996 ¦ 28-2,29-1,30-1,30-2,31-1 ¦ ¦ ¦ 3a ¦ 06/12/1996 ¦ 32-1,33-1,33-2,33-3,34-1 ¦ ¦ ¦ 3a ¦ 06/12/1996 ¦ 34-2,34-3,34-4,34-5,34-6 ¦ ¦ ¦ 3a ¦ 06/12/1996 ¦ 35-1,73-1,77-1,78-1 ¦ ¦ ¦ 3b ¦ 07/31/1996 ¦ HIGHLIGHTS OF REV.,DEFINITIONS ¦ ¦ ¦ 3b ¦ 07/31/1996 ¦ 34-1,34-2,34-3,34-4,34-5 ¦ ¦ ¦ 3b ¦ 07/31/1996 ¦ 34-6,34-7 ¦ ¦ ¦ 3c ¦ 07/01/1997 ¦ HIGHLIGHTS OF REV.,DEFINITIONS ¦ ¦ ¦ 3c ¦ 07/01/1997 ¦ 34-1,34-7 ¦ ¦ ¦ 4 ¦ 02/17/1998 ¦ HIGHLIGHTS OF REV.,DEFINITIONS ¦ ¦ ¦ 4 ¦ 02/17/1998 ¦ GUIDELINES ¦ ¦ ¦ 4 ¦ 02/17/1998 ¦ 21-1,21-2,22-1,22-2,23-2 ¦ ¦ ¦ 4 ¦ 02/17/1998 ¦ 23-3,27-1,28-1,28-2,30-1 ¦ ¦ ¦ 4 ¦ 02/17/1998 ¦ 30-2,33-1,33-3,34-1,34-7 ¦ ¦ ¦ 4 ¦ 02/17/1998 ¦ 35-1,73-1,77-1,78-1 ¦ ¦ ¦ 5 ¦ 08/12/2002 ¦ HIGHLIGHTS OF REV.,DEFINITIONS ¦ ¦ ¦ 5 ¦ 08/12/2002 ¦ GUIDELINES ¦ ¦ ¦ 5 ¦ 08/12/2002 ¦ 21-1,21-2,22-1,22-2,23-1 ¦ ¦ ¦ 5 ¦ 08/12/2002 ¦ 23-2,23-3,23-4,24-1,24-2 ¦ ¦ ¦ 5 ¦ 08/12/2002 ¦ 25-1,25-2,25-3,25-4,25-5 ¦ ¦ ¦ 5 ¦ 08/12/2002 ¦ 26-1,26-2,26-3,27-1,28-1 ¦ ¦ ¦ 5 ¦ 08/12/2002 ¦ 28-2,29-1,30-1,30-2,31-1 ¦ ¦ ¦ 5 ¦ 08/12/2002 ¦ 31-2,32-1,33-1,33-2,33-3 ¦ ¦ ¦ 5 ¦ 08/12/2002 ¦ 34-1,34-2,34-3,34-4,34-5 ¦ ¦ ¦ 5 ¦ 08/12/2002 ¦ 34-6,34-7,34-8,34-9,34-10 ¦ ¦ ¦ 5 ¦ 08/12/2002 ¦ 35-1,35-2,52-1,73-1,74-1 ¦ ¦ ¦ 5 ¦ 08/12/2002 ¦ 77-1,78-1 ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ----------------------------------------------------------------------

FEDERAL AVIATION ADMINISTRATION Page: III Revision: 5 MASTER MINIMUM EQUIPMENT LIST Date: 08/12/2002 MU-300, MU-300-10, BE-400, BE-400A Control Page SYSTEM PAGE REV NO. CURRENT DATE Cover Page - 5 08/12/2002 Table of Contents I 5 08/12/2002 Log of Revisions II 5 08/12/2002 Control Page III 5 08/12/2002 IV 5 08/12/2002 Highlights of Change V 5 08/12/2002 VI 5 08/12/2002 VII 5 08/12/2002 VIII 5 08/12/2002 IX 5 08/12/2002 X 5 08/12/2002 XI 5 08/12/2002 XII 5 08/12/2002 XIII 5 08/12/2002 XIV 5 08/12/2002 XV 5 08/12/2002 Definitions XVI 6 01/31/1995 XVII 6 01/31/1995 XVIII 6 01/31/1995 XIX 6 01/31/1995 XX 6 01/31/1995 XXI 6 01/31/1995 XXII 6 01/31/1995 XXIII 6 01/31/1995 Preamble XXIV 2 06/14/1989 XXV 2 06/14/1989 Guidelines for (O) & (M) Procedures XXVI 5 08/12/2002 XXVII 5 08/12/2002 XXVIII 5 08/12/2002 XXIX 5 08/12/2002 XXX 5 08/12/2002 XXXI 5 08/12/2002 21 21-1 5 08/12/2002 21-2 5 08/12/2002 22 22-1 5 08/12/2002 22-2 5 08/12/2002 23 23-1 5 08/12/2002 23-2 5 08/12/2002 23-3 5 08/12/2002 23-4 5 08/12/2002

FEDERAL AVIATION ADMINISTRATION Page: IV Revision: 5 MASTER MINIMUM EQUIPMENT LIST Date: 08/12/2002 MU-300, MU-300-10, BE-400, BE-400A Control Page SYSTEM PAGE REV NO. CURRENT DATE 24 24-1 5 08/12/2002 24-2 5 08/12/2002 25 25-1 5 08/12/2002 25-2 5 08/12/2002 25-3 5 08/12/2002 25-4 5 08/12/2002 25-5 5 08/12/2002 26 26-1 5 08/12/2002 26-2 5 08/12/2002 26-3 5 08/12/2002 27 27-1 5 08/12/2002 28 28-1 5 08/12/2002 28-2 5 08/12/2002 29 29-1 5 08/12/2002 30 30-1 5 08/12/2002 30-2 5 08/12/2002 31 31-1 5 08/12/2002 31-2 5 08/12/2002 32 32-1 5 08/12/2002 33 33-1 5 08/12/2002 33-2 5 08/12/2002 33-3 5 08/12/2002 34 34-1 5 08/12/2002 34-2 5 08/12/2002 34-3 5 08/12/2002 34-4 5 08/12/2002 34-5 5 08/12/2002 34-6 5 08/12/2002 34-7 5 08/12/2002 34-8 5 08/12/2002 34-9 5 08/12/2002 34-10 5 08/12/2002 35 35-1 5 08/12/2002 35-2 5 08/12/2002 52 52-1 5 08/12/2002 73 73-1 5 08/12/2002 74 74-1 5 08/12/2002 77 77-1 5 08/12/2002 78 78-1 5 08/12/2002

FEDERAL AVIATION ADMINISTRATION Page: V Revision: 5 MASTER MINIMUM EQUIPMENT LIST Date: 08/12/2002 MU-300, MU-300-10, BE-400, BE-400A Highlights of Change 21-2 Removed the word OR in accordance with Policy Letter 31. Changed proviso punctuation. 21-10 Removed the word OR in accordance with Policy Letter 31. 21-13 Added relief for Cabin Dump Valve. 21-14 Added the word System to Ventilation Blower and added Maintenance proviso. 21-16 Added the word System to Vapor Cycle Air Conditioning. 21-17 Added the word System to Auxiliary Ground Heater. 21-18 Added relief for Emergency Exit Seal System. 22-1 Added Rudder Boost requirement to proviso. 22-3 Changed proviso in accordance with Policy Letter 93. 22-7 Added (***) 23-1 Revised in accordance with Policy Letter 95 designated as Global Change 111. Changed Proviso for clarification. High Frequency (HF) moved to ATA 23-16 in accordance with Policy Letter 16 designated as Global Change 89. 23-2 Changed proviso in accordance with Policy Letter 29 designated as Global Change 48. 23-3 Revised in accordance with Policy Letter 58 designated as Global Change 100. 23-5 Changed proviso in accordance with Policy Letter 9 designated as Global Change 109. 23-7 Changed repair category to "D" in accordance with Policy Letter 52. 23-9 Changed column 2&3 to (-)variable. 23-10 Added relief for Push to Talk Switch.

FEDERAL AVIATION ADMINISTRATION Page: VI Revision: 5 MASTER MINIMUM EQUIPMENT LIST Date: 08/12/2002 MU-300, MU-300-10, BE-400, BE-400A Highlights of Change 23-11 Added relief for Observer Headset Audio Jack. 23-12 Added relief for Ground Communication Power System. 23-13 Added relief for Crew Intercom System. 23-14 Added relief for Recorded Passenger System. 23-15 Added relief for Static Discharge Wicks. 23-16 Added relief for High Frequency (HF) Communication System in accordance with Policy Letter 106 designated as Global Change 89. 24-12 Added relief for External Power System. 25-1 Changed category to "D" in accordance with Policy Letter 52 and added proviso. 25-2 Changed category to "D" in accordance with Policy Letter 52. Added proviso. 25-3 Changed category to "D" in accordance with Policy Letter 52 and added proviso. 25-4-1 Added relief for ELT Remote Switch. 25-10 Changed relief to category "D" in accordance with Policy Letter 79 designated as Global Change 55. Added relief for Arm Rests and Electrical/Electronic Systems and components. 25-11 Revised in accordance with Policy Letter 33 designated as Global Change 99. 25-14 Renamed from First Aid Kits to Emergency Medical Equipment in accordance with Policy Letter 73 designated as Global Change 104. 25-15 Added relief for EMS Equipment (Air Ambulance). 25-16 Added relief for Protective Breathing Equipment in accordance with Policy Letter 43. 25-17 Added relief for Lavatory Waste System in accordance with Policy Letter 83 designated as Global Change 108.

FEDERAL AVIATION ADMINISTRATION Page: VII Revision: 5 MASTER MINIMUM EQUIPMENT LIST Date: 08/12/2002 MU-300, MU-300-10, BE-400, BE-400A Highlights of Change 25-18 Added relief for Cockpit Door. 25-19 Added relief for Lavatory Door. 25-20 Added relief for Galley Waste Receptables in accordance with Policy Letter 96 designated as Global Change 98. 25-21 Added relief for Cargo Restraint System in accordance with Policy Letter 100 designated as Global Change 73. 25-22 Added relief for Flashlight/Stowage Assembly. 25-23 Added relief for Cockpit Sun Visors. 25-24 Added relief for External Mounted Airspeed Indicator Bugs. 25-25 Added relief for Crewmember Seats. 25-26 Added relief for SmartStart Security System. 26-2 Revised in accordance with Policy Letter 102 designated as Global Change 77. 26-4 Removed the word OR in accordance with Policy Letter 31. 26-5 Removed the word OR in accordance with Policy Letter 31. Changed proviso in accordance with Policy Letter 24 designated as Global Change 106. 30-2 Added *** to reflect fleet variability of installation. 31-3 Changed proviso in accordance with Policy Letter 87 designated as Global Change 101. 31-4 Added relief for Unassigned Annunciators. 31-5 Added relief for Master Caution Annunciator. 31-6 Added relief for Master Warning Annunciator. 32-1 Added (O) procedure requirement.

FEDERAL AVIATION ADMINISTRATION Page: VIII Revision: 5 MASTER MINIMUM EQUIPMENT LIST Date: 08/12/2002 MU-300, MU-300-10, BE-400, BE-400A Highlights of Change 32-3 Added relief for Landing Gear Handle Solenoid with (O) procedure. 33-1-1 Added relief for Tail Position Light in accordance with Policy Letter 91. 33-1-2 Added relief for Wingtip Position Lights. 33-3 Added the word (Flashing) in ITEM column to include older installations, at the request of Raytheon Aircraft Company. 33-13 Added the word 'partially' to the proviso for clarification. 33-14 Added relief for Pulse Light System. 34-4 Reformat Provisos only. No change in text. 34-5 Changed proviso in accordance with Policy Letter 98 designated as Global Change 71. Added Flight Management System (FMS). 34-6 Added relief for Thunderstorm Detection Equipment. 34-7 Revised in accordance with Policy Letter 76 designated as Global Change 110. 34-9 Added the word "System". Added (O) Procedure. 34-10 Changed proviso in accordance with Policy Letter 84 designated as Global Change 59. 34-13 Changed proviso in accordance with Policy Letter 10. 34-15 Changed proviso in accordance with Policy Letter 32 designated as Global Change 81. 34-16 Changed category "D" to "C" in accordance with Policy Letter 32 designated as Global Change 81. Note: System and sequence numbers changed for ATA 34 beginning with item 17. 34-17 Added relief for Traffic Alert Collision Avoidance Device. (TCAD)

FEDERAL AVIATION ADMINISTRATION Page: IX Revision: 5 MASTER MINIMUM EQUIPMENT LIST Date: 08/12/2002 MU-300, MU-300-10, BE-400, BE-400A Highlights of Change 34-18 Changed proviso in accordance with Policy Letter 54 designated as Global Change 107. 34-19 Changed relief for Flight Profile Advisory System (FPAS). 34-22 Changed repair category to "D" in accordance with Policy Letter 52. 34-27 Changed proviso in accordance with Policy Letter 98 designated as Global Change 71. 34-28 Added relief for Windshear Warning and Flight Guidance System in accordance with Policy Letter 67 designated as Global Change 88. 34-29 Added relief for Windshear Detection and Avoidance System in accordance with Policy Letter 67 designated as Global Change 88. 34-30 Added relief for Sonalert Standby Power Indicator. 34-31 Added relief for Standby Power Annunciator. 35-4 Changed repair interval from "B" to "C" and revised remarks. 35-4-1 Added relief for Passenger Oxygen Masks. 35-4-2 Added relief for Passenger Oxygen Mask Access Panels. 35-4-3 Added relief for Passenger Oxygen Cannisters. 35-5 Added relief for Protective Breathing Equipment. 52-1 Added relief for Door Annunciator System. 52-2 Added relief for Cabin Step Snubber and Latch. 52-3 Added relief for Baggage Door Snubber. 52-4 Added relief for Cabin Step Cable (BE-400 and BE-400A). 74-1 Added relief for Ignitor Indicator Lights. 77-1 Revised remarks section. 78-1 Revised remarks section.

FEDERAL AVIATION ADMINISTRATION Page: X Revision: 5 MASTER MINIMUM EQUIPMENT LIST Date: 08/12/2002 MU-300, MU-300-10, BE-400, BE-400A Highlights of Change

FEDERAL AVIATION ADMINISTRATION Page: XI Revision: 5 MASTER MINIMUM EQUIPMENT LIST Date: 08/12/2002 MU-300, MU-300-10, BE-400, BE-400A Highlights of Change

FEDERAL AVIATION ADMINISTRATION Page: XII Revision: 5 MASTER MINIMUM EQUIPMENT LIST Date: 08/12/2002 MU-300, MU-300-10, BE-400, BE-400A Highlights of Change

FEDERAL AVIATION ADMINISTRATION Page: XIII Revision: 5 MASTER MINIMUM EQUIPMENT LIST Date: 08/12/2002 MU-300, MU-300-10, BE-400, BE-400A Highlights of Change

FEDERAL AVIATION ADMINISTRATION Page: XIV Revision: 5 MASTER MINIMUM EQUIPMENT LIST Date: 08/12/2002 MU-300, MU-300-10, BE-400, BE-400A Highlights of Change

FEDERAL AVIATION ADMINISTRATION Page: XV Revision: 5 MASTER MINIMUM EQUIPMENT LIST Date: 08/12/2002 MU-300, MU-300-10, BE-400, BE-400A Highlights of Change

FEDERAL AVIATION ADMINISTRATION Page: XVI Revision: 6 MASTER MINIMUM EQUIPMENT LIST Date: 01/31/1995 MU-300, MU-300-10, BE-400, BE-400A 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: XVII Revision: 6 MASTER MINIMUM EQUIPMENT LIST Date: 01/31/1995 MU-300, MU-300-10, BE-400, BE-400A 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: XVIII Revision: 6 MASTER MINIMUM EQUIPMENT LIST Date: 01/31/1995 MU-300, MU-300-10, BE-400, BE-400A 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: XIX Revision: 6 MASTER MINIMUM EQUIPMENT LIST Date: 01/31/1995 MU-300, MU-300-10, BE-400, BE-400A 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: XX Revision: 6 MASTER MINIMUM EQUIPMENT LIST Date: 01/31/1995 MU-300, MU-300-10, BE-400, BE-400A 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: XXI Revision: 6 MASTER MINIMUM EQUIPMENT LIST Date: 01/31/1995 MU-300, MU-300-10, BE-400, BE-400A 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: XXII Revision: 6 MASTER MINIMUM EQUIPMENT LIST Date: 01/31/1995 MU-300, MU-300-10, BE-400, BE-400A 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: XXIII Revision: 6 MASTER MINIMUM EQUIPMENT LIST Date: 01/31/1995 MU-300, MU-300-10, BE-400, BE-400A 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: XXIV Revision: 2 MASTER MINIMUM EQUIPMENT LIST Date: 06/14/1989 MU-300, MU-300-10, BE-400, BE-400A 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: XXV Revision: 2 MASTER MINIMUM EQUIPMENT LIST Date: 06/14/1989 MU-300, MU-300-10, BE-400, BE-400A 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.

FEDERAL AVIATION ADMINISTRATION Page Revision: 5 MASTER MINIMUM EQUIPMENT LIST Date: 08/12/2002 MU-300, MU-300-10, BE-400, BE-400A Guidelines for (O) & (M) Procedures The FOEB has identified a need for certain procedures to provide an adequate level of safety while providing relief for the following items. These procedures must be established by the operator. The following guidelines are to help establish these required procedures. Guidelines are included only for those items identified by an (O) or (M) in column 4, Remarks or Exceptions. (O) or (M) designations are not included in Column 4 when the procedure is obvious or detailed in the Remarks. 21-2 (O) Procedure to configure and operate aircraft unpressurized. 21-3 (O) Procedure to configure and operate aircraft unpressurized. 21-6 (O) Procedure to configure and operate aircraft unpressurized. 21-9 (M) Procedure to ensure Outflow Valves are in OPEN position. (O) Procedure to configure and operate aircraft unpressurized. 21-10 (O) Procedure to configure and operate aircraft unpressurized. 21-13 (O) Procedure to operate A/C in Unpressurized configuration. 21-13 (M) Procedure to secure Dump Valve in the OPEN position. 21-14 (M) Procedure to insure that the ECS is operational and secured ON. 21-16 (M) Procedure to deactivate and secure the system. (O) Procedure to flight plan and conduct flight with inoperative component. 21-17 (M) Procedure to deactivate and secure the system. 21-18 (O) Procedure to conduct flight in unpressurized condition. 22-1 (M) Procedure to disable Autopilot and determine that servos do not cause binding of the control cables.

FEDERAL AVIATION ADMINISTRATION Page Revision: 5 MASTER MINIMUM EQUIPMENT LIST Date: 08/12/2002 MU-300, MU-300-10, BE-400, BE-400A Guidelines for (O) & (M) Procedures 22-2 (O) Procedure to comply with AFM Limitations. 22-5, 6, 7, 8, 9 (O) Procedure to verify proper annunciation(s) are displayed. 23-5 (O) Procedure to brief passengers by alternate means. 23-14 (O) Procedure to brief passengers. 23-16 (O) Procedure to ensure all FAR's pertinent to the flight are complied with. 24-5 (M) Procedure to disconnect and remove standby battery. 24-12 (M) Procedure to ensure the fault will not have an effect on any other systems. 25-4 (M) Maintenance procedure to disconnect ELT Remote Switch from the ELT and manually arm the ELT. Always disconnect the Remote ELT Switch in accordance with the ELT Manufacturers Instructions. 25-10-1 (M) Procedure to secure Arm Rests in the upright position. 25-10-2 (M) Procedure to deactivate and secure system. 25-10-3 (M) Procedure to deactivate and secure system. 25-15 (M) Procedure to deactivate and secure EMS equipment. 25-17 (M) Procedure to deactivate or isolate equipment. 25-20 (O) Procedure to insure that sufficient receptacles are available for all Waste. 25-20 (M) Maintenance procedure to prevent Waste introductions into inoperative receptacle. 25-24 (O) Procedure to ensure crewmember awareness of specific airspeed information.

FEDERAL AVIATION ADMINISTRATION Page Revision: 5 MASTER MINIMUM EQUIPMENT LIST Date: 08/12/2002 MU-300, MU-300-10, BE-400, BE-400A Guidelines for (O) & (M) Procedures 25-25-1 (M) Procedure to ensure seat is locked in a position that permits normal pilot visibility, full flight control movement and is acceptable to the flight crew. 25-25-2 (M) Procedure to secure affected arm rest in full up position. 25-26 (M) Maintenance procedure to deactivate and secure System. 26-4 (O) Procedure to ensure Waste receptacle is empty and used by crewmembers only. (M) Procedure to lock and placard Lavatory Door. 26-5 (O) Procedure to ensure Waste receptacle is empty and Lavatory is used by crewmembers only. (M) Procedure to secure and placard Lavatory Door. 27-1 (O) Procedure to secure control surfaces via alternate method. 28-6 (M) Procedure to deactivate Fuselage Tank Fill System. 30-10 (O) Procedure to operate aircraft in accordance with engine anti-ice on performance. 30-11 (O) Procedure to comply with AFM limitations. 31-2 (O) Procedure to record flight hours via alternate method. 32-1 (O) Operation procedure to ensure Anti Skid Switch remains in the OFF position and that the proper performance charts are used so as not to exceed AFM/POH limitations. 32-3 (O) Procedure to ensure crew awareness that Landing Gear Handle Soleniod is inoperative. (M) Mainenance procedure to verify that the Release Solenoid is working properly.

FEDERAL AVIATION ADMINISTRATION Page Revision: 5 MASTER MINIMUM EQUIPMENT LIST Date: 08/12/2002 MU-300, MU-300-10, BE-400, BE-400A Guidelines for (O) & (M) Procedures 33-7 (O) Procedure to alert passengers via alternate means. 34-5 (O) Procedure to: 1)ensure current Aeronautical Charts are used. 2)verify status and suitability of the Nav Facilities used to define route of flight. 3)use manual tuning of Approach Nav Radios. 34-9 (O) Procedures to operate with the Flight Director inoperative. 34-10 (O) Procedure for crew coordination of altitude awareness. 34-13 (O) Changed proviso in accordance with Policy Letter 10. 34-15 (O) Procedure to ensure and the use of alternate procedures. (M) Procedure to ensure the system is deactivated and secured. 2) (O) Procedure to ensure TA and RA visual and audio functions are operative on flying pilot side. (O) Procedure to ensure non-flying pilot monitors pilot display. (O) Procedure to ensure TA ONLY mode is selected and all TA functions/elements are operative. 3) (O) Procedure to ensure all RA display/functions are operative. 34-16 (M) Procedure to ensure the system is deactivated and secured. (O) Procedure to ensure enroute and approach procedures do not require it's use. 34-18 (O) Procedure to ensure crew awareness of inoperative GPWS. 34-18-1 (O) Procedure to establish alternate methods of operating without the inoperative mode. 34-18-4 (O) Procedure to establish alternate methods of operating without advisory callouts.

FEDERAL AVIATION ADMINISTRATION Page Revision: 5 MASTER MINIMUM EQUIPMENT LIST Date: 08/12/2002 MU-300, MU-300-10, BE-400, BE-400A Guidelines for (O) & (M) Procedures 34-18-5 (O) Procedure to establish alternate methods of operating without the windshear mode. 34-23, 24 (O) Procedure to configure and use operative displays to obtain information normally available on inoperative display. 34-27-1(O) Operation procedures to operate with the database out of currency. 34-27-2(O) Operation procedures to operate with the database out of currency. 34-28 (O) Operation procedures to operate with the Windshear Warning and Flight Guidance System inoperative. 34-29 (O) Operation procedures to operate with the Windshear Detection and Flight Guidance System inoperative. 35-4-2 (M) Maintenance procedure to Secure Mask Access Panels. 35-4-3 (M) Maintenance procedure to remove and secure Oxygen Cannister. 52-1 (O) Procedure to ensure door is latched prior to each departure. 52-2 (O) Procedure to safely operate with inoperative Snubber. 52-4 (O) Pracedure to safely operate door with Step Cable missing. 74-1 (O) Procedure to ensure flights are not conducted into known or forecasted weather. 77-3 (O) Procedure to ensure Oil Pressure Gauge is monitored during flight. 78-1 (O) Procedure to operate aircraft with TR's pinned. (M) Procedure to secure Thrust Reverser in the forward thrust position.

FEDERAL AVIATION ADMINISTRATION Page Revision: 5 MASTER MINIMUM EQUIPMENT LIST Date: 08/12/2002 MU-300, MU-300-10, BE-400, BE-400A Guidelines for (O) & (M) Procedures

------------------------------------------------------------------------------- ¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦ ¦ FEDERAL AVIATION ADMINISTRATION ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT: ¦ REVISION NO: 5 ¦ PAGE: ¦ ¦ MU-300, MU-300-10, BE-400, BE-400A ¦ ¦ ¦ ¦ ¦ DATE: 08/12/2002 ¦ 21-1 ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ 1. ¦ 2. NUMBER INSTALLED ¦ ¦ SYSTEM & ¦ -------------------------------------------- ¦ ¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦ ¦ NUMBERS ¦ ¦ --------------------------------------- ¦ ¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦ ¦ 21 AIR CONDITIONING ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ 1. Cabin Altitude C ¦ 1 ¦ 0 ¦ May be inoperative provided ¦ ¦ Warning System ¦ ¦ ¦ Cabin Altitude and Differential ¦ ¦ ¦ ¦ ¦ Pressure Indicators are monitored. ¦ ¦ ¦ ¦ ¦ ¦ ¦ 2. Automatic C ¦ 1 ¦ 0 ¦ May be inoperative provided: ¦ ¦ Pressurization ¦ ¦ ¦ a) Manual Pressurization | ¦ ¦ Controller ¦ ¦ ¦ Control is operative, and | ¦ ¦ ¦ ¦ ¦ b) Autopilot is operative. ¦ ¦ ¦ ¦ ¦ ¦ ¦ C ¦ 1 ¦ 0 ¦ (O)Airplane is operated in an ¦ ¦ ¦ ¦ ¦ unpressurized configuration. ¦ ¦ ¦ ¦ ¦ ¦ ¦ 3. Manual C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided ¦ ¦ Pressurization ¦ ¦ ¦ the airplane is operated in an ¦ ¦ Controller ¦ ¦ ¦ unpressurized configuration. ¦ ¦ ¦ ¦ ¦ ¦ ¦ 4. Automatic C ¦ - ¦ 0 ¦ May be inoperative provided Manual ¦ ¦ Temperature Control ¦ ¦ ¦ Temperature Control System is ¦ ¦ System ¦ ¦ ¦ operative. ¦ ¦ (cockpit or cabin) ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ 5. Manual Temperature C ¦ - ¦ 0 ¦ May be inoperative provided ¦ ¦ Control System ¦ ¦ ¦ Automatic Temperature Control ¦ ¦ (cockpit or cabin) ¦ ¦ ¦ System is operative. ¦ ¦ ¦ ¦ ¦ ¦ ¦ 6. Door Seal System C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided the ¦ ¦ ¦ ¦ ¦ airplane is operated in an ¦ ¦ ¦ ¦ ¦ unpressurized configuration. ¦ ¦ ¦ ¦ ¦ ¦ ¦ 7. Deleted ¦ ¦ ¦ Deleted prior to Rev 3. ¦ ¦ ¦ ¦ ¦ ¦ ¦ 8. Deleted ¦ ¦ ¦ Deleted prior to Rev 3. ¦ ¦ ¦ ¦ ¦ ¦ ¦ 9. Outflow Valves C ¦ 2 ¦ 0 ¦ (M)(O)May be inoperative OPEN ¦ ¦ ¦ ¦ ¦ provided the airplane is operated ¦ ¦ ¦ ¦ ¦ in an unpressurized configuration. ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ -------------------------------------------------------------------------------

------------------------------------------------------------------------------- ¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦ ¦ FEDERAL AVIATION ADMINISTRATION ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT: ¦ REVISION NO: 5 ¦ PAGE: ¦ ¦ MU-300, MU-300-10, BE-400, BE-400A ¦ ¦ ¦ ¦ ¦ DATE: 08/12/2002 ¦ 21-2 ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ 1. ¦ 2. NUMBER INSTALLED ¦ ¦ SYSTEM & ¦ -------------------------------------------- ¦ ¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦ ¦ NUMBERS ¦ ¦ --------------------------------------- ¦ ¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦ ¦ 21 AIR CONDITIONING ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ 10. Cabin Altitude and C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided ¦ ¦ Differential ¦ ¦ ¦ Airplane is operated in an ¦ ¦ Pressure Indicator ¦ ¦ ¦ unpressurized configuration. ¦ ¦ ¦ ¦ ¦ ¦ ¦ C ¦ 1 ¦ 0 ¦ May be inoperative provided: | ¦ ¦ ¦ ¦ ¦ a) Cabin Altitude Indicator is ¦ ¦ ¦ ¦ ¦ operative, and ¦ ¦ ¦ ¦ ¦ b) Chart is available for crew ¦ ¦ ¦ ¦ ¦ to convert cabin altitude to ¦ ¦ ¦ ¦ ¦ differential pressure. ¦ ¦ ¦ ¦ ¦ ¦ ¦ 11. Cabin Rate of C ¦ 1 ¦ 0 ¦ ¦ ¦ Climb Indicator ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ 12. Cabin Ceiling C ¦ 1 ¦ 0 ¦ ¦ ¦ Outlet System ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ 13. Cabin Dump Valve C ¦ 1 ¦ 0 ¦ (M)(O) May be inoperative provided | ¦ ¦ ¦ ¦ ¦ the Dump Valve is secured | ¦ ¦ ¦ ¦ ¦ in the OPEN position and | ¦ ¦ ¦ ¦ ¦ and the aircraft is | ¦ ¦ ¦ ¦ ¦ operated in an unpressurized | ¦ ¦ ¦ ¦ ¦ configuration. | ¦ ¦ ¦ ¦ ¦ ¦ ¦ 14. Ventilation Blower C ¦ 1 ¦ 0 ¦ (M)May be inoperative provided | ¦ ¦ System ¦ ¦ ¦ ECS is operational and ON. | ¦ ¦ ¦ ¦ ¦ ¦ ¦ 15. Cabin Temperature C ¦ 1 ¦ 0 ¦ ¦ ¦ Indicating System ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ 16. Vapor Cycle Air C ¦ 1 ¦ 0 ¦ (M) ¦ ¦ Conditioning ¦ ¦ ¦ ¦ ¦ ***System ¦ ¦ ¦ | ¦ ¦ ¦ ¦ ¦ ¦ ¦ 17. Auxiliary Ground C ¦ 1 ¦ 0 ¦ (M) ¦ ¦ *** Heater System ¦ ¦ ¦ | ¦ ¦ ¦ ¦ ¦ ¦ ¦ 18. Emergency Exit C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided the | ¦ ¦ Seal System ¦ ¦ ¦ airplane is operated in an | ¦ ¦ ¦ ¦ ¦ unpressurized configuration. | ¦ -------------------------------------------------------------------------------

------------------------------------------------------------------------------- ¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦ ¦ FEDERAL AVIATION ADMINISTRATION ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT: ¦ REVISION NO: 5 ¦ PAGE: ¦ ¦ MU-300, MU-300-10, BE-400, BE-400A ¦ ¦ ¦ ¦ ¦ DATE: 08/12/2002 ¦ 22-1 ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ 1. ¦ 2. NUMBER INSTALLED ¦ ¦ SYSTEM & ¦ -------------------------------------------- ¦ ¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦ ¦ NUMBERS ¦ ¦ --------------------------------------- ¦ ¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦ ¦ 22 AUTO FLIGHT ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ 1. Autopilot System C ¦ 1 ¦ 0 ¦ (M)May be inoperative except | ¦ ¦ ¦ ¦ ¦ where approach minimums or enroute | ¦ ¦ ¦ ¦ ¦ operations require its use and | ¦ ¦ ¦ ¦ ¦ (Rudder Boost must be operative on | ¦ ¦ ¦ ¦ ¦ BE-400A). | ¦ ¦ ¦ ¦ ¦ ¦ ¦ 2. Yaw Damper C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided ¦ ¦ ¦ ¦ ¦ AFM limitations are applied. ¦ ¦ ¦ ¦ ¦ ¦ ¦ 3. Autopilot Control C ¦ 2 ¦ 1 ¦ One may be inoperative provided | ¦ ¦ Wheel Disengage ¦ ¦ ¦ the autopilot is not utilized at | ¦ ¦ Switches ¦ ¦ ¦ less than initial approach | ¦ ¦ ¦ ¦ ¦ altitude. | ¦ ¦ ¦ ¦ ¦ ¦ ¦ 4. Autopilot C ¦ 1 ¦ 0 ¦ May be inoperative provided: ¦ ¦ Go-Around Switch ¦ ¦ ¦ a) Approach minimums do not ¦ ¦ ¦ ¦ ¦ require its use, and ¦ ¦ ¦ ¦ ¦ b) Alternate procedures are ¦ ¦ ¦ ¦ ¦ established and used to ¦ ¦ ¦ ¦ ¦ disconnect autopilot and ¦ ¦ ¦ ¦ ¦ establish initial pitch ¦ ¦ ¦ ¦ ¦ and wings level attitude. ¦ ¦ ¦ ¦ ¦ ¦ ¦ 5. Autopilot Control C ¦ - ¦ 0 ¦ (O)May be inoperative provided the ¦ ¦ Panel Mode ¦ ¦ ¦ affected mode(s)is/are selected ¦ ¦ Annunciator Lamps ¦ ¦ ¦ momentarily prior to departure to ¦ ¦ ¦ ¦ ¦ verify that proper mode ¦ ¦ ¦ ¦ ¦ annunciation is displayed on ¦ ¦ ¦ ¦ ¦ the attitude indicator(s). ¦ ¦ ¦ ¦ ¦ ¦ ¦ 6. Flight Director C ¦ - ¦ 0 ¦ (O)May be inoperative provided the ¦ ¦ Mode Select Panel ¦ ¦ ¦ affected mode(s) is/are selected ¦ ¦ Mode Annunciator ¦ ¦ ¦ momentarily prior to departure to ¦ ¦ Lamps ¦ ¦ ¦ verify that proper mode ¦ ¦ ¦ ¦ ¦ annunciation is displayed on the ¦ ¦ ¦ ¦ ¦ attitude indicator. ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ -------------------------------------------------------------------------------

------------------------------------------------------------------------------- ¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦ ¦ FEDERAL AVIATION ADMINISTRATION ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT: ¦ REVISION NO: 5 ¦ PAGE: ¦ ¦ MU-300, MU-300-10, BE-400, BE-400A ¦ ¦ ¦ ¦ ¦ DATE: 08/12/2002 ¦ 22-2 ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ 1. ¦ 2. NUMBER INSTALLED ¦ ¦ SYSTEM & ¦ -------------------------------------------- ¦ ¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦ ¦ NUMBERS ¦ ¦ --------------------------------------- ¦ ¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦ ¦ 22 AUTO FLIGHT ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ 7. Reversionary C ¦ - ¦ 0 ¦ (O)Individual annunciator lights ¦ ¦ Mode Selection Panel ¦ ¦ ¦ may be inoperative provided a ¦ ¦ *** Switch Lights ¦ ¦ ¦ duplicate annunciation is visible | ¦ ¦ ¦ ¦ ¦ to both the pilot and copilot. ¦ ¦ ¦ ¦ ¦ ¦ ¦ 8. Autopilot Pitch C ¦ - ¦ - ¦ (O)May be inoperative provided a ¦ ¦ Trim Fail Remote ¦ ¦ ¦ duplicate annunciation is visible ¦ ¦ Annunciators ¦ ¦ ¦ to both the pilot and copilot. ¦ ¦ ¦ ¦ ¦ ¦ ¦ 9. Autopilot Roll C ¦ - ¦ - ¦ (O)May be inoperative provided a ¦ ¦ Trim Fail Remote ¦ ¦ ¦ duplicate annunciation is visible ¦ ¦ Annunciators ¦ ¦ ¦ to both the pilot and copilot. ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ -------------------------------------------------------------------------------

------------------------------------------------------------------------------- ¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦ ¦ FEDERAL AVIATION ADMINISTRATION ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT: ¦ REVISION NO: 5 ¦ PAGE: ¦ ¦ MU-300, MU-300-10, BE-400, BE-400A ¦ ¦ ¦ ¦ ¦ DATE: 08/12/2002 ¦ 23-1 ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ 1. ¦ 2. NUMBER INSTALLED ¦ ¦ SYSTEM & ¦ -------------------------------------------- ¦ ¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦ ¦ NUMBERS ¦ ¦ --------------------------------------- ¦ ¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦ ¦ 23 COMMUNICATIONS ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ 1. Communications D ¦ - ¦ - ¦ Any in excess of those required by | ¦ ¦ Systems ¦ ¦ ¦ FAR may be inoperative, provided | ¦ ¦ (VHF, UHF) ¦ ¦ ¦ it is not powered by the Emergency | ¦ ¦ ¦ ¦ ¦ AC Bus, Emergency DC Bus, Battery | ¦ ¦ ¦ ¦ ¦ Bus, Battery Direct Bus, or the DC | ¦ ¦ ¦ ¦ ¦ Transfer Bus and not required for | ¦ ¦ ¦ ¦ ¦ Emergency Procedures. | ¦ ¦ ¦ ¦ ¦ ¦ ¦ 1)VHF Communication ¦ ¦ ¦ | ¦ ¦ Control Panels ¦ ¦ ¦ | ¦ ¦ ¦ ¦ ¦ ¦ ¦ a)Frequency C ¦ - ¦ 0 ¦ | ¦ ¦ Transfer ¦ ¦ ¦ | ¦ ¦ Light ¦ ¦ ¦ | ¦ ¦ ¦ ¦ ¦ ¦ ¦ b)Frequency C ¦ - ¦ 0 ¦ | ¦ ¦ Transfer ¦ ¦ ¦ | ¦ ¦ ¦ ¦ ¦ ¦ ¦ c)Frequency C ¦ - ¦ 2 ¦ | ¦ ¦ Transfer ¦ ¦ ¦ | ¦ ¦ Knob ¦ ¦ ¦ | ¦ ¦ ¦ ¦ ¦ ¦ ¦ d)Frequency C ¦ - ¦ 2 ¦ | ¦ ¦ Indication ¦ ¦ ¦ | ¦ ¦ ¦ ¦ ¦ ¦ ¦ 2. Cockpit Voice A ¦ 1 ¦ 0 ¦ May be inoperative provided: | ¦ ¦ Recorder(CVR) ¦ ¦ ¦ a) Flight Data Recorder (FDR) | ¦ ¦ (With Flight Data ¦ ¦ ¦ operates normally, and | ¦ ¦ Recorder). ¦ ¦ ¦ b) Repairs are made within | ¦ ¦ ¦ ¦ ¦ three flight days. | ¦ ¦ ¦ ¦ ¦ ¦ ¦ Cockpit Voice A ¦ 1 ¦ 0 ¦ May be inoperative provided | ¦ ¦ Recorder(CVR) ¦ ¦ ¦ repairs are made within three | ¦ ¦ (Without Flight ¦ ¦ ¦ flight days. | ¦ ¦ Data Recorder) ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ -------------------------------------------------------------------------------

------------------------------------------------------------------------------- ¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦ ¦ FEDERAL AVIATION ADMINISTRATION ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT: ¦ REVISION NO: 5 ¦ PAGE: ¦ ¦ MU-300, MU-300-10, BE-400, BE-400A ¦ ¦ ¦ ¦ ¦ DATE: 08/12/2002 ¦ 23-2 ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ 1. ¦ 2. NUMBER INSTALLED ¦ ¦ SYSTEM & ¦ -------------------------------------------- ¦ ¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦ ¦ NUMBERS ¦ ¦ --------------------------------------- ¦ ¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦ ¦ 23 COMMUNICATIONS ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ 3. Boom Microphones (If ¦ ¦ ¦ ¦ ¦ FDR Required by FAR) ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ 1) Cockpit Voice A ¦ - ¦ 0 ¦ May be inoperative provided: ¦ ¦ Recorder Equipped ¦ ¦ ¦ a) Flight Data Recorder(FDR) ¦ ¦ to Record Boom ¦ ¦ ¦ operates normally, and ¦ ¦ Microphone per ¦ ¦ ¦ b) Repairs are made within ¦ ¦ FAR 135.151(d) ¦ ¦ ¦ three flight days. ¦ ¦ ¦ ¦ ¦ ¦ ¦ 2) Cockpit Voice D ¦ - ¦ 0 ¦ Any in excess of those required by | ¦ ¦ Recorder not ¦ ¦ ¦ FAR may be inoperative. | ¦ ¦ Equipped to Record ¦ ¦ ¦ ¦ ¦ Boom Microphone ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ Boom Microphones ¦ ¦ ¦ ¦ ¦ (If No FDR Required by ¦ ¦ ¦ ¦ ¦ FAR) ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ 1) Cockpit Voice A ¦ - ¦ 0 ¦ May be inoperative provided repairs ¦ ¦ Recorder Equipped ¦ ¦ ¦ are made within three flight days. ¦ ¦ to Record ¦ ¦ ¦ ¦ ¦ Boom Microphones ¦ ¦ ¦ ¦ ¦ per FAR 135.151(d) ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ 2) Cockpit Voice D ¦ - ¦ 0 ¦ ¦ ¦ *** Recorder Not ¦ ¦ ¦ | ¦ ¦ Equipped to Record ¦ ¦ ¦ ¦ ¦ Boom Microphone ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ 4. Radio Tuning Units C ¦ 2 ¦ 1 ¦ One may be inoperative provided ¦ ¦ (BE-400A) ¦ ¦ ¦ one FMS control display unit (CDU) ¦ ¦ ¦ ¦ ¦ is operative. ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ -------------------------------------------------------------------------------

------------------------------------------------------------------------------- ¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦ ¦ FEDERAL AVIATION ADMINISTRATION ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT: ¦ REVISION NO: 5 ¦ PAGE: ¦ ¦ MU-300, MU-300-10, BE-400, BE-400A ¦ ¦ ¦ ¦ ¦ DATE: 08/12/2002 ¦ 23-3 ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ 1. ¦ 2. NUMBER INSTALLED ¦ ¦ SYSTEM & ¦ -------------------------------------------- ¦ ¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦ ¦ NUMBERS ¦ ¦ --------------------------------------- ¦ ¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦ ¦ 23 COMMUNICATIONS ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ 5. Passenger Address ¦ ¦ ¦ ¦ ¦ *** System (PA) ¦ ¦ ¦ | ¦ ¦ ¦ ¦ ¦ ¦ ¦ 1) Passenger C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided: | ¦ ¦ Configuration ¦ ¦ ¦ a) PA not required by FAR, and | ¦ ¦ ¦ ¦ ¦ b) Alternate, normal and | ¦ ¦ ¦ ¦ ¦ emergency procedures and/or | ¦ ¦ ¦ ¦ ¦ operating restrictions are | ¦ ¦ ¦ ¦ ¦ established and used. | ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ Note: Any station that | ¦ ¦ ¦ ¦ ¦ operates normally may | ¦ ¦ ¦ ¦ ¦ be used. | ¦ ¦ ¦ ¦ ¦ ¦ ¦ 2) Cargo D ¦ 1 ¦ 0 ¦ May be inoperative unless | ¦ ¦ Configuration ¦ ¦ ¦ procedures require its use. | ¦ ¦ ¦ ¦ ¦ ¦ ¦ 6. Flight Deck C ¦ 2 ¦ 1 ¦ One may be inoperative provided one ¦ ¦ Speakers ¦ ¦ ¦ speaker is operative and one ¦ ¦ ¦ ¦ ¦ headset is operative and worn by a ¦ ¦ ¦ ¦ ¦ crewmember. ¦ ¦ ¦ ¦ ¦ ¦ ¦ 7. Headsets D ¦ - ¦ - ¦ Any in excess of those required by | ¦ ¦ ¦ ¦ ¦ FAR may be inoperative. | ¦ ¦ ¦ ¦ ¦ ¦ ¦ 8. Hand Microphones C ¦ 2 ¦ 1 ¦ One may be inoperative provided one ¦ ¦ ¦ ¦ ¦ boom microphone and one hand ¦ ¦ ¦ ¦ ¦ microphone are operative. ¦ ¦ ¦ ¦ ¦ ¦ ¦ 9. Flight Phone D ¦ - ¦ - ¦ | ¦ ¦ *** Systems ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ 10. Push to Talk C ¦ 2 ¦ 1 ¦ One may be inoperative provided the | ¦ ¦ Switch ¦ ¦ ¦ hand held microphone on affected | ¦ ¦ ¦ ¦ ¦ side is operative. | ¦ ¦ ¦ ¦ ¦ ¦ ¦ 11. Observers Headset C ¦ - ¦ - ¦ May be inoperative provided an | ¦ ¦ *** Audio Jack ¦ ¦ ¦ alternative audio source is | ¦ ¦ ¦ ¦ ¦ available. | ¦ ¦ ¦ ¦ ¦ ¦ -------------------------------------------------------------------------------

------------------------------------------------------------------------------- ¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦ ¦ FEDERAL AVIATION ADMINISTRATION ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT: ¦ REVISION NO: 5 ¦ PAGE: ¦ ¦ MU-300, MU-300-10, BE-400, BE-400A ¦ ¦ ¦ ¦ ¦ DATE: 08/12/2002 ¦ 23-4 ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ 1. ¦ 2. NUMBER INSTALLED ¦ ¦ SYSTEM & ¦ -------------------------------------------- ¦ ¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦ ¦ NUMBERS ¦ ¦ --------------------------------------- ¦ ¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦ ¦ 23 COMMUNICATIONS ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ 12. Ground Comm Power D ¦ - ¦ 0 ¦ | ¦ ¦ *** System ¦ ¦ ¦ | ¦ ¦ ¦ ¦ ¦ ¦ ¦ 13. Crew Intercom B ¦ 1 ¦ 0 ¦ May be inoperative provided | ¦ ¦ System ¦ ¦ ¦ headsets are not required. | ¦ ¦ ¦ ¦ ¦ ¦ ¦ 14. Recorded Passenger D ¦ - ¦ 0 ¦ (O)May be inoperative. | ¦ ¦ *** Briefing System ¦ ¦ ¦ | ¦ ¦ ¦ ¦ ¦ ¦ ¦ 15. Static Discharge C ¦ - ¦ - ¦ One may be broken or missing from | ¦ ¦ Wicks ¦ ¦ ¦ each Aileron Trim Tab or the | ¦ ¦ ¦ ¦ ¦ Vertical Stabilizer. | ¦ ¦ ¦ ¦ ¦ ¦ ¦ 16. High Frequency (HF) D ¦ - ¦ - ¦ Any in excess of those required by | ¦ ¦ Communications ¦ ¦ ¦ FAR may be inoperative. | ¦ ¦ *** System ¦ ¦ ¦ | ¦ ¦ ¦ ¦ ¦ ¦ ¦ C ¦ - ¦ 1 ¦ (O)May be inoperative while | ¦ ¦ ¦ ¦ ¦ conducting operations that require | ¦ ¦ ¦ ¦ ¦ two LRCS provided: | ¦ ¦ ¦ ¦ ¦ a)SATCOM (High or Low Gain Data | ¦ ¦ ¦ ¦ ¦ Link System operates normally, | ¦ ¦ ¦ ¦ ¦ and | ¦ ¦ ¦ ¦ ¦ b)SATCOM Data Link communication | ¦ ¦ ¦ ¦ ¦ operates normally over the | ¦ ¦ ¦ ¦ ¦ intended route of flight. | ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ -------------------------------------------------------------------------------

------------------------------------------------------------------------------- ¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦ ¦ FEDERAL AVIATION ADMINISTRATION ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT: ¦ REVISION NO: 5 ¦ PAGE: ¦ ¦ MU-300, MU-300-10, BE-400, BE-400A ¦ ¦ ¦ ¦ ¦ DATE: 08/12/2002 ¦ 24-1 ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ 1. ¦ 2. NUMBER INSTALLED ¦ ¦ SYSTEM & ¦ -------------------------------------------- ¦ ¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦ ¦ NUMBERS ¦ ¦ --------------------------------------- ¦ ¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦ ¦ 24 ELECTRICAL POWER ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ 1. DC Starter ¦ ¦ ¦ Deleted Rev 3. ¦ ¦ Generators ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ 2. DC Voltmeter ¦ ¦ ¦ Deleted Rev 3. ¦ ¦ ¦ ¦ ¦ ¦ ¦ 3. DC Ammeters B ¦ 2 ¦ 1 ¦ One may be inoperative provided ¦ ¦ ¦ ¦ ¦ crew monitors associated voltage ¦ ¦ ¦ ¦ ¦ during flight. ¦ ¦ ¦ ¦ ¦ ¦ ¦ 4. Battery ¦ ¦ ¦ Deleted Rev 3. ¦ ¦ ¦ ¦ ¦ ¦ ¦ 5. Standby Power B ¦ 1 ¦ 0 ¦ (M)May be inoperative provided: ¦ ¦ System ¦ ¦ ¦ a) Airplane is operated in ¦ ¦ ¦ ¦ ¦ day VMC only, and ¦ ¦ ¦ ¦ ¦ b) Standby battery is ¦ ¦ ¦ ¦ ¦ disconnected and removed. ¦ ¦ ¦ ¦ ¦ ¦ ¦ 6. DC Generator C ¦ 2 ¦ 1 ¦ One may be inoperative ¦ ¦ Failure Advisory ¦ ¦ ¦ provided: ¦ ¦ Annunciators ¦ ¦ ¦ a) Both ammeters are operative, ¦ ¦ ¦ ¦ ¦ and ¦ ¦ ¦ ¦ ¦ b) Generator loads are ¦ ¦ ¦ ¦ ¦ monitored. ¦ ¦ ¦ ¦ ¦ ¦ ¦ 7. AC Inverters ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ 1) (MU-300, B ¦ 2 ¦ 1 ¦ One may be inoperative ¦ ¦ MU-300-10 and ¦ ¦ ¦ provided: ¦ ¦ BE-400) ¦ ¦ ¦ a) Airplane is operated in day ¦ ¦ ¦ ¦ ¦ VMC, ¦ ¦ ¦ ¦ ¦ b) AC Voltmeter is operative, ¦ ¦ ¦ ¦ ¦ and ¦ ¦ ¦ ¦ ¦ c) AFM procedures are applied. ¦ ¦ ¦ ¦ ¦ ¦ ¦ 2) (BE-400A) C ¦ 2 ¦ 1 ¦ One may be inoperative provided ¦ ¦ ¦ ¦ ¦ AC Voltmeter is operative. ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ -------------------------------------------------------------------------------

------------------------------------------------------------------------------- ¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦ ¦ FEDERAL AVIATION ADMINISTRATION ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT: ¦ REVISION NO: 5 ¦ PAGE: ¦ ¦ MU-300, MU-300-10, BE-400, BE-400A ¦ ¦ ¦ ¦ ¦ DATE: 08/12/2002 ¦ 24-2 ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ 1. ¦ 2. NUMBER INSTALLED ¦ ¦ SYSTEM & ¦ -------------------------------------------- ¦ ¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦ ¦ NUMBERS ¦ ¦ --------------------------------------- ¦ ¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦ ¦ 24 ELECTRICAL POWER ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ 8. AC Inverter Failure ¦ ¦ ¦ ¦ ¦ Advisory Lights ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ 1) (MU-300, C ¦ 2 ¦ 1 ¦ One may be inoperative provided ¦ ¦ MU-300-10 and ¦ ¦ ¦ both AC inverters are operative. ¦ ¦ BE-400) ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ 2) (BE-400A) C ¦ 2 ¦ 1 ¦ One may be inoperative provided ¦ ¦ ¦ ¦ ¦ AC Voltmeter is operative. ¦ ¦ ¦ ¦ ¦ ¦ ¦ 9. Deleted ¦ ¦ ¦ Deleted prior to Rev 3. ¦ ¦ ¦ ¦ ¦ ¦ ¦ 10. Deleted ¦ ¦ ¦ Deleted prior to Rev 3. ¦ ¦ ¦ ¦ ¦ ¦ ¦ 11. AC Voltmeter C ¦ 1 ¦ 0 ¦ May be inoperative provided ¦ ¦ ¦ ¦ ¦ both AC Inverter Failure Advisory ¦ ¦ ¦ ¦ ¦ Lights are operative. ¦ ¦ ¦ ¦ ¦ ¦ ¦ 12. External Power D ¦ 1 ¦ 0 ¦ (M)May be inoperative. | ¦ ¦ System ¦ ¦ ¦ | ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ -------------------------------------------------------------------------------

------------------------------------------------------------------------------- ¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦ ¦ FEDERAL AVIATION ADMINISTRATION ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT: ¦ REVISION NO: 5 ¦ PAGE: ¦ ¦ MU-300, MU-300-10, BE-400, BE-400A ¦ ¦ ¦ ¦ ¦ DATE: 08/12/2002 ¦ 25-1 ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ 1. ¦ 2. NUMBER INSTALLED ¦ ¦ SYSTEM & ¦ -------------------------------------------- ¦ ¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦ ¦ NUMBERS ¦ ¦ --------------------------------------- ¦ ¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦ ¦ 25 EQUIPMENT/FURNISHINGS ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ 1. Flotation Devices D ¦ - ¦ - ¦ Any in excess of those required by | ¦ ¦ *** ¦ ¦ ¦ FAR may be inoperative or missing | ¦ ¦ ¦ ¦ ¦ provided required distribution is | ¦ ¦ ¦ ¦ ¦ maintained. | ¦ ¦ ¦ ¦ ¦ ¦ ¦ 2. Life Rafts D ¦ - ¦ - ¦ Any in excess of those required by | ¦ ¦ *** ¦ ¦ ¦ FAR may be inoperative or missing | ¦ ¦ ¦ ¦ ¦ provided required distribution is | ¦ ¦ ¦ ¦ ¦ maintained. | ¦ ¦ ¦ ¦ ¦ ¦ ¦ 3. Pyrotechnic D ¦ - ¦ - ¦ Any in excess of those required by | ¦ ¦ *** Signaling Devices ¦ ¦ ¦ FAR may be inoperative or missing | ¦ ¦ ¦ ¦ ¦ provided required distribution is | ¦ ¦ ¦ ¦ ¦ maintained. | ¦ ¦ ¦ ¦ ¦ ¦ ¦ 4. Emergency Locator C ¦ - ¦ 0 ¦ As required by FAR. ¦ ¦ *** Transmitter ¦ ¦ ¦ | ¦ ¦ C ¦ - ¦ 0 ¦ May be inoperative for published ¦ ¦ ¦ ¦ ¦ scheduled flights in scheduled air ¦ ¦ ¦ ¦ ¦ carrier service. ¦ ¦ ¦ ¦ ¦ ¦ ¦ 1)ELT Remote C ¦ 1 ¦ 0 ¦ (M) May be inoperative provided: | ¦ ¦ Switch ¦ ¦ ¦ a) Remote switch is | ¦ ¦ ¦ ¦ ¦ disconnected, and | ¦ ¦ ¦ ¦ ¦ b) ELT is manually armed. | ¦ ¦ ¦ ¦ ¦ ¦ ¦ 5. Seat Belts ¦ ¦ ¦ Deleted Rev 3. ¦ ¦ ¦ ¦ ¦ ¦ ¦ 6. Crewmember Shoulder ¦ ¦ ¦ Deleted Rev 3. ¦ ¦ Harness ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ 7. Deleted ¦ ¦ ¦ Deleted prior to Rev 3. ¦ ¦ ¦ ¦ ¦ ¦ ¦ 8. Deleted ¦ ¦ ¦ Deleted prior to Rev 3. ¦ ¦ ¦ ¦ ¦ ¦ ¦ 9. Seat Belt/Shoulder C ¦ - ¦ 0 ¦ May be inoperative or missing ¦ ¦ *** Harness Side Facing ¦ ¦ ¦ provided seat is blocked and not ¦ ¦ Seats ¦ ¦ ¦ occupied. ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ -------------------------------------------------------------------------------

------------------------------------------------------------------------------- ¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦ ¦ FEDERAL AVIATION ADMINISTRATION ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT: ¦ REVISION NO: 5 ¦ PAGE: ¦ ¦ MU-300, MU-300-10, BE-400, BE-400A ¦ ¦ ¦ ¦ ¦ DATE: 08/12/2002 ¦ 25-2 ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ 1. ¦ 2. NUMBER INSTALLED ¦ ¦ SYSTEM & ¦ -------------------------------------------- ¦ ¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦ ¦ NUMBERS ¦ ¦ --------------------------------------- ¦ ¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦ ¦ 25 EQUIPMENT/FURNISHINGS ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ 10. Passenger Seats D ¦ - ¦ - ¦ May be inoperative provided: | ¦ ¦ ¦ ¦ ¦ a) Seat does not block an | ¦ ¦ ¦ ¦ ¦ Emergency Exit. | ¦ ¦ ¦ ¦ ¦ b) Seat does not restrict any | ¦ ¦ ¦ ¦ ¦ passenger from access to the | ¦ ¦ ¦ ¦ ¦ main aircraft aisle, and | ¦ ¦ ¦ ¦ ¦ c) The affected seat(s) are | ¦ ¦ ¦ ¦ ¦ blocked and placarded - | ¦ ¦ ¦ ¦ ¦ "DO NOT OCCUPY" | ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ Note 1: A seat with an | ¦ ¦ ¦ ¦ ¦ inoperative seat belt is | ¦ ¦ ¦ ¦ ¦ considered inoperative. | ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ Note 2: Affected seat(s) may | ¦ ¦ ¦ ¦ ¦ include the seat(s) behind | ¦ ¦ ¦ ¦ ¦ and/or adjacent outboard seats. | ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ 1)Recline D ¦ - ¦ - ¦ (M)May be inoperative and seat | ¦ ¦ Mechanism ¦ ¦ ¦ occupied provided seat is secured | ¦ ¦ ¦ ¦ ¦ in the up-right position. | ¦ ¦ ¦ ¦ ¦ ¦ ¦ 2)Arm Rests D ¦ - ¦ - ¦ (M)May be inoperative. | ¦ ¦ ¦ ¦ ¦ ¦ ¦ 3)Electrical/ C ¦ - ¦ - ¦ (M)May be inoperative and the seat | ¦ ¦ Electronic Systems ¦ ¦ ¦ occupied provided associated | ¦ ¦ and Components. ¦ ¦ ¦ component(s) is deactivated. | ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ -------------------------------------------------------------------------------

------------------------------------------------------------------------------- ¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦ ¦ FEDERAL AVIATION ADMINISTRATION ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT: ¦ REVISION NO: 5 ¦ PAGE: ¦ ¦ MU-300, MU-300-10, BE-400, BE-400A ¦ ¦ ¦ ¦ ¦ DATE: 08/12/2002 ¦ 25-3 ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ 1. ¦ 2. NUMBER INSTALLED ¦ ¦ SYSTEM & ¦ -------------------------------------------- ¦ ¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦ ¦ NUMBERS ¦ ¦ --------------------------------------- ¦ ¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦ ¦ 25 EQUIPMENT/FURNISHINGS ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ 11. Passenger ¦ - ¦ 0 ¦ Passenger convenience items, as ¦ ¦ *** Convenience Item(s) ¦ ¦ ¦ expressed in this MMEL, are those | ¦ ¦ ¦ ¦ ¦ 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. 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. | ¦ ¦ ¦ ¦ ¦ ¦ ¦ 12. Megaphones ¦ ¦ ¦ Deleted, Revision 3a. ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ 13. Forward Observer ¦ ¦ ¦ Deleted, Revision 3a. ¦ ¦ *** Seat ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ 14. Emergency Medical D ¦ - ¦ - ¦ Any in excess of those required by | ¦ ¦ Equipment ¦ ¦ ¦ FAR may be incomplete or missing | ¦ ¦ ¦ ¦ ¦ provided the required distribution ¦ ¦ ¦ ¦ ¦ is maintained. ¦ ¦ ¦ ¦ ¦ ¦ ¦ 15. EMS Equipment D ¦ - ¦ - ¦ (M)May be inoperative provided the | ¦ ¦ *** (Air Ambulance) ¦ ¦ ¦ equipment is deactivated and | ¦ ¦ ¦ ¦ ¦ secured. | ¦ ¦ ¦ ¦ ¦ ¦ ¦ 16. Protective D ¦ - ¦ - ¦ Any in excess of those required by | ¦ ¦ Breathing ¦ ¦ ¦ FAR may be inoperative. | ¦ ¦ *** Equipment ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ -------------------------------------------------------------------------------

------------------------------------------------------------------------------- ¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦ ¦ FEDERAL AVIATION ADMINISTRATION ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT: ¦ REVISION NO: 5 ¦ PAGE: ¦ ¦ MU-300, MU-300-10, BE-400, BE-400A ¦ ¦ ¦ ¦ ¦ DATE: 08/12/2002 ¦ 25-4 ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ 1. ¦ 2. NUMBER INSTALLED ¦ ¦ SYSTEM & ¦ -------------------------------------------- ¦ ¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦ ¦ NUMBERS ¦ ¦ --------------------------------------- ¦ ¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦ ¦ 25 EQUIPMENT/FURNISHINGS ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ 17. Lavatory Waste 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 system which | ¦ ¦ ¦ ¦ ¦ operates normally may be | ¦ ¦ ¦ ¦ ¦ used. | ¦ ¦ ¦ ¦ ¦ ¦ ¦ 18. Cockpit Door C ¦ 1 ¦ 0 ¦ (M) May be inoperative provided | ¦ ¦ ¦ ¦ ¦ the door is secured in the OPEN | ¦ ¦ ¦ ¦ ¦ position and does not block egress | ¦ ¦ ¦ ¦ ¦ to any exit. | ¦ ¦ ¦ ¦ ¦ ¦ ¦ 19. Lavatory Door C ¦ 1 ¦ 0 ¦ (M) May be inoperative provided: | ¦ ¦ ¦ ¦ ¦ a) Door is secured, | ¦ ¦ ¦ ¦ ¦ b) Secured door does not block | ¦ ¦ ¦ ¦ ¦ access to any exit, and | ¦ ¦ ¦ ¦ ¦ c) Door is placarded, | ¦ ¦ ¦ ¦ ¦ "INOPERATIVE - DO NOT USE". | ¦ ¦ ¦ ¦ ¦ ¦ ¦ 20. Galley Waste C ¦ - ¦ - ¦ (M)(O)May be inoperative provided: | ¦ ¦ Receptables Access ¦ ¦ ¦ a)The container is empty and | ¦ ¦ *** Doors/Covers/Drawers ¦ ¦ ¦ the access is secured to | ¦ ¦ ¦ ¦ ¦ to prevent waste | ¦ ¦ ¦ ¦ ¦ introductions into the | ¦ ¦ ¦ ¦ ¦ compartment, and | ¦ ¦ ¦ ¦ ¦ b)Procedures are established | ¦ ¦ ¦ ¦ ¦ to ensure that sufficient | ¦ ¦ ¦ ¦ ¦ Galley Waste Receptacles | ¦ ¦ ¦ ¦ ¦ are available to | ¦ ¦ ¦ ¦ ¦ accomodate all waste that | ¦ ¦ ¦ ¦ ¦ may be generated on the | ¦ ¦ ¦ ¦ ¦ flight. | ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ -------------------------------------------------------------------------------

------------------------------------------------------------------------------- ¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦ ¦ FEDERAL AVIATION ADMINISTRATION ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT: ¦ REVISION NO: 5 ¦ PAGE: ¦ ¦ MU-300, MU-300-10, BE-400, BE-400A ¦ ¦ ¦ ¦ ¦ DATE: 08/12/2002 ¦ 25-5 ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ 1. ¦ 2. NUMBER INSTALLED ¦ ¦ SYSTEM & ¦ -------------------------------------------- ¦ ¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦ ¦ NUMBERS ¦ ¦ --------------------------------------- ¦ ¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦ ¦ 25 EQUIPMENT/FURNISHINGS ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ 21. Cargo Restraint C ¦ - ¦ - ¦ May be missing or inoperative | ¦ ¦ *** Systems ¦ ¦ ¦ provided no Cargo is carried in | ¦ ¦ ¦ ¦ ¦ associated Cargo Compartment. | ¦ ¦ ¦ ¦ ¦ ¦ ¦ 22. Flashlight D ¦ - ¦ - ¦ Any in excess of those required by | ¦ ¦ *** Stowage Assembly ¦ ¦ ¦ FAR may be inoperative or missing. | ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ 23. Cockpit C ¦ 2 ¦ 0 ¦ May be inoperative or missing | ¦ ¦ Sun Visors ¦ ¦ ¦ provided there are no visual | ¦ ¦ ¦ ¦ ¦ restrictions to the flight crew. | ¦ ¦ ¦ ¦ ¦ ¦ ¦ 24. External Mounted C ¦ - ¦ 0 ¦ (O)May be inoperative, missing | ¦ ¦ Airspeed Indicator ¦ ¦ ¦ or broken. | ¦ ¦ *** Bugs ¦ ¦ ¦ | ¦ ¦ ¦ ¦ ¦ ¦ ¦ 25. Crew Seats ¦ ¦ ¦ | ¦ ¦ 1) Seat A ¦ - ¦ 0 ¦ (M)May be inoperative provided: | ¦ ¦ Adjustments ¦ ¦ ¦ a)Seat(s) are locked in a | ¦ ¦ ¦ ¦ ¦ position that permits normal | ¦ ¦ ¦ ¦ ¦ pilot visibility, | ¦ ¦ ¦ ¦ ¦ b)Full flight control movement | ¦ ¦ ¦ ¦ ¦ is available, | ¦ ¦ ¦ ¦ ¦ c)The position of the affected | ¦ ¦ ¦ ¦ ¦ seat is acceptable to the | ¦ ¦ ¦ ¦ ¦ crew member, and | ¦ ¦ ¦ ¦ ¦ d)Repairs are made within one | ¦ ¦ ¦ ¦ ¦ flight day. | ¦ ¦ ¦ ¦ ¦ ¦ ¦ 2) Arm Rests C ¦ - ¦ 0 ¦ (M) May be inoperative provided arm | ¦ ¦ ¦ ¦ ¦ rest is secured in the full up | ¦ ¦ ¦ ¦ ¦ position. | ¦ ¦ ¦ ¦ ¦ ¦ ¦ 26. SmartStart C ¦ 1 ¦ 0 ¦ (M) | ¦ ¦ *** Security System ¦ ¦ ¦ | ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ -------------------------------------------------------------------------------

------------------------------------------------------------------------------- ¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦ ¦ FEDERAL AVIATION ADMINISTRATION ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT: ¦ REVISION NO: 5 ¦ PAGE: ¦ ¦ MU-300, MU-300-10, BE-400, BE-400A ¦ ¦ ¦ ¦ ¦ DATE: 08/12/2002 ¦ 26-1 ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ 1. ¦ 2. NUMBER INSTALLED ¦ ¦ SYSTEM & ¦ -------------------------------------------- ¦ ¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦ ¦ NUMBERS ¦ ¦ --------------------------------------- ¦ ¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦ ¦ 26 FIRE PROTECTION ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ 1. Portable Fire D ¦ - ¦ - ¦ Any in excess of those required by ¦ ¦ Extinguishers ¦ ¦ ¦ FAR may be inoperative or missing ¦ ¦ ¦ ¦ ¦ provided: ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ a) The inoperative fire ¦ ¦ ¦ ¦ ¦ extinguisher is tagged inoperative, ¦ ¦ ¦ ¦ ¦ removed from the installed ¦ ¦ ¦ ¦ ¦ location, and placed out of sight ¦ ¦ ¦ ¦ ¦ so it can not be mistaken for a ¦ ¦ ¦ ¦ ¦ functional unit, and ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ b) The required distribution is ¦ ¦ ¦ ¦ ¦ maintained. ¦ ¦ ¦ ¦ ¦ ¦ ¦ 2. Tail Cone Baggage C ¦ 1 ¦ 0 ¦ May be inoperative provided no ¦ ¦ *** Compartment Smoke ¦ ¦ ¦ baggage or cargo is carried in tail ¦ ¦ Detection Systems ¦ ¦ ¦ cone baggage compartment. | ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ Note: This does not preclude the | ¦ ¦ ¦ ¦ ¦ carriage of empty cargo | ¦ ¦ ¦ ¦ ¦ containers, pallets, ballast, | ¦ ¦ ¦ ¦ ¦ etc. | ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ Note: Class E cargo compartments | ¦ ¦ ¦ ¦ ¦ require only the installation | ¦ ¦ ¦ ¦ ¦ of smoke or fire detection | ¦ ¦ ¦ ¦ ¦ systems, (not suppression). | ¦ ¦ ¦ ¦ ¦ ¦ ¦ 3. Cabin Smoke C ¦ 1 ¦ 0 ¦ ¦ ¦ *** Detector ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ -------------------------------------------------------------------------------

------------------------------------------------------------------------------- ¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦ ¦ FEDERAL AVIATION ADMINISTRATION ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT: ¦ REVISION NO: 5 ¦ PAGE: ¦ ¦ MU-300, MU-300-10, BE-400, BE-400A ¦ ¦ ¦ ¦ ¦ DATE: 08/12/2002 ¦ 26-2 ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ 1. ¦ 2. NUMBER INSTALLED ¦ ¦ SYSTEM & ¦ -------------------------------------------- ¦ ¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦ ¦ NUMBERS ¦ ¦ --------------------------------------- ¦ ¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦ ¦ 26 FIRE PROTECTION ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ 4. Lavatory Smoke C ¦ - ¦ - ¦ (M)(O) Lavatory Smoke Detection | ¦ ¦ *** Detection Systems ¦ ¦ ¦ System may be inoperative provided: | ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ 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 ¦ ¦ ¦ ¦ ¦ intended to prohibit ¦ ¦ ¦ ¦ ¦ lavatory inspections ¦ ¦ ¦ ¦ ¦ by crewmembers. ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ NOTE 2: A lavatory smoke detection ¦ ¦ ¦ ¦ ¦ system is not required for ¦ ¦ ¦ ¦ ¦ all-cargo operations. ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ -------------------------------------------------------------------------------

------------------------------------------------------------------------------- ¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦ ¦ FEDERAL AVIATION ADMINISTRATION ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT: ¦ REVISION NO: 5 ¦ PAGE: ¦ ¦ MU-300, MU-300-10, BE-400, BE-400A ¦ ¦ ¦ ¦ ¦ DATE: 08/12/2002 ¦ 26-3 ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ 1. ¦ 2. NUMBER INSTALLED ¦ ¦ SYSTEM & ¦ -------------------------------------------- ¦ ¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦ ¦ NUMBERS ¦ ¦ --------------------------------------- ¦ ¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦ ¦ 26 FIRE PROTECTION ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ 5. Lavatory Fire C ¦ - ¦ - ¦ Lavatory Fire Extinguisher System | ¦ ¦ *** Extinguisher Systems ¦ ¦ ¦ may be inoperative provided | ¦ ¦ ¦ ¦ ¦ Lavatory Smoke Detector System | ¦ ¦ ¦ ¦ ¦ operates normally. | ¦ ¦ ¦ ¦ ¦ | ¦ ¦ C ¦ - ¦ - ¦ (M)(O) For each lavatory, the | ¦ ¦ ¦ ¦ ¦ lavatory fire extinguisher | ¦ ¦ ¦ ¦ ¦ system may be inoperative | ¦ ¦ ¦ ¦ ¦ provided: | ¦ ¦ ¦ ¦ ¦ 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 ¦ ¦ ¦ ¦ ¦ intended to prohibit ¦ ¦ ¦ ¦ ¦ lavatory inspections by ¦ ¦ ¦ ¦ ¦ crewmembers. ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ NOTE 2: A lavatory fire ¦ ¦ ¦ ¦ ¦ extinguisher system is not ¦ ¦ ¦ ¦ ¦ required for all-cargo ¦ ¦ ¦ ¦ ¦ operations. ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ -------------------------------------------------------------------------------

------------------------------------------------------------------------------- ¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦ ¦ FEDERAL AVIATION ADMINISTRATION ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT: ¦ REVISION NO: 5 ¦ PAGE: ¦ ¦ MU-300, MU-300-10, BE-400, BE-400A ¦ ¦ ¦ ¦ ¦ DATE: 08/12/2002 ¦ 27-1 ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ 1. ¦ 2. NUMBER INSTALLED ¦ ¦ SYSTEM & ¦ -------------------------------------------- ¦ ¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦ ¦ NUMBERS ¦ ¦ --------------------------------------- ¦ ¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦ ¦ 27 FLIGHT CONTROLS ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ 1. Gust Control Lock C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided an ¦ ¦ ¦ ¦ ¦ alternate means of securing the ¦ ¦ ¦ ¦ ¦ control surfaces is provided. ¦ ¦ ¦ ¦ ¦ ¦ ¦ 2. Angle of Attack ¦ ¦ ¦ Deleted Rev 3. ¦ ¦ Indicating System ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ 3. Stick Shaker ¦ ¦ ¦ Deleted Rev 3. ¦ ¦ Systems ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ 4. Angle of Attack C ¦ 1 ¦ 0 ¦ ¦ ¦ *** (AOA) Indexer ¦ ¦ ¦ ¦ ¦ (Glareshield) ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ -------------------------------------------------------------------------------

------------------------------------------------------------------------------- ¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦ ¦ FEDERAL AVIATION ADMINISTRATION ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT: ¦ REVISION NO: 5 ¦ PAGE: ¦ ¦ MU-300, MU-300-10, BE-400, BE-400A ¦ ¦ ¦ ¦ ¦ DATE: 08/12/2002 ¦ 28-1 ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ 1. ¦ 2. NUMBER INSTALLED ¦ ¦ SYSTEM & ¦ -------------------------------------------- ¦ ¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦ ¦ NUMBERS ¦ ¦ --------------------------------------- ¦ ¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦ ¦ 28 FUEL ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ 1. Wing Fuel Quantity C ¦ 2 ¦ 1 ¦ One may be inoperative provided: ¦ ¦ Indicating Systems ¦ ¦ ¦ a) Wing fuel level is visually ¦ ¦ ¦ ¦ ¦ confirmed to be full before ¦ ¦ ¦ ¦ ¦ departure, and ¦ ¦ ¦ ¦ ¦ b) Fuel totalizer is ¦ ¦ ¦ ¦ ¦ operative. ¦ ¦ ¦ ¦ ¦ ¦ ¦ 2. Fuselage Tank Fuel ¦ ¦ ¦ ¦ ¦ Transfer System ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ 1) (MU-300, C ¦ 1 ¦ 0 ¦ May be inoperative provided ¦ ¦ MU-300-10 ¦ ¦ ¦ flight is predicated on wing fuel ¦ ¦ and BE-400) ¦ ¦ ¦ only. ¦ ¦ ¦ ¦ ¦ ¦ ¦ 2) (BE-400A) C ¦ 2 ¦ 1 ¦ One may be inoperative ¦ ¦ ¦ ¦ ¦ provided: ¦ ¦ ¦ ¦ ¦ a) Fuel Crossfeed System is ¦ ¦ ¦ ¦ ¦ operative, ¦ ¦ ¦ ¦ ¦ b) Both Wing Fuel Quantity ¦ ¦ ¦ ¦ ¦ Indicating Systems are ¦ ¦ ¦ ¦ ¦ operative, and ¦ ¦ ¦ ¦ ¦ c) AFM limitations are ¦ ¦ ¦ ¦ ¦ applied. ¦ ¦ ¦ ¦ ¦ ¦ ¦ C ¦ 2 ¦ 0 ¦ Both may be inoperative provided ¦ ¦ ¦ ¦ ¦ flight is predicated on wing fuel ¦ ¦ ¦ ¦ ¦ only. ¦ ¦ ¦ ¦ ¦ ¦ ¦ 3. Fuel Totalizer C ¦ 1 ¦ 0 ¦ May be inoperative provided all ¦ ¦ ¦ ¦ ¦ Fuel Quantity Indicating Systems ¦ ¦ ¦ ¦ ¦ are operative. ¦ ¦ ¦ ¦ ¦ ¦ ¦ 4. Fuel Temperature ¦ ¦ ¦ Deleted Rev 3. ¦ ¦ Indicator ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ 5. Fuselage Tank C ¦ - ¦ 0 ¦ May be inoperative provided ¦ ¦ *** Fill System ¦ ¦ ¦ alternate refueling procedures are ¦ ¦ ¦ ¦ ¦ established and used. ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ -------------------------------------------------------------------------------

------------------------------------------------------------------------------- ¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦ ¦ FEDERAL AVIATION ADMINISTRATION ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT: ¦ REVISION NO: 5 ¦ PAGE: ¦ ¦ MU-300, MU-300-10, BE-400, BE-400A ¦ ¦ ¦ ¦ ¦ DATE: 08/12/2002 ¦ 28-2 ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ 1. ¦ 2. NUMBER INSTALLED ¦ ¦ SYSTEM & ¦ -------------------------------------------- ¦ ¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦ ¦ NUMBERS ¦ ¦ --------------------------------------- ¦ ¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦ ¦ 28 FUEL ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ 6. Fuselage Tank Fuel C ¦ 1 ¦ 0 ¦ (M)May be inoperative provided: ¦ ¦ Quantity Indicator ¦ ¦ ¦ a) Fuselage tank is verified ¦ ¦ ¦ ¦ ¦ full, or ¦ ¦ ¦ ¦ ¦ b) Fuselage Tank is verified ¦ ¦ ¦ ¦ ¦ empty, and ¦ ¦ ¦ ¦ ¦ c) Fuselage Tank Fill System, ¦ ¦ ¦ ¦ ¦ if installed, is ¦ ¦ ¦ ¦ ¦ deactivated. ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ -------------------------------------------------------------------------------

------------------------------------------------------------------------------- ¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦ ¦ FEDERAL AVIATION ADMINISTRATION ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT: ¦ REVISION NO: 5 ¦ PAGE: ¦ ¦ MU-300, MU-300-10, BE-400, BE-400A ¦ ¦ ¦ ¦ ¦ DATE: 08/12/2002 ¦ 29-1 ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ 1. ¦ 2. NUMBER INSTALLED ¦ ¦ SYSTEM & ¦ -------------------------------------------- ¦ ¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦ ¦ NUMBERS ¦ ¦ --------------------------------------- ¦ ¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦ ¦ 29 HYDRAULIC POWER ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ 1. Main System C ¦ 1 ¦ 0 ¦ May be inoperative provided both ¦ ¦ Pressure Gauge ¦ ¦ ¦ HYD PUMP PRESS LO annunciators are ¦ ¦ ¦ ¦ ¦ operative. ¦ ¦ ¦ ¦ ¦ ¦ ¦ 2. Hydraulic Pump C ¦ 2 ¦ 1 ¦ One may be inoperative provided: ¦ ¦ Pressure Low ¦ ¦ ¦ a) Main System Pressure Gauge ¦ ¦ Annunciators ¦ ¦ ¦ is operative, and ¦ ¦ ¦ ¦ ¦ b) Engine with inoperative ¦ ¦ ¦ ¦ ¦ annunciator is started ¦ ¦ ¦ ¦ ¦ first and hydraulic ¦ ¦ ¦ ¦ ¦ pressure is verified. ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ -------------------------------------------------------------------------------

------------------------------------------------------------------------------- ¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦ ¦ FEDERAL AVIATION ADMINISTRATION ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT: ¦ REVISION NO: 5 ¦ PAGE: ¦ ¦ MU-300, MU-300-10, BE-400, BE-400A ¦ ¦ ¦ ¦ ¦ DATE: 08/12/2002 ¦ 30-1 ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ 1. ¦ 2. NUMBER INSTALLED ¦ ¦ SYSTEM & ¦ -------------------------------------------- ¦ ¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦ ¦ NUMBERS ¦ ¦ --------------------------------------- ¦ ¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦ ¦ 30 ICE AND RAIN ¦ ¦ ¦ ¦ ¦ PROTECTION ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ 1. Windshield Heat C ¦ 2 ¦ 1 ¦ One may be inoperative ¦ ¦ Systems-High ¦ ¦ ¦ provided: ¦ ¦ Position ¦ ¦ ¦ a) Low position is operative, ¦ ¦ ¦ ¦ ¦ b) Airplane is not operated ¦ ¦ ¦ ¦ ¦ into known or forecast icing ¦ ¦ ¦ ¦ ¦ conditions, and ¦ ¦ ¦ ¦ ¦ c) AFM Limitations are applied. ¦ ¦ ¦ ¦ ¦ ¦ ¦ 2. Windshield Wipers C ¦ 2 ¦ 0 ¦ May be inoperative provided the ¦ ¦ *** ¦ ¦ ¦ airplane is not operated in | ¦ ¦ ¦ ¦ ¦ precipitation within 5 NM of the ¦ ¦ ¦ ¦ ¦ airport of takeoff or intended ¦ ¦ ¦ ¦ ¦ landing. ¦ ¦ ¦ ¦ ¦ ¦ ¦ 3. Conditioned Air ¦ ¦ ¦ Deleted, Revision 4. ¦ ¦ Right Side Window ¦ ¦ ¦ ¦ ¦ Defog System ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ 4. Electric Side C ¦ 2 ¦ 0 ¦ ¦ ¦ Window Defog Blower ¦ ¦ ¦ ¦ ¦ Systems ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ 5. Stall Warning Vane B ¦ 2 ¦ 1 ¦ ¦ ¦ Heaters ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ 6. Pitot Heaters B ¦ 2 ¦ 1 ¦ Heater element in one probe may be ¦ ¦ ¦ ¦ ¦ inoperative provided the airplane ¦ ¦ ¦ ¦ ¦ is not operated in visible ¦ ¦ ¦ ¦ ¦ moisture, or in known or forecast ¦ ¦ ¦ ¦ ¦ icing conditions. ¦ ¦ ¦ ¦ ¦ ¦ ¦ 7. Static Port Heat B ¦ 2 ¦ 1 ¦ ¦ ¦ Systems ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ 8. Wing Anti-Ice C ¦ 1 ¦ 0 ¦ May be inoperative provided ¦ ¦ System ¦ ¦ ¦ airplane is not operated into known ¦ ¦ ¦ ¦ ¦ or forecast icing conditions. ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ -------------------------------------------------------------------------------

------------------------------------------------------------------------------- ¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦ ¦ FEDERAL AVIATION ADMINISTRATION ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT: ¦ REVISION NO: 5 ¦ PAGE: ¦ ¦ MU-300, MU-300-10, BE-400, BE-400A ¦ ¦ ¦ ¦ ¦ DATE: 08/12/2002 ¦ 30-2 ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ 1. ¦ 2. NUMBER INSTALLED ¦ ¦ SYSTEM & ¦ -------------------------------------------- ¦ ¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦ ¦ NUMBERS ¦ ¦ --------------------------------------- ¦ ¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦ ¦ 30 ICE AND RAIN ¦ ¦ ¦ ¦ ¦ PROTECTION ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ 9. Tail Heat System C ¦ 1 ¦ 0 ¦ May be inoperative provided the ¦ ¦ ¦ ¦ ¦ airplane is not operated into ¦ ¦ ¦ ¦ ¦ known or forecast icing conditions. ¦ ¦ ¦ ¦ ¦ ¦ ¦ 10. Engine Nacelle Heat B ¦ 2 ¦ 0 ¦ (O)Nacelle heat may be inoperative ¦ ¦ Systems ¦ ¦ ¦ provided: ¦ ¦ ¦ ¦ ¦ a) The nacelle heat is failed ¦ ¦ ¦ ¦ ¦ to the "ON" position and RAT ¦ ¦ ¦ ¦ ¦ is maintained at less than ¦ ¦ ¦ ¦ ¦ +10 degrees C, or ¦ ¦ ¦ ¦ ¦ b) Aircraft is not operated in ¦ ¦ ¦ ¦ ¦ known or forecast icing or ¦ ¦ ¦ ¦ ¦ in visible moisture. ¦ ¦ ¦ ¦ ¦ ¦ ¦ 11. Ice Detector C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided AFM ¦ ¦ *** ¦ ¦ ¦ Limitations are applied. ¦ ¦ ¦ ¦ ¦ ¦ ¦ 12. Pitot Heat B ¦ 2 ¦ 1 ¦ May be inoperative provided: ¦ ¦ Indicator Lights ¦ ¦ ¦ a) All other elements of the ¦ ¦ ¦ ¦ ¦ pitot heat system operate ¦ ¦ ¦ ¦ ¦ normally, and ¦ ¦ ¦ ¦ ¦ b) The airplane is not ¦ ¦ ¦ ¦ ¦ operated in known or ¦ ¦ ¦ ¦ ¦ forecast icing conditions. ¦ ¦ ¦ ¦ ¦ ¦ ¦ 13. AOA Heat B ¦ 2 ¦ 0 ¦ May be inoperative provided: ¦ ¦ Indicator ¦ ¦ ¦ a) All other elements of the ¦ ¦ ¦ ¦ ¦ AOA system operate ¦ ¦ ¦ ¦ ¦ normally, and ¦ ¦ ¦ ¦ ¦ b) The airplane is not ¦ ¦ ¦ ¦ ¦ operated in known or ¦ ¦ ¦ ¦ ¦ forecast icing conditions. ¦ ¦ ¦ ¦ ¦ ¦ ¦ 14. Static Port Heat B ¦ 2 ¦ 1 ¦ May be inoperative provided: ¦ ¦ Indicator Lights ¦ ¦ ¦ a) All other elements of the ¦ ¦ ¦ ¦ ¦ static systems operate ¦ ¦ ¦ ¦ ¦ normally, and ¦ ¦ ¦ ¦ ¦ b) The airplane is not ¦ ¦ ¦ ¦ ¦ operated in known or ¦ ¦ ¦ ¦ ¦ forecast icing conditions. ¦ -------------------------------------------------------------------------------

------------------------------------------------------------------------------- ¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦ ¦ FEDERAL AVIATION ADMINISTRATION ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT: ¦ REVISION NO: 5 ¦ PAGE: ¦ ¦ MU-300, MU-300-10, BE-400, BE-400A ¦ ¦ ¦ ¦ ¦ DATE: 08/12/2002 ¦ 31-1 ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ 1. ¦ 2. NUMBER INSTALLED ¦ ¦ SYSTEM & ¦ -------------------------------------------- ¦ ¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦ ¦ NUMBERS ¦ ¦ --------------------------------------- ¦ ¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦ ¦ 31 INDICATING/RECORDING ¦ ¦ ¦ ¦ ¦ SYSTEMS ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ 1. Clocks C ¦ - ¦ - ¦ As required by FAR. ¦ ¦ ¦ ¦ ¦ ¦ ¦ 2. Flight Hour Meter C ¦ 1 ¦ 0 ¦ (O) ¦ ¦ *** ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ 3. Flight Data C ¦ - ¦ 1 ¦ Any in excess of those required by | ¦ ¦ *** Recorder System ¦ ¦ ¦ FAR may be inoperative. | ¦ ¦ (FDR) ¦ ¦ ¦ | ¦ ¦ A ¦ - ¦ 0 ¦ May be inoperative provided: | ¦ ¦ ¦ ¦ ¦ a) Cockpit Voice Recorder (CVR) | ¦ ¦ ¦ ¦ ¦ operates normally, | ¦ ¦ ¦ ¦ ¦ b) Airplane is not dispatched from | ¦ ¦ ¦ ¦ ¦ a designated airport as listed | ¦ ¦ ¦ ¦ ¦ in the operator's MEL unless: | ¦ ¦ ¦ ¦ ¦ 1. The FDR failure occurs after | ¦ ¦ ¦ ¦ ¦ pushback but prior to | ¦ ¦ ¦ ¦ ¦ takeoff, or | ¦ ¦ ¦ ¦ ¦ 2. The 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 accomplished | ¦ ¦ ¦ ¦ ¦ prior to dispatch, and | ¦ ¦ ¦ ¦ ¦ d) Repairs are made within three | ¦ ¦ ¦ ¦ ¦ flight days. | ¦ ¦ ¦ ¦ ¦ | ¦ ¦ FDR Recording A ¦ - ¦ - ¦ May be inoperative provided: | ¦ ¦ Parameters ¦ ¦ ¦ a) Cockpit Voice Recording (CVR) | ¦ ¦ required by FAR ¦ ¦ ¦ operates normally, and | ¦ ¦ ¦ ¦ ¦ b) Repairs are made within 20 | ¦ ¦ ¦ ¦ ¦ calendar days. | ¦ ¦ ¦ ¦ ¦ ¦ ¦ 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: 5 ¦ PAGE: ¦ ¦ MU-300, MU-300-10, BE-400, BE-400A ¦ ¦ ¦ ¦ ¦ DATE: 08/12/2002 ¦ 31-2 ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ 1. ¦ 2. NUMBER INSTALLED ¦ ¦ SYSTEM & ¦ -------------------------------------------- ¦ ¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦ ¦ NUMBERS ¦ ¦ --------------------------------------- ¦ ¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦ ¦ 31 INDICATING/RECORDING ¦ ¦ ¦ ¦ ¦ SYSTEMS ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ 4. Unassigned D ¦ - ¦ 0 ¦ | ¦ ¦ Annunciators ¦ ¦ ¦ | ¦ ¦ ¦ ¦ ¦ ¦ ¦ 5. Master Caution B ¦ 2 ¦ 1 ¦ | ¦ ¦ Annunciator ¦ ¦ ¦ | ¦ ¦ ¦ ¦ ¦ ¦ ¦ 6. Master Warning A ¦ 2 ¦ 1 ¦ One may be inoperative provided | ¦ ¦ Annunciator ¦ ¦ ¦ repairs are made within one flight | ¦ ¦ ¦ ¦ ¦ day. | ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ -------------------------------------------------------------------------------

------------------------------------------------------------------------------- ¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦ ¦ FEDERAL AVIATION ADMINISTRATION ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT: ¦ REVISION NO: 5 ¦ PAGE: ¦ ¦ MU-300, MU-300-10, BE-400, BE-400A ¦ ¦ ¦ ¦ ¦ DATE: 08/12/2002 ¦ 32-1 ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ 1. ¦ 2. NUMBER INSTALLED ¦ ¦ SYSTEM & ¦ -------------------------------------------- ¦ ¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦ ¦ NUMBERS ¦ ¦ --------------------------------------- ¦ ¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦ ¦ 1. Wheel Brake C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided: | ¦ ¦ Anti-Skid System ¦ ¦ ¦ a)The Anti-Skid Switch remains | ¦ ¦ ¦ ¦ ¦ in the OFF position, and | ¦ ¦ ¦ ¦ ¦ b)AFM/POH limitations and | ¦ ¦ ¦ ¦ ¦ performance charts are | ¦ ¦ ¦ ¦ ¦ applied. | ¦ ¦ ¦ ¦ ¦ ¦ ¦ 2. Parking Brake ¦ ¦ ¦ Deleted Rev 3. ¦ ¦ ¦ ¦ ¦ ¦ ¦ 3. Landing Gear C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided | ¦ ¦ Handle Solenoid ¦ ¦ ¦ Downlock Release Latch is | ¦ ¦ ¦ ¦ ¦ operative. | ¦ ¦ ¦ ¦ ¦ (Applicable to RK-98, 110 and | ¦ ¦ ¦ ¦ ¦ after). | ¦ ¦ ¦ ¦ ¦ | ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ -------------------------------------------------------------------------------

------------------------------------------------------------------------------- ¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦ ¦ FEDERAL AVIATION ADMINISTRATION ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT: ¦ REVISION NO: 5 ¦ PAGE: ¦ ¦ MU-300, MU-300-10, BE-400, BE-400A ¦ ¦ ¦ ¦ ¦ DATE: 08/12/2002 ¦ 33-1 ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ 1. ¦ 2. NUMBER INSTALLED ¦ ¦ SYSTEM & ¦ -------------------------------------------- ¦ ¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦ ¦ NUMBERS ¦ ¦ --------------------------------------- ¦ ¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦ ¦ 33 LIGHTS ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ 1. Position Lights C ¦ 1 ¦ 0 ¦ May be inoperative provided ¦ ¦ System ¦ ¦ ¦ aircraft is not operated at night. ¦ ¦ ¦ ¦ ¦ ¦ ¦ 1)Tail Position C ¦ 1 ¦ 0 ¦ May be inoperative provided the | ¦ ¦ Light ¦ ¦ ¦ Anti-Collision Light (Strobe) is | ¦ ¦ ¦ ¦ ¦ ON during night operations. | ¦ ¦ ¦ ¦ ¦ ¦ ¦ 2)Wing Tip Nav C ¦ 4 ¦ 2 ¦ May be inoperative provided one | ¦ ¦ Light ¦ ¦ ¦ lightbulb on each wing tip is | ¦ ¦ ¦ ¦ ¦ operative. | ¦ ¦ ¦ ¦ ¦ ¦ ¦ 2. Anti-Collision C ¦ 1 ¦ 0 ¦ May be inoperative provided ¦ ¦ Light System (Strobe) ¦ ¦ ¦ airplane is not operated at night. ¦ ¦ ¦ ¦ ¦ ¦ ¦ 3. Rotating Beacon C ¦ 1 ¦ 0 ¦ ¦ ¦ *** (Flashing) ¦ ¦ ¦ | ¦ ¦ ¦ ¦ ¦ ¦ ¦ 4. Landing/Taxi C ¦ 2 ¦ 1 ¦ ¦ ¦ Lights ¦ ¦ ¦ ¦ ¦ C ¦ 2 ¦ 0 ¦ May be inoperative provided ¦ ¦ ¦ ¦ ¦ airplane is not operated at night. ¦ ¦ ¦ ¦ ¦ ¦ ¦ 5. Wing Inspection C ¦ - ¦ 0 ¦ May be inoperative provided a ¦ ¦ Lights ¦ ¦ ¦ portable lamp/light of adequate ¦ ¦ ¦ ¦ ¦ capacity for wing and/or control ¦ ¦ ¦ ¦ ¦ surface inspection is available for ¦ ¦ ¦ ¦ ¦ night operations in icing ¦ ¦ ¦ ¦ ¦ conditions. ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ -------------------------------------------------------------------------------

------------------------------------------------------------------------------- ¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦ ¦ FEDERAL AVIATION ADMINISTRATION ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT: ¦ REVISION NO: 5 ¦ PAGE: ¦ ¦ MU-300, MU-300-10, BE-400, BE-400A ¦ ¦ ¦ ¦ ¦ DATE: 08/12/2002 ¦ 33-2 ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ 1. ¦ 2. NUMBER INSTALLED ¦ ¦ SYSTEM & ¦ -------------------------------------------- ¦ ¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦ ¦ NUMBERS ¦ ¦ --------------------------------------- ¦ ¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦ ¦ 33 LIGHTS ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ 6. Cockpit and C ¦ - ¦ - ¦ Individual lights may be ¦ ¦ Instrument ¦ ¦ ¦ inoperative provided the remaining ¦ ¦ Lighting Systems ¦ ¦ ¦ lights are: ¦ ¦ ¦ ¦ ¦ a) Sufficient to clearly illuminate ¦ ¦ ¦ ¦ ¦ all required instruments, ¦ ¦ ¦ ¦ ¦ controls, and other devices for ¦ ¦ ¦ ¦ ¦ which it is provided, ¦ ¦ ¦ ¦ ¦ b) Positioned so that direct rays ¦ ¦ ¦ ¦ ¦ are shielded from crewmembers ¦ ¦ ¦ ¦ ¦ eyes, and ¦ ¦ ¦ ¦ ¦ c) Lighting configuration and ¦ ¦ ¦ ¦ ¦ intensity is acceptable to the ¦ ¦ ¦ ¦ ¦ flight crew. ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ 7. Passenger Notice C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided ¦ ¦ System ¦ ¦ ¦ procedures are established and used ¦ ¦ ¦ ¦ ¦ for alerting the passengers when ¦ ¦ ¦ ¦ ¦ seat belts should be fastened and ¦ ¦ ¦ ¦ ¦ smoking is prohibited. ¦ ¦ 8. Cabin Interior C ¦ - ¦ - ¦ May be partially inoperative ¦ ¦ Lighting System ¦ ¦ ¦ provided: ¦ ¦ ¦ ¦ ¦ a) Cabin emergency lighting ¦ ¦ ¦ ¦ ¦ is operative, ¦ ¦ ¦ ¦ ¦ b) Sufficient lighting is ¦ ¦ ¦ ¦ ¦ available for crew to ¦ ¦ ¦ ¦ ¦ perform required duties, and ¦ ¦ ¦ ¦ ¦ c) Lighting configuration at ¦ ¦ ¦ ¦ ¦ dispatch is acceptable to ¦ ¦ ¦ ¦ ¦ the flight crew. ¦ ¦ ¦ ¦ ¦ ¦ ¦ 9. Emergency Lighting ¦ ¦ ¦ Deleted Rev 3. ¦ ¦ System ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ 10. Recognition C ¦ 1 ¦ 0 ¦ ¦ ¦ *** Lighting System ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ 11. Baggage Compartment C ¦ 1 ¦ 0 ¦ ¦ ¦ *** Light ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ -------------------------------------------------------------------------------

------------------------------------------------------------------------------- ¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦ ¦ FEDERAL AVIATION ADMINISTRATION ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT: ¦ REVISION NO: 5 ¦ PAGE: ¦ ¦ MU-300, MU-300-10, BE-400, BE-400A ¦ ¦ ¦ ¦ ¦ DATE: 08/12/2002 ¦ 33-3 ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ 1. ¦ 2. NUMBER INSTALLED ¦ ¦ SYSTEM & ¦ -------------------------------------------- ¦ ¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦ ¦ NUMBERS ¦ ¦ --------------------------------------- ¦ ¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦ ¦ 33 LIGHTS ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ 12. Tail Logo Lights C ¦ 2 ¦ 0 ¦ ¦ ¦ *** ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ 13. Floor Proximity C ¦ - ¦ - ¦ Individual lights may be partially ¦ ¦ *** Lighting System ¦ ¦ ¦ inoperative provided it is verified ¦ ¦ ¦ ¦ ¦ that the FAA approved minimum ¦ ¦ ¦ ¦ ¦ acceptable lighting levels ¦ ¦ ¦ ¦ ¦ specified in one of the following ¦ ¦ ¦ ¦ ¦ documents are complied with: ¦ ¦ ¦ ¦ ¦ a) FAA engineering approval ¦ ¦ ¦ ¦ ¦ letter. ¦ ¦ ¦ ¦ ¦ b) FAA approved report of the ¦ ¦ ¦ ¦ ¦ type design holder. ¦ ¦ ¦ ¦ ¦ c) Limitations and Conditions ¦ ¦ ¦ ¦ ¦ section of the applicable ¦ ¦ ¦ ¦ ¦ Supplemental Type ¦ ¦ ¦ ¦ ¦ Certificate (STC). ¦ ¦ ¦ ¦ ¦ d) FAA approved report ¦ ¦ ¦ ¦ ¦ incorporated in the Master ¦ ¦ ¦ ¦ ¦ Drawing List for the ¦ ¦ ¦ ¦ ¦ applicable STC. ¦ ¦ ¦ ¦ ¦ ¦ ¦ 14. Pulse Light C ¦ 1 ¦ 0 ¦ May be inoperative. | ¦ ¦ *** ¦ ¦ ¦ | ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ -------------------------------------------------------------------------------

------------------------------------------------------------------------------- ¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦ ¦ FEDERAL AVIATION ADMINISTRATION ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT: ¦ REVISION NO: 5 ¦ PAGE: ¦ ¦ MU-300, MU-300-10, BE-400, BE-400A ¦ ¦ ¦ ¦ ¦ DATE: 08/12/2002 ¦ 34-1 ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ 1. ¦ 2. NUMBER INSTALLED ¦ ¦ SYSTEM & ¦ -------------------------------------------- ¦ ¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦ ¦ NUMBERS ¦ ¦ --------------------------------------- ¦ ¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦ ¦ 34 NAVIGATION ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ 1. Attitude Indicators/ ¦ ¦ ¦ Deleted Rev 3. ¦ ¦ Vertical Gyro Systems ¦ ¦ ¦ ¦ ¦ (Horizon Indicators) ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ 2. Directional Gyro ¦ ¦ ¦ Deleted Rev 3. ¦ ¦ Compass Systems ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ 3. Standby Attitude ¦ ¦ ¦ Deleted Rev 3. ¦ ¦ Indicator ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ 4. Turn Indication C ¦ - ¦ 0 ¦ May be inoperative provided: | ¦ ¦ Systems ¦ ¦ ¦ a) Airplane is operated in day | ¦ ¦ ¦ ¦ ¦ VMC only, and | ¦ ¦ ¦ ¦ ¦ b) Two independent Primary | ¦ ¦ ¦ ¦ ¦ Attitude Systems are | ¦ ¦ ¦ ¦ ¦ operative. | ¦ ¦ ¦ ¦ ¦ ¦ ¦ C ¦ - ¦ 0 ¦ May be inoperative provided: | ¦ ¦ ¦ ¦ ¦ a) A third gyroscopic bank and | ¦ ¦ ¦ ¦ ¦ pitch indicator (Standby | ¦ ¦ ¦ ¦ ¦ Attitude) is operative, and | ¦ ¦ ¦ ¦ ¦ b) Two independent Primary | ¦ ¦ ¦ ¦ ¦ Attitude Systems are | ¦ ¦ ¦ ¦ ¦ operative. | ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ -------------------------------------------------------------------------------

------------------------------------------------------------------------------- ¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦ ¦ FEDERAL AVIATION ADMINISTRATION ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT: ¦ REVISION NO: 5 ¦ PAGE: ¦ ¦ MU-300, MU-300-10, BE-400, BE-400A ¦ ¦ ¦ ¦ ¦ DATE: 08/12/2002 ¦ 34-2 ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ 1. ¦ 2. NUMBER INSTALLED ¦ ¦ SYSTEM & ¦ -------------------------------------------- ¦ ¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦ ¦ NUMBERS ¦ ¦ --------------------------------------- ¦ ¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦ ¦ 34 NAVIGATION ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ 5. Navigation Systems C ¦ - ¦ - ¦ (O) As required by FAR. | ¦ ¦ (VOR/ILS, GPS, LORAN, ¦ ¦ ¦ | ¦ ¦ Doppler, RNAV, INS, ¦ ¦ ¦ | ¦ ¦ Omega/VLF),FMS ¦ ¦ ¦ | ¦ ¦ ¦ ¦ ¦ ¦ ¦ 6. Weather Radar C ¦ 1 ¦ - ¦ As required by FAR. ¦ ¦ System ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ a) Thunderstorm C ¦ 1 ¦ - ¦ | ¦ ¦ Detection ¦ ¦ ¦ | ¦ ¦ Equipment ¦ ¦ ¦ | ¦ ¦ ¦ ¦ ¦ ¦ ¦ 7. ATC Transponders C ¦ - ¦ 0 ¦ May be inoperative provided: | ¦ ¦ and Automatic ¦ ¦ ¦ a) Enroute operations do no require | ¦ ¦ Altitude Reporting ¦ ¦ ¦ its use, and | ¦ ¦ Systems ¦ ¦ ¦ b) Prior to 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. | ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ 8. Deleted ¦ ¦ ¦ Deleted prior to Rev 3. ¦ ¦ ¦ ¦ ¦ ¦ ¦ 9. Flight Director C ¦ - ¦ 0 ¦ (O)May be inoperative provided | ¦ ¦ System ¦ ¦ ¦ approach minimums do not require | ¦ ¦ ¦ ¦ ¦ its use. ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ -------------------------------------------------------------------------------

------------------------------------------------------------------------------- ¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦ ¦ FEDERAL AVIATION ADMINISTRATION ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT: ¦ REVISION NO: 5 ¦ PAGE: ¦ ¦ MU-300, MU-300-10, BE-400, BE-400A ¦ ¦ ¦ ¦ ¦ DATE: 08/12/2002 ¦ 34-3 ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ 1. ¦ 2. NUMBER INSTALLED ¦ ¦ SYSTEM & ¦ -------------------------------------------- ¦ ¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦ ¦ NUMBERS ¦ ¦ --------------------------------------- ¦ ¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦ ¦ 34 NAVIGATION ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ 10. Altitude Alerting A ¦ - ¦ 0 ¦ (O)Except where enroute operations | ¦ ¦ System ¦ ¦ ¦ require its use, may be | ¦ ¦ ¦ ¦ ¦ inoperative provided: | ¦ ¦ ¦ ¦ ¦ a) Autopilot with altitude | ¦ ¦ ¦ ¦ ¦ hold is operative, and | ¦ ¦ ¦ ¦ ¦ b) Repairs are made within | ¦ ¦ ¦ ¦ ¦ three flight days. | ¦ ¦ ¦ ¦ ¦ ¦ ¦ 11. Radio Altimeter C ¦ 1 ¦ 0 ¦ As required by FAR. ¦ ¦ System ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ NOTE: Comply with Flight Director ¦ ¦ ¦ ¦ ¦ Limitations in AFM. ¦ ¦ ¦ ¦ ¦ ¦ ¦ 12. Air Data System ¦ ¦ ¦ Deleted Rev 3. ¦ ¦ ¦ ¦ ¦ ¦ ¦ 13. Nonstabilized B ¦ 1 ¦ 0 ¦ May be inoperative provided any | ¦ ¦ Magnetic Compass ¦ ¦ ¦ combination of three Gyro or INS | ¦ ¦ ¦ ¦ ¦ (IRU) stabilized Compass Systems | ¦ ¦ ¦ ¦ ¦ are operative. | ¦ ¦ ¦ ¦ ¦ ¦ ¦ B ¦ 1 ¦ 0 ¦ May be inoperative provided: | ¦ ¦ ¦ ¦ ¦ a) Any combination of two Gyro | ¦ ¦ ¦ ¦ ¦ INS Stabilized Compass Systems | ¦ ¦ ¦ ¦ ¦ operate normally, 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 ¦ May be inoperative for flights | ¦ ¦ ¦ ¦ ¦ that are entirely within areas of | ¦ ¦ ¦ ¦ ¦ magnetic unreliability provided at | ¦ ¦ ¦ ¦ ¦ least two Stabilized Directional | ¦ ¦ ¦ ¦ ¦ Gyro Systems are installed, | ¦ ¦ ¦ ¦ ¦ operate normally, and used in | ¦ ¦ ¦ ¦ ¦ conjunction with approved Free Gyro | ¦ ¦ ¦ ¦ ¦ Navigation Techniques. | ¦ ¦ ¦ ¦ ¦ ¦ -------------------------------------------------------------------------------

------------------------------------------------------------------------------- ¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦ ¦ FEDERAL AVIATION ADMINISTRATION ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT: ¦ REVISION NO: 5 ¦ PAGE: ¦ ¦ MU-300, MU-300-10, BE-400, BE-400A ¦ ¦ ¦ ¦ ¦ DATE: 08/12/2002 ¦ 34-4 ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ 1. ¦ 2. NUMBER INSTALLED ¦ ¦ SYSTEM & ¦ -------------------------------------------- ¦ ¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦ ¦ NUMBERS ¦ ¦ --------------------------------------- ¦ ¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦ ¦ 34 NAVIGATION ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ 14. Marker Beacon C ¦ - ¦ 0 ¦ May be inoperative provided ¦ ¦ System ¦ ¦ ¦ approach minimums do not require ¦ ¦ ¦ ¦ ¦ its use. ¦ ¦ ¦ ¦ ¦ ¦ ¦ 15. Traffic Alert B ¦ - ¦ 0 ¦ (M)May be inoperative provided: | ¦ ¦ Collision Avoidance ¦ ¦ ¦ a)System is deactivated and | ¦ ¦ System (TCAS) II ¦ ¦ ¦ secured, and | ¦ ¦ ¦ ¦ ¦ b)Enroute or approach procedures | ¦ ¦ ¦ ¦ ¦ do not require its use. | ¦ ¦ ¦ ¦ ¦ ¦ ¦ C ¦ 2 ¦ 1 ¦ (M)(O)May be inoperative provided: | ¦ ¦ ¦ ¦ ¦ a)Not required by FAR, | ¦ ¦ ¦ ¦ ¦ b)System is deactivated and | ¦ ¦ ¦ ¦ ¦ secured, and | ¦ ¦ ¦ ¦ ¦ c)Enroute or approach procedures | ¦ ¦ ¦ ¦ ¦ do not require its use. | ¦ ¦ ¦ ¦ ¦ ¦ ¦ 1)Combined Traffic C ¦ 2 ¦ 1 ¦ May be inoperative on the | ¦ ¦ Alert (TA) and ¦ ¦ ¦ non-flying pilot side provided: | ¦ ¦ Resolution Advisory ¦ ¦ ¦ a)TA and RA display is operative | ¦ ¦ (RA) Dual Display ¦ ¦ ¦ on the flying pilot side, and | ¦ ¦ System(s) ¦ ¦ ¦ flying pilot side, and | ¦ ¦ ¦ ¦ ¦ b)TA and RA audio function is | ¦ ¦ ¦ ¦ ¦ operative on flying pilot | ¦ ¦ ¦ ¦ ¦ side. | ¦ ¦ ¦ ¦ ¦ ¦ ¦ 2)Resolution C ¦ 2 ¦ 1 ¦ (O)One may be inoperative on | ¦ ¦ Advisory (RA) ¦ ¦ ¦ non-flying pilot side. | ¦ ¦ Display System(s) ¦ ¦ ¦ | ¦ ¦ ¦ ¦ ¦ ¦ ¦ C ¦ - ¦ 0 ¦ (O)May be inoperative provided: | ¦ ¦ ¦ ¦ ¦ a)Traffic Alert (TA) visual | ¦ ¦ ¦ ¦ ¦ display and audio functions | ¦ ¦ ¦ ¦ ¦ are operative, | ¦ ¦ ¦ ¦ ¦ operative, and | ¦ ¦ ¦ ¦ ¦ b TA only mode is selected | ¦ ¦ ¦ ¦ ¦ by the crew. and | ¦ ¦ ¦ ¦ ¦ c)Enroute or approach procedures | ¦ ¦ ¦ ¦ ¦ do not require its use. | ¦ ¦ (CON'T.) ¦ ¦ ¦ | ¦ -------------------------------------------------------------------------------

------------------------------------------------------------------------------- ¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦ ¦ FEDERAL AVIATION ADMINISTRATION ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT: ¦ REVISION NO: 5 ¦ PAGE: ¦ ¦ MU-300, MU-300-10, BE-400, BE-400A ¦ ¦ ¦ ¦ ¦ DATE: 08/12/2002 ¦ 34-5 ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ 1. ¦ 2. NUMBER INSTALLED ¦ ¦ SYSTEM & ¦ -------------------------------------------- ¦ ¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦ ¦ NUMBERS ¦ ¦ --------------------------------------- ¦ ¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦ ¦ 34 NAVIGATION ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ 15. Traffic Alert ¦ ¦ ¦ | ¦ ¦ Colision Avoidance ¦ ¦ ¦ | ¦ ¦ System (TCAS II) ¦ ¦ ¦ | ¦ ¦ (CON'T.) ¦ ¦ ¦ | ¦ ¦ ¦ ¦ ¦ ¦ ¦ 3) TA Display C ¦ - ¦ 0 ¦ (O)May be inoperative provided | ¦ ¦ system(s) ¦ ¦ ¦ all installed RA display and | ¦ ¦ ¦ ¦ ¦ audio functions are operative | ¦ ¦ ¦ ¦ ¦ ¦ ¦ 16. TCAS I B ¦ - ¦ 0 ¦ (M)(O)May be inoperative provided: | ¦ ¦ ¦ ¦ ¦ a)System is deactivated and | ¦ ¦ ¦ ¦ ¦ secured, and | ¦ ¦ ¦ ¦ ¦ b)Enroute or approach procedures | ¦ ¦ ¦ ¦ ¦ do not require its use. | ¦ ¦ ¦ ¦ ¦ ¦ ¦ C ¦ - ¦ 0 ¦ (M)(O)May be inoperative provided: | ¦ ¦ ¦ ¦ ¦ a)Not required by FAR, | ¦ ¦ ¦ ¦ ¦ b)System is deactivated and | ¦ ¦ ¦ ¦ ¦ secured, and | ¦ ¦ ¦ ¦ ¦ c)Enroute or approach procedures | ¦ ¦ ¦ ¦ ¦ do not require its use. | ¦ ¦ ¦ ¦ ¦ ¦ ¦ 17. Traffic Alert C ¦ 1 ¦ 0 ¦ | ¦ ¦ *** Collision Avoidance ¦ ¦ ¦ | ¦ ¦ Device (TCAD) ¦ ¦ ¦ | ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ -------------------------------------------------------------------------------

------------------------------------------------------------------------------- ¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦ ¦ FEDERAL AVIATION ADMINISTRATION ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT: ¦ REVISION NO: 5 ¦ PAGE: ¦ ¦ MU-300, MU-300-10, BE-400, BE-400A ¦ ¦ ¦ ¦ ¦ DATE: 08/12/2002 ¦ 34-6 ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ 1. ¦ 2. NUMBER INSTALLED ¦ ¦ SYSTEM & ¦ -------------------------------------------- ¦ ¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦ ¦ NUMBERS ¦ ¦ --------------------------------------- ¦ ¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦ ¦ 34 NAVIGATION ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ 18. Ground Proximity A ¦ - ¦ 1 ¦ (O)May be inoperative provided: | ¦ ¦ *** Warning System ¦ ¦ ¦ a)Alternate procedures are | ¦ ¦ ¦ ¦ ¦ established and used, and | ¦ ¦ ¦ ¦ ¦ b)Repairs are made within | ¦ ¦ ¦ ¦ ¦ two flight days. | ¦ ¦ ¦ ¦ ¦ ¦ ¦ 1) Modes 1-4 A ¦ - ¦ 0 ¦ (O)May be inoperative provided: | ¦ ¦ ¦ ¦ ¦ a)Alternate procedures are | ¦ ¦ ¦ ¦ ¦ established and used, and | ¦ ¦ ¦ ¦ ¦ b)Repairs are made within | ¦ ¦ ¦ ¦ ¦ two flight days. | ¦ ¦ ¦ ¦ ¦ ¦ ¦ 2) Test Mode A ¦ 1 ¦ 0 ¦ May be inoperative provided: | ¦ ¦ ¦ ¦ ¦ a)The GPWS is considered | ¦ ¦ ¦ ¦ ¦ inoperative, and | ¦ ¦ ¦ ¦ ¦ b)Repairs are made within | ¦ ¦ ¦ ¦ ¦ two flight days. | ¦ ¦ ¦ ¦ ¦ ¦ ¦ 3) Glideslope B ¦ 2 ¦ 0 ¦ ¦ ¦ Deviation ¦ ¦ ¦ ¦ ¦ (Mode 5) ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ 4) Advisory C ¦ - ¦ 0 ¦ (O)May be inoperative provided ¦ ¦ *** Callouts ¦ ¦ ¦ alternate procedures are ¦ ¦ ¦ ¦ ¦ established and used. ¦ ¦ ¦ ¦ ¦ ¦ ¦ 5) Windshear Mode C ¦ - ¦ 0 ¦ (O)May be inoperative provided ¦ ¦ ¦ ¦ ¦ alternate procedures are ¦ ¦ ¦ ¦ ¦ established and used. ¦ ¦ ¦ ¦ ¦ ¦ ¦ 6) TAWS C ¦ - ¦ 0 ¦ ¦ ¦ ¦ *** ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ 19. Flight Profile D ¦ - ¦ - ¦ May be inoperative. ¦ ¦ ¦ Advisory System ¦ ¦ ¦ ¦ ¦ ¦ *** (FPAS) ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ -------------------------------------------------------------------------------

------------------------------------------------------------------------------- ¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦ ¦ FEDERAL AVIATION ADMINISTRATION ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT: ¦ REVISION NO: 5 ¦ PAGE: ¦ ¦ MU-300, MU-300-10, BE-400, BE-400A ¦ ¦ ¦ ¦ ¦ DATE: 08/12/2002 ¦ 34-7 ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ 1. ¦ 2. NUMBER INSTALLED ¦ ¦ SYSTEM & ¦ -------------------------------------------- ¦ ¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦ ¦ NUMBERS ¦ ¦ --------------------------------------- ¦ ¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦ ¦ 34 NAVIGATION ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ 20. Automatic C ¦ - ¦ - ¦ As required by FAR ¦ ¦ Direction Finding ¦ ¦ ¦ ¦ ¦ (ADF) Systems ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ 21. Vertical Speed C ¦ 2 ¦ 1 ¦ ¦ ¦ Indicators (VSI) ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ 22. DME D ¦ - ¦ - ¦ Any in excess of those required by ¦ ¦ ¦ ¦ ¦ ¦ the FAR may be inoperative. ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ 23. MFD/ND C ¦ - ¦ - ¦ (O)The maximum number of displays ¦ ¦ ¦ ¦ ¦ (EFD's, PFD's, RTU's, CDU's, SDU's) ¦ ¦ ¦ ¦ ¦ that may be simultaneously ¦ ¦ ¦ ¦ ¦ inoperative is as follows: ¦ ¦ ¦ ¦ ¦ 4 Tube Acft - the MFD and/or ¦ ¦ ¦ ¦ ¦ the ND ¦ ¦ ¦ ¦ ¦ 3 Tube Acft - the MFD ¦ ¦ ¦ ¦ ¦ 2 Tube Acft - the MFD ¦ ¦ ¦ ¦ ¦ NOTE: Radar display will be ¦ ¦ ¦ ¦ ¦ unavailable. See Weather ¦ ¦ ¦ ¦ ¦ Radar System dispatch ¦ ¦ ¦ ¦ ¦ limitations. ¦ ¦ ¦ ¦ ¦ ¦ ¦ 24. CDU's C ¦ 2 ¦ 1 ¦ (O)For a 3 or 4 tube configured ¦ ¦ ¦ ¦ ¦ aircraft, a CDU may be inoperative ¦ ¦ ¦ ¦ ¦ provided: ¦ ¦ ¦ ¦ ¦ a) Both RTU's are operative, ¦ ¦ ¦ ¦ ¦ and ¦ ¦ ¦ ¦ ¦ b) Both SDU's are operative. ¦ ¦ ¦ ¦ ¦ ¦ ¦ 25. SDU's C ¦ 2 ¦ 1 ¦ (O)For a 3 or 4 tube configured ¦ ¦ ¦ ¦ ¦ aircraft, the copilot SDU may be ¦ ¦ ¦ ¦ ¦ inoperative provided both CDU's are ¦ ¦ ¦ ¦ ¦ operative. ¦ ¦ ¦ ¦ ¦ ¦ ¦ 26. Slip/Skid C ¦ 2 ¦ 1 ¦ ¦ ¦ Indicators ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ -------------------------------------------------------------------------------

------------------------------------------------------------------------------- ¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦ ¦ FEDERAL AVIATION ADMINISTRATION ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT: ¦ REVISION NO: 5 ¦ PAGE: ¦ ¦ MU-300, MU-300-10, BE-400, BE-400A ¦ ¦ ¦ ¦ ¦ DATE: 08/12/2002 ¦ 34-8 ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ 1. ¦ 2. NUMBER INSTALLED ¦ ¦ SYSTEM & ¦ -------------------------------------------- ¦ ¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦ ¦ NUMBERS ¦ ¦ --------------------------------------- ¦ ¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦ ¦ 34 NAVIGATION ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ 27. Navigation ¦ ¦ ¦ | ¦ ¦ *** Databases ¦ ¦ ¦ | ¦ ¦ ¦ ¦ ¦ ¦ ¦ 1) Flight C ¦ - ¦ - ¦ (O)May be out of currency provided: | ¦ ¦ Management ¦ ¦ ¦ a)Current Aeronautical Charts | ¦ ¦ System ¦ ¦ ¦ are used to verify Navigation | ¦ ¦ ¦ ¦ ¦ Fixes prior to dispatch, | ¦ ¦ ¦ ¦ ¦ | ¦ ¦ ¦ ¦ ¦ b)Procedures are established | ¦ ¦ ¦ ¦ ¦ and used to verify status and | ¦ ¦ ¦ ¦ ¦ suitability of Navigation | ¦ ¦ ¦ ¦ ¦ Facilities used to define | ¦ ¦ ¦ ¦ ¦ route of flight, and | ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ c)Approach Navigation Radios | ¦ ¦ ¦ ¦ ¦ are manually tuned and | ¦ ¦ ¦ ¦ ¦ identified. | ¦ ¦ ¦ ¦ ¦ ¦ ¦ 2) Navigation C ¦ - ¦ - ¦ (O)May be out of currency provided: | ¦ ¦ Management ¦ ¦ ¦ a)Current Aeronautical Charts | ¦ ¦ System ¦ ¦ ¦ are used to verify Navigation | ¦ ¦ ¦ ¦ ¦ Fixes prior to dispatch, | ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ b)Procedures are established and | ¦ ¦ ¦ ¦ ¦ used to verify status and | ¦ ¦ ¦ ¦ ¦ suitability of Navigation | ¦ ¦ ¦ ¦ ¦ Facilities used to define | ¦ ¦ ¦ ¦ ¦ route of flight, and | ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ c)Approach Navigation Radios | ¦ ¦ ¦ ¦ ¦ are manually tuned and | ¦ ¦ ¦ ¦ ¦ identified. | ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ -------------------------------------------------------------------------------

------------------------------------------------------------------------------- ¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦ ¦ FEDERAL AVIATION ADMINISTRATION ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT: ¦ REVISION NO: 5 ¦ PAGE: ¦ ¦ MU-300, MU-300-10, BE-400, BE-400A ¦ ¦ ¦ ¦ ¦ DATE: 08/12/2002 ¦ 34-9 ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ 1. ¦ 2. NUMBER INSTALLED ¦ ¦ SYSTEM & ¦ -------------------------------------------- ¦ ¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦ ¦ NUMBERS ¦ ¦ --------------------------------------- ¦ ¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦ ¦ 34 NAVIGATION ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ 28. Windshear C ¦ - ¦ 0 ¦ (O)May be inoperative provided: | ¦ ¦ *** Warning and ¦ ¦ ¦ a)Alternate procedures are | ¦ ¦ Flight Guidance ¦ ¦ ¦ established and used, and | ¦ ¦ System ¦ ¦ ¦ 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. | ¦ ¦ ¦ ¦ ¦ ¦ ¦ 29. Windshear C ¦ - ¦ 0 ¦ (O)May be inoperative provided: | ¦ ¦ *** Detection and ¦ ¦ ¦ a)Alternate procedures are | ¦ ¦ Avoidance System ¦ ¦ ¦ established and used, and | ¦ ¦ ¦ ¦ ¦ b)Windshear Warning and | ¦ ¦ ¦ ¦ ¦ Guidance System operates | ¦ ¦ ¦ ¦ ¦ normally. | ¦ ¦ ¦ ¦ ¦ ¦ ¦ C ¦ - ¦ 0 ¦ (O)May be inoperative provided: | ¦ ¦ ¦ ¦ ¦ a)Alternate procedures are | ¦ ¦ ¦ ¦ ¦ established and used, and | ¦ ¦ ¦ ¦ ¦ b)Takeoffs and landings not | ¦ ¦ ¦ ¦ ¦ conducted in known or | ¦ ¦ ¦ ¦ ¦ forecast windshear conditions. | ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ -------------------------------------------------------------------------------

------------------------------------------------------------------------------- ¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦ ¦ FEDERAL AVIATION ADMINISTRATION ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT: ¦ REVISION NO: 5 ¦ PAGE: ¦ ¦ MU-300, MU-300-10, BE-400, BE-400A ¦ ¦ ¦ ¦ ¦ DATE: 08/12/2002 ¦ 34-10 ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ 1. ¦ 2. NUMBER INSTALLED ¦ ¦ SYSTEM & ¦ -------------------------------------------- ¦ ¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦ ¦ NUMBERS ¦ ¦ --------------------------------------- ¦ ¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦ ¦ 34 NAVIGATION ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ 30. Sonalert Standby B ¦ 1 ¦ 0 ¦ May be inoperative provided the | ¦ ¦ *** Power Indicator ¦ ¦ ¦ Standby Power Annunciator is | ¦ ¦ ¦ ¦ ¦ operative. | ¦ ¦ ¦ ¦ ¦ ¦ ¦ 31. Standby Power B ¦ 1 ¦ 0 ¦ May be inoperative provided the | ¦ ¦ *** Annunciator ¦ ¦ ¦ Sonalert Standby Power Aural | ¦ ¦ ¦ ¦ ¦ Warning is operative. | ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ -------------------------------------------------------------------------------

------------------------------------------------------------------------------- ¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦ ¦ FEDERAL AVIATION ADMINISTRATION ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT: ¦ REVISION NO: 5 ¦ PAGE: ¦ ¦ MU-300, MU-300-10, BE-400, BE-400A ¦ ¦ ¦ ¦ ¦ DATE: 08/12/2002 ¦ 35-1 ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ 1. ¦ 2. NUMBER INSTALLED ¦ ¦ SYSTEM & ¦ -------------------------------------------- ¦ ¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦ ¦ NUMBERS ¦ ¦ --------------------------------------- ¦ ¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦ ¦ 35 OXYGEN ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ 1. Crew Oxygen System ¦ ¦ ¦ Deleted Rev 3. ¦ ¦ ¦ ¦ ¦ ¦ ¦ 2. Crew Oxygen Quick ¦ ¦ ¦ Deleted Rev 3. ¦ ¦ Donning Masks ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ 3. Crew Smoke Goggles ¦ ¦ ¦ Deleted Rev 3. ¦ ¦ ¦ ¦ ¦ ¦ ¦ 4. Passenger Oxygen C ¦ 1 ¦ - ¦ As required by FAR. | ¦ ¦ ¦ ¦ ¦ ¦ ¦ 1)Passenger Oxygen C ¦ - ¦ 0 ¦ May be inoperative provided: | ¦ ¦ Masks ¦ ¦ ¦ a)Corresponding passenger seat | ¦ ¦ ¦ ¦ ¦ is blocked and placarded, | ¦ ¦ ¦ ¦ ¦ "DO NOT OCCUPY", and | ¦ ¦ ¦ ¦ ¦ b)Affected mask is removed and | ¦ ¦ ¦ ¦ ¦ does not permit flow when the | ¦ ¦ ¦ ¦ ¦ system is activiated. | ¦ ¦ ¦ ¦ ¦ ¦ ¦ 2)Passenger Oxygen C ¦ - ¦ 0 ¦ (M)May be inoperative provided: | ¦ ¦ Mask Access Panels ¦ ¦ ¦ a)Corresponding passenger seat | ¦ ¦ (Manual or Auto) ¦ ¦ ¦ is blocked and placarded | ¦ ¦ ¦ ¦ ¦ "DO NOT OCCUPY", and | ¦ ¦ ¦ ¦ ¦ b)Affected panel is secured | ¦ ¦ ¦ ¦ ¦ CLOSED. | ¦ ¦ ¦ ¦ ¦ ¦ ¦ 3)Passenger Oxygen C ¦ - ¦ 0 ¦ (M)May be inoperative provided: | ¦ ¦ ***Cannisters ¦ ¦ ¦ a)Corresponding passenger seat | ¦ ¦ ¦ ¦ ¦ is blocked and placarded, | ¦ ¦ ¦ ¦ ¦ "DO NOT OCCUPY", and | ¦ ¦ ¦ ¦ ¦ b)Affected cannister is removed | ¦ ¦ ¦ ¦ ¦ or rendered inert, and | ¦ ¦ ¦ ¦ ¦ c)Associated oxygen mask access | ¦ ¦ ¦ ¦ ¦ panel is secured CLOSED. | ¦ ¦ ¦ ¦ ¦ ¦ ¦ 5. Protective Breathing D ¦ - ¦ - ¦ Any in excess of those required by | ¦ ¦ Equipment ¦ ¦ ¦ FAR may be inoperative. | ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ -------------------------------------------------------------------------------

------------------------------------------------------------------------------- ¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦ ¦ FEDERAL AVIATION ADMINISTRATION ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT: ¦ REVISION NO: 5 ¦ PAGE: ¦ ¦ MU-300, MU-300-10, BE-400, BE-400A ¦ ¦ ¦ ¦ ¦ DATE: 08/12/2002 ¦ 35-2 ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ 1. ¦ 2. NUMBER INSTALLED ¦ ¦ SYSTEM & ¦ -------------------------------------------- ¦ ¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦ ¦ NUMBERS ¦ ¦ --------------------------------------- ¦ ¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦ ¦ 35 OXYGEN ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ 6. Walkaround Oxygen C ¦ - ¦ - ¦ As required by FAR. ¦ ¦ *** Dispensing Units ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ -------------------------------------------------------------------------------

------------------------------------------------------------------------------- ¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦ ¦ FEDERAL AVIATION ADMINISTRATION ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT: ¦ REVISION NO: 5 ¦ PAGE: ¦ ¦ MU-300, MU-300-10, BE-400, BE-400A ¦ ¦ ¦ ¦ ¦ DATE: 08/12/2002 ¦ 52-1 ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ 1. ¦ 2. NUMBER INSTALLED ¦ ¦ SYSTEM & ¦ -------------------------------------------- ¦ ¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦ ¦ NUMBERS ¦ ¦ --------------------------------------- ¦ ¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦ ¦ 52 DOORS ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ 1. Door Annunciator C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided: | ¦ ¦ System ¦ ¦ ¦ a)Crew member verifies by visual | ¦ ¦ ¦ ¦ ¦ inspection before each | ¦ ¦ ¦ ¦ ¦ departure that the entry door | ¦ ¦ ¦ ¦ ¦ is CLOSED and LOCKED, | ¦ ¦ ¦ ¦ ¦ b)Passengers must wear seat | ¦ ¦ ¦ ¦ ¦ belts during the entire | ¦ ¦ ¦ ¦ ¦ flight, and | ¦ ¦ ¦ ¦ ¦ c)FASTEN SEAT BELT sign remains | ¦ ¦ ¦ ¦ ¦ ON for the entire flight. | ¦ ¦ ¦ ¦ ¦ ¦ ¦ 2. Cabin Step Snubber C ¦ 1 ¦ 0 ¦ (O)May be missing or inoperative. | ¦ ¦ and Latch ¦ ¦ ¦ | ¦ ¦ ¦ ¦ ¦ ¦ ¦ 3. Baggage Door C ¦ 1 ¦ 0 ¦ | ¦ ¦ Snubber ¦ ¦ ¦ | ¦ ¦ ¦ ¦ ¦ ¦ ¦ 4. Cabin Step Cable C ¦ 1 ¦ 0 ¦ (O)May be missing or inoperative. | ¦ ¦ (BE-400 and BE-400A) ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ -------------------------------------------------------------------------------

------------------------------------------------------------------------------- ¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦ ¦ FEDERAL AVIATION ADMINISTRATION ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT: ¦ REVISION NO: 5 ¦ PAGE: ¦ ¦ MU-300, MU-300-10, BE-400, BE-400A ¦ ¦ ¦ ¦ ¦ DATE: 08/12/2002 ¦ 73-1 ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ 1. ¦ 2. NUMBER INSTALLED ¦ ¦ SYSTEM & ¦ -------------------------------------------- ¦ ¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦ ¦ NUMBERS ¦ ¦ --------------------------------------- ¦ ¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦ ¦ 73 ENGINE FUEL & CONTROL ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ 1. Fuel Flow C ¦ 2 ¦ 1 ¦ One may be inoperative provided: ¦ ¦ Indicators ¦ ¦ ¦ a) All fuel quantity gauges ¦ ¦ ¦ ¦ ¦ are operative, ¦ ¦ ¦ ¦ ¦ b) Fuel totalizer is ¦ ¦ ¦ ¦ ¦ operative, and ¦ ¦ ¦ ¦ ¦ c) N1 and N2 analog indicators ¦ ¦ ¦ ¦ ¦ are operative. ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ -------------------------------------------------------------------------------

------------------------------------------------------------------------------- ¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦ ¦ FEDERAL AVIATION ADMINISTRATION ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT: ¦ REVISION NO: 5 ¦ PAGE: ¦ ¦ MU-300, MU-300-10, BE-400, BE-400A ¦ ¦ ¦ ¦ ¦ DATE: 08/12/2002 ¦ 74-1 ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ 1. ¦ 2. NUMBER INSTALLED ¦ ¦ SYSTEM & ¦ -------------------------------------------- ¦ ¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦ ¦ NUMBERS ¦ ¦ --------------------------------------- ¦ ¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦ ¦ 74 IGNITION ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ 74 IGNITION ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ 1. Ignitor Indicator A ¦ 2 ¦ 1 ¦ (O)May be inoperative provided: | ¦ ¦ Lights ¦ ¦ ¦ a)Repairs are made within | ¦ ¦ ¦ ¦ ¦ three flight days. | ¦ ¦ ¦ ¦ ¦ b)No flights into known or | ¦ ¦ ¦ ¦ ¦ forecast icing conditions. | ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ -------------------------------------------------------------------------------

------------------------------------------------------------------------------- ¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦ ¦ FEDERAL AVIATION ADMINISTRATION ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT: ¦ REVISION NO: 5 ¦ PAGE: ¦ ¦ MU-300, MU-300-10, BE-400, BE-400A ¦ ¦ ¦ ¦ ¦ DATE: 08/12/2002 ¦ 77-1 ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ 1. ¦ 2. NUMBER INSTALLED ¦ ¦ SYSTEM & ¦ -------------------------------------------- ¦ ¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦ ¦ NUMBERS ¦ ¦ --------------------------------------- ¦ ¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦ ¦ 77 ENGINE INDICATING ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ 1. Tachometers C ¦ 2 ¦ 1 ¦ The digital portion of one N1 ¦ ¦ (N1) ¦ ¦ ¦ indicator may be inoperative ¦ ¦ ¦ ¦ ¦ provided both N2 indicators, ¦ ¦ ¦ ¦ ¦ digital and analog portions are | ¦ ¦ ¦ ¦ ¦ operative. | ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ (N2) C ¦ 2 ¦ 1 ¦ The digital portion of one N2 ¦ ¦ ¦ ¦ ¦ indicator may be inoperative ¦ ¦ ¦ ¦ ¦ provided both N1 indicators, ¦ ¦ ¦ ¦ ¦ digital and analog portions are | ¦ ¦ ¦ ¦ ¦ operative. | ¦ ¦ ¦ ¦ ¦ ¦ ¦ 2. Engine C ¦ 1 ¦ 0 ¦ ¦ ¦ *** Synchronizer System ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ 3. Oil Pressure Low C ¦ 2 ¦ 1 ¦ (O)One may be inoperative provided ¦ ¦ Annunciators ¦ ¦ ¦ associated oil pressure gauge is ¦ ¦ ¦ ¦ ¦ operative and monitored. ¦ ¦ ¦ ¦ ¦ ¦ ¦ 4. Engine Vibration B ¦ 2 ¦ 0 ¦ ¦ ¦ Meters ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ -------------------------------------------------------------------------------

------------------------------------------------------------------------------- ¦ U.S. DEPARTMENT OF TRANSPORTATION ¦ ¦ ¦ ¦ MASTER MINIMUM EQUIPMENT LIST ¦ ¦ FEDERAL AVIATION ADMINISTRATION ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT: ¦ REVISION NO: 5 ¦ PAGE: ¦ ¦ MU-300, MU-300-10, BE-400, BE-400A ¦ ¦ ¦ ¦ ¦ DATE: 08/12/2002 ¦ 78-1 ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ 1. ¦ 2. NUMBER INSTALLED ¦ ¦ SYSTEM & ¦ -------------------------------------------- ¦ ¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦ ¦ NUMBERS ¦ ¦ --------------------------------------- ¦ ¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦ ¦ 78 ENGINE EXHAUST ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ 1. Thrust Reverser B ¦ 2 ¦ 0 ¦ (M)One or both may be inoperative ¦ ¦ Systems ¦ ¦ ¦ provided inoperative thrust ¦ ¦ ¦ ¦ ¦ reverser(s) are secured in the ¦ ¦ ¦ ¦ ¦ forward thrust position. | ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ (O)Operate in accordance with the | ¦ ¦ ¦ ¦ ¦ AFM procedures. | ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ ¦ -------------------------------------------------------------------------------