Date: 03/21/2005

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

********************************** *  For Part 91 Operations Only   * **********************************

FALCON 200

/S/

JAMES M. EITEL, CHAIRMAN DA-200

FLIGHT OPERATIONS EVALUATION BOARD

Federal Aviation Administration

Flight Standards Division

AIRCRAFT EVALUATION GROUP, SEA-AEG

1601 LIND AVE. S.W.

RENTON, WASHINGTON  98055-4056

TELEPHONE: COMM: (425) 917-6600

FAX:  (425) 917-6638

DEPARTMENT OF TRANSPORTATION     Revision: 3

  Revision: 3

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FALCON 200

Table of Contents

SYSTEM NO.  SYSTEM                                  PAGE

--     Table of Contents                       I

--     Log of Revisions                        II

--     Control Page                            III, IV

--     Highlights of Change                    V, VI

--     Definitions                             VII, VIII, IX, X --     Definitions                             XI, XII, XIII, XIV --     Preamble                                XV, XVI

21     Air Conditioning                        21-1, 2, 3, 4

22     Auto Flight                             22-1

23     Communications                          23-1, 2, 3, 4, 5 23     Communications                          23-6, 7

24     Electrical Power                        24-1

25     Equipment/Furnishings                   25-1, 2, 3

26     Fire Protection                         26-1

27     Flight Controls                         27-1, 2, 3

28     Fuel                                    28-1, 2

29     Hydraulic Power                         29-1, 2

30     Ice and Rain Protection                 30-1, 2

31     Indicating/Recording Systems            31-1, 2

32     Landing Gear                            32-1, 2

33     Lights                                  33-1, 2, 3

34     Navigation                              34-1, 2, 3, 4, 5 34     Navigation                              34-6  THRU 10

34     Navigation                              34-11  THRU 14 35     Oxygen                                  35-1

36     Pneumatic                               36-1 49     Airborne Auxiliary Power                49-1 73     Engine Fuel & Control                   73-1 74     Ignition                                74-1 77     Engine Indicating                       77-1 78     Engine Exhaust                          78-1 79     Engine Oil                              79-1 80     Starting                                80-1

FEDERAL AVIATION ADMINISTRATION     Page: I

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Log of Revisions

¦ REV.NO.  ¦  DATE      ¦ PAGE NUMBERS                   ¦ INITIALS  ¦

¦ 1        ¦ 04/03/1990 ¦ ALL PAGES                      ¦           ¦ ¦ 2        ¦ 10/12/1993 ¦ HIGHLIGHTS OF REV.,DEFINITIONS ¦           ¦ ¦ 2        ¦ 10/12/1993 ¦ 21-1,21-2,21-3,21-4,22-1       ¦           ¦ ¦ 2        ¦ 10/12/1993 ¦ 23-1,23-2,23-3,24-1,25-1       ¦           ¦ ¦ 2        ¦ 10/12/1993 ¦ 25-2,26-1,27-1,27-2,27-3       ¦           ¦ ¦ 2        ¦ 10/12/1993 ¦ 28-1,28-2,29-1,29-2,30-1       ¦           ¦ ¦ 2        ¦ 10/12/1993 ¦ 30-2,31-1,32-1,33-1,33-2       ¦           ¦ ¦ 2        ¦ 10/12/1993 ¦ 33-3,34-1,34-2,34-3,34-4       ¦           ¦ ¦ 2        ¦ 10/12/1993 ¦ 34-5,34-6,34-7,34-8,34-9       ¦           ¦ ¦ 2        ¦ 10/12/1993 ¦ 35-1,36-1,49-1,73-1,74-1       ¦           ¦ ¦ 2        ¦ 10/12/1993 ¦ 77-1,78-1,79-1,80-1            ¦           ¦ ¦ 2a       ¦ 07/07/1998 ¦ HIGHLIGHTS OF REV.,DEFINITIONS ¦           ¦ ¦ 2a       ¦ 07/07/1998 ¦ 21-4,22-1,23-1,23-2,23-3       ¦           ¦ ¦ 2a       ¦ 07/07/1998 ¦ 25-2,26-1,31-1,33-1,34-1       ¦           ¦ ¦ 2a       ¦ 07/07/1998 ¦ 34-2,34-3,34-4,34-5,34-6       ¦           ¦ ¦ 2a       ¦ 07/07/1998 ¦ 34-7,34-8,34-9,34-10           ¦           ¦ ¦ 2b       ¦ 02/02/2001 ¦ HIGHLIGHTS OF REV.,DEFINITIONS ¦           ¦ ¦ 2b       ¦ 02/02/2001 ¦ 22-1,23-1,23-2,23-3,25-1       ¦           ¦ ¦ 2b       ¦ 02/02/2001 ¦ 25-3,31-1,31-2,33-3,34-1       ¦           ¦ ¦ 2b       ¦ 02/02/2001 ¦ 34-2,34-3,34-4,34-5,34-6       ¦           ¦ ¦ 2b       ¦ 02/02/2001 ¦ 34-7,34-8,34-9,34-10,34-11     ¦           ¦ ¦ 2b       ¦ 02/02/2001 ¦ 34-12,34-13                    ¦           ¦ ¦ 3        ¦            ¦ HIGHLIGHTS OF REV.,DEFINITIONS ¦           ¦ ¦ 3        ¦            ¦ 22-1,23-1,23-2,23-3,23-4       ¦           ¦ ¦ 3        ¦            ¦ 23-5,23-6,23-7,32-1,32-2       ¦           ¦ ¦ 3        ¦            ¦ 33-2,34-3,34-4,34-5,34-6       ¦           ¦ ¦ 3        ¦            ¦ 34-7,34-8,34-9,34-10,34-11     ¦           ¦ ¦ 3        ¦            ¦ 34-12,34-13,34-14              ¦           ¦

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FALCON 200

Control Page

SYSTEM                                   PAGE  REV NO.  CURRENT DATE

Cover Page                               -       3        03/21/2005 Table of Contents                        I       3        03/21/2005 Log of Revisions                         II      3        03/21/2005 Control Page                             III     3        03/21/2005 IV      3        03/21/2005 Highlights of Change                     V       3        03/21/2005 VI      3        03/21/2005 Definitions                              VII     6        01/31/1995 VIII    6                01/31/1995 IX      6        01/31/1995 X       6         01/31/1995 XI      6        01/31/1995 XII     6        01/31/1995 XIII    6        01/31/1995 XIV     6        01/31/1995 Preamble                                 XV      1        07/05/1990 XVI     1        07/05/1990 21                                       21-1    2                10/12/1993 21-2    2        10/12/1993 21-3    2        10/12/1993 21-4    2 a      07/07/1998 22                                       22-1    3        03/21/2005 23                                        23-1    3        03/21/2005 23-2    3        03/21/2005 23-3    3        03/21/2005 23-4    3        03/21/2005 23-5    3                03/21/2005 23-6    3        03/21/2005 23-7    3        03/21/2005 24                                       24-1    2        10/12/1993 25                                       25-1    2 b       02/02/2001 25-2    2 a      07/07/1998 25-3    2 b      02/02/2001 26                                       26-1    2 a      07/07/1998 27                                       27-1    2        10/12/1993 27-2    2        10/12/1993 27-3    2        10/12/1993 28                                       28-1    2        10/12/1993 28-2    2        10/12/1993 29                                       29-1    2                                                              10/12/1993

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Control Page

SYSTEM                                   PAGE  REV NO.  CURRENT DATE

                                         29-2    2        10/12/1993 30                                       30-1    2        10/12/1993 30-2    2        10/12/1993 31                                       31-1    2 b      02/02/2001 31-2    2 b      02/02/2001 32                                       32-1    3        03/21/2005 32-2    3        03/21/2005 33                                       33-1    2 a     07/07/1998 33-2    3        03/21/2005 33-3    2 b      02/02/2001 34                                       34-1    2 b      02/02/2001 34-2    2 b      02/02/2001 34-3    3        03/21/2005 34-4    3        03/21/2005 34-5    3        03/21/2005 34-6    3        03/21/2005 34-7    3        03/21/2005 34-8    3        03/21/2005 34-9    3        03/21/2005 34-10   3        03/21/2005 34-11   3        03/21/2005 34-12   3        03/21/2005 34-13   3        03/21/2005 34-14   3        03/21/2005 35                                       35-1    2        10/12/1993 36                                       36-1    2       10/12/1993 49                                       49-1    2        10/12/1993 73                                       73-1    2        10/12/1993 74                                       74-1    2        10/12/1993 77                                       77-1    2        10/12/1993 78                                       78-1    2        10/12/1993 79                                       79-1    2        10/12/1993 80                                       80-1    2        10/12/1993

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FALCON 200

Highlights of Change

EFFECTIVE ABOVE DATE, The Falcon 200 Master Minimum Equipment List has been revised.  Please replace affected pages of the previous list with Revision 3 for a complete up-to-date MMEL.  Change bars have been included to aid the user in identifying any changes as a result of this revision.

22.  AUTO FLIGHT

Item 1, Autopilot Systems: Amended to Policy Letter 101, (rev 1).

23.  COMMUNICATIONS

Item 1, Passenger Address System: Amended to Policy Letter 9, (rev 7).

Item 2, Communications Systems: Amended to Policy Letter 95, (rev 1).

Item 5, Cockpit Voice Recorder: Amended to Policy Letter 29, (rev 4).

Item 13, Boom Microphones: Amended to Policy Letter 58, (rev. 3).

Item 14, Emergency Locator Transmitter: New item.

Item 15, High frequency Communication System: New item, reference Policy Letter 106 (rev 2).

32.  LANDING GEAR

Item 3, Anti-Skid System: Amended to Policy Letter 113.

33.   LIGHTS

Item 6, Landing Lights: Added category "C" to second proviso.

34.  NAVIGATION

Item 9, Ground Proximity Warning System: Amended to Policy Letter 54, (rev 7).

Item 16, ATC Transponder and Automatic Reporting System: Amended to Policy Letter 76, (rev 3).

Item 17, Altitude Alerting System: Amended to Policy Letter 39 (rev 3).

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Highlights of Change

Item 18, Standby Attitude Indicator: Amended to Policy Letter, (rev 1).

Item 44, Traffic Alert and Collision Avoidance System: Amended to Policy Letter 32 (rev 6).

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MASTER MINIMUM EQUIPMENT LIST      Date: 01/31/1995

FALCON 200

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

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FALCON 200

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

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MASTER MINIMUM EQUIPMENT LIST      Date: 01/31/1995

FALCON 200

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

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FALCON 200

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

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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, ¦

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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)                                           ¦

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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

  D."

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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

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MASTER MINIMUM EQUIPMENT LIST    Date: 07/05/1990

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Preamble

(Effective 7/05/1990)

      This preamble is applicable to, and will be included in, master minimum equipment lists (MMEL) issued under the provisions of Section 91.30(a) NEW Section 91.213(a)(2).It is not applicable to MMEL's issued under the provisions of Parts 121, 125, 129, and 135 of the FAR.

Except as provided in Section 91.30(d) NEW Section 91.213(d), or under the provisions of an approved MMEL, all equipment installed on an aircraft in compliance with the airworthiness standards or operating rules must be operative. Experience has shown that with the various levels of redundancy designed into modern aircraft, operation of every system or component installed may not be necessary when the remaining equipment can provide an acceptable level of safety.

An 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 only those items of equipment which the Administrator finds may be inoperative and yet maintain an acceptable level of safety by appropriate conditions and limitations. The MMEL and FAA-issued letter of authorization are used as an MEL by an operator and permit operation of the aircraft with inoperative equipment.

The MMEL includes all items of installed equipment that are permitted to be inoperative. Equipment required by the FAR, and optional equipment in excess of FAR requirements, is included with appropriate conditions and limitations. For each listed item, the installed equipment configuration considered to be normal for the aircraft is specified. Items of equipment installed on aircraft (except for passenger convenience items such as galley equipment and passenger entertainment devices), such as "TCAS," windshear detection devices, and ground proximity warning systems (GPWS) that are in excess of what is required, and are not listed on the MMEL, must be operational for dispatch unless MMEL relief is sought through the FSDO having jurisdiction for the operator. If MMEL relief is sought, the operator must notify the FSDO who will make a request of the FOEB to convene and consider adding the equipment to the MMEL. The operator may then dispatch with the equipment disabled, or rendered inoperative, in accordance with all FAR. It is incumbent on the operator to endeavor to determine if O and/or M procedures for that equipment must be developed. If so, any procedures developed must comply with all FAR. Procedures developed to use the MMEL must not conflict with either the aircraft flight manual limitations, emergency procedures, or with airworthiness directives (AD), all of which take precedence over the MMEL and those procedures.

FEDERAL AVIATION ADMINISTRATION   Page: XV

  FEDERAL AVIATION ADMINISTRATION   Page: XVI

Revision: 1

MASTER MINIMUM EQUIPMENT LIST    Date: 07/05/1990

FALCON 200

Preamble

(Effective 7/05/1990)

Suitable conditions and limitations in the form of placards, maintenance procedures, crew operating procedures, and other restrictions, as necessary, are required to be accomplished by the operator to ensure that an acceptable level of safety is maintained. Those procedures should be developed from guidance provided in the manufacturer's aircraft flight and/or maintenance manuals, manufacturer's recommendations, engineering specifications, and other appropriate sources. Procedures must not be contrary to any FAR. Wherever the statement "as required by FAR" appears in the MMEL, the operator must either list the specific FAR by part and section and carry the FAR on board the aircraft or specify the requirements and/or limitations to conduct the flight in accordance with the appropriate FAR.

The MMEL is intended to permit operations with inoperative items of equipment for the minimum period of time necessary until repairs can be accomplished. It is important that repairs be accomplished at the earliest opportunity in order to return the aircraft to its design level of safety and reliability. Inoperative equipment in all cases must be repaired, or inspected and deferred, by qualified maintenance personnel at the next required inspection Section 91.165(c), NEW Section 91.405(c). The repair intervals indicated by the Letters A, B, and C inserted adjacent to column 2 are NOT applicable to this MMEL.

The MMEL 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 records. The item is then either repaired or deferred per the MMEL or other approved means acceptable to the Administrator prior to further operation. In addition to the specific MMEL conditions and limitations, determination by the operator that the aircraft is in condition for safe operations under anticipated flight conditions must be made for all items of inoperative equipment. When these requirements are met, the aircraft may be considered airworthy and returned to service. 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 interrelationship between those items, and the effect on aircraft operation and crew workload, must be considered. Operators are expected to establish a controlled and sound repair program, including the parts, personnel, facilities, procedures, and schedules to ensure timely repair.

WHEN USING THE MMEL, COMPLIANCE WITH THE STATED INTENT OF THE PREAMBLE, DEFINITIONS, CONDITIONS, AND LIMITATIONS SPECIFIED IN THE MMEL IS REQUIRED.

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 2        ¦ PAGE:    ¦ ¦                FALCON 200                ¦                       ¦          ¦ ¦                                          ¦ DATE: 10/12/1993      ¦ 21-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 21  AIR CONDITIONING      ¦    ¦    ¦                                       ¦

¦ 1.  Out-Flow/Safety     C ¦ 2  ¦ 0  ¦ (M)May be inoperative provided:       ¦ ¦     Valves                ¦    ¦    ¦     a) Valves are secured OPEN,       ¦ ¦     21-30-10              ¦    ¦    ¦     b) Flight remains at or below     ¦ ¦                           ¦    ¦    ¦        10,000 feet MSL, and           ¦ ¦                           ¦    ¦    ¦     c) Extended overwater             ¦ ¦                           ¦    ¦    ¦        operations are prohibited.     ¦

¦ 2.  Cabin Altitude/     C ¦ 1  ¦ 0  ¦ (O)May be inoperative provided:       ¦ ¦     Door (CABIN)          ¦    ¦    ¦     a) Cabin altimeter operates       ¦ ¦     Warning Light         ¦    ¦    ¦        normally,                      ¦ ¦     31-50-00              ¦    ¦    ¦     b) Cabin altitude warning horn    ¦ ¦                           ¦    ¦    ¦        operates normally, and         ¦ ¦                           ¦    ¦    ¦     c) A crewmember determines by     ¦ ¦                           ¦    ¦    ¦        visual inspection that all     ¦ ¦                           ¦    ¦    ¦        doors are closed and locked    ¦ ¦                           ¦    ¦    ¦        before each departure.         ¦

¦ 3.  Cabin Altitude/     C ¦ 1  ¦ 0  ¦ (M)May be inoperative provided:       ¦ ¦     Overpressure          ¦    ¦    ¦     a) Flight remains at or below     ¦ ¦     Warning Horn          ¦    ¦    ¦        10,000 feet MSL.               ¦ ¦     31-50-00              ¦    ¦    ¦           OR                          ¦ ¦                         C ¦    ¦    ¦     b) Flight is conducted in an      ¦ ¦                           ¦    ¦    ¦        unpressurized configuration.   ¦

¦ 4.  Triple Cabin          ¦    ¦    ¦                                       ¦ ¦     Indicator             ¦    ¦    ¦                                       ¦ ¦     21-30-20              ¦    ¦    ¦                                       ¦

¦     1) Cabin Altitude   C ¦ 1  ¦ 0  ¦ (M)May be inoperative provided:       ¦ ¦        Indication         ¦    ¦    ¦     a) Cabin differential pressure    ¦ ¦                           ¦    ¦    ¦        indicator operates normally,   ¦ ¦                           ¦    ¦    ¦        and                            ¦ ¦                           ¦    ¦    ¦     b) A chart is provided to         ¦ ¦                           ¦    ¦    ¦        convert cabin differential     ¦ ¦                           ¦    ¦    ¦        pressure to cabin altitude.    ¦ ¦                           ¦    ¦    ¦           OR                          ¦ ¦                         C ¦    ¦    ¦     c) Flight is conducted in an      ¦ ¦                           ¦    ¦    ¦        unpressurized configuration.   ¦

¦                           ¦    ¦    ¦ (Continued)                           ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 2        ¦ PAGE:    ¦ ¦                FALCON 200                ¦                       ¦          ¦ ¦                                          ¦ DATE: 10/12/1993      ¦ 21-2     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 21  AIR CONDITIONING      ¦    ¦    ¦                                       ¦

¦ 4.  Triple Cabin          ¦    ¦    ¦                                       ¦ ¦     Indicator (Cont'd)    ¦    ¦    ¦                                       ¦

¦     2) Cabin            C ¦ 1  ¦ 0  ¦ (M)May be inoperative provided:       ¦ ¦        Differential       ¦    ¦    ¦     a) Cabin altimeter operates       ¦ ¦        Pressure           ¦    ¦    ¦        normally, and                  ¦ ¦        Indication         ¦    ¦    ¦     b) A chart is provided to         ¦ ¦                           ¦    ¦    ¦        convert cabin altitude to      ¦ ¦                           ¦    ¦    ¦        cabin differential pressure.   ¦ ¦                           ¦    ¦    ¦           OR                          ¦ ¦                         C ¦    ¦    ¦     c) Flight is conducted in an      ¦ ¦                           ¦    ¦    ¦        unpressurized configuration.   ¦

¦     3) Cabin Vertical   C ¦ 1  ¦ 0  ¦ (M)May be inoperative provided:       ¦ ¦        Speed Indication   ¦    ¦    ¦     a) Automatic cabin pressuriza-    ¦ ¦        Indication         ¦    ¦    ¦        tion control system operates   ¦ ¦                           ¦    ¦    ¦        normally, and                  ¦ ¦                           ¦    ¦    ¦     b) Cabin differential pressure    ¦ ¦                           ¦    ¦    ¦        indicator and cabin            ¦ ¦                           ¦    ¦    ¦        altimeter operate normally.    ¦ ¦                           ¦    ¦    ¦           OR                          ¦ ¦                         C ¦    ¦    ¦     c) Flight is conducted in an      ¦ ¦                           ¦    ¦    ¦        unpressurized configuration.   ¦

¦ 5.  Pilot Foot Warmer   C ¦ 1  ¦ 0  ¦ May be inoperative CLOSED (Bleed      ¦ ¦     21-20-10              ¦    ¦    ¦ Air) or OFF (Electric).               ¦

¦ 6.  Automatic           C ¦ 1  ¦ 0  ¦ May be inoperative provided manual    ¦ ¦     Temperature Control   ¦    ¦    ¦ temperature control operates          ¦ ¦     System                ¦    ¦    ¦ normally.                             ¦ ¦     21-60-10              ¦    ¦    ¦                                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 2        ¦ PAGE:    ¦ ¦                FALCON 200                ¦                       ¦          ¦ ¦                                          ¦ DATE: 10/12/1993      ¦ 21-3     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 21  AIR CONDITIONING      ¦    ¦    ¦                                       ¦

¦ 7.  Cabin Pressurization  ¦    ¦    ¦                                       ¦ ¦     Control System        ¦    ¦    ¦                                       ¦ ¦     21-30-20              ¦    ¦    ¦                                       ¦

¦     1) Automatic        C ¦ 1  ¦ 0  ¦ (M)(O)May be inoperative provided:    ¦ ¦                           ¦    ¦    ¦     a) Manual cabin pressure          ¦ ¦                           ¦    ¦    ¦        control system operates        ¦ ¦                           ¦    ¦    ¦        normally, and                  ¦ ¦                           ¦    ¦    ¦     b) Cabin altimeter and cabin      ¦ ¦                           ¦    ¦    ¦        differential pressure          ¦ ¦                           ¦    ¦    ¦        indicator operates normally.   ¦ ¦                           ¦    ¦    ¦           OR                          ¦ ¦                         C ¦    ¦    ¦     c) Flight is conducted in an      ¦ ¦                           ¦    ¦    ¦        unpressurized configuration.   ¦

¦     2) Manual           C ¦ 1  ¦ 0  ¦ (M)(O)May be inoperative provided:    ¦ ¦                           ¦    ¦    ¦     a) Automatic cabin pressure       ¦ ¦                           ¦    ¦    ¦        control system operates        ¦ ¦                           ¦    ¦    ¦        normally, and                  ¦ ¦                           ¦    ¦    ¦     b) Cabin altimeter and cabin      ¦ ¦                           ¦    ¦    ¦        differential pressure          ¦ ¦                           ¦    ¦    ¦        indicator operate normally.    ¦ ¦                           ¦    ¦    ¦           OR                          ¦ ¦                         C ¦    ¦    ¦     c) Flight is conducted in an      ¦ ¦                           ¦    ¦    ¦        unpressurized configuration.   ¦

¦ 8.  Cabin Temperature   C ¦ 1  ¦ 0  ¦                                       ¦ ¦     Remote Control        ¦    ¦    ¦                                       ¦ ¦     21-60-10              ¦    ¦    ¦                                       ¦

¦ 9.  Temperature         C ¦ 1  ¦ 0  ¦                                       ¦ ¦     Control Valve         ¦    ¦    ¦                                       ¦ ¦     Position Indicator    ¦    ¦    ¦                                       ¦ ¦     21-60-10              ¦    ¦    ¦                                       ¦

¦ 10. Cabin Temperature   C ¦ 1  ¦ 0  ¦                                       ¦ ¦     Indicator             ¦    ¦    ¦                                       ¦ ¦     21-60-10              ¦    ¦    ¦                                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 2 a      ¦ PAGE:    ¦ ¦                FALCON 200                ¦                       ¦          ¦ ¦                                          ¦ DATE: 07/07/1998      ¦ 21-4     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 21  AIR CONDITIONING      ¦    ¦    ¦                                       ¦

¦ 11. Cabin Air           C ¦ 1  ¦ 0  ¦ (M)(O)May be inoperative OPEN         ¦ ¦     Conditioning Valve    ¦    ¦    ¦ provided:                             ¦ ¦     21-50-10              ¦    ¦    ¦     a) Both bleed valves operate      ¦ ¦                           ¦    ¦    ¦        normally,                      ¦ ¦                           ¦    ¦    ¦     b) Both bleed valves are          ¦ ¦                           ¦    ¦    ¦        selected OFF for takeoff       ¦ ¦                           ¦    ¦    ¦        and second segment climb,      ¦ ¦                           ¦    ¦    ¦     c) Cabin altitude warning         ¦ ¦                           ¦    ¦    ¦        light operates normally,       ¦ ¦                           ¦    ¦    ¦        and                            ¦ ¦                           ¦    ¦    ¦     d) Cabin altitude warning horn    ¦ ¦                           ¦    ¦    ¦        operates normally.             ¦

¦ 12. Cockpit Gasper      C ¦ 2  ¦ 1  ¦                                       ¦ ¦     Outlets               ¦    ¦    ¦                                       ¦ ¦     21-20-20              ¦    ¦    ¦                                       ¦

¦ 13. Electrical Rack       ¦    ¦    ¦ Deleted Revision 2a.                  ¦ ¦     Blowers               ¦    ¦    ¦                                       ¦ ¦     21-20-60              ¦    ¦    ¦                                       ¦

¦ 14. Flood Duct System   C ¦ 1  ¦ 0  ¦                                       ¦

¦ 15. Vacuum Jet Pump     C ¦ 1  ¦ 0  ¦ (M)May be inoperative provided        ¦ ¦     21-30-10              ¦    ¦    ¦ flight is conducted in an             ¦ ¦                           ¦    ¦    ¦ unpressurized configuration.          ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 3        ¦ PAGE:    ¦ ¦                FALCON 200                ¦                       ¦          ¦ ¦                                          ¦ DATE: 03/21/2005      ¦ 22-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 22  AUTO FLIGHT           ¦    ¦    ¦                                       ¦

¦ 1.  Autopilot Systems   C ¦ -  ¦ 1  ¦                                     | ¦ ¦     22-10-00              ¦    ¦    ¦                                       ¦ ¦                         B ¦ -  ¦ 0  ¦ May be inoperative provided           ¦ ¦                           ¦    ¦    ¦ approach minimums do not require      ¦ ¦                           ¦    ¦    ¦ their use.                            ¦

¦                           ¦    ¦    ¦ NOTE: Any mode which operates         ¦ ¦                           ¦    ¦    ¦       normally may be used.           ¦

¦ 2.  Autopilot Alert     C ¦ 3  ¦ 0  ¦ May be inoperative provided auto-     ¦ ¦     Lights (AP, AP TRIM   ¦    ¦    ¦ pilot is not used.                    ¦ ¦     and MISTRIM)          ¦    ¦    ¦                                       ¦ ¦     31-50-10              ¦    ¦    ¦                                       ¦

¦ 3.  Control Wheel       C ¦ 2  ¦ 1  ¦ One may be inoperative provided       ¦ ¦     Autopilot             ¦    ¦    ¦ autopilot is not utilized at less     ¦ ¦     Disengage Buttons     ¦    ¦    ¦ than initial approach altitude.       ¦

¦                         C ¦ 2  ¦ 0  ¦ May be inoperative provided           ¦ ¦                           ¦    ¦    ¦ autopilot is not used.                ¦

¦ 4.  Yaw Damper          C ¦ 1  ¦ 0  ¦                                       ¦ ¦     22-10-20              ¦    ¦    ¦                                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 3        ¦ PAGE:    ¦ ¦                FALCON 200                ¦                       ¦          ¦ ¦                                          ¦ DATE: 03/21/2005      ¦ 23-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 23  COMMUNICATIONS        ¦    ¦    ¦                                       ¦

¦ 1.  Passenger Address     ¦    ¦    ¦                                       ¦ ¦     System (PA)           ¦    ¦    ¦                                       ¦

¦     1) Passenger        B ¦ 1  ¦ 0  ¦ (O)May be inoperative provided:       ¦ ¦        Configuration      ¦    ¦    ¦     a) Alternate, normal and          ¦ ¦                           ¦    ¦    ¦        emergency procedures and/or    ¦ ¦                           ¦    ¦    ¦        operating restrictions are     ¦ ¦                           ¦    ¦    ¦        established and used, and      ¦ ¦                           ¦    ¦    ¦     b) Flight attendant alerting    | ¦ ¦                           ¦    ¦    ¦        system (audio and visual)    | ¦ ¦                           ¦    ¦    ¦        operates normally.           | ¦

¦                           ¦    ¦    ¦ NOTE: Any station function(s) that  | ¦ ¦                           ¦    ¦    ¦       operate normally may be used. | ¦

¦                         C ¦ 1  ¦ 0  ¦ (O)May be inoperative provided:     | ¦ ¦                           ¦    ¦    ¦     a) PA not required by FAR, and  | ¦ ¦                           ¦    ¦    ¦     b) Alternate, normal and        | ¦ ¦                           ¦    ¦    ¦        emergency procedures, and/or | ¦ ¦                           ¦    ¦    ¦        operating restrictions are   | ¦ ¦                           ¦    ¦    ¦        established and used.        | ¦

¦                           ¦    ¦    ¦ NOTE: Any station function(s) that  | ¦ ¦                           ¦    ¦    ¦       operate normally may be used. | ¦

¦        a) Lavatory      C ¦ -  ¦ 0  ¦ (O)May be inoperative provided      | ¦ ¦           Speakers        ¦    ¦    ¦ alternate procedures are            | ¦ ¦                           ¦    ¦    ¦ established and used.               | ¦

¦     2) Cargo            C ¦ 1  ¦ 0  ¦ May be inoperative provided         | ¦ ¦        Configuration      ¦    ¦    ¦ alternate, normal and emergency     | ¦ ¦        (Courier/          ¦    ¦    ¦ procedures, and/or operating        | ¦ ¦        Supernumerary      ¦    ¦    ¦ restrictions are established        | ¦ ¦        Address System)    ¦    ¦    ¦ and used.                           | ¦

¦                         D ¦ 1  ¦ 0  ¦ May be inoperative provided         | ¦ ¦                           ¦    ¦    ¦ procedures do not require its use.  | ¦

¦                           ¦    ¦    ¦ (Continued)                           ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 3        ¦ PAGE:    ¦ ¦                FALCON 200                ¦                       ¦          ¦ ¦                                          ¦ DATE: 03/21/2005      ¦ 23-2     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 23  COMMUNICATIONS        ¦    ¦    ¦                                       ¦

¦ 1.  Passenger Address     ¦    ¦    ¦                                       ¦ ¦     System (PA) (Cont'd)  ¦    ¦    ¦                                       ¦

¦     2) Cargo              ¦    ¦    ¦                                       ¦ ¦        Configuration      ¦    ¦    ¦                                       ¦ ¦        (Courier/          ¦    ¦    ¦                                       ¦ ¦        Supernumerary      ¦    ¦    ¦                                       ¦ ¦        Address System)    ¦    ¦    ¦                                       ¦

¦        a) Lavatory      C ¦ 1  ¦ 0  ¦ (O)May be inoperative provided      | ¦ ¦           Speakers        ¦    ¦    ¦ alternate procedures are            | ¦ ¦                           ¦    ¦    ¦ established and used.               | ¦

¦                         D ¦ 1  ¦ 0  ¦ May be inoperative provided         | ¦ ¦                           ¦    ¦    ¦ procedures do not require its use.  | ¦

¦ 2.  Communications      D ¦ -  ¦ -  ¦ Any in excess of those required by    ¦ ¦     Systems (VHF,         ¦    ¦    ¦ FAR may be inoperative provided it  | ¦ ¦     UHF)                  ¦    ¦    ¦ 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 Comm           ¦    ¦    ¦                                       ¦ ¦        Control Panels     ¦    ¦    ¦                                     | ¦

¦        a) Frequency     C ¦ -  ¦ 0  ¦                                       ¦ ¦           Transfer        ¦    ¦    ¦                                       ¦ ¦           Light           ¦    ¦    ¦                                       ¦

¦        b) Frequency     C ¦ -  ¦ 0  ¦                                       ¦ ¦           Transfer        ¦    ¦    ¦                                       ¦ ¦           Switch          ¦    ¦    ¦                                       ¦

¦        c) Frequency     C ¦ -  ¦ 2  ¦                                       ¦ ¦           Selector        ¦    ¦    ¦                                       ¦ ¦           Knob            ¦    ¦    ¦                                       ¦

¦        d) Frequency     C ¦ -  ¦ 2  ¦                                       ¦ ¦           Indication      ¦    ¦    ¦                                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 3        ¦ PAGE:    ¦ ¦                FALCON 200                ¦                       ¦          ¦ ¦                                          ¦ DATE: 03/21/2005      ¦ 23-3     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 23  COMMUNICATIONS        ¦    ¦    ¦                                       ¦

¦ 3.  Flight Deck         C ¦ -  ¦ -  ¦ May be inoperative provided:          ¦ ¦     Speakers              ¦    ¦    ¦     a) Procedures do not require      ¦ ¦                           ¦    ¦    ¦        their use, and                 ¦ ¦                           ¦    ¦    ¦     b) Headsets are installed and     ¦ ¦                           ¦    ¦    ¦        operate normally.              ¦

¦ 4.  Crewmember Inter-   C ¦ -  ¦ 1  ¦                                     | ¦ ¦     phone System(s)       ¦    ¦    ¦                                     | ¦

¦     1) Passenger          ¦    ¦    ¦                                     | ¦ ¦        Configuration      ¦    ¦    ¦                                     | ¦

¦        a) Flight Deck   B ¦ -  ¦ -  ¦ (O)May be inoperative provided:     | ¦ ¦           to Cabin,       ¦    ¦    ¦     a) Flight deck to cabin and     | ¦ ¦           Cabin to        ¦    ¦    ¦        cabin to flight deck inter-  | ¦ ¦           Flight Deck     ¦    ¦    ¦        phone functions operate      | ¦ ¦           Functions       ¦    ¦    ¦        normally on at least fifty   | ¦ ¦                           ¦    ¦    ¦        percent of the cabin         | ¦ ¦                           ¦    ¦    ¦        headsets, and                | ¦ ¦                           ¦    ¦    ¦     b) Alternate communications     | ¦ ¦                           ¦    ¦    ¦        procedures between the       | ¦ ¦                           ¦    ¦    ¦        affected flight attendants   | ¦ ¦                           ¦    ¦    ¦        station(s) are established   | ¦ ¦                           ¦    ¦    ¦        and used.                    | ¦

¦                           ¦    ¦    ¦ NOTE: Any station function(s) that  | ¦ ¦                           ¦    ¦    ¦       operate normally may be used. | ¦

¦        b) Flight Deck   C ¦ -  ¦ 0  ¦ (O)May be inoperative alternate     | ¦ ¦           to Ground       ¦    ¦    ¦ procedures are established and      | ¦ ¦           Function        ¦    ¦    ¦ used.                               | ¦

¦                         D ¦ -  ¦ 0  ¦ May be inoperative provided         | ¦ ¦                           ¦    ¦    ¦ procedures do not require its use.  | ¦

¦                           ¦    ¦    ¦ (Continued)                           ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 3        ¦ PAGE:    ¦ ¦                FALCON 200                ¦                       ¦          ¦ ¦                                          ¦ DATE: 03/21/2005      ¦ 23-4     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 23  COMMUNICATIONS        ¦    ¦    ¦                                       ¦

¦ 4.  Crewmember Inter-     ¦    ¦    ¦                                     | ¦ ¦     phone System(s)       ¦    ¦    ¦                                     | ¦ ¦     (Cont'd)              ¦    ¦    ¦                                       ¦

¦     2) Cargo              ¦    ¦    ¦                                     | ¦ ¦        Configuration      ¦    ¦    ¦                                     | ¦

¦        a) Flight Deck   C ¦ 1  ¦ 0  ¦ (O)May be inoperative provided      | ¦ ¦           to Cabin,       ¦    ¦    ¦ alternate, normal and emergency     | ¦ ¦           Cabin to        ¦    ¦    ¦ procedures, and/or operating        | ¦ ¦           Flight Deck     ¦    ¦    ¦ restrictions are established        | ¦ ¦           Functions       ¦    ¦    ¦ and used.                           | ¦

¦                         D ¦ -  ¦ 0  ¦ May be inoperative provided         | ¦ ¦                           ¦    ¦    ¦ procedures do not require its use.  | ¦

¦        b) Flight Deck   C ¦ -  ¦ 0  ¦ (O)May be inoperative alternate     | ¦ ¦           to Ground       ¦    ¦    ¦ procedures are established and      | ¦ ¦           Function        ¦    ¦    ¦ used.                               | ¦

¦                         D ¦ -  ¦ 0  ¦ May be inoperative provided         | ¦ ¦                           ¦    ¦    ¦ procedures do not require its use.  | ¦

¦ 5.  Cockpit Voice         ¦    ¦    ¦                                       ¦ ¦     Recorder              ¦    ¦    ¦                                       ¦

¦     1) Part 135           ¦    ¦    ¦                                       ¦ ¦        Operators          ¦    ¦    ¦                                       ¦

¦        a) Flight Data   A ¦ 1  ¦ 0  ¦ May be inoperative provided:          ¦ ¦           Recorder        ¦    ¦    ¦     a) Flight Data Recorder (FDR)     ¦ ¦           Installed       ¦    ¦    ¦        operates normally, and         ¦ ¦                           ¦    ¦    ¦     b) Repairs are made within        ¦ ¦                           ¦    ¦    ¦        three flight days.             ¦

¦        b) Flight Data   A ¦ 1  ¦ 0  ¦ May be inoperative provided repairs   ¦ ¦           Recorder Not    ¦    ¦    ¦ are made within three flight days.    ¦ ¦           Installed       ¦    ¦    ¦                                       ¦

¦     2) Part 91          A ¦ 1  ¦ 0  ¦ As required by FAR.                   ¦ ¦        Operators          ¦    ¦    ¦                                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 3        ¦ PAGE:    ¦ ¦                FALCON 200                ¦                       ¦          ¦ ¦                                          ¦ DATE: 03/21/2005      ¦ 23-5     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 23  COMMUNICATIONS        ¦    ¦    ¦                                       ¦

¦ 6.  Airphone System     D ¦ 1  ¦ 0  ¦                                       ¦

¦ 7.  Selective Call      C ¦ 1  ¦ 0  ¦                                       ¦ ¦     System (SELCAL)       ¦    ¦    ¦                                       ¦ ¦     23-20-10              ¦    ¦    ¦                                       ¦

¦ 8.  Automatic Cabin     D ¦ 1  ¦ 0  ¦ (O)May be inoperative provided        ¦ ¦     Briefer               ¦    ¦    ¦ alternate procedures are estab-       ¦ ¦                           ¦    ¦    ¦ lished and used.                      ¦

¦ 9.  Microphones         C ¦ -  ¦ 2  ¦ May be inoperative provided one       ¦ ¦     23-50-20              ¦    ¦    ¦ microphone operates normally at       ¦ ¦                           ¦    ¦    ¦ each pilot station.                   ¦

¦ 10. Radio Master        C ¦ 1  ¦ 0  ¦ May be inoperative ON.                ¦ ¦     Switch                ¦    ¦    ¦                                       ¦

¦ 11. Standby Battery     C ¦ 1  ¦ 0  ¦ May be inoperative provided           ¦ ¦ *** Pack for Comm/ATC     ¦    ¦    ¦ procedures do not require its use.    ¦

¦ 12. Electronic Cockpit  C ¦ 1  ¦ 0  ¦ (O)May be inoperative provided        ¦ ¦ *** Checklist             ¦    ¦    ¦ procedures do not require its use.    ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 3        ¦ PAGE:    ¦ ¦                FALCON 200                ¦                       ¦          ¦ ¦                                          ¦ DATE: 03/21/2005      ¦ 23-6     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 23  COMMUNICATIONS        ¦    ¦    ¦                                       ¦

¦ 13. Boom Microphones      ¦    ¦    ¦                                       ¦

¦     (With Flight Data     ¦    ¦    ¦                                       ¦ ¦     Recorder Installed)   ¦    ¦    ¦                                       ¦

¦     1) Cockpit Voice    A ¦ -  ¦ 0  ¦ May be inoperative provided:          ¦ ¦        Recorder           ¦    ¦    ¦     a) Flight data recorder (FDR)     ¦ ¦        Equipped to        ¦    ¦    ¦        operates normally, and         ¦ ¦        Record Boom        ¦    ¦    ¦     b) Repairs are made within        ¦ ¦        Microphone per     ¦    ¦    ¦        three flight days.             ¦ ¦        FAR 121.359(g),    ¦    ¦    ¦                                       ¦ ¦        135.151(d) or      ¦    ¦    ¦                                       ¦ ¦        125.277(e)         ¦    ¦    ¦                                       ¦

¦ *** 2) Cockpit Voice    D ¦ -  ¦ 0  ¦ Any in excess of those required by    ¦ ¦        Recorder Not       ¦    ¦    ¦ FAR may be inoperative.               ¦ ¦        Equipped to        ¦    ¦    ¦                                       ¦ ¦        Record Boom        ¦    ¦    ¦                                       ¦ ¦        Microphone         ¦    ¦    ¦                                       ¦

¦     (Without Flight       ¦    ¦    ¦                                       ¦ ¦     Data Recorder         ¦    ¦    ¦                                       ¦ ¦     Installed)            ¦    ¦    ¦                                       ¦

¦     1) Cockpit Voice    A ¦ -  ¦ 0  ¦ May be inoperative provided           ¦ ¦        Recorder           ¦    ¦    ¦ repairs are made within three         ¦ ¦        Equipped to        ¦    ¦    ¦ flight days.                          ¦ ¦        Record Boom        ¦    ¦    ¦                                       ¦ ¦        Microphone per     ¦    ¦    ¦                                       ¦ ¦        FAR 121.359(g),    ¦    ¦    ¦                                       ¦ ¦        135.151(d) or      ¦    ¦    ¦                                       ¦ ¦        125.227(e)         ¦    ¦    ¦                                       ¦

¦ *** 2) Cockpit Voice    D ¦ -  ¦ 0  ¦ Any in excess of those required by    ¦ ¦        Recorder Not       ¦    ¦    ¦ FAR may be inoperative.               ¦ ¦        Equipped to        ¦    ¦    ¦                                       ¦ ¦        Record Boom        ¦    ¦    ¦                                       ¦ ¦        Microphone         ¦    ¦    ¦                                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 3        ¦ PAGE:    ¦ ¦                FALCON 200                ¦                       ¦          ¦ ¦                                          ¦ DATE: 03/21/2005      ¦ 23-7     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 23  COMMUNICATIONS        ¦    ¦    ¦                                       ¦

¦ 14. Emergency Locator   D ¦ -  ¦ -  ¦ Any in excess of those required by  | ¦ ¦ *** Transmitter (ELT)     ¦    ¦    ¦ FAR may be inoperative.             | ¦

¦ 15. High Frequency      C ¦ -  ¦ 1  ¦ (O)May be inoperative while         | ¦ ¦     (HF) Communication    ¦    ¦    ¦ conducting operations that require  | ¦ ¦     System                ¦    ¦    ¦ 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.             | ¦

¦                         D ¦ -  ¦ -  ¦ Any in excess of those required     | ¦ ¦                           ¦    ¦    ¦ by FAR may be inoperative.          | ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 2        ¦ PAGE:    ¦ ¦                FALCON 200                ¦                       ¦          ¦ ¦                                          ¦ DATE: 10/12/1993      ¦ 24-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 24  ELECTRICAL POWER      ¦    ¦    ¦                                       ¦

¦ 1.  Inverters           B ¦ 3  ¦ 2  ¦ One may be inoperative provided VMC   ¦ ¦     24-20-10              ¦    ¦    ¦ flight conditions exist at both       ¦ ¦                           ¦    ¦    ¦ departure and arrival airports.       ¦

¦ 2.  DC Voltmeters       C ¦ 2  ¦ 1  ¦ One may be inoperative provided all   ¦ ¦     24-30-50              ¦    ¦    ¦ other generator system components     ¦ ¦                           ¦    ¦    ¦ operate normally.                     ¦

¦ 3.  AC Voltmeter        C ¦ 1  ¦ 0  ¦ May be inoperative provided AC1       ¦ ¦     24-20-50              ¦    ¦    ¦ and AC2 lights operate normally.      ¦

¦ 4.  Battery             C ¦ 1  ¦ 1  ¦ One meter indication may be           ¦ ¦     Temperature           ¦    ¦    ¦ inoperative provided battery          ¦ ¦     Indicator System      ¦    ¦    ¦ temperature warning light system      ¦ ¦     24-30-50              ¦    ¦    ¦ operates normally.                    ¦

¦ 5.  Generator Warning   C ¦ 2  ¦ 1  ¦ (O)One may be inoperative provided    ¦ ¦     Lights                ¦    ¦    ¦ the DC voltmeter operates normally.   ¦ ¦     24-30-50              ¦    ¦    ¦                                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 2 b      ¦ PAGE:    ¦ ¦                FALCON 200                ¦                       ¦          ¦ ¦                                          ¦ DATE: 02/02/2001      ¦ 25-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 25  EQUIPMENT/FURNISHINGS ¦    ¦    ¦                                       ¦

¦ 1.  Crewmember            ¦    ¦    ¦ Deleted, Rev. 1.                      ¦ ¦     Shoulder Harness      ¦    ¦    ¦                                       ¦ ¦     25-10-10              ¦    ¦    ¦                                       ¦

¦ 2.  Emergency Locator   C ¦ -  ¦ 0  ¦ As required by FAR.                   ¦ ¦     Transmitter (ELT)     ¦    ¦    ¦                                       ¦ ¦     25-60-20              ¦    ¦    ¦                                       ¦

¦ 3.  Passenger Seats     D ¦ -  ¦ -  ¦ May be inoperative provided:          ¦ ¦     and Belts             ¦    ¦    ¦     a) Seat does not block an         ¦ ¦                           ¦    ¦    ¦        Emergency Exit,                ¦ ¦                           ¦    ¦    ¦     b) Seat does not restrict any     ¦ ¦                           ¦    ¦    ¦        passenger from access to       ¦ ¦                           ¦    ¦    ¦        main aircraft aisle, and       ¦ ¦                           ¦    ¦    ¦     c) Affected seat is blocked and   ¦ ¦                           ¦    ¦    ¦        placarded "Do Not Occupy".     ¦

¦                           ¦    ¦    ¦ NOTE 1: A seat with inoperative       ¦ ¦                           ¦    ¦    ¦         seat belt is considered       ¦ ¦                           ¦    ¦    ¦         inoperative.                  ¦

¦                           ¦    ¦    ¦ NOTE 2: Inoperative seat(s) do not    ¦ ¦                           ¦    ¦    ¦         affect the required number    ¦ ¦                           ¦    ¦    ¦         of Flight Attendants.         ¦

¦     1) Recline          D ¦ -  ¦ -  ¦ May be inoperative and seat           ¦ ¦        Mechanism          ¦    ¦    ¦ occupied provided seat is secured     ¦ ¦                           ¦    ¦    ¦ in the up-right position.             ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 2 a      ¦ PAGE:    ¦ ¦                FALCON 200                ¦                       ¦          ¦ ¦                                          ¦ DATE: 07/07/1998      ¦ 25-2     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 25  EQUIPMENT/FURNISHINGS ¦    ¦    ¦                                       ¦

¦ 4.  Crewmember Seat       ¦    ¦    ¦                                       ¦ ¦     Adjustments           ¦    ¦    ¦                                       ¦ ¦     25-10-10              ¦    ¦    ¦                                       ¦

¦     1) Electrical       C ¦ 2  ¦ 0  ¦ (M)May be inoperative provided        ¦ ¦                           ¦    ¦    ¦ manual adjustment operates            ¦ ¦                           ¦    ¦    ¦ normally.                             ¦

¦     2) Manual           C ¦ 2  ¦ 2  ¦ (M)Adjustment in a vertical mode      ¦ ¦                           ¦    ¦    ¦ may be inoperative provided:          ¦ ¦                           ¦    ¦    ¦     a) Seat is secured at the         ¦ ¦                           ¦    ¦    ¦        individual crewmember's        ¦ ¦                           ¦    ¦    ¦        requirements, and              ¦ ¦                           ¦    ¦    ¦     b) Fore-aft adjustment operates   ¦ ¦                           ¦    ¦    ¦        normally.                      ¦

¦ 5.   Passenger            ¦ -  ¦ 0  ¦ Passenger convenience items, as       ¦ ¦ ***  Convenience Item(s)  ¦    ¦    ¦ expressed in the MMEL, are those      ¦ ¦                           ¦    ¦    ¦ related to passenger convenience,     ¦ ¦                           ¦    ¦    ¦ comfort or entertainment such as,     ¦ ¦                           ¦    ¦    ¦ but not limited to, galley equip-     ¦ ¦                           ¦    ¦    ¦ ment, movie equipment, ash trays,     ¦ ¦                           ¦    ¦    ¦ stereo equipment, overhead reading    ¦ ¦                           ¦    ¦    ¦ lamps, etc.  Items addressed else-    ¦ ¦                           ¦    ¦    ¦ where in this document shall not be   ¦ ¦                           ¦    ¦    ¦ included.  (M) and (O) procedures     ¦ ¦                           ¦    ¦    ¦ may be required and included in the   ¦ ¦                           ¦    ¦    ¦ operator's appropriate document.      ¦

¦                           ¦    ¦    ¦ NOTE: Lavatory door ashtrays are      ¦ ¦                           ¦    ¦    ¦       not considered convenience      ¦ ¦                           ¦    ¦    ¦       items.                          ¦

¦ 6.   First Aid Kits     D ¦ -  ¦ -  ¦ Any in excess of those required by    ¦ ¦                           ¦    ¦    ¦ FAR may be incomplete or missing      ¦ ¦                           ¦    ¦    ¦ provided required distribution is     ¦ ¦                           ¦    ¦    ¦ maintained.                           ¦

¦ 7.   Lavatory Door      A ¦ 1  ¦ 0  ¦ May be missing provided it is         ¦ ¦      Ashtray              ¦    ¦    ¦ replaced within 3 calendar days.      ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 2 b      ¦ PAGE:    ¦ ¦                FALCON 200                ¦                       ¦          ¦ ¦                                          ¦ DATE: 02/02/2001      ¦ 25-3     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 25  EQUIPMENT/FURNISHINGS ¦    ¦    ¦                                       ¦

¦ 8.  Galley Waste        C ¦ -  ¦ -  ¦ (M)May be inoperative provided the    ¦ ¦     Receptacles           ¦    ¦    ¦ container is empty and the access     ¦ ¦     Access Doors/         ¦    ¦    ¦ is secured to prevent waste           ¦ ¦     Covers                ¦    ¦    ¦ introduction into the compartment.    ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 2 a      ¦ PAGE:    ¦ ¦                FALCON 200                ¦                       ¦          ¦ ¦                                          ¦ DATE: 07/07/1998      ¦ 26-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 26  FIRE PROTECTION       ¦    ¦    ¦                                       ¦

¦ 1.  Fire Extinguisher   C ¦ -  ¦ 0  ¦ (M)May be missing provided pressure   ¦ ¦     Thermal Discharge     ¦    ¦    ¦ indicators are checked once each      ¦ ¦     Discs                 ¦    ¦    ¦ flight day to determine adequate      ¦ ¦     26-20-20              ¦    ¦    ¦ charge.                               ¦

¦ 2.  APU Fire Warning    C ¦ 1  ¦ 0  ¦ May be inoperative provided APU       ¦ ¦     System 26-10-30       ¦    ¦    ¦ is not used.                          ¦

¦ 3.  APU Fire            C ¦ 1  ¦ 0  ¦ May be inoperative provided APU       ¦ ¦     Extinguisher System   ¦    ¦    ¦ is not used.                          ¦ ¦     26-20-20              ¦    ¦    ¦                                       ¦

¦ 4.  Aft Baggage Smoke   C ¦ 1  ¦ 0  ¦ May be inoperative provided the       ¦ ¦     Detector/             ¦    ¦    ¦ compartment remains empty, or         ¦ ¦     Extinguisher System   ¦    ¦    ¦ only non-combustible materials        ¦ ¦                           ¦    ¦    ¦ (including supplemental avionics)     ¦ ¦                           ¦    ¦    ¦ are carried therein.                  ¦

¦ 5.  Portable Fire       D ¦ -  ¦ -  ¦ Any is 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) Required distribution is       ¦ ¦                           ¦    ¦    ¦        maintained.                    ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 2        ¦ PAGE:    ¦ ¦                FALCON 200                ¦                       ¦          ¦ ¦                                          ¦ DATE: 10/12/1993      ¦ 27-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 27  FLIGHT CONTROLS       ¦    ¦    ¦                                       ¦

¦ 1.  Arthur Q Units      B ¦ 2  ¦ 0  ¦ (M)(O)May be inoperative in the low   ¦ ¦     (Aileron and          ¦    ¦    ¦ speed position provided airspeed      ¦ ¦     Elevator)             ¦    ¦    ¦ remains at or below 200 KIAS.         ¦ ¦     27-10-50, 27-30-40    ¦    ¦    ¦                                       ¦

¦ 2.  Arthur Q Unit       B ¦ 1  ¦ 0  ¦ (M)(O)May be inoperative provided:    ¦ ¦     Warning Light         ¦    ¦    ¦     a) Associated Arthur Q units      ¦ ¦     System                ¦    ¦    ¦        are secured in the low         ¦ ¦     31-50-10              ¦    ¦    ¦        speed position, and            ¦ ¦                           ¦    ¦    ¦     b) Airspeed remains at or below   ¦ ¦                           ¦    ¦    ¦        below 200 KIAS.                ¦

¦ 3.  Air Brake System   C  ¦ 2  ¦ 1  ¦ (O)One may be inoperative provided:   ¦ ¦     Warning Lights        ¦    ¦    ¦     a) Airbrakes operate normally,    ¦ ¦     27-60-10              ¦    ¦    ¦     b) Verify airbrakes are proper-   ¦ ¦                           ¦    ¦    ¦        ly set before departure, and   ¦ ¦                           ¦    ¦    ¦     c) T/O configuration warning      ¦ ¦                           ¦    ¦    ¦        operates normally.             ¦

¦ 4.  AUTO SLATS Light    C ¦ 1  ¦ 0  ¦ (O)May be inoperative provided        ¦ ¦     System                ¦    ¦    ¦ airspeed remains at or below 240      ¦ ¦     31-50-10              ¦    ¦    ¦ KIAS.                                 ¦

¦ 5.  FLAP ASYM Warning   C ¦ 1  ¦ 0  ¦ (M)(O)May be inoperative provided     ¦ ¦     System                ¦    ¦    ¦ flap asymmetry protection system is   ¦ ¦     27-50-30              ¦    ¦    ¦ verified to operate normally before   ¦ ¦                           ¦    ¦    ¦ each departure.                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 2        ¦ PAGE:    ¦ ¦                FALCON 200                ¦                       ¦          ¦ ¦                                          ¦ DATE: 10/12/1993      ¦ 27-2     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 27  FLIGHT CONTROLS       ¦    ¦    ¦                                       ¦

¦ 6.  Slat Position       C ¦ 1  ¦ 0  ¦ (O)May be inoperative provided:       ¦ ¦     Indicator             ¦    ¦    ¦     a) It is verified visually        ¦ ¦     27-80-40              ¦    ¦    ¦        that slats are properly        ¦ ¦                           ¦    ¦    ¦        positioned following each      ¦ ¦                           ¦    ¦    ¦        commanded control movement,    ¦ ¦                           ¦    ¦    ¦        and                            ¦ ¦                           ¦    ¦    ¦     b) Takeoff warning system slat    ¦ ¦                           ¦    ¦    ¦        function operates normally.    ¦

¦ 7.  Horizontal          C ¦ 1  ¦ 0  ¦ (O)May be inoperative provided:       ¦ ¦     Stabilizer Trim       ¦    ¦    ¦     a) Takeoff trim position is       ¦ ¦     Indicator             ¦    ¦    ¦        visually verified using the    ¦ ¦     24-40-10              ¦    ¦    ¦        reference marks on the         ¦ ¦                           ¦    ¦    ¦        vertical stabilizer before     ¦ ¦                           ¦    ¦    ¦        departure, and                 ¦ ¦                           ¦    ¦    ¦     b) Horizontal stabilizer trim     ¦ ¦                           ¦    ¦    ¦        operating aural alert system   ¦ ¦                           ¦    ¦    ¦        operates normally.             ¦

¦ 8.  Takeoff Warning     C ¦ 1  ¦ 1  ¦ Light only may be inoperative.        ¦ ¦     System                ¦    ¦    ¦                                       ¦

¦ 9.  Horizontal          C ¦ 1  ¦ 0  ¦ (O)May be inoperative provided:       ¦ ¦     Stabilizer Trim       ¦    ¦    ¦     a) Horizontal stabilizer trim     ¦ ¦     Operating Aural       ¦    ¦    ¦        position indicator operates    ¦ ¦     Alert (Clacker)       ¦    ¦    ¦        normally,                      ¦ ¦     31-50-00              ¦    ¦    ¦     b) Takeoff warning system         ¦ ¦                           ¦    ¦    ¦        stabilizer function operates   ¦ ¦                           ¦    ¦    ¦        normally, and                  ¦ ¦                           ¦    ¦    ¦     c) Autopilot is not used.         ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 2        ¦ PAGE:    ¦ ¦                FALCON 200                ¦                       ¦          ¦ ¦                                          ¦ DATE: 10/12/1993      ¦ 27-3     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 27  FLIGHT CONTROLS       ¦    ¦    ¦                                       ¦

¦ 10. Aileron Trim        C ¦ 1  ¦ 0  ¦ (O)May be inoperative provided:       ¦ ¦     Indicator             ¦    ¦    ¦     a) Aileron trim is verified       ¦ ¦     27-10-50              ¦    ¦    ¦        properly set before each       ¦ ¦                           ¦    ¦    ¦        departure, and                 ¦ ¦                           ¦    ¦    ¦     b) Aileron trim system is         ¦ ¦                           ¦    ¦    ¦        verified to operate normally   ¦ ¦                           ¦    ¦    ¦        before each departure.         ¦

¦ 11. Rudder Trim         C ¦ 1  ¦ 0  ¦ (M)(O)May be inoperative provided:    ¦ ¦     Indicator             ¦    ¦    ¦     a) Rudder trim is verified        ¦ ¦     27-20-40              ¦    ¦    ¦        properly set before each       ¦ ¦                           ¦    ¦    ¦        departure, and                 ¦ ¦                           ¦    ¦    ¦     b) Rudder trim system is          ¦ ¦                           ¦    ¦    ¦        verified to operate normally   ¦ ¦                           ¦    ¦    ¦        before each departure.         ¦

¦ 12. Stall Warning Horn  C ¦ 2  ¦ 1  ¦ (M)One may be inoperative provided    ¦ ¦     Test (Stall 1         ¦    ¦    ¦ stall warning system is verified to   ¦ ¦     and Stall 2)          ¦    ¦    ¦ operate normally before each          ¦ ¦                           ¦    ¦    ¦ departure by actuating the stall      ¦ ¦                           ¦    ¦    ¦ vane for the affected system          ¦ ¦                           ¦    ¦    ¦ checking auto slat, ignition, audio   ¦ ¦                           ¦    ¦    ¦ warning.                              ¦

¦ 13. Rudder Pedal        C ¦ 2  ¦ 0  ¦ May be inoperative provided rudder    ¦ ¦     Adjustments           ¦    ¦    ¦ pedals are in a position which        ¦ ¦     27-20-15              ¦    ¦    ¦ permit full rudder travel and brake   ¦ ¦                           ¦    ¦    ¦ application without restriction.      ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 2        ¦ PAGE:    ¦ ¦                FALCON 200                ¦                       ¦          ¦ ¦                                          ¦ DATE: 10/12/1993      ¦ 28-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 28  FUEL                  ¦    ¦    ¦                                       ¦

¦ 1.  Booster Pumps       C ¦ 2  ¦ 1  ¦ (M)(O)One may be inoperative          ¦ ¦     28-20-20              ¦    ¦    ¦ provided:                             ¦ ¦                           ¦    ¦    ¦     a) Both transfer pumps operate    ¦ ¦                           ¦    ¦    ¦        normally,                      ¦ ¦                           ¦    ¦    ¦     b) Feeder tank pressurization     ¦ ¦                           ¦    ¦    ¦        is verified to operate         ¦ ¦                           ¦    ¦    ¦        normally before each           ¦ ¦                           ¦    ¦    ¦        departure, and                 ¦ ¦                           ¦    ¦    ¦     c) Crossfeed valve operates       ¦ ¦                           ¦    ¦    ¦        normally.                      ¦

¦ 2.  Transfer Pumps      C ¦ 2  ¦ 1  ¦ (O)One may be inoperative provided:   ¦ ¦     28-10-40              ¦    ¦    ¦     a) Both booster pumps operate     ¦ ¦                           ¦    ¦    ¦        normally,                      ¦ ¦                           ¦    ¦    ¦     b) Wing XFR INTERCOM operates     ¦ ¦                           ¦    ¦    ¦        normally, and is used to       ¦ ¦                           ¦    ¦    ¦        prevent fuel imbalance, and    ¦ ¦                           ¦    ¦    ¦     c) Crossfeed valve operates       ¦ ¦                           ¦    ¦    ¦        normally.                      ¦

¦ 3.  Fuel Used Counters  C ¦ 2  ¦ 0  ¦ (O)May be inoperative provided:       ¦ ¦     28-40-10              ¦    ¦    ¦     a) All other fuel indications     ¦ ¦                           ¦    ¦    ¦        for the associated system      ¦ ¦                           ¦    ¦    ¦        operate normally, and          ¦ ¦                           ¦    ¦    ¦     b) Fuel Used/Gross weight         ¦ ¦                           ¦    ¦    ¦        indication system is not       ¦ ¦                           ¦    ¦    ¦        used.                          ¦

¦ 4.  FUEL LEVEL Light    C ¦ 1  ¦ 0  ¦ (M)(O)May be inoperative provided:    ¦ ¦     System                ¦    ¦    ¦     a) Associated rear fuel gauging   ¦ ¦     31-50-10              ¦    ¦    ¦        system is verified to          ¦ ¦                           ¦    ¦    ¦        operate normally before        ¦ ¦                           ¦    ¦    ¦        each departure, and            ¦ ¦                           ¦    ¦    ¦     b) Rear tank quantity is          ¦ ¦                           ¦    ¦    ¦        closely monitored during       ¦ ¦                           ¦    ¦    ¦        flight.                        ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 2        ¦ PAGE:    ¦ ¦                FALCON 200                ¦                       ¦          ¦ ¦                                          ¦ DATE: 10/12/1993      ¦ 28-2     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 28  FUEL                  ¦    ¦    ¦                                       ¦

¦ 5.  Wing XFR INTERCOM   C ¦ 1  ¦ 0  ¦ (O)May be inoperative provided all    ¦ ¦     28-10-40              ¦    ¦    ¦ fuel system components operate        ¦ ¦                           ¦    ¦    ¦ normally.                             ¦

¦ 6.  Total (TOT) Fuel    C ¦ 2  ¦ 1  ¦ (M)One may be inoperative             ¦ ¦     Quantity Indication   ¦    ¦    ¦ provided:                             ¦ ¦     Systems               ¦    ¦    ¦     a) Fuel quantity in associated    ¦ ¦     28-40-10              ¦    ¦    ¦        system is verified adequate    ¦ ¦                           ¦    ¦    ¦        before each departure,         ¦ ¦                           ¦    ¦    ¦     b) Both Fuel Flow/Fuel Used       ¦ ¦                           ¦    ¦    ¦        indicators operate normally,   ¦ ¦                           ¦    ¦    ¦        and                            ¦ ¦                           ¦    ¦    ¦     c) Rear quantity indications      ¦ ¦                           ¦    ¦    ¦        operate normally.              ¦

¦ 7.  Pressure Fueling    C ¦ 1  ¦ 0  ¦ (M)May be inoperative provided:       ¦ ¦     System                ¦    ¦    ¦     a) System is deactivated and      ¦ ¦     28-20-10              ¦    ¦    ¦        secured in accordance with     ¦ ¦                           ¦    ¦    ¦        an acceptable procedure, and   ¦ ¦                           ¦    ¦    ¦     b) All cockpit fuel quantity      ¦ ¦                           ¦    ¦    ¦        indicators operate normally.   ¦

¦ 8.  Gross Weight        C ¦ 1  ¦ 0  ¦                                       ¦ ¦     Counter               ¦    ¦    ¦                                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 2        ¦ PAGE:    ¦ ¦                FALCON 200                ¦                       ¦          ¦ ¦                                          ¦ DATE: 10/12/1993      ¦ 29-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 29  HYDRAULIC POWER       ¦    ¦    ¦                                       ¦

¦ 1.  Hydraulic Quantity  C ¦ 2  ¦ 0  ¦ (M)(O)May be inoperative provided:    ¦ ¦     Indicators            ¦    ¦    ¦     a) Hydraulic quantity in the      ¦ ¦     29-11-10              ¦    ¦    ¦        associated reservoir(s) is     ¦ ¦                           ¦    ¦    ¦        verified adequate before       ¦ ¦                           ¦    ¦    ¦        each departure, and            ¦ ¦                           ¦    ¦    ¦     b) All other hydraulic system     ¦ ¦                           ¦    ¦    ¦        indicators and warning         ¦ ¦                           ¦    ¦    ¦        lights operate normally.       ¦

¦ 2.  Main System         C ¦ 2  ¦ 0  ¦ (O)May be inoperative provided all    ¦ ¦     Pressure Warning      ¦    ¦    ¦ other hydraulic system pressure       ¦ ¦     Lights (HYDR1         ¦    ¦    ¦ indicators and warning lights         ¦ ¦     AND HYDR2)            ¦    ¦    ¦ operate normally.                     ¦ ¦     29-11-10, 29-15-10    ¦    ¦    ¦                                       ¦

¦ 3.  Standby Pump Light  C ¦ 1  ¦ 0  ¦ (O)May be inoperative provided:       ¦ ¦                           ¦    ¦    ¦     a) Standby pump is checked for    ¦ ¦                           ¦    ¦    ¦        cycling 1500-2100 PSI before   ¦ ¦                           ¦    ¦    ¦        engine starts, and             ¦ ¦                           ¦    ¦    ¦     b) Pump is left OFF except for    ¦ ¦                           ¦    ¦    ¦        takeoff, or if system #2       ¦ ¦                           ¦    ¦    ¦        normal pressure is lost        ¦ ¦                           ¦    ¦    ¦        in-flight.                     ¦

¦ 4.  Hydraulic Tank      B ¦ 2  ¦ 0  ¦ (M)(O)May be inoperative provided:    ¦ ¦     Pressurization        ¦    ¦    ¦     a) Reservoir pressurization is    ¦ ¦     Warning Lights        ¦    ¦    ¦        verified to operate normally   ¦ ¦     29-30-10              ¦    ¦    ¦        before each departure.         ¦ ¦                           ¦    ¦    ¦           OR                          ¦ ¦                         C ¦    ¦    ¦     b) Flight remains at or below     ¦ ¦                           ¦    ¦    ¦        below FL 200.                  ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 2        ¦ PAGE:    ¦ ¦                FALCON 200                ¦                       ¦          ¦ ¦                                          ¦ DATE: 10/12/1993      ¦ 29-2     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 29  HYDRAULIC POWER       ¦    ¦    ¦                                       ¦

¦ 5.  Hydraulic Pressure  C ¦ 2  ¦ 1  ¦ (O)One may be inoperative provided    ¦ ¦     Indicators            ¦    ¦    ¦ all other hydraulic system pressure   ¦ ¦     29-30-10              ¦    ¦    ¦ indicators and warning lights         ¦ ¦                           ¦    ¦    ¦ operate normally.                     ¦

¦ 6.  Hydraulic Pump Low  C ¦ 2  ¦ 0  ¦ (O)May be inoperative provided:       ¦ ¦     Pressure Warning      ¦    ¦    ¦     a) All other hydraulic system     ¦ ¦     Lights                ¦    ¦    ¦        pressure indicators and        ¦ ¦     (PUMP1 and PUMP2)     ¦    ¦    ¦        warning lights operate         ¦ ¦     29-11-10, 29-15-10    ¦    ¦    ¦        normally, and                  ¦ ¦                           ¦    ¦    ¦     b) Associated pressures and       ¦ ¦                           ¦    ¦    ¦        quantities are closely         ¦ ¦                           ¦    ¦    ¦        monitored throughout flight.   ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 2        ¦ PAGE:    ¦ ¦                FALCON 200                ¦                       ¦          ¦ ¦                                          ¦ DATE: 10/12/1993      ¦ 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.  Wing Anti-Icing     C ¦ 1  ¦ 0  ¦ May be inoperative CLOSED provided    ¦ ¦     System                ¦    ¦    ¦ the airplane is not operated in       ¦ ¦     30-10-00              ¦    ¦    ¦ known or forecast icing conditions.   ¦

¦ 2.  Engine Inlet        B ¦ 2  ¦ 1  ¦ (O)One may be inoperative CLOSED      ¦ ¦     Anti-Icing Systems    ¦    ¦    ¦ provided the airplane is not          ¦ ¦                           ¦    ¦    ¦ operated in known or forecast icing   ¦ ¦                           ¦    ¦    ¦ conditions.                           ¦

¦ 3.  Pitot/Static        B ¦ 2  ¦ 1  ¦ One may be inoperative provided:      ¦ ¦     Heater Systems        ¦    ¦    ¦     a) Airplane is not operated in    ¦ ¦                           ¦    ¦    ¦        visible moisture, or known     ¦ ¦                           ¦    ¦    ¦        or forecast icing              ¦ ¦                           ¦    ¦    ¦        conditions, and                ¦ ¦                           ¦    ¦    ¦     b) Neither taxiway nor runway     ¦ ¦                           ¦    ¦    ¦        is covered with standing       ¦ ¦                           ¦    ¦    ¦        water or slush.                ¦

¦ 4.  Pitot/Static        B ¦ 2  ¦ 1  ¦ (O)One may be inoperative provided:   ¦ ¦     Heater Light          ¦    ¦    ¦     a) Associated heater element      ¦ ¦     Systems               ¦    ¦    ¦        operates normally, and         ¦ ¦     30-30-10              ¦    ¦    ¦     b) Airplane is not operated in    ¦ ¦                           ¦    ¦    ¦        known or forecast icing        ¦ ¦                           ¦    ¦    ¦        conditions.                    ¦

¦ 5.  Windshield Heat     C ¦ 1  ¦ 0  ¦ (M)May be inoperative provided the    ¦ ¦     XFER Light System     ¦    ¦    ¦ transfer systems and heating net-     ¦ ¦     30-40-10              ¦    ¦    ¦ works are verified to operate         ¦ ¦                           ¦    ¦    ¦ normally before each departure into   ¦ ¦                           ¦    ¦    ¦ known or forecast icing conditions.   ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 2        ¦ PAGE:    ¦ ¦                FALCON 200                ¦                       ¦          ¦ ¦                                          ¦ DATE: 10/12/1993      ¦ 30-2     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 30  ICE AND RAIN          ¦    ¦    ¦                                       ¦ ¦     PROTECTION            ¦    ¦    ¦                                       ¦

¦ 6.  Windshield Heating  C ¦ 2  ¦ 1  ¦ (O)One may be inoperative provided:   ¦ ¦     Systems               ¦    ¦    ¦     a) Airplane is not operated       ¦ ¦     30-40-10              ¦    ¦    ¦        in known or forecast icing     ¦ ¦                           ¦    ¦    ¦        conditions, and                ¦ ¦                           ¦    ¦    ¦     b) Windshield de-fog system       ¦ ¦                           ¦    ¦    ¦        operates normally.             ¦

¦ 7.  Side Window         C ¦ 1  ¦ 0  ¦                                       ¦ ¦     Heating System        ¦    ¦    ¦                                       ¦ ¦     30-40-10              ¦    ¦    ¦                                       ¦

¦ 8.  Windshield Wipers   C ¦ 2  ¦ 0  ¦ May be inoperative provided the       ¦ ¦     30-40-30              ¦    ¦    ¦ airplane is not flown in precipi-     ¦ ¦                           ¦    ¦    ¦ tation within 5 nautical miles of     ¦ ¦                           ¦    ¦    ¦ the airport of takeoff or intended    ¦ ¦                           ¦    ¦    ¦ landing.                              ¦

¦ 9.  Windshield Defog    C ¦ 1  ¦ 0  ¦ May be inoperative provided all       ¦ ¦     System                ¦    ¦    ¦ windshield heating systems operate    ¦ ¦     30-40-30              ¦    ¦    ¦ normally.                             ¦

¦ 10. Angle of Attack     C ¦ 1  ¦ 0  ¦ May be inoperative provided the       ¦ ¦     Heating System        ¦    ¦    ¦ airplane is not operated in known     ¦ ¦     (for Speed Index)     ¦    ¦    ¦ or forecast icing conditions.         ¦

¦ 11.  Stall Warning      C ¦ 2  ¦ 1  ¦ One may be inoperative provided       ¦ ¦      Sensor Heating       ¦    ¦    ¦ the airplane is not operated in       ¦ ¦      Systems              ¦    ¦    ¦ known or forecast icing conditions.   ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 2 b      ¦ PAGE:    ¦ ¦                FALCON 200                ¦                       ¦          ¦ ¦                                          ¦ DATE: 02/02/2001      ¦ 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 ¦ -  ¦ 1  ¦ One may be inoperative at either      ¦ ¦     31-20-10              ¦    ¦    ¦ the pilot's or copliot's station.     ¦

¦ 2.  Flight Data         C ¦ -  ¦ 1  ¦                                       ¦ ¦ *** Recorder System       ¦    ¦    ¦                                       ¦ ¦     (FDR)               A ¦ -  ¦ 0  ¦ May be inoperative provided:          ¦ ¦     31-30-00              ¦    ¦    ¦     a) Cockpit Voice Recorder (CVR)   ¦ ¦                           ¦    ¦    ¦        operates normally,             ¦ ¦                           ¦    ¦    ¦     b) Airplane is not dispatched     ¦ ¦                           ¦    ¦    ¦        from a designated airport      ¦ ¦                           ¦    ¦    ¦        where repairs or replace-      ¦ ¦                           ¦    ¦    ¦        ments can be made, and         ¦ ¦                           ¦    ¦    ¦     c) Repairs are made within        ¦ ¦                           ¦    ¦    ¦        three flight days.             ¦

¦     1) FDR Recording    A ¦ -  ¦ -  ¦ May be inoperative provided:          ¦ ¦        Parameters         ¦    ¦    ¦     a) Cockpit Voice Recorder         ¦ ¦        Required by FAR    ¦    ¦    ¦        operates normally, and         ¦ ¦                           ¦    ¦    ¦     b) Repairs are made within        ¦ ¦                           ¦    ¦    ¦        20 calendar days.              ¦

¦     2) FDR Recording    A ¦ -  ¦ -  ¦ May be inoperative provided           ¦ ¦        Parameters         ¦    ¦    ¦ repairs are made prior to the         ¦ ¦        Not Required       ¦    ¦    ¦ completion of the next heavy          ¦ ¦        by FAR             ¦    ¦    ¦ maintenance visit.                    ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 2 b      ¦ PAGE:    ¦ ¦                FALCON 200                ¦                       ¦          ¦ ¦                                          ¦ DATE: 02/02/2001      ¦ 31-2     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 31  INDICATING/RECORDING  ¦    ¦    ¦                                       ¦ ¦     SYSTEMS               ¦    ¦    ¦                                       ¦

¦ 3.  TAS Indicator       C ¦ 1  ¦ 0  ¦                                       ¦

¦ 4.  SAT/TAT/TAS         C ¦ 1  ¦ 0  ¦ May be inoperative provided:          ¦ ¦     Indicator             ¦    ¦    ¦     a) Airplane is not operated       ¦ ¦                           ¦    ¦    ¦        in know or forecast icing      ¦ ¦                           ¦    ¦    ¦        conditions, and                ¦ ¦                           ¦    ¦    ¦     b) Minimum fuel quantity for      ¦ ¦                           ¦    ¦    ¦        flight is increased five       ¦ ¦                           ¦    ¦    ¦        percent.                       ¦

¦ 5.  TAT Indicator         ¦    ¦    ¦ Deleted, Rev. 2.                      ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 3        ¦ PAGE:    ¦ ¦                FALCON 200                ¦                       ¦          ¦ ¦                                          ¦ DATE: 03/21/2005      ¦ 32-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 32  LANDING GEAR          ¦    ¦    ¦                                       ¦

¦ 1.  Landing Gear        C ¦ 1  ¦ 0  ¦ (O)May be inoperative provided the    ¦ ¦     Selector Handle       ¦    ¦    ¦ landing gear position indicators      ¦ ¦     Warning Light         ¦    ¦    ¦ and warning horn operate normally.    ¦ ¦     32-30-60              ¦    ¦    ¦                                       ¦

¦ 2.  Parking Brake       C ¦ 1  ¦ 0  ¦ (O)May be inoperative provided:       ¦ ¦     Annunciator           ¦    ¦    ¦     a) Emergency brake accumulator    ¦ ¦     Light (P Brake)       ¦    ¦    ¦        pressure is verified normal    ¦ ¦     32-40-80              ¦    ¦    ¦        before each departure, and     ¦ ¦                           ¦    ¦    ¦     b) Number 2 braking system        ¦ ¦                           ¦    ¦    ¦        operates normally.             ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 3        ¦ PAGE:    ¦ ¦                FALCON 200                ¦                       ¦          ¦ ¦                                          ¦ DATE: 03/21/2005      ¦ 32-2     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 32  LANDING GEAR          ¦    ¦    ¦                                       ¦

¦ 3.  Anti-Skid System      ¦    ¦    ¦                                       ¦ ¦     (Includes             ¦    ¦    ¦                                     | ¦ ¦     Annunciator Lights)   ¦    ¦    ¦                                     | ¦

¦     1) Dry Runways      C ¦ 1  ¦ 0  ¦ (O)May be inoperative provided      | ¦ ¦                           ¦    ¦    ¦ operations are conducted in         | ¦ ¦                           ¦    ¦    ¦ accordance with the Performance     | ¦ ¦                           ¦    ¦    ¦ Data of the AFM.                    | ¦

¦     2) Wet Runways      C ¦ 1  ¦ 0  ¦ (O)May be inoperative provided:     | ¦ ¦        (No standing       ¦    ¦    ¦     a) Operations are limited to    | ¦ ¦        water present      ¦    ¦    ¦        utilization of PFCO or       | ¦ ¦        in areas of        ¦    ¦    ¦        or grooved runways,          | ¦ ¦        takeoff ground     ¦    ¦    ¦     b) Thrust reversers operate     | ¦ ¦        roll, no snow,     ¦    ¦    ¦        normally,                    | ¦ ¦        no icy runway      ¦    ¦    ¦     c) Acceptable Performance Data  | ¦ ¦        conditions.)       ¦    ¦    ¦        from an analysis of the      | ¦ ¦                           ¦    ¦    ¦        Accelerate Stop Capability   | ¦ ¦                           ¦    ¦    ¦        on Wet Runway Surfaces is    | ¦ ¦                           ¦    ¦    ¦        developed and used,          | ¦ ¦                           ¦    ¦    ¦     d) The cross wind component for | ¦ ¦                           ¦    ¦    ¦        both departure and arrival   | ¦ ¦                           ¦    ¦    ¦        runways is forecast to be    | ¦ ¦                           ¦    ¦    ¦        15 knots or less,            | ¦ ¦                           ¦    ¦    ¦     e) Acceptable Performance Data  | ¦ ¦                           ¦    ¦    ¦        Report is referenced in the  | ¦ ¦                           ¦    ¦    ¦        Operator's Minimum Equipment | ¦ ¦                           ¦    ¦    ¦        List (MEL) by Report Name,   | ¦ ¦                           ¦    ¦    ¦        Number, Revision Number,     | ¦ ¦                           ¦    ¦    ¦        and Acceptance Data,         | ¦ ¦                           ¦    ¦    ¦     f) Performance Data Report      | ¦ ¦                           ¦    ¦    ¦        assumes that reverse thrust  | ¦ ¦                           ¦    ¦    ¦        action is terminated at      | ¦ ¦                           ¦    ¦    ¦        60 knots, and                | ¦ ¦                           ¦    ¦    ¦     g) Wet runway landing opera-    | ¦ ¦                           ¦    ¦    ¦        tions are conducted in       | ¦ ¦                           ¦    ¦    ¦        accordance with available    | ¦ ¦                           ¦    ¦    ¦        landing performance data     | ¦ ¦                           ¦    ¦    ¦        in the AFM.                  | ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 2 a      ¦ PAGE:    ¦ ¦                FALCON 200                ¦                       ¦          ¦ ¦                                          ¦ DATE: 07/07/1998      ¦ 33-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 33  LIGHTS                ¦    ¦    ¦                                       ¦

¦ 1.  Cockpit/Flight      C ¦ -  ¦ -  ¦ Individual lights may be inopera-     ¦ ¦     Deck/Flight           ¦    ¦    ¦ tive provided remaining lights are:   ¦ ¦     Compartment and       ¦    ¦    ¦     a) Sufficient to clearly          ¦ ¦     Instrument Lighting   ¦    ¦    ¦        illuminate all required        ¦ ¦     33-10-00              ¦    ¦    ¦        instruments, controls and      ¦ ¦                           ¦    ¦    ¦        other devices for which it     ¦ ¦                           ¦    ¦    ¦        is provided,                   ¦ ¦                           ¦    ¦    ¦     b) Positioned so that direct      ¦ ¦                           ¦    ¦    ¦        rays are shielded from         ¦ ¦                           ¦    ¦    ¦        flight crewmember's            ¦ ¦                           ¦    ¦    ¦        eyes, and                      ¦ ¦                           ¦    ¦    ¦     c) Lighting configuration at      ¦ ¦                           ¦    ¦    ¦        dispatch is acceptable to      ¦ ¦                           ¦    ¦    ¦        the flight crew.               ¦

¦ 2.  Cabin Interior      C ¦ -  ¦ -  ¦ May be inoperative provided:          ¦ ¦     Lights                ¦    ¦    ¦     a) Adjacent light operates        ¦ ¦     33-20-05              ¦    ¦    ¦        normally, and                  ¦ ¦                           ¦    ¦    ¦     b) Inoperative lights do not      ¦ ¦                           ¦    ¦    ¦        exceed 50 percent of the       ¦ ¦                           ¦    ¦    ¦        total installed.               ¦

¦ 3.  Passenger Notice    C ¦ -  ¦ -  ¦ (O)"No Smoking/Fasten Seat Belt"      ¦ ¦     System (No            ¦    ¦    ¦ signs may be inoperative and the      ¦ ¦     Smoking/Fasten        ¦    ¦    ¦ associated passenger seat(s) may      ¦ ¦     Seat Belt" Signs)     ¦    ¦    ¦ occupied provided:                    ¦ ¦     33-20-50              ¦    ¦    ¦     a) Passenger Address System       ¦ ¦                           ¦    ¦    ¦        operates normally, and can     ¦ ¦                           ¦    ¦    ¦        be clearly heard throughout    ¦ ¦                           ¦    ¦    ¦        the cabin during flight, and   ¦ ¦                           ¦    ¦    ¦     b) An acceptable procedure is     ¦ ¦                           ¦    ¦    ¦        used to notify passengers      ¦ ¦                           ¦    ¦    ¦        when seat belts must be        ¦ ¦                           ¦    ¦    ¦        fastened or smoking is         ¦ ¦                           ¦    ¦    ¦        prohibited.                    ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 3        ¦ PAGE:    ¦ ¦                FALCON 200                ¦                       ¦          ¦ ¦                                          ¦ DATE: 03/21/2005      ¦ 33-2     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 33  LIGHTS                ¦    ¦    ¦                                       ¦

¦ 4.  Aft Compartment     C ¦ 1  ¦ 0  ¦                                       ¦ ¦     Lighting System       ¦    ¦    ¦                                       ¦ ¦     33-30-10              ¦    ¦    ¦                                       ¦

¦ 5.  Baggage             C ¦ 1  ¦ 0  ¦                                       ¦ ¦     Compartment           ¦    ¦    ¦                                       ¦ ¦     Lighting System       ¦    ¦    ¦                                       ¦ ¦     33-30-10              ¦    ¦    ¦                                       ¦

¦ 6.  Landing Lights      C ¦ 2  ¦ 1  ¦ One may be inoperative for night      ¦ ¦     33-40-30              ¦    ¦    ¦ operations provided taxi light        ¦ ¦                           ¦    ¦    ¦ operates normally.                    ¦

¦                         C ¦ 2  ¦ 0  ¦ May be inoperative for day            ¦ ¦                           ¦    ¦    ¦ operations.                           ¦

¦ 7.  Taxi Light          C ¦ 1  ¦ 0  ¦ May be inoperative for night          ¦ ¦     33-40-40              ¦    ¦    ¦ operations provided both landing      ¦ ¦                           ¦    ¦    ¦ lights operate normally.              ¦

¦                         C ¦ 1  ¦ 0  ¦ May be inoperative for day            ¦ ¦                           ¦    ¦    ¦ operations.                           ¦

¦ 8.  Position Lights     C ¦ 1  ¦ 0  ¦ May be inoperative for day            ¦ ¦     System                ¦    ¦    ¦ operations.                           ¦ ¦     33-40-20              ¦    ¦    ¦                                       ¦

¦ 9.  Anti-Collision      B ¦ -  ¦ 0  ¦ May be inoperative for night          ¦ ¦     Lights                ¦    ¦    ¦ operations provided strobe light      ¦ ¦     33-40-20              ¦    ¦    ¦ system is installed and operates      ¦ ¦                           ¦    ¦    ¦ normally.                             ¦

¦                         C ¦ -  ¦ 0  ¦ May be inoperative for day            ¦ ¦                           ¦    ¦    ¦ operations.                           ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 2 b      ¦ PAGE:    ¦ ¦                FALCON 200                ¦                       ¦          ¦ ¦                                          ¦ DATE: 02/02/2001      ¦ 33-3     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 33  LIGHTS                ¦    ¦    ¦                                       ¦

¦ 10. Wing Ice Detection  C ¦ -  ¦ 0  ¦ May be inoperative provided ground    ¦ ¦     Lights                ¦    ¦    ¦ deicing procedures to not require     ¦ ¦     33-40-50              ¦    ¦    ¦ their use.                            ¦

¦ 11. Exterior Emergency  C ¦ 1  ¦ 0  ¦ May be inoperative for day            ¦ ¦     Lighting System       ¦    ¦    ¦ operations.                           ¦ ¦     33-50-10              ¦    ¦    ¦                                       ¦

¦ 12. Logo Light System   D ¦ 1  ¦ 0  ¦                                       ¦

¦ 13. Wing Strobe         C ¦ 1  ¦ 0  ¦ May be inoperative for night          ¦ ¦     Light System          ¦    ¦    ¦ operations provided anti-collision    ¦ ¦     33-40-10              ¦    ¦    ¦ lights operate normally.              ¦

¦ 14. Pulse Light System  D ¦ -  ¦ 0  ¦                                       ¦ ¦ ***                       ¦    ¦    ¦                                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 2 b      ¦ PAGE:    ¦ ¦                FALCON 200                ¦                       ¦          ¦ ¦                                          ¦ DATE: 02/02/2001      ¦ 34-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 34  NAVIGATION            ¦    ¦    ¦                                       ¦

¦ 1.  Rate of Climb       C ¦ 2  ¦ 1  ¦ One may be inoperative for day        ¦ ¦     Indicators            ¦    ¦    ¦ VMC flight only.                      ¦ ¦     34-10-10              ¦    ¦    ¦                                       ¦

¦ 2.  Angle of Attack     C ¦ -  ¦ 0  ¦ May be inoperative provided stall     ¦ ¦     Systems               ¦    ¦    ¦ warning systems operate normally.     ¦ ¦     34-10-90              ¦    ¦    ¦                                       ¦

¦ 3.  Turn and Bank         ¦    ¦    ¦                                       ¦ ¦     Indicators            ¦    ¦    ¦                                       ¦

¦ *** 1) Rate of Turn     C ¦ 2  ¦ 1  ¦                                       ¦ ¦        Indicators         ¦    ¦    ¦                                       ¦ ¦                         C ¦ 2  ¦ 0  ¦ May be inoperative provided Standby   ¦ ¦                           ¦    ¦    ¦ Horizon Indicator operates            ¦ ¦                           ¦    ¦    ¦ normally.                             ¦

¦ 4.  Non-Stabilized      B ¦ 1  ¦ 0  ¦ (O)May be inoperative provided any    ¦ ¦     Magnetic Compass      ¦    ¦    ¦ magnetic compass combination of       ¦ ¦                           ¦    ¦    ¦ three Gryo or INS (IRU) stabilized    ¦ ¦                           ¦    ¦    ¦ Compass Systems are operative.        ¦

¦                         B ¦ 1  ¦ 0  ¦ (O)May be inoperative provided:       ¦ ¦                           ¦    ¦    ¦     a) Any combination of two Gyro    ¦ ¦                           ¦    ¦    ¦        Stabilized Compass Systems     ¦ ¦                           ¦    ¦    ¦        operate normally, and          ¦ ¦                           ¦    ¦    ¦     b) Airplane is operated with      ¦ ¦                           ¦    ¦    ¦        Dual Independent Navigation    ¦ ¦                           ¦    ¦    ¦        Capability and under           ¦ ¦                           ¦    ¦    ¦        Positive Radar Control by      ¦ ¦                           ¦    ¦    ¦        ATC on the en route portion    ¦ ¦                           ¦    ¦    ¦        of the flight.                 ¦

¦                         B ¦ 1  ¦ 0  ¦ (O)May be inoperative for flights     ¦ ¦                           ¦    ¦    ¦ that are entirely within areas of     ¦ ¦                           ¦    ¦    ¦ magnetic unreliability provided at    ¦ ¦                           ¦    ¦    ¦ least two Stabilized Directional      ¦ ¦                           ¦    ¦    ¦ Gyro Systems are installed,           ¦ ¦                           ¦    ¦    ¦ operate normally, and used in         ¦ ¦                           ¦    ¦    ¦ conjunction with approved Free        ¦ ¦                           ¦    ¦    ¦ Gryo Navigation Techniques.           ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 2 b      ¦ PAGE:    ¦ ¦                FALCON 200                ¦                       ¦          ¦ ¦                                          ¦ DATE: 02/02/2001      ¦ 34-2     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 34  NAVIGATION            ¦    ¦    ¦                                       ¦

¦ 5.  Flight Director     C ¦ 2  ¦ 0  ¦ May be inoperative provided           ¦ ¦     Systems               ¦    ¦    ¦ approach minimums do not require      ¦ ¦                           ¦    ¦    ¦ their use.                            ¦

¦ 6.  Distance Measuring  D ¦ -  ¦ -  ¦ Any in excess of those required       ¦ ¦     Equipment (DME)       ¦    ¦    ¦ by FAR may be inoperative.            ¦ ¦     34-50-30              ¦    ¦    ¦                                       ¦

¦ 7.  Weather Radar       C ¦ -  ¦ -  ¦ As required by FAR.                   ¦ ¦ *** 34-40-10              ¦    ¦    ¦                                       ¦

¦     1) Windshear        C ¦ -  ¦ 0  ¦ (O)May be inoperative provided:       ¦ ¦        Detection and      ¦    ¦    ¦     a) Alternate procedures are       ¦ ¦        Avoidance          ¦    ¦    ¦        established and used, and      ¦ ¦        System             ¦    ¦    ¦     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 are      ¦ ¦                           ¦    ¦    ¦        not conducted in known or      ¦ ¦                           ¦    ¦    ¦        forecast windshear             ¦ ¦                           ¦    ¦    ¦        conditions.                    ¦

¦ 8.  VHF Navigation      C ¦ -  ¦ -  ¦ As required by FAR.                   ¦ ¦     System                ¦    ¦    ¦                                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 3        ¦ PAGE:    ¦ ¦                FALCON 200                ¦                       ¦          ¦ ¦                                          ¦ DATE: 03/21/2005      ¦ 34-3     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 34  NAVIGATION            ¦    ¦    ¦                                       ¦

¦ 9.  Ground Proximity    A ¦ -  ¦ 0  ¦ May be inoperative provided:          ¦ ¦ *** Warning System        ¦    ¦    ¦     a) Alternate procedures are       ¦ ¦                           ¦    ¦    ¦        established and used, and      ¦ ¦                           ¦    ¦    ¦     b) Repairs are made within two    ¦ ¦                           ¦    ¦    ¦        flight days.                   ¦

¦                         C ¦ -  ¦ 0  ¦ (O)May be inoperative provided:     | ¦ ¦                           ¦    ¦    ¦     a) It is not required by FAR,   | ¦ ¦                           ¦    ¦    ¦        and                          | ¦ ¦                           ¦    ¦    ¦     b) Alternate procedures are     | ¦ ¦                           ¦    ¦    ¦        established and used.        | ¦

¦     1) Modes 1 - 4      A ¦ -  ¦ 0  ¦ (O)May be inoperative provided:       ¦ ¦                           ¦    ¦    ¦     a) Alternate procedures are       ¦ ¦                           ¦    ¦    ¦        established and used, and      ¦ ¦                           ¦    ¦    ¦     b) Repairs are made within two    ¦ ¦                           ¦    ¦    ¦        flight days.                   ¦

¦                         C ¦ -  ¦ 0  ¦ (O)May be inoperative provided:     | ¦ ¦                           ¦    ¦    ¦     a) It is not required by FAR,   | ¦ ¦                           ¦    ¦    ¦        and                          | ¦ ¦                           ¦    ¦    ¦     b) Alternate procedures are     | ¦ ¦                           ¦    ¦    ¦        established and used.        | ¦

¦     2) Test Mode        A ¦ 1  ¦ 0  ¦ May be inoperative provided:          ¦ ¦                           ¦    ¦    ¦     a) GPWS is considered             ¦ ¦                           ¦    ¦    ¦        inoperative, and               ¦ ¦                           ¦    ¦    ¦     b) Repairs are made within        ¦ ¦                           ¦    ¦    ¦        two flight days.               ¦

¦                         C ¦ -  ¦ 0  ¦ (O)May be inoperative provided:     | ¦ ¦                           ¦    ¦    ¦     a) It is not required by FAR,   | ¦ ¦                           ¦    ¦    ¦        and                          | ¦ ¦                           ¦    ¦    ¦     b) GPWS is considered           | ¦ ¦                           ¦    ¦    ¦        inoperative.                 | ¦

¦                           ¦    ¦    ¦ (Continued)                           ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 3        ¦ PAGE:    ¦ ¦                FALCON 200                ¦                       ¦          ¦ ¦                                          ¦ DATE: 03/21/2005      ¦ 34-4     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 34  NAVIGATION            ¦    ¦    ¦                                       ¦

¦ 9.  Ground Proximity      ¦    ¦    ¦                                       ¦ ¦ *** Warning System        ¦    ¦    ¦                                       ¦ ¦     (GPWS)(Cont'd)        ¦    ¦    ¦                                       ¦

¦     3) Glideslope       B ¦ 2  ¦ 0  ¦                                       ¦ ¦        Deviation          ¦    ¦    ¦                                       ¦ ¦        (Mode 5)         C ¦ 2  ¦ 0  ¦ May be inoperative provided it is     ¦ ¦                           ¦    ¦    ¦ not required by FAR.                  ¦

¦ *** 4) Advisory         C ¦ -  ¦ 0  ¦ (O)May be inoperative provided        ¦ ¦        Callouts           ¦    ¦    ¦ alternate procedures are              ¦ ¦                           ¦    ¦    ¦ established and used.                 ¦

¦     5) Windshear        C ¦ -  ¦ 0  ¦ (O)May be inoperative provided:       ¦ ¦        Mode               ¦    ¦    ¦     a) Alternate procedures are       ¦ ¦                           ¦    ¦    ¦        established and used, and      ¦ ¦                           ¦    ¦    ¦     b) Windshear Detection and        ¦ ¦                           ¦    ¦    ¦        Avoidance System operates      ¦ ¦                           ¦    ¦    ¦        normally.                      ¦

¦                         C ¦ -  ¦ 0  ¦ (O)May be inoperative provided:       ¦ ¦                           ¦    ¦    ¦     a) Alternate procedures are       ¦ ¦                           ¦    ¦    ¦        established and used, and      ¦ ¦                           ¦    ¦    ¦     b) Takeoffs and landings are      ¦ ¦                           ¦    ¦    ¦        not conducted in known or      ¦ ¦                           ¦    ¦    ¦        forecast windshear             ¦ ¦                           ¦    ¦    ¦        conditions.                    ¦

¦ *** 6) TAWS             C ¦ -  ¦ 0  ¦                                       ¦

¦ 10. Radio Altimeter     C ¦ -  ¦ 0  ¦ May be inoperative provided           ¦ ¦     System                ¦    ¦    ¦ approach minimum do not require       ¦ ¦     34-40-20              ¦    ¦    ¦ its use.                              ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 3        ¦ PAGE:    ¦ ¦                FALCON 200                ¦                       ¦          ¦ ¦                                          ¦ DATE:  03/21/2005     ¦ 34-5     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 34  NAVIGATION            ¦    ¦    ¦                                       ¦

¦ 11. Instrument          C ¦ -  ¦ 0  ¦ May be inoperative provided           ¦ ¦     Comparator            ¦    ¦    ¦ approach minimums do not require      ¦ ¦                           ¦    ¦    ¦ its use.                              ¦

¦ 12. Marker Beacon       C ¦ -  ¦ 0  ¦ May be inoperative provided           ¦ ¦                           ¦    ¦    ¦ approach minimums do not require      ¦ ¦                           ¦    ¦    ¦ its use.                              ¦

¦ 13. Radio Compass       D ¦ -  ¦ -  ¦ Any in excess of those required by    ¦ ¦     (ADF) System          ¦    ¦    ¦ FAR may be inoperative.               ¦ ¦     34-50-40              ¦    ¦    ¦                                       ¦

¦ 14. Glide Slope         C ¦ -  ¦ -  ¦ As required by FAR.                   ¦ ¦     Receiver              ¦    ¦    ¦                                       ¦

¦ 15. MACH/Airspeed       B ¦ 1  ¦ 0  ¦ (O)May be inoperative provided:       ¦ ¦     Warning               ¦    ¦    ¦     a) Airspeed remains at or below   ¦ ¦     34-10-20              ¦    ¦    ¦        Vmo - 330 kts, KIAS Mmo -      ¦ ¦                           ¦    ¦    ¦        .82M., and                     ¦ ¦                           ¦    ¦    ¦     b) Both mach/airspeed indi-       ¦ ¦                           ¦    ¦    ¦        cators operate normally.       ¦

¦ 16. ATC Transponders    B ¦ -  ¦ 0  ¦ May be inoperative provided:        | ¦ ¦     and Automatic         ¦    ¦    ¦     a) Enroute operations do not      ¦ ¦     Reporting Systems     ¦    ¦    ¦        require its use, and           ¦ ¦                           ¦    ¦    ¦     b) Prior to flight, approval      ¦ ¦                           ¦    ¦    ¦        is obtained from ATC           ¦ ¦                           ¦    ¦    ¦        facilities having jurisdic-    ¦ ¦                           ¦    ¦    ¦        tion over the planned          ¦ ¦                           ¦    ¦    ¦        route of flight.               ¦

¦                         D ¦ -  ¦ -  ¦ Any in excess of those required by    ¦ ¦                           ¦    ¦    ¦ FAR may be inoperative.               ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 3        ¦ PAGE:    ¦ ¦                FALCON 200                ¦                       ¦          ¦ ¦                                          ¦ DATE: 03/21/2005      ¦ 34-6     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 34  NAVIGATION            ¦    ¦    ¦                                       ¦

¦ 17. Altitude Alerting   A ¦ -  ¦ 0  ¦ (O)May be inoperative provided:       ¦ ¦     System                ¦    ¦    ¦     a) Autopilot with altitude        ¦ ¦                           ¦    ¦    ¦        hold is operative,             ¦ ¦                           ¦    ¦    ¦     b) Enroute operations do not      ¦ ¦                           ¦    ¦    ¦        require its use, and           ¦ ¦                           ¦    ¦    ¦     c) Repairs are made within        ¦ ¦                           ¦    ¦    ¦        three flight days.             ¦

¦                         C ¦ -  ¦ 0  ¦ May be inoperative provided it is     ¦ ¦                           ¦    ¦    ¦ not required by FAR.                  ¦

¦ 18. Standby Attitude    C ¦ -  ¦ 0  ¦ May be inoperative provided not       ¦ ¦     Indicator             ¦    ¦    ¦ required by FAR.                      ¦

¦                         B ¦ -  ¦ 0  ¦ May be inoperative provided:          ¦ ¦                           ¦    ¦    ¦     a) Operations are conducted in    ¦ ¦                           ¦    ¦    ¦        Day VMC only, and              ¦ ¦                           ¦    ¦    ¦     b) Operations are not conducted   ¦ ¦                           ¦    ¦    ¦        into known or forecast         ¦ ¦                           ¦    ¦    ¦        over-the-top conditions.     | ¦

¦                           ¦    ¦    ¦ NOTE: The Standby Attitude            ¦ ¦                           ¦    ¦    ¦       Indicator must be operative     ¦ ¦                           ¦    ¦    ¦       at dispatch for aircraft        ¦ ¦                           ¦    ¦    ¦       equipped with the Pro Line 4    ¦ ¦                           ¦    ¦    ¦       system.                         ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 3        ¦ PAGE:    ¦ ¦                FALCON 200                ¦                       ¦          ¦ ¦                                          ¦ DATE: 03/21/2005      ¦ 34-7     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 34  NAVIGATION            ¦    ¦    ¦                                       ¦

¦ 19. RMIs                C ¦ -  ¦ -  ¦                                       ¦

¦ 20. Inertial Naviga-    C ¦ -  ¦ -  ¦ As required by FAR.                   ¦ ¦     tion System (INS)     ¦    ¦    ¦                                       ¦ ¦     34-40-30              ¦    ¦    ¦                                       ¦

¦ 21. Flight Management   C ¦ -  ¦ 0  ¦ May be inoperative provided re-       ¦ ¦     System (FMS)          ¦    ¦    ¦ quired navigation and communica-      ¦ ¦                           ¦    ¦    ¦ tions system are not affected.        ¦

¦ 22. Vertical            C ¦ -  ¦ 0  ¦                                       ¦ ¦     Navigation System     ¦    ¦    ¦                                       ¦

¦ 23. VLF/OMEGA System    C ¦ -  ¦ -  ¦ As required by FAR.                   ¦

¦ 24. Microwave Landing   C ¦ -  ¦ 0  ¦ As required by FAR.                   ¦ ¦     System (MLS)          ¦    ¦    ¦                                       ¦

¦ 25. GPS/LORAN System    C ¦ -  ¦ 0  ¦ As required by FAR.                   ¦

¦ 26. RNAV System         C ¦ -  ¦ 0  ¦ As required by FAR.                   ¦

¦ 27. EFIS Display        C ¦ -  ¦ 1  ¦ One may be inoperative provided:      ¦ ¦     Source Select         ¦    ¦    ¦     a) Pilot and copilot EFIS         ¦ ¦     Switches              ¦    ¦    ¦        systems remain connected       ¦ ¦                           ¦    ¦    ¦        to independent sources,        ¦ ¦                           ¦    ¦    ¦     b) Associated sources operate     ¦ ¦                           ¦    ¦    ¦        normally,                      ¦ ¦                           ¦    ¦    ¦     c) All EFIS CRT's operate         ¦ ¦                           ¦    ¦    ¦        normally, and                  ¦ ¦                           ¦    ¦    ¦     d) Inoperative switches are not   ¦ ¦                           ¦    ¦    ¦        moved in flight.               ¦

¦ 28. EFIS Symbol         C ¦ 3  ¦ 2  ¦ One may be inoperative provided       ¦ ¦     Generator Units       ¦    ¦    ¦ each pilot's EFIS is driven by an     ¦ ¦     (SGU, DPU and/or      ¦    ¦    ¦ independent symbol generator unit     ¦ ¦     MPU)                  ¦    ¦    ¦ (SGU, DPU or MPU) which operates      ¦ ¦                           ¦    ¦    ¦ normally.                             ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 3        ¦ PAGE:    ¦ ¦                FALCON 200                ¦                       ¦          ¦ ¦                                          ¦ DATE: 03/21/2005      ¦ 34-8     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 34  NAVIGATION            ¦    ¦    ¦                                       ¦

¦ 29. Multifunction       C ¦ 1  ¦ 0  ¦ (O)May be inoperative provided:       ¦ ¦     Display (MFD)         ¦    ¦    ¦     a) Procedures do not require      ¦ ¦                           ¦    ¦    ¦        its use, and                   ¦ ¦                           ¦    ¦    ¦     b) When radar is required, at     ¦ ¦                           ¦    ¦    ¦        least one radar display        ¦ ¦                           ¦    ¦    ¦        operates normally.             ¦

¦ 30. EADI Annunciators/    ¦    ¦    ¦                                       ¦ ¦     Displays              ¦    ¦    ¦                                       ¦

¦     1) FAST/Slow        C ¦ 2  ¦ 0  ¦                                       ¦ ¦        Indications        ¦    ¦    ¦                                       ¦

¦     2) Flight Director  C ¦ 2  ¦ 0  ¦ May be inoperative provided           ¦ ¦        Bars               ¦    ¦    ¦ approach minimums do not require      ¦ ¦                           ¦    ¦    ¦ its use.                              ¦

¦     3) Radio Altitude   C ¦ 2  ¦ 0  ¦                                       ¦

¦     4) ILS Deviation    C ¦ 2  ¦ 0  ¦ As required by FAR.                   ¦

¦     5) Marker           C ¦ 2  ¦ 0  ¦ May be inoperative provided           ¦ ¦        Indications        ¦    ¦    ¦ approach minimums do not require      ¦ ¦                           ¦    ¦    ¦ its use.                              ¦

¦     6) Composite/Mix    C ¦ 2  ¦ 1  ¦                                       ¦ ¦        Mode               ¦    ¦    ¦                                       ¦

¦     7) Airspeed         C ¦ 2  ¦ 0  ¦ (O)May be inoperative provided        ¦ ¦                           ¦    ¦    ¦ airspeed information is not           ¦ ¦                           ¦    ¦    ¦ displayed.                            ¦

¦     8) Speed Trend      C ¦ 2  ¦ 0  ¦ (O)May be inoperative provided        ¦ ¦                           ¦    ¦    ¦ trend information is not displayed.   ¦

¦     9) Mach Indication  C ¦ 2  ¦ 0  ¦ (O)May be inoperative provided mach   ¦ ¦                           ¦    ¦    ¦ information is not displayed.         ¦

¦                           ¦    ¦    ¦ (Continued)                           ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 3        ¦ PAGE:    ¦ ¦                FALCON 200                ¦                       ¦          ¦ ¦                                          ¦ DATE: 03/21/2005      ¦ 34-9     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 34  NAVIGATION            ¦    ¦    ¦                                       ¦

¦ 30. EADI Annunciations/   ¦    ¦    ¦                                       ¦ ¦     Displays (Cont'd)     ¦    ¦    ¦                                       ¦

¦    10) Accel/Decel      C ¦ 2  ¦ 0  ¦                                       ¦ ¦        Indication         ¦    ¦    ¦                                       ¦

¦    11) DH Set           C ¦ 2  ¦ 0  ¦ May be inoperative provided           ¦ ¦                           ¦    ¦    ¦ approach minimums do not require      ¦ ¦                           ¦    ¦    ¦ its use.                              ¦

¦ 31. EHSI Annunciations/   ¦    ¦    ¦                                       ¦ ¦     Displays              ¦    ¦    ¦                                       ¦

¦     1) Selected Heading C ¦ 2  ¦ 0  ¦                                       ¦

¦     2) Selected Course  C ¦ 2  ¦ 0  ¦ May be inoperative provided           ¦ ¦                           ¦    ¦    ¦ navigation does not require its       ¦ ¦                           ¦    ¦    ¦ use.                                  ¦

¦     3) Bearing          C ¦ 4  ¦ 0  ¦ May be inoperative provided           ¦ ¦        Pointers           ¦    ¦    ¦ adjacent RMI(s) operates normally.    ¦

¦     4) DME Display      C ¦ 2  ¦ 0  ¦ As required by FAR.                   ¦

¦     5) Groundspeed/     C ¦ 2  ¦ 0  ¦                                       ¦ ¦        Time To Go         ¦    ¦    ¦                                       ¦

¦     6) ARC Mode         C ¦ 2  ¦ 0  ¦ NOTE: Weather radar requirements      ¦ ¦                           ¦    ¦    ¦       must be considered if both      ¦ ¦                           ¦    ¦    ¦       ARC modes are inoperative.      ¦

¦     7) Second Course    C ¦ 2  ¦ 0  ¦                                       ¦

¦     8) Elapsed Time/TAS C ¦ 2  ¦ 0  ¦                                       ¦

¦     9) Wind Speed       C ¦ 2  ¦ 0  ¦                                       ¦ ¦        Vector             ¦    ¦    ¦                                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 3        ¦ PAGE:    ¦ ¦                FALCON 200                ¦                       ¦          ¦ ¦                                          ¦ DATE:  03/21/2005     ¦ 34-10    ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 34  NAVIGATION            ¦    ¦    ¦                                       ¦

¦ 32. VOR Angular/Linear  C ¦ 2  ¦ 0  ¦ May be inoperative provided at        ¦ ¦     Deviation Selector    ¦    ¦    ¦ least one VOR system is operating     ¦ ¦                           ¦    ¦    ¦ normally in the angular mode.         ¦

¦ 33. Navigation Data     C ¦ -  ¦ 0  ¦                                       ¦ ¦     Bank                  ¦    ¦    ¦                                       ¦

¦ *** 1) Navigation       C ¦ -  ¦ -  ¦ (O)May be out of currency provided:   ¦ ¦        Databases          ¦    ¦    ¦     a) Current Aeronautical Charts    ¦ ¦                           ¦    ¦    ¦        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.                    ¦

¦ 34. Storm Scope         C ¦ -  ¦ -  ¦ As required by FAR.                   ¦

¦ 35. NAV/COM Preselect   C ¦ -  ¦ 0  ¦ May be inoperative provided direct    ¦ ¦     Tuning Functions      ¦    ¦    ¦ tuning mode is installed and          ¦ ¦                           ¦    ¦    ¦ operates normally for each affected   ¦ ¦                           ¦    ¦    ¦ unit.                                 ¦

¦ 36. Voice Advisory/     C ¦ 1  ¦ 0  ¦                                       ¦ ¦     Flight Profile        ¦    ¦    ¦                                       ¦ ¦     Advisory System       ¦    ¦    ¦                                       ¦

¦ 37. NAV/COMM/ADF/TDR    C ¦ -  ¦ 0  ¦ May be inoperative provided manual    ¦ ¦     Memory Channels       ¦    ¦    ¦ tuning operates normally.             ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 3        ¦ PAGE:    ¦ ¦                FALCON 200                ¦                       ¦          ¦ ¦                                          ¦ DATE: 03/21/2005      ¦ 34-11    ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 34  NAVIGATION            ¦    ¦    ¦                                       ¦

¦ 38. NAV/COMM/ADF/TDR    C ¦ -  ¦ 1  ¦ One may be inoperative on either      ¦ ¦     Digital Frequency     ¦    ¦    ¦ pilot's or copilot's side provided:   ¦ ¦     Selector/LCD/LED      ¦    ¦    ¦     a) Manual remote tune or dual     ¦ ¦     Display Units         ¦    ¦    ¦        FMS/CDU tune capability        ¦ ¦                           ¦    ¦    ¦        operates normally, and         ¦ ¦                           ¦    ¦    ¦     b) All digital Frequency          ¦ ¦                           ¦    ¦    ¦        Selector/LCD/LED display       ¦ ¦                           ¦    ¦    ¦        units on opposite pilot side   ¦ ¦                           ¦    ¦    ¦        operate normally.              ¦

¦ 39. Compass Transfer    C ¦ -  ¦ 0  ¦ May be inoperative provided compass   ¦ ¦     System                ¦    ¦    ¦ information remains in the normal     ¦ ¦                           ¦    ¦    ¦ (onside) selection.                   ¦

¦ 40. ADI Transfer        C ¦ 2  ¦ 0  ¦ May be inoperative provided:          ¦ ¦     System                ¦    ¦    ¦     a) Pilot and copilot attitude     ¦ ¦                           ¦    ¦    ¦        displays remains connected     ¦ ¦                           ¦    ¦    ¦        to independent sources, and    ¦ ¦                           ¦    ¦    ¦     b) Associated sources operate     ¦ ¦                           ¦    ¦    ¦        normally.                      ¦

¦ 41. Radar Auto          C ¦ 1  ¦ 0  ¦ May be inoperative provided the       ¦ ¦     Inhibit               ¦    ¦    ¦ primary radar indicator operates      ¦ ¦                           ¦    ¦    ¦ normally.                             ¦

¦ 42. Radarnav/Datanav    C ¦ 1  ¦ 0  ¦                                       ¦ ¦     System                ¦    ¦    ¦                                       ¦

¦ 43. Airborne Flight     C ¦ 1  ¦ 0  ¦                                       ¦ ¦     Information System    ¦    ¦    ¦                                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 3        ¦ PAGE:    ¦ ¦                FALCON 200                ¦                       ¦          ¦ ¦                                          ¦ DATE: 03/21/2005      ¦ 34-12    ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 34  NAVIGATION            ¦    ¦    ¦                                       ¦

¦ 44. Traffic Alert       B ¦ -  ¦ 0  ¦ (M)(O)May be inoperative provided:    ¦ ¦ *** and Collision         ¦    ¦    ¦     a) System is deactivated and      ¦ ¦     Avoidance System      ¦    ¦    ¦        secured, and                   ¦ ¦     (TCAS I)              ¦    ¦    ¦     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.                       ¦

¦ *** Traffic Alert       B ¦ -  ¦ 0  ¦ (M)May be inoperative provided:       ¦ ¦     and Collision         ¦    ¦    ¦     a) System is deactivated          ¦ ¦     Avoidance System      ¦    ¦    ¦        and secured, and               ¦ ¦     (TCAS II)             ¦    ¦    ¦     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.                       ¦

¦ *** 1) Combined Traf-   C ¦ 2  ¦ 1  ¦ (O)May be inoperative on the          ¦ ¦        fic Alert (TA)     ¦    ¦    ¦ non-flying pilot side provided:       ¦ ¦        and Resolution     ¦    ¦    ¦     a) TA and RA visual display is    ¦ ¦        Advisory (RA)      ¦    ¦    ¦        operative on the flying        ¦ ¦        Dual Display       ¦    ¦    ¦        pilot side, and                ¦ ¦                           ¦    ¦    ¦     b) TA and RA audio function is    ¦ ¦                           ¦    ¦    ¦        operative on the flying        ¦ ¦                           ¦    ¦    ¦        pilot side.                    ¦

¦                           ¦    ¦    ¦ (Continued)                           ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 3        ¦ PAGE:    ¦ ¦                FALCON 200                ¦                       ¦          ¦ ¦                                          ¦ DATE: 03/21/2005      ¦ 34-13    ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 34  NAVIGATION            ¦    ¦    ¦                                       ¦

¦ 44. Traffic Alert and     ¦    ¦    ¦                                       ¦ ¦ *** Collision Avoidance   ¦    ¦    ¦                                       ¦ ¦     System (TCAS II)      ¦    ¦    ¦                                       ¦ ¦     (Cont'd)              ¦    ¦    ¦                                       ¦

¦     2) Resolution       C ¦ 2  ¦ 1  ¦ (O)One may be inoperative on the      ¦ ¦        Advisory (RA)      ¦    ¦    ¦ non-flying pilot side.                ¦ ¦        Display Systems    ¦    ¦    ¦                                       ¦ ¦                         C ¦ -  ¦ 0  ¦ (O)May be inoperative provided:       ¦ ¦                           ¦    ¦    ¦     a) Traffic Alert (TA) visual    | ¦ ¦                           ¦    ¦    ¦        display and audio functions  | ¦ ¦                           ¦    ¦    ¦        are operative,                 ¦ ¦                           ¦    ¦    ¦     b) TA only mode is selected by    ¦ ¦                           ¦    ¦    ¦        the crew, and                | ¦ ¦                           ¦    ¦    ¦     c) Enroute or approach          | ¦ ¦                           ¦    ¦    ¦        procedures do not require    | ¦ ¦                           ¦    ¦    ¦        its use.                     | ¦

¦     3) Traffic Alert    C ¦ -  ¦ 0  ¦ (O)May be inoperative provided:     | ¦ ¦        Display            ¦    ¦    ¦     a) RA visual display and audio  | ¦ ¦        System(s)          ¦    ¦    ¦        functions are operative, and | ¦ ¦                           ¦    ¦    ¦     b) Enroute or approach          | ¦ ¦                           ¦    ¦    ¦        procedures do not require    | ¦ ¦                           ¦    ¦    ¦        its use.                     | ¦

¦ 45. Windshear             ¦    ¦    ¦ Incorporated into Item 34-7           ¦ ¦ *** Detection and         ¦    ¦    ¦ Revision 2 b.                         ¦ ¦     Guidance Systems      ¦    ¦    ¦                                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 3        ¦ PAGE:    ¦ ¦                FALCON 200                ¦                       ¦          ¦ ¦                                          ¦ DATE: 03/21/2005      ¦ 34-14    ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 34  NAVIGATION            ¦    ¦    ¦                                       ¦

¦ 46. Flight Profile        ¦    ¦    ¦                                       ¦ ¦ *** Advisory System       ¦    ¦    ¦                                       ¦

¦     1) Gear Mode        A ¦ 1  ¦ 0  ¦ (O)May be inoperative provided:       ¦ ¦                           ¦    ¦    ¦     a) Alternate procedures are       ¦ ¦                           ¦    ¦    ¦        established and used, and      ¦ ¦                           ¦    ¦    ¦     b) Repairs are made within        ¦ ¦                           ¦    ¦    ¦        two flight days.               ¦

¦     2) Minimums Mode    A ¦ 1  ¦ 0  ¦ (O)May be inoperative provided:       ¦ ¦                           ¦    ¦    ¦     a) Alternate procedures are       ¦ ¦                           ¦    ¦    ¦        established and used, and      ¦ ¦                           ¦    ¦    ¦     b) Repairs are made within        ¦ ¦                           ¦    ¦    ¦        two flight days.               ¦

¦     3) Radio Altitude   A ¦ 1  ¦ 0  ¦ (O)May be inoperative provided:       ¦ ¦        Mode               ¦    ¦    ¦     a) Alternate procedures are       ¦ ¦                           ¦    ¦    ¦        established and used, and      ¦ ¦                           ¦    ¦    ¦     b) Repairs are made with          ¦ ¦                           ¦    ¦    ¦        two flight days.               ¦

¦     4) Test Mode        A ¦ 1  ¦ 0  ¦ May be inoperative provided:          ¦ ¦                           ¦    ¦    ¦     a) The FPA is considered          ¦ ¦                           ¦    ¦    ¦        inoperative, and               ¦ ¦                           ¦    ¦    ¦     b) Repairs are made within        ¦ ¦                           ¦    ¦    ¦        two flight days.               ¦

¦     5) Glideslope       B ¦ 1  ¦ 0  ¦                                       ¦ ¦        Deviation Mode     ¦    ¦    ¦                                       ¦

¦     6) Advisory         C ¦ -  ¦ 0  ¦ (O)May be inoperative provided        ¦ ¦        Callouts           ¦    ¦    ¦ alternate procedures are              ¦ ¦                           ¦    ¦    ¦ established and used.                 ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 2        ¦ PAGE:    ¦ ¦                FALCON 200                ¦                       ¦          ¦ ¦                                          ¦ DATE: 10/12/1993      ¦ 35-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 35  OXYGEN                ¦    ¦    ¦                                       ¦

¦ 1.  Passenger Oxygen    C ¦ -  ¦ 0  ¦ As required by FAR.                   ¦ ¦     System                ¦    ¦    ¦                                       ¦ ¦     35-20-00              ¦    ¦    ¦                                       ¦

¦ 2.  First Aid Oxygen    C ¦ -  ¦ -  ¦ As required by FAR.                   ¦

¦ 3.  Portable Oxygen     D ¦ -  ¦ -  ¦ Any in excess of those required by    ¦ ¦     System                ¦    ¦    ¦ FAR may be inoperative.               ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 2        ¦ PAGE:    ¦ ¦                FALCON 200                ¦                       ¦          ¦ ¦                                          ¦ DATE: 10/12/1993      ¦ 36-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 36  PNEUMATIC             ¦    ¦    ¦                                       ¦

¦ 1.  HP Bleed Valves     C ¦ 2  ¦ 1  ¦ (M)One may be inoperative CLOSED.     ¦ ¦     (PRV)                 ¦    ¦    ¦                                       ¦

¦ 2.  Bleed Valves (LP)   C ¦ 2  ¦ 1  ¦ (O)One may be inoperative CLOSED      ¦ ¦                           ¦    ¦    ¦ provided flight remains at or         ¦ ¦                           ¦    ¦    ¦ below FL 250.                         ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 2        ¦ PAGE:    ¦ ¦                FALCON 200                ¦                       ¦          ¦ ¦                                          ¦ DATE: 10/12/1993      ¦ 49-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 49  AIRBORNE AUXILIARY    ¦    ¦    ¦                                       ¦ ¦     POWER                 ¦    ¦    ¦                                       ¦

¦ 1.  Auxiliary Power     C ¦ 1  ¦ 0  ¦ May be inoperative provided           ¦ ¦     Unit                  ¦    ¦    ¦ procedures do not require its use.    ¦ ¦     49-10-00              ¦    ¦    ¦                                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 2        ¦ PAGE:    ¦ ¦                FALCON 200                ¦                       ¦          ¦ ¦                                          ¦ DATE: 10/12/1993      ¦ 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 Flowmeters     B ¦ 2  ¦ 1  ¦ One may be inoperative provided:      ¦ ¦     73-30-10              ¦    ¦    ¦     a) All other engine instruments   ¦ ¦                           ¦    ¦    ¦        for the associated engine      ¦ ¦                           ¦    ¦    ¦        operate normally, and          ¦ ¦                           ¦    ¦    ¦     b) All fuel quantity gauges       ¦ ¦                           ¦    ¦    ¦        operate normally.              ¦

¦ 2.  Engine Synchroni-   C ¦ 1  ¦ 0  ¦ (M)May be inoperative provided it     ¦ ¦     zation System         ¦    ¦    ¦ is deactivated and secured.           ¦ ¦     77-30-10              ¦    ¦    ¦                                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 2        ¦ PAGE:    ¦ ¦                FALCON 200                ¦                       ¦          ¦ ¦                                          ¦ DATE: 10/12/1993      ¦ 74-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 74  IGNITION              ¦    ¦    ¦                                       ¦

¦ 1.  Igniter Indicator   C ¦ 2  ¦ 1  ¦ (M)One may be inoperative provided    ¦ ¦     Lights                ¦    ¦    ¦ all modes of the associated           ¦ ¦     74-20-10              ¦    ¦    ¦ ignition system operate normally.     ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 2        ¦ PAGE:    ¦ ¦                FALCON 200                ¦                       ¦          ¦ ¦                                          ¦ DATE: 10/12/1993      ¦ 77-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 77  ENGINE INDICATING     ¦    ¦    ¦                                       ¦

¦ 1.  N1 Indicators         ¦    ¦    ¦                                       ¦ ¦     77-10-10              ¦    ¦    ¦                                       ¦

¦     1) Digital          C ¦ 2  ¦ 0  ¦                                       ¦ ¦        Readout(s)         ¦    ¦    ¦                                       ¦

¦ 2.  ITT Indicators        ¦    ¦    ¦                                       ¦ ¦     77-20-10              ¦    ¦    ¦                                       ¦

¦     1) Digital          C ¦ 2  ¦ 0  ¦                                       ¦ ¦        Readout(s)         ¦    ¦    ¦                                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 2        ¦ PAGE:    ¦ ¦                FALCON 200                ¦                       ¦          ¦ ¦                                          ¦ DATE: 10/12/1993      ¦ 78-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 78  ENGINE EXHAUST        ¦    ¦    ¦                                       ¦

¦ 1.  Thrust Reversers    C ¦ 2  ¦ 0  ¦ (M)(O)May be inoperative provided:    ¦ ¦     78-30-00              ¦    ¦    ¦     a) No damage to the thrust        ¦ ¦                           ¦    ¦    ¦        reverser system exists which   ¦ ¦                           ¦    ¦    ¦        would adversely affect         ¦ ¦                           ¦    ¦    ¦        operation of the airplane,     ¦ ¦                           ¦    ¦    ¦        and                            ¦ ¦                           ¦    ¦    ¦     b) A procedure is established     ¦ ¦                           ¦    ¦    ¦        and used to determine that     ¦ ¦                           ¦    ¦    ¦        the associated thrust          ¦ ¦                           ¦    ¦    ¦        reverser is locked in the      ¦ ¦                           ¦    ¦    ¦        closed (forward thrust)        ¦ ¦                           ¦    ¦    ¦        position by use of the         ¦ ¦                           ¦    ¦    ¦        safety pin.                    ¦

¦ 2.  Thrust Reverser     C ¦ 2  ¦ 0  ¦ (M)May be inoperative provided:       ¦ ¦     Indicating Light      ¦    ¦    ¦     a) It is verified that the        ¦ ¦     Systems               ¦    ¦    ¦        fault is in the indicating     ¦ ¦                           ¦    ¦    ¦        system only, and               ¦ ¦                           ¦    ¦    ¦     b) Reverser is deactivated and    ¦ ¦                           ¦    ¦    ¦        secured in the stowed          ¦ ¦                           ¦    ¦    ¦        position by use of the         ¦ ¦                           ¦    ¦    ¦        safety pins.                   ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 2        ¦ PAGE:    ¦ ¦                FALCON 200                ¦                       ¦          ¦ ¦                                          ¦ DATE: 10/12/1993      ¦ 79-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 79  ENGINE OIL            ¦    ¦    ¦                                       ¦

¦ 1.  Oil Pressure        C ¦ 2  ¦ 1  ¦ (M)(O)One may be inoperative          ¦ ¦     Warning Lights        ¦    ¦    ¦ provided:                             ¦ ¦     79-30-00              ¦    ¦    ¦     a) Malfunction is in the          ¦ ¦                           ¦    ¦    ¦        warning system,                ¦ ¦                           ¦    ¦    ¦     b) Oil pressure and oil temp-     ¦ ¦                           ¦    ¦    ¦        erature indicators are         ¦ ¦                           ¦    ¦    ¦        monitored closely during       ¦ ¦                           ¦    ¦    ¦        flight, and                    ¦ ¦                           ¦    ¦    ¦     c) A light that remains           ¦ ¦                           ¦    ¦    ¦        illuminated must be            ¦ ¦                           ¦    ¦    ¦        deactivated.                   ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 2        ¦ PAGE:    ¦ ¦                FALCON 200                ¦                       ¦          ¦ ¦                                          ¦ DATE: 10/12/1993      ¦ 80-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 80  STARTING              ¦    ¦    ¦                                       ¦

¦ 1.  Automatic Starter   C ¦ 2  ¦ 0  ¦ May be inoperative provided starter   ¦ ¦     Cutouts               ¦    ¦    ¦ is disengaged manually at 50% N1      ¦ ¦     80-10-00              ¦    ¦    ¦ during start.                         ¦