Date: 03/31/2003

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

BEECH MODEL 1900/1900C SERIES

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT EVALUATION GROUP

1201 E WALNUT ST, SUITE 900

KANSAS CITY, MO   64106

TELEPHONE:  (816) 426-3946

FAX:        (816) 426-3084

DEPARTMENT OF TRANSPORTATION     Revision: 10

  Revision: 10

MASTER MINIMUM EQUIPMENT LIST      Date: 03/31/2003

BEECH MODEL 1900/1900C SERIES

Table of Contents

SYSTEM NO.  SYSTEM                                  PAGE

--     Table of Contents                       I

--     Log of Revisions                        II, III

--     Control Page                            IV, V

--     Highlights of Change                    VI, VII, VIII

--     Definitions                             IX, X, XI, XII

--     Definitions                             XIII, XIV, XV, XVI --     Preamble                                XVII, XVIII

--     Guidelines for (O) & (M) Procedures     XIX, XX, XXI, XXII --     Guidelines for (O) & (M) Procedures     XXIII, XXIV, XXV 21     Air Conditioning                        21-1, 2, 3

22     Auto Flight                             22-1

23     Communications                          23-1, 2, 3, 4

24     Electrical Power                        24-1, 2

25     Equipment/Furnishings                   25-1, 2, 3

26     Fire Protection                         26-1, 2

27     Flight Controls                         27-1

28     Fuel                                    28-1, 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

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

34     Navigation                              34-11  THRU 12 35     Oxygen                                  35-1

37     Vacuum/Pressure                         37-1 38     Water/Waste                             38-1 52     Doors                                   52-1 61     Propellers                              61-1 79     Engine Oil                              79-1

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Log of Revisions

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

¦ ORIGINAL ¦ 12/23/1983 ¦ N/A                            ¦           ¦ ¦ 1        ¦ 10/10/1985 ¦ All Pages                      ¦           ¦ ¦ 2        ¦ 08/11/1986 ¦ III, 52-1                      ¦           ¦ ¦ 3        ¦ 11/06/1986 ¦ 52-1                           ¦           ¦ ¦ 4        ¦ 07/12/1988 ¦ 23-1                           ¦           ¦ ¦ 5        ¦ 03/01/1989 ¦ All Pages                      ¦           ¦ ¦ 6        ¦ 06/19/1989 ¦ Definitions, Preamble          ¦           ¦ ¦ 7        ¦ 04/11/1991 ¦ HIGHLIGHTS OF REV.,DEFINITIONS ¦           ¦ ¦ 7        ¦ 04/11/1991 ¦ PREAMBLE,GUIDELINES            ¦           ¦ ¦ 7        ¦ 04/11/1991 ¦ 21-1,21-2,21-3,22-1,23-1       ¦           ¦ ¦ 7        ¦ 04/11/1991 ¦ 23-2,24-1,24-2,25-1,25-2       ¦           ¦ ¦ 7        ¦ 04/11/1991 ¦ 27-1,27-2,28-1,28-2,30-1       ¦           ¦ ¦ 7        ¦ 04/11/1991 ¦ 30-2,30-3,31-1,32-1,32-2       ¦           ¦ ¦ 7        ¦ 04/11/1991 ¦ 33-1,33-2,33-3,34-1,34-2       ¦           ¦ ¦ 7        ¦ 04/11/1991 ¦ 34-3,35-1,37-1,52-1,52-2       ¦           ¦ ¦ 7        ¦ 04/11/1991 ¦ 56-1,61-1,77-1                 ¦           ¦ ¦ 8        ¦ 12/05/1991 ¦ HIGHLIGHTS OF REV.,GUIDELINES  ¦           ¦ ¦ 8        ¦ 12/05/1991 ¦ 21-1,21-2,21-3,22-1,23-1       ¦           ¦ ¦ 8        ¦ 12/05/1991 ¦ 23-2,24-1,24-2                 ¦           ¦ ¦ 8        ¦ 12/05/1991 ¦ 27-1,27-2,28-1,28-2            ¦           ¦ ¦ 8        ¦ 12/05/1991 ¦ 31-1,32-1,32-2                 ¦           ¦ ¦ 8        ¦ 12/05/1991 ¦ 33-1,33-2,33-3,34-1,34-2       ¦           ¦ ¦ 8        ¦ 12/05/1991 ¦ 34-3,34-4,37-1                 ¦           ¦ ¦ 8a       ¦ 02/14/1992 ¦ HIGHLIGHTS OF REV.             ¦           ¦ ¦ 8a       ¦ 02/14/1992 ¦ 23-1,23-2,23-3                 ¦           ¦ ¦ 9        ¦ 03/02/1992 ¦ HIGHLIGHTS OF REV.             ¦           ¦ ¦ 9        ¦ 03/02/1992 ¦ 32-1,32-2                      ¦           ¦ ¦ 9a       ¦ 07/23/1993 ¦ HIGHLIGHTS OF REV.,DEFINITIONS ¦           ¦ ¦ 9a       ¦ 07/23/1993 ¦ 21-1,21-2,21-3,22-1,23-1       ¦           ¦ ¦ 9a       ¦ 07/23/1993 ¦ 23-2,23-3,24-1,24-2,25-1       ¦           ¦ ¦ 9a       ¦ 07/23/1993 ¦ 25-2,27-1,27-2,28-1,28-2       ¦           ¦ ¦ 9a       ¦ 07/23/1993 ¦ 28-3,30-1,30-2,30-3,31-1       ¦           ¦ ¦ 9a       ¦ 07/23/1993 ¦ 32-1,32-2,33-1,33-2,33-3       ¦           ¦ ¦ 9a       ¦ 07/23/1993 ¦ 34-1,34-2,34-3,34-4,34-5       ¦           ¦ ¦ 9a       ¦ 07/23/1993 ¦ 34-6,35-1,37-1,52-1,52-2       ¦           ¦ ¦ 9a       ¦ 07/23/1993 ¦ 61-1,79-1                      ¦           ¦ ¦ 9b       ¦ 12/09/1993 ¦ HIGHLIGHTS OF REV.,GUIDELINES  ¦           ¦ ¦ 9b       ¦ 12/09/1993 ¦ 34-1,34-2,34-3,34-4,34-5       ¦           ¦ ¦ 9b       ¦ 12/09/1993 ¦ 34-6                           ¦           ¦ ¦ 9c       ¦ 05/23/1995 ¦ HIGHLIGHTS OF REV.,DEFINITIONS ¦           ¦ ¦ 9c       ¦ 05/23/1995 ¦ GUIDELINES                     ¦           ¦ ¦ 9c       ¦ 05/23/1995 ¦ 21-1,21-2,21-3,22-1,23-1       ¦           ¦ ¦ 9c       ¦ 05/23/1995 ¦ 23-2,23-3,24-1,24-2,25-1       ¦           ¦

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MASTER MINIMUM EQUIPMENT LIST    Date: 03/31/2003

BEECH MODEL 1900/1900C SERIES

Log of Revisions

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

¦ 9c       ¦ 05/23/1995 ¦ 25-2,26-1,27-1,27-2,28-1       ¦           ¦ ¦ 9c       ¦ 05/23/1995 ¦ 28-2,28-3,30-1,30-2,30-3       ¦           ¦ ¦ 9c       ¦ 05/23/1995 ¦ 31-1,32-1,32-2,33-1,33-2       ¦           ¦ ¦ 9c       ¦ 05/23/1995 ¦ 33-3,34-1,34-2,34-3,34-4       ¦           ¦ ¦ 9c       ¦ 05/23/1995 ¦ 34-5,34-6,35-1,37-1,52-1       ¦           ¦ ¦ 9c       ¦ 05/23/1995 ¦ 52-2,61-1,79-1                 ¦           ¦ ¦ 9d       ¦ 12/08/1995 ¦ HIGHLIGHTS OF REV.,DEFINITIONS ¦           ¦ ¦ 9d       ¦ 12/08/1995 ¦ GUIDELINES                     ¦           ¦ ¦ 9d       ¦ 12/08/1995 ¦ 34-3                           ¦           ¦ ¦ 9e       ¦ 02/15/1996 ¦ HIGHLIGHTS OF REV.,DEFINITIONS ¦           ¦ ¦ 9e       ¦ 02/15/1996 ¦ 23-1,23-2,23-3                 ¦           ¦ ¦ 9f       ¦ 10/23/1996 ¦ HIGHLIGHTS OF REV.,DEFINITIONS ¦           ¦ ¦ 9f       ¦ 10/23/1996 ¦ 33-1,33-2,33-3                 ¦           ¦ ¦ 10       ¦ 03/31/2003 ¦ HIGHLIGHTS OF REV.,DEFINITIONS ¦           ¦ ¦ 10       ¦ 03/31/2003 ¦ GUIDELINES                     ¦           ¦ ¦ 10       ¦ 03/31/2003 ¦ 21-1,21-2,21-3,22-1,23-1       ¦           ¦ ¦ 10       ¦ 03/31/2003 ¦ 23-2,23-3,23-4,24-1,24-2       ¦           ¦ ¦ 10       ¦ 03/31/2003 ¦ 25-1,25-2,25-3,26-1,26-2       ¦           ¦ ¦ 10       ¦ 03/31/2003 ¦ 27-1,28-1,28-2,30-1,30-2       ¦           ¦ ¦ 10       ¦ 03/31/2003 ¦ 30-3,31-1,31-2,32-1,32-2       ¦           ¦ ¦ 10       ¦ 03/31/2003 ¦ 33-1,33-2,33-3,34-1,34-2       ¦           ¦ ¦ 10       ¦ 03/31/2003 ¦ 34-3,34-4,34-5,34-6,34-7       ¦           ¦ ¦ 10       ¦ 03/31/2003 ¦ 34-8,34-9,34-10,34-11,34-12    ¦           ¦ ¦ 10       ¦ 03/31/2003 ¦ 35-1,37-1,38-1,52-1,61-1       ¦           ¦ ¦ 10       ¦ 03/31/2003 ¦ 79-1                           ¦           ¦

FEDERAL AVIATION ADMINISTRATION   Page: III

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Control Page

SYSTEM                                   PAGE  REV NO.  CURRENT DATE

Cover Page                               -       10       03/31/2003 Table of Contents                        I       10       03/31/2003 Log of Revisions                         II      10       03/31/2003 III     10       03/31/2003 Control Page                             IV      10       03/31/2003 V       10       03/31/2003 Highlights of Change                     VI      10       03/31/2003 VII     10       03/31/2003 VIII    10       03/31/2003 Definitions                                    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 XV      6        01/31/1995 XVI     6        01/31/1995 Preamble                                         XVII    2        06/14/1989 XVIII   2        06/14/1989 Guidelines for (O) & (M) Procedures      XIX     10       03/31/2003 XX      10       03/31/2003 XXI     10       03/31/2003 XXII    10       03/31/2003 XXIII   10       03/31/2003 XXIV    10       03/31/2003 XXV     10       03/31/2003 21                                               21-1    10       03/31/2003 21-2    10       03/31/2003 21-3    10       03/31/2003 22                                       22-1    10       03/31/2003 23                                        23-1    10       03/31/2003 23-2    10       03/31/2003 23-3    10       03/31/2003 23-4    10       03/31/2003 24                                       24-1    10       03/31/2003 24-2    10       03/31/2003 25                                       25-1    10               03/31/2003 25-2    10       03/31/2003 25-3    10       03/31/2003 26                                       26-1    10                                                                 03/31/2003

FEDERAL AVIATION ADMINISTRATION     Page: IV

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Control Page

SYSTEM                                   PAGE  REV NO.  CURRENT DATE

                                         26-2    10       03/31/2003 27                                       27-1    10       03/31/2003 28                                       28-1    10       03/31/2003 28-2    10       03/31/2003 30                                       30-1    10       03/31/2003 30-2    10       03/31/2003 31                                       31-1    10       03/31/2003 31-2    10       03/31/2003 32                                       32-1    10       03/31/2003 32-2    10       03/31/2003 33                                       33-1    10       03/31/2003 33-2    10       03/31/2003 34                                       34-1    10       03/31/2003 34-2    10       03/31/2003 34-3    10       03/31/2003 34-4    10       03/31/2003 34-5    10       03/31/2003 34-6    10       03/31/2003 34-7    10       03/31/2003 34-8    10       03/31/2003 34-9    10       03/31/2003 34-10   10       03/31/2003 34-11   10       03/31/2003 34-12   10       03/31/2003 35                                       35-1    10       03/31/2003 37                                       37-1    10       03/31/2003 38                                       38-1    10       03/31/2003 52                                       52-1    10       03/31/2003 61                                       61-1    10       03/31/2003 79                                       79-1    10       03/31/2003

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  89.

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Highlights of Change

Removed the word "OR" from Column 4 (Remarks or Exceptions) in accordance with Policy Letter 31 designated as Global Change 83.

22-1  Revised Autopilot relief in accordance with Policy Letter 101 designated as Global Change 103.

22-3  Added Autopilot Disconnect relief in accordance with Policy Letter 93.

23-1  Revised Passenger Address relief in accordance with Policy Letter 9 designated as Global Change 109.

23-4  Revised communications relief in accordance with Policy Letter       95 designated as Global Change 111. (HF moved to 23-12)

23-6  Revised Cockpit Voice Recorder (CVR) relief in accordance with           Policy Letter 29 designated as Global Change 48.

23-12 Added relief for High Frequency (HF) Communication System in

accordance with Policy Letter 106 designated as Global Change 89.

25-3  Revised Passenger Seat relief in accordance with Policy Letter                  79 designated as Global Change 96.

25-7  Renamed to Emergency Medical Equipment and revised in accordance         with Policy Letter 73 designated as Global Change 104.

25-9  Revised Seat Belt sign relief in accordance with Policy Letter

26-2  Added Lavatory Fire Extinguisher relief in accordance with        Policy Letter 24 designated as Global Change 106.

26-3  Added Lavatory Smoke Detector relief in accordance with       Policy Letter 24 designated as Global Change 106.

26-4  Added Cargo Compartment Fire Detection/Suppression System relief       in accordance with Policy Letter 102 designated as Global

Change 77.

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BEECH MODEL 1900/1900C SERIES

Highlights of Change

31-3  Revised Flight Data Recorder (FDR) relief in accordance with                         Policy Letter 87.

31-5  Added Aircraft Data Acquisition System (ADAS) relief.

33-4  No Smoking/Fasten Seat Belt sign moved to 25-9.

33-12 Revised Wing Illumination Light relief in accordance with        Policy Letter 72 designated as Global Change 54.

34-5  Revised Magnetic Compass System relief in accordance with Policy                               Letter 10

34-7  Revised Transponder/Altitude Reporting relief in accordance with           Policy Letter 76 designated as Global Change 110.

34-9  Altitude Encoder relief combined with 34-7 in accordance with          Policy Letter 76 designated as Global Change 110.

34-10 Revised Distance Measuring Equipment (DME) System relief in                 accordance with Policy Letter 3.

34-14 Revised Altitude Alert System relief in accordance with       Policy Letter 39 designated as Global Change 95.

34-16 Revised TCAS I relief in accordance with Policy Letter 32                designated as Global Change 115.

34-17 Revised TCAS II relief in accordance with Policy Letter 32                 designated as Global Change 115.

34-18 Revised Standby Attitude Indicator relief in accordance with         Policy Letter 111 designated as Global Change 113.

34-20 Revised GPWS relief in accordance with Policy Letter 54               designated as Global Change 107.

34-22 Added Windshear Warning and Flight Guidance System relief in

accordance with Policy Letter 67 designated as Global Change 88.

34-23 Added Windshear Detection and Avoidance System relief in

accordance with Policy Letter 67 designated as Global Change 88.

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Highlights of Change

34-24 Added Flight Management System Navigation Database relief in

accordance with Policy Letter 98 designated as Global Change 71.

34-25 Added Navigation Management System Navigation Database in

accordance with Policy Letter 98 designated as Global Change 71.

34-26 Added Automatic Dependent Surveillance-Broadcast (ADS-B) System   relief in accordance with Policy Letter 105 designated as Global                              Change 86.

35-4  Added Protective Breathing Equipment (PBE) relief in accordance                        with Policy Letter 43.

38-1  Added Potable Water relief in accordance with Policy Letter 83                   designated as Global Change 108.

38-2  Added Lavatory Waste System relief in accordance with Policy             Letter 83 designated as Global Change 108.

52-4  Added Operations procedure to Guidelines for (O) & (M)                       procedures page.

  Revision: 6

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BEECH MODEL 1900/1900C SERIES

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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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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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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BEECH MODEL 1900/1900C SERIES

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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Definitions

record/logbook.  For example, if it were recorded at 10 a.m. on January 26th, the three day interval would begin at midnight the 26th and end at midnight the 29th.

     Category C.  Items in this category shall be repaired within ten (10) consecutive calendar days (240 hours), excluding the day the malfunction was recorded in the aircraft maintenance record/logbook.  For example, if it were recorded at 10 a.m. on January 26th, the 10 day interval would begin at midnight the 26th and end at midnight February 5th.

     Category D.  Items in this category shall be repaired within one hundred and twenty (120) consecutive calendar days (2880 hours), excluding the day the malfunction was recorded in the aircraft maintenance log and/or record.

The letter designators are inserted adjacent to Column 2.

23. Electronic fault alerting system - General                  ¦

New generation aircraft display system fault indications to the ¦ flight crew by use of computerized display systems.  Each       ¦ aircraft manufacturer has incorporated individual design        ¦ philosophies in determining the data that would be              ¦ represented.  The following are customized definitions (specific¦ to each manufacturer) to help determine the level of messages   ¦ affecting the aircraft's dispatch status.  When preparing the   ¦ MEL document, operators are to select the proper Definition No. ¦ 23 for their aircraft, if appropriate.                          ¦

a.   BOEING  (B-757/767, B-747-400, B-777)                      ¦

Boeing airplanes equipped with Engine Indicating and Crew       ¦ Alerting  Systems (EICAS), provide different priority levels of ¦ system messages (WARNING,  CAUTION, ADVISORY, STATUS and        ¦ MAINTENANCE).  Any messages that affects airplane dispatch      ¦ status will be displayed at a STATUS message level or  higher.  ¦ The absence of an EICAS STATUS or higher level (WARNING,        ¦ CAUTION, ADVISORY) indicates that the system/component is       ¦ operating within its approved operating limits or tolerances.   ¦

System conditions that result only in a maintenance level       ¦ message, i.e. no correlation with a higher level EICAS message, ¦

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MASTER MINIMUM EQUIPMENT LIST      Date: 01/31/1995

BEECH MODEL 1900/1900C SERIES

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

FEDERAL AVIATION ADMINISTRATION     Page: XV

  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: 06/14/1989

BEECH MODEL 1900/1900C SERIES

Preamble

(Effective 6/14/89)

The following is applicable for authorized certificate holders operating under Federal Aviation Regulations (FAR) Parts 121, 125, 129, 135: The FAR require that all equipment installed on an aircraft in compliance with the Airworthiness Standards and the Operating Rules must be operative.  However, the Rules also permit the publication of a Minimum Equipment List (MEL) where compliance with certain equipment requirements is not necessary in the interests of safety under all operating conditions.  Experience has shown that with the various levels of redundancy designed into aircraft, operation of every system or installed component may not be necessary when the remaining operative equipment can provide an acceptable level of safety.  A Master Minimum Equipment List (MMEL) is developed by the FAA, with participation by the aviation industry, to improve aircraft utilization and thereby provide more convenient and economic air transportation for the public.  The FAA approved MMEL includes those items of equipment related to airworthiness and operating regulations and other items of equipment which the Administrator finds may be inoperative and yet maintain an acceptable level of safety by appropriate conditions and limitations;  it does not contain obviously required items such as wings, flaps, and rudders.  The MMEL is the basis for development of individual operator MELs which take into consideration the operator's particular aircraft equipment configuration and operational conditions. Operator MELs, for administrative control, may include items not contained in the

MMEL;  however, relief for administrative control items must be approved by the Administrator.  An operator's MEL may differ in format from the MMEL, but cannot be less restrictive than the MMEL. The individual operator's MEL, when approved and authorized, permits operation of the aircraft with inoperative equipment.

Equipment not required by the operation being conducted and equipment in excess of FAR requirements are included in the MEL with appropriate conditions and limitations.  The MEL must not deviate from the Aircraft Flight Manual Limitations, Emergency Procedures or with Airworthiness Directives.  It is important to remember that all equipment related to the airworthiness and the operating regulations of the aircraft not listed on the MMEL must be operative.

 

FEDERAL AVIATION ADMINISTRATION   Page: XVIII Revision: 2 MASTER MINIMUM EQUIPMENT LIST    Date: 06/14/1989

BEECH MODEL 1900/1900C SERIES

Preamble

(Effective 6/14/89)

Suitable conditions and limitations in the form of placards, maintenance procedures, crew operating procedures and other restrictions as necessary are specified in the MEL to ensure that an acceptable level of safety is maintained.

The MEL is intended to permit operation with inoperative items of equipment for a period of time until repairs can be accomplished.  It is important that repairs be accomplished at the earliest opportunity.  In order to maintain an acceptable level of safety and reliability the MMEL establishes limitations on the duration of and conditions for operation with inoperative equipment.  The MEL provides for release of the aircraft for flight with inoperative equipment.  When an item of equipment is discovered to be inoperative, it is reported by making an entry in the Aircraft Maintenance Record/Logbook as prescribed by FAR. The item is then either repaired or may be deferred per the MEL or other approved means acceptable to the Administrator prior to further operation.  MEL conditions and limitations, do not relieve the operator from determining that the aircraft is in condition for safe operation with items of equipment inoperative.

When these requirements are met, an Airworthiness Release, Aircraft Maintenance Record/Logbook entry, or other approved documentation is issued as prescribed by FAR.  Such documentation is required prior to operation with any item of equipment inoperative.

Operators are responsible for exercising the necessary operational control to ensure that an acceptable level of safety is maintained. When operating with multiple inoperative items, the interrelationships between those items and the effect on aircraft operation and crew workload will be considered.

Operators are to establish a controlled and sound repair program including the parts, personnel, facilities, procedures, and schedules to ensure timely repair.

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

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Guidelines for (O) & (M) Procedures

The FOEB has identified a need for certain procedures to provide an adequate level of safety while providing relief for the following items.  These procedures must be established by the operator.  The following guidelines are to help establish these required procedures:

21-3  (O)Operations procedure to verify environmental bleed air and instrument air valves on inoperative side are closed prior to each flight.

(O)Operations procedure to verify environmental bleed air and instrument air valves on inoperative side are closed prior to each flight.

21-4  (O)Operations procedure to verify environmental bleed air valve air valve is closed prior to every flight.

21-8  (M)Maintenance procedure for securing outflow/safety valve open.

21-10 (M)Maintenance procedure for securing outflow/safety valve open.

21-16 (O)Operations procedure to verify inoperative environmental bleed air valve is closed prior to each flight.

21-17 (O)Operations procedure to verify inoperative environmental bleed air valve is closed prior to each flight.

22-1  (M)Maintenance procedure to disable the autopilot and determine that the servos do not cause binding of the control cables.

22-2  (M)Maintenance procedure to disable the yaw damper and determine that the rudder servo does not cause binding of the control cables.

23-1  (O)Operations procedure to specify how passengers will be briefed.

23-2  (O)Operations procedure to specify how passengers will be briefed.

23-12 (O)Operations procedure to ensure SATCOM Data Link System operates normally.

FEDERAL AVIATION ADMINISTRATION   Page XIX

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Guidelines for (O) & (M) Procedures

24-1  (M)Maintenance procedure to determine the inoperative condition is not caused by broken wire or short which could cause a fire.

24-3  (O)Operations procedure to ensure the electrical load is less than 50% on the operative side generator prior to take-off and at all times during flight and that loads are not added if the generator on the operative side fails.

24-6  (M)Maintenance procedure to ensure ground power relay is open.

24-7  (O)Operations procedure to ensure connection/disconnection of power cart is verified.

24-11 (O)Operations procedure to verify generator tie relay is closed.

25-3-2(O)Operations procedure to placard the affected seat and ensure baggage is not stored under the affected seat.

25-5  (M)Maintenance procedure to disconnect the remote switch from ELT and manually arm the ELT per manufacturer instructions.  Care must be exercised to insure the G-Switch is NOT disabled.

25-9  (O)Operations procedure to brief the passengers.

26-2  (M)Maintenance procedure to lock and placard Lavatory Door.

(O)Operations procedure to ensure Lavatory Waste Receptacle is empty and lavatory used only by crew members.

26-3  (M)Maintenance procedure to lock and placard Lavatory Door.

(O)Operations procedure to ensure Lavatory Waste Receptacle is empty and lavatory used only by crew members.

27-2  (O)Operations procedure to verify the flaps are secure and in the up position and the circuit breaker is pulled.

27-4  (M)Maintenance procedure to determine servos do not cause binding of trim cables.

FEDERAL AVIATION ADMINISTRATION   Page XX

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Guidelines for (O) & (M) Procedures

28-2  (M)Maintenance procedure to determine failure will not cause damage to engine or restriction in fuel flow.

28-3  (O)Operations procedure to ensure fuel quantity meets regulatory

requirements for the flight.  (A reliable means for determining fuel quantity is to fill fuel tanks and calculate fuel burn from full tanks and to operate within AFM limitations).

28-5  (O)Operations procedure to verify standby fuel pumps are operating.

28-6  (M)Maintenance procedure to determine inoperative condition is not caused by leaks or broken fuel lines.

28-7  (M)Maintenance procedure to deactivate the pump and ensure no electrical power is supplied to it.

30-3  (M)Maintenance procedure to determine inoperative motor does not affect other actuator motor.

(M)Maintenance procedure to establish a method of securing vanes in the extended position

30-4  (O)Operations procedure for flight crewmember to verify operation of vanes prior to each departure.

(M)Maintenance procedure to secure vanes in extended position.

30-12 (M)Maintenance procedure to secure shutoff valves in the closed position.

31-2  (O)Operations procedure for recording aircraft time for maintenance purposes.

31-4  (O)Operations procedure to ensure preflight procedures are accomplished in accordance with Beechcraft directive.

FEDERAL AVIATION ADMINISTRATION   Page XXI

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Guidelines for (O) & (M) Procedures

32-3  (M)Maintenance procedure to ensure nose wheel is in the free castor mode.

(O)Operations procedure to operate within AFM restrictions.

32-5  (O)Operations procedure to advise crew that nose steering is in the free castor mode.

(M)Maintenance procedure to disable and band circuit breaker.

32-6  (O)Operations procedure to ensure flight crew is aware of change in nose wheel steering.

(M)Maintenance procedure to disconnect and secure actuator.

32-9  (O)Operation procedure to secure aircraft during ground

emergencies and prior to releasing toe brakes during normal operations.

32-10 (O)Operation procedure to advise flight crew of the requirement to manually move down lock latch.

34-4  (O)Operation procedure to advise flight crew of the need to regularly check/reset directional gyro.

34-5  (O)Operation procedure to ensure a minimum of three compass systems are operational.

(O)Operation procedure to ensure aircraft is operated with dual independent navigation capability.

(O)Operation procedure to ensure at least two stabilized    directional gyros are installed and operate normally.

34-14 (O)Operations procedure to ensure Autopilot and Altitude Hold                                                       is operative.

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Guidelines for (O) & (M) Procedures

34-16   (M)Maintenance procedure to deactivate and secure the system.

(O)Operation procedure to ensure enroute or approach procedures                                         do not require its use.

(M)Maintenance procedure to deactivate and secure the system.

(O)Operation procedure to ensure enroute or approach procedures                                         do not require its use.

34-17    (M)Maintenance procedure to ensure system is deactivated and                                                              secured.

(O)Operations procedure to ensure enroute and approach                     procedures do not require its use.

(M)Maintenance procedure to ensure system is deactivated and                                                     secured.

(O)Operations procedure to ensure enroute and approach

procedures do not require its use and  not require by FAR.

34-17-1  (O)Operations procedure to ensure TA and RA visual and audio                     functions are operative on the flying pilot side.

34-17-2  (O)Operations procedure to ensure TA and RA visual and audio    functions are operative on the flying pilot side, TA only mode is                         selected, and enroute and approach procedures

do not require its use.

34-17-3  (O)Operations procedure to ensure RA visual and audio functions are operative, and enroute and approach procedures                                        do not require its use.

34-19-1  (O)Operations procedure to ensure alternate procedures are                                 established and used for Gear mode.

34-19-2  (O)Operations procedure to ensure alternate procedures are                             established and used for Minimums mode.

34-19-3  (O)Operations procedure to ensure alternate procedures are                       established and used for Radio Altitude mode.

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Guidelines for (O) & (M) Procedures

34-20  (O)Operations procedure to ensure alternate procedures are                                             established and used.

(O)Operations procedure to ensure alternate procedures are                                      established and used.

34-20-1(O)Operations procedure to ensure alternate procedures are            established and used for appropriate inoperative mode.

34-20-4(O)Operations procedure to ensure alternate procedures are                  established and used for inoperative callout(s).

34-20-5(O)Operations procedure to ensure alternate procedures are              established and used for inoperative windshear mode.

34-22  (O)Operations procedure to ensure alternate procedures are   established and used and the Windshear Detection and Avoidance                                         System operates normally.

(O)Operations procedure to ensure alternate procedures are   established and used and that takeoffs and landings are   not conducted in known or forecast windshear conditions.

34-23  (O)Operations procedure to ensure alternate procedures are      established and used and the Windshear Warning and Guidance                                         System operates normally.

(O)Operations procedure to ensure alternate procedures are   established and used and that takeoffs and landings are   not conducted in known or forecast windshear conditions.

34-24  (O)Operations procedure to ensure Aeronautical Charts used to verify navigation fixes are current, procedures are established and      used to verify status of applicable navigation facilities, and                       approach navigation radios are manually tuned.

34-25  (O)Operations procedure to ensure Aeronautical Charts used to verify navigation fixes are current, procedures are established and      used to verify status of applicable navigation facilities, and                       approach navigation radios are manually tuned.

FEDERAL AVIATION ADMINISTRATION   Page XXIV

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Guidelines for (O) & (M) Procedures

35-3     (M)Maintenance procedure to ensure oxygen flow from affected                                                 outlet is prohibited.

37-2     (O)Operations procedure to verify inoperative valve is in the                                                       closed position.

(O)Operations procedure to verify inoperative valve is in the                                              closed position.

38-1     (M)Maintenance procedure to ensure inoperative components                                       are deactivated or isolated.

(M)Maintenance procedure to ensure system is drained and                      cannot be serviced prior to repair.

38-2     (M)Maintenance procedure to ensure inoperative components                                       are deactivated or isolated.

52-4     (M)Maintenance procedure to inspect door latching mechanism.

(O)Operations procedure to ensure Nose Baggage Compartment    is empty and that all latches and fasteners are secure                                      prior to each flight.

52-5     (O)Operations procedure to ensure door is lowered manually to                               prevent damage to aircraft or personnel.

FEDERAL AVIATION ADMINISTRATION   Page

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 10       ¦ PAGE:    ¦ ¦      BEECH MODEL 1900/1900C SERIES       ¦                       ¦          ¦ ¦                                          ¦ DATE: 03/31/2003      ¦ 21-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 21  AIR CONDITIONING      ¦    ¦    ¦                                       ¦

¦ 1.  Air Cycle Air       C ¦ 1  ¦ 0  ¦                                       ¦ ¦     Conditioning System   ¦    ¦    ¦                                       ¦

¦ 2.  Vapor Cycle Air     C ¦ 1  ¦ 0  ¦                                       ¦ ¦     Conditioning System   ¦    ¦    ¦                                       ¦

¦ 3.  Bleed Air Fail      C ¦ 2  ¦ 1  ¦ (O)One may be inoperative for         ¦ ¦     Annunciator           ¦    ¦    ¦ aircraft in which all gyroscopic      ¦ ¦     System                ¦    ¦    ¦ instruments except for the right      ¦ ¦                           ¦    ¦    ¦ side rate of turn/slip skid           ¦ ¦                           ¦    ¦    ¦ indicator are electrically powered    ¦ ¦                           ¦    ¦    ¦ provided:                             ¦ ¦                           ¦    ¦    ¦     a) The environmental and          ¦ ¦                           ¦    ¦    ¦        instrument air valves are      ¦ ¦                           ¦    ¦    ¦        closed on inoperative side,    ¦ ¦                           ¦    ¦    ¦        and                            ¦ ¦                           ¦    ¦    ¦     b) Aircraft is not operated in    ¦ ¦                           ¦    ¦    ¦        known or forecast icing        ¦ ¦                           ¦    ¦    ¦        conditions.                    ¦

¦                         C ¦ 2  ¦ 1  ¦ (O)One may be inoperative for VFR     ¦ ¦                           ¦    ¦    ¦ flights for aircraft equipped with    ¦ ¦                           ¦    ¦    ¦ an air driven copilot's attitude      ¦ ¦                           ¦    ¦    ¦ indicator provided the                ¦ ¦                           ¦    ¦    ¦ environmental and instrument air      ¦ ¦                           ¦    ¦    ¦ valves are closed on the              ¦ ¦                           ¦    ¦    ¦ inoperative side.                     ¦

¦ 4.  L or R ENVIR FAIL   C ¦ 2  ¦ 1  ¦ (O)One may be inoperative provided    ¦ ¦     Annunciation System   ¦    ¦    ¦ the environmental bleed air valve     ¦ ¦                           ¦    ¦    ¦ on the inoperative side is closed.    ¦

¦ 5.  CABIN ALTITUDE      C ¦ 1  ¦ 0  ¦ May be inoperative for flight at or   ¦ ¦     Annunciator System    ¦    ¦    ¦ below 10,000 feet MSL.                ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 10       ¦ PAGE:    ¦ ¦      BEECH MODEL 1900/1900C SERIES       ¦                       ¦          ¦ ¦                                          ¦ DATE: 03/31/2003      ¦ 21-2     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 21  AIR CONDITIONING      ¦    ¦    ¦                                       ¦

¦ 6.  Cabin Rate of       C ¦ 1  ¦ 0  ¦ May be inoperative for pressurized    ¦ ¦     Climb Indicator       ¦    ¦    ¦ flight provided cabin altimeter and   ¦ ¦                           ¦    ¦    ¦ differential pressure gauges are      ¦ ¦                           ¦    ¦    ¦ operative.                            ¦

¦                         C ¦ 1  ¦ 0  ¦ May be inoperative for                ¦ ¦                           ¦    ¦    ¦ unpressurized flight provided the     ¦ ¦                           ¦    ¦    ¦ dump valve is in the open position.   ¦

¦ 7.  Differential        C ¦ 1  ¦ 0  ¦ May be inoperative for                ¦ ¦     Pressure/Cabin        ¦    ¦    ¦ unpressurized flight provided the     ¦ ¦     Altitude Indicator    ¦    ¦    ¦ dump valve is in the open position.   ¦

¦ 8.  Outflow/Safety      C ¦ 2  ¦ 0  ¦ (M)May be inoperative for             ¦ ¦     Valves                ¦    ¦    ¦ unpressurized flight provided one     ¦ ¦                           ¦    ¦    ¦ valve is removed or secured in the    ¦ ¦                           ¦    ¦    ¦ open position.                        ¦

¦ 9.  Pressurization        ¦    ¦    ¦ Deleted, Revision 8                   ¦ ¦     Controller            ¦    ¦    ¦                                       ¦

¦ 10. Pressurization      C ¦ 1  ¦ 0  ¦ (M)May be inoperative provided one    ¦ ¦     System                ¦    ¦    ¦ outflow/safety valve is removed or    ¦ ¦                           ¦    ¦    ¦ secured in the open position.         ¦

¦ 11. Automatic           C ¦ 1  ¦ 0  ¦ May be inoperative provided           ¦ ¦     Temperature Control   ¦    ¦    ¦ manual control system is operative.   ¦

¦ 12. Manual Temperature  C ¦ 1  ¦ 0  ¦ May be inoperative provided           ¦ ¦     Control               ¦    ¦    ¦ automatic control system is           ¦ ¦                           ¦    ¦    ¦ operative.                            ¦

¦ 13. Vent Blowers        C ¦ 2  ¦ 0  ¦                                       ¦

¦ 14. Air Conditioning N1 C ¦ 1  ¦ 0  ¦                                       ¦ ¦     Low Annunciator       ¦    ¦    ¦                                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 10       ¦ PAGE:    ¦ ¦      BEECH MODEL 1900/1900C SERIES       ¦                       ¦          ¦ ¦                                          ¦ DATE: 03/31/2003      ¦ 21-3     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 21  AIR CONDITIONING      ¦    ¦    ¦                                       ¦

¦ 15. Cabin Temperature   C ¦ 1  ¦ 0  ¦                                       ¦ ¦     Gauge                 ¦    ¦    ¦                                       ¦

¦ 16. Bleed Air Shutoff   C ¦ 2  ¦ 1  ¦ (O)One may be inoperative             ¦ ¦     Valves                ¦    ¦    ¦ provided:                             ¦ ¦                           ¦    ¦    ¦     a) The environmental air valve    ¦ ¦                           ¦    ¦    ¦        on the inoperative side is     ¦ ¦                           ¦    ¦    ¦        closed, and                    ¦ ¦                           ¦    ¦    ¦     b) The Environmental Fail         ¦ ¦                           ¦    ¦    ¦        Annunciators are operative.    ¦

¦ 17. Precooler and       C ¦ 2  ¦ 1  ¦ (O)One may be inoperative             ¦ ¦     Bypass Valve Systems  ¦    ¦    ¦ provided:                             ¦ ¦                           ¦    ¦    ¦     a) The environmental air          ¦ ¦                           ¦    ¦    ¦        valve on the inoperative       ¦ ¦                           ¦    ¦    ¦        side is closed, and            ¦ ¦                           ¦    ¦    ¦     b) The Environmental Fail         ¦ ¦                           ¦    ¦    ¦        Annunciators are operative.    ¦

¦ 18. L or R ENVIR OFF    C ¦ 2  ¦ 1  ¦                                       ¦ ¦     Annunciator Systems   ¦    ¦    ¦                                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 10       ¦ PAGE:    ¦ ¦      BEECH MODEL 1900/1900C SERIES       ¦                       ¦          ¦ ¦                                          ¦ DATE: 03/31/2003      ¦ 22-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 22  AUTO FLIGHT           ¦    ¦    ¦                                       ¦

¦ 1.  Autopilot System    C ¦ -  ¦ 0  ¦ (M)May be inoperative provided      | ¦ ¦ ***                       ¦    ¦    ¦ operations do not require its use.  | ¦

¦ 2.  Yaw Damper          C ¦ 1  ¦ 0  ¦ (M)                                   ¦

¦ 3.  Autopilot           C ¦ -  ¦ -  ¦ May be inoperative provided the     | ¦ ¦     Disconnect            ¦    ¦    ¦ autopilot is not utilized at less   | ¦ ¦                           ¦    ¦    ¦ than initial approach altitude.     | ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 10       ¦ PAGE:    ¦ ¦      BEECH MODEL 1900/1900C SERIES       ¦                       ¦          ¦ ¦                                          ¦ DATE: 03/31/2003      ¦ 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                ¦    ¦    ¦                                       ¦

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

¦                           ¦    ¦    ¦ Note:  Any station that operates    | ¦ ¦                           ¦    ¦    ¦        normally may be used.        | ¦

¦     2) Other            D ¦ 1  ¦ 0  ¦ May be inoperative unless           | ¦ ¦        Operations         ¦    ¦    ¦ procedures require its use.         | ¦

¦ 2.  Recorded Passenger  C ¦ 1  ¦ 0  ¦ (O)                                   ¦ ¦ *** Briefing Unit         ¦    ¦    ¦                                       ¦

¦ 3.  Static Discharge    C ¦ -  ¦ -  ¦ One wick may be missing or broken     ¦ ¦     Wicks                 ¦    ¦    ¦ from:                                 ¦ ¦                           ¦    ¦    ¦     a) Each wing (includes aileron)   ¦ ¦                           ¦    ¦    ¦     b) Each side of horizontal        ¦ ¦                           ¦    ¦    ¦        stabilizer,                    ¦ ¦                           ¦    ¦    ¦     c) Vertical stabilizer            ¦ ¦                           ¦    ¦    ¦        (includes stabilon, tail       ¦ ¦                           ¦    ¦    ¦        cone, and ventral fin(s).      ¦

¦                           ¦    ¦    ¦ Maximum of 5 wicks may be missing.    ¦

¦ 4.  Communications      C ¦ -  ¦ -  ¦ As required by FAR.                 | ¦ ¦     Equipment             ¦    ¦    ¦                                     | ¦ ¦     (VHF, UHF)            ¦    ¦    ¦                                     | ¦

¦ 5.  Flight Deck         C ¦ 2  ¦ 1  ¦ One may be inoperative.               ¦ ¦     Speakers              ¦    ¦    ¦                                       ¦ ¦                         C ¦ 2  ¦ 0  ¦ May be inoperative provided an        ¦ ¦                           ¦    ¦    ¦ operative headset is used by each     ¦ ¦                           ¦    ¦    ¦ flight crew member.                   ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 10       ¦ PAGE:    ¦ ¦      BEECH MODEL 1900/1900C SERIES       ¦                       ¦          ¦ ¦                                          ¦ DATE: 03/31/2003      ¦ 23-2     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 23  COMMUNICATIONS        ¦    ¦    ¦                                       ¦

¦ 6.  Cockpit Voice         ¦    ¦    ¦                                     | ¦ ¦     Recorder (CVR)        ¦    ¦    ¦                                     | ¦

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

¦     2) Without Flight   A ¦ 1  ¦ 0  ¦ May be inoperative provided         | ¦ ¦        Data Recorder      ¦    ¦    ¦ repairs are made within three       | ¦ ¦        (FDR) Installed    ¦    ¦    ¦ flight days.                        | ¦

¦ 7.  Ground              C ¦ 1  ¦ 0  ¦                                       ¦ ¦ *** Communications System ¦    ¦    ¦                                       ¦

¦ 8.  Push To Talk          ¦    ¦    ¦                                       ¦ ¦     Switch (Radio)        ¦    ¦    ¦                                       ¦

¦     1) Aircraft         C ¦ 2  ¦ 1  ¦ One may be inoperative provided       ¦ ¦        equipped with      ¦    ¦    ¦ hand microphone on affected side      ¦ ¦        separate hand held ¦    ¦    ¦ is operative.                         ¦ ¦        microphone plug-in ¦    ¦    ¦                                       ¦ ¦        (Second in Command ¦    ¦    ¦                                       ¦ ¦        Required)          ¦    ¦    ¦                                       ¦

¦     2) Aircraft         C ¦ 2  ¦ 1  ¦ Right side may be inoperative.        ¦ ¦        equipped with      ¦    ¦    ¦                                       ¦ ¦       `separate hand held ¦    ¦    ¦                                       ¦ ¦        microphone plug-in ¦    ¦    ¦                                       ¦ ¦        (Second in Command ¦    ¦    ¦                                       ¦ ¦        not Required)      ¦    ¦    ¦                                       ¦

¦     3) Aircraft         C ¦ 2  ¦ 1  ¦ Right side may be inoperative.        ¦ ¦        without separate   ¦    ¦    ¦                                       ¦ ¦        separate hand held ¦    ¦    ¦                                       ¦ ¦        microphone plug-in ¦    ¦    ¦                                       ¦ ¦        (Second in Command ¦    ¦    ¦                                       ¦ ¦        not Required.      ¦    ¦    ¦                                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 10       ¦ PAGE:    ¦ ¦      BEECH MODEL 1900/1900C SERIES       ¦                       ¦          ¦ ¦                                          ¦ DATE: 03/31/2003      ¦ 23-3     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 23  COMMUNICATIONS        ¦    ¦    ¦                                       ¦

¦ 9.  Crew Intercom       B ¦ 1  ¦ 0  ¦ May be inoperative for single pilot   ¦ ¦     System                ¦    ¦    ¦ operations.                           ¦

¦ 10. SELCAL/CALSEL       C ¦ 1  ¦ 0  ¦                                       ¦ ¦ *** Systems               ¦    ¦    ¦                                       ¦

¦ 11. Boom Microphones      ¦    ¦    ¦                                       ¦ ¦     (CVR and FDR          ¦    ¦    ¦                                       ¦ ¦     Installations)        ¦    ¦    ¦                                       ¦

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

¦ *** 2) Cockpit Voice    D ¦ -  ¦ 0  ¦                                       ¦ ¦        Recorder Not       ¦    ¦    ¦                                       ¦ ¦        Equipped to Record ¦    ¦    ¦                                       ¦ ¦        Boom Microphone    ¦    ¦    ¦                                       ¦

¦     Boom Microphones      ¦    ¦    ¦                                       ¦ ¦     (CVR Installation     ¦    ¦    ¦                                       ¦ ¦     Only)                 ¦    ¦    ¦                                       ¦

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

¦ *** 2) Cockpit Voice    D ¦ -  ¦ 0  ¦                                       ¦ ¦        Recorder Not       ¦    ¦    ¦                                       ¦ ¦        Equipped To Record ¦    ¦    ¦                                       ¦ ¦        Boom Microphone    ¦    ¦    ¦                                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 10       ¦ PAGE:    ¦ ¦      BEECH MODEL 1900/1900C SERIES       ¦                       ¦          ¦ ¦                                          ¦ DATE: 03/31/2003      ¦ 23-4     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 23  COMMUNICATIONS        ¦    ¦    ¦                                       ¦

¦ 12. High Frequency (HF) D ¦ -  ¦ -  ¦ Any in excess of those required by  | ¦ ¦     Communication         ¦    ¦    ¦ FAR may be inoperative.             | ¦ ¦     System                ¦    ¦    ¦                                     | ¦ ¦                         C ¦ -  ¦ 1  ¦ (O) May be inoperative while        | ¦ ¦                           ¦    ¦    ¦ conducting operations that require  | ¦ ¦                           ¦    ¦    ¦ two LRCS provided:                  | ¦ ¦                           ¦    ¦    ¦     a) SATCOM (High or Low Gain)    | ¦ ¦                           ¦    ¦    ¦        Data Link System operates    | ¦ ¦                           ¦    ¦    ¦        normally, and                | ¦ ¦                           ¦    ¦    ¦     b) SATCOM Data Link             | ¦ ¦                           ¦    ¦    ¦        communication operates       | ¦ ¦                           ¦    ¦    ¦        normally over the intended   | ¦ ¦                           ¦    ¦    ¦        route of flight.             | ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 10       ¦ PAGE:    ¦ ¦      BEECH MODEL 1900/1900C SERIES       ¦                       ¦          ¦ ¦                                          ¦ DATE: 03/31/2003      ¦ 24-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 24  ELECTRICAL POWER      ¦    ¦    ¦                                       ¦

¦ 1.  AC volt/freq.       B ¦ 1  ¦ 0  ¦ (M)May be inoperative for VMC         ¦ ¦     meter                 ¦    ¦    ¦ provided Inverter Annunciator         ¦ ¦                           ¦    ¦    ¦ System is operative.                  ¦

¦ 2.  L or R DC GEN       B ¦ 2  ¦ 1  ¦ One may be inoperative.               ¦ ¦     Annunciator Systems   ¦    ¦    ¦                                       ¦

¦ 3.  DC Loadmeters       B ¦ 2  ¦ 1  ¦ (O)One may be inoperative             ¦ ¦                           ¦    ¦    ¦ provided:                             ¦ ¦                           ¦    ¦    ¦     a) The electrical load is         ¦ ¦                           ¦    ¦    ¦        maintained within the          ¦ ¦                           ¦    ¦    ¦        capacity of one generator at   ¦ ¦                           ¦    ¦    ¦        all times,                     ¦ ¦                           ¦    ¦    ¦     b) Both DC generator              ¦ ¦                           ¦    ¦    ¦        annunciators are operative,    ¦ ¦                           ¦    ¦    ¦        and                            ¦ ¦                           ¦    ¦    ¦     c) Aircraft is not operated in    ¦ ¦                           ¦    ¦    ¦        known or forecast icing        ¦ ¦                           ¦    ¦    ¦        conditions.                    ¦

¦ 4.  Inverters           B ¦ 2  ¦ 1  ¦ One may be inoperative for day        ¦ ¦                           ¦    ¦    ¦ VFR.                                  ¦

¦ 5.  INVERTER            B ¦ 1  ¦ 0  ¦ May be inoperative provided:          ¦ ¦     Annunciator System    ¦    ¦    ¦     a) Both inverters are             ¦ ¦                           ¦    ¦    ¦        operative, and                 ¦ ¦                           ¦    ¦    ¦     b) AC volt/frequency meter is     ¦ ¦                           ¦    ¦    ¦        operative.                     ¦

¦ 6.  External Power      C ¦ 1  ¦ 0  ¦ (M)                                   ¦ ¦     System                ¦    ¦    ¦                                       ¦

¦ 7.  EXTERNAL POWER      C ¦ 1  ¦ 0  ¦ (O)                                   ¦ ¦     Annunciator System    ¦    ¦    ¦                                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 10       ¦ PAGE:    ¦ ¦      BEECH MODEL 1900/1900C SERIES       ¦                       ¦          ¦ ¦                                          ¦ DATE: 03/31/2003      ¦ 24-2     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 24  ELECTRICAL POWER      ¦    ¦    ¦                                       ¦

¦ 8.  Ground Power          ¦    ¦    ¦      Deleted, Revision 7              ¦ ¦     Receptacle            ¦    ¦    ¦                                       ¦

¦ 9.  External Power        ¦    ¦    ¦      Deleted, Revision 7              ¦ ¦     Switch                ¦    ¦    ¦                                       ¦

¦ 10. Generator Bus Tie   B ¦ 2  ¦ 1  ¦ One may be inoperative for day        ¦ ¦                           ¦    ¦    ¦ VMC provided both DC generator        ¦ ¦                           ¦    ¦    ¦ annunciators are operative.           ¦

¦ 11. L or R GEN TIE OPEN B ¦ 2  ¦ 0  ¦ (O)May be inoperative provided:       ¦ ¦     Annunciator System    ¦    ¦    ¦     a) Generator tie relay is         ¦ ¦                           ¦    ¦    ¦        verified closed prior to       ¦ ¦                           ¦    ¦    ¦        each departure, and            ¦ ¦                           ¦    ¦    ¦     b) Both DC GEN annunciators are   ¦ ¦                           ¦    ¦    ¦        operative.                     ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 10       ¦ PAGE:    ¦ ¦      BEECH MODEL 1900/1900C SERIES       ¦                       ¦          ¦ ¦                                          ¦ DATE: 03/31/2003      ¦ 25-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 25  EQUIPMENT/FURNISHINGS ¦    ¦    ¦                                       ¦

¦ 1.  Approved Flotation  D ¦ -  ¦ 0  ¦ Any in excess of those required by    ¦ ¦     Device                ¦    ¦    ¦ FAR may be inoperative.               ¦

¦ 2.  Cockpit Crewmember  C ¦ 2  ¦ 1  ¦ Right side may be inoperative         ¦ ¦     Shoulder Harness      ¦    ¦    ¦ provided a second in command is not   ¦ ¦                           ¦    ¦    ¦ required and seat is not occupied.    ¦

¦ 3.  Passenger Seat(s)   C ¦ -  ¦ 0  ¦ May be inoperative provided:        | ¦ ¦                           ¦    ¦    ¦     a)Seat does not block an        | ¦ ¦                           ¦    ¦    ¦       emergency exit,               | ¦ ¦                           ¦    ¦    ¦     b)Seat does not restrict any    | ¦ ¦                           ¦    ¦    ¦       passenger from access to the  | ¦ ¦                           ¦    ¦    ¦       main aircraft aisle, and      | ¦ ¦                           ¦    ¦    ¦     c)The affected seat(s) are      | ¦ ¦                           ¦    ¦    ¦       blocked and placarded "DO     | ¦ ¦                           ¦    ¦    ¦       NOT OCCUPY".                  | ¦

¦                           ¦    ¦    ¦ NOTE: A seat with an inoperative    | ¦ ¦                           ¦    ¦    ¦       seat belt is considered to be | ¦ ¦                           ¦    ¦    ¦       inoperative.                  | ¦

¦                           ¦    ¦    ¦ NOTE: Affected seat(s) may include  | ¦ ¦                           ¦    ¦    ¦       the seat(s) behind and/or     | ¦ ¦                           ¦    ¦    ¦       adjacent to the outboard      | ¦ ¦                           ¦    ¦    ¦       seats.                        | ¦

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

¦     2)Underseat         D ¦ -  ¦ -  ¦ (O)May be inoperative provided:     | ¦ ¦       Baggage             ¦    ¦    ¦    a)Baggage is not stowed under    | ¦ ¦       Restraining Bars    ¦    ¦    ¦      seat with inoperative          | ¦ ¦                           ¦    ¦    ¦      restraining bar,               | ¦ ¦                           ¦    ¦    ¦    b)Associated seat is placarded   | ¦ ¦                           ¦    ¦    ¦      "DO NOT STOW BAGGAGE UNDER     | ¦ ¦                           ¦    ¦    ¦      THIS SEAT", and                | ¦ ¦                           ¦    ¦    ¦    c)Procedures are established to  | ¦ ¦                           ¦    ¦    ¦      alert crew of inoperative      | ¦ ¦                           ¦    ¦    ¦      restraining bar.               | ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 10       ¦ PAGE:    ¦ ¦      BEECH MODEL 1900/1900C SERIES       ¦                       ¦          ¦ ¦                                          ¦ DATE: 03/31/2003      ¦ 25-2     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 25  EQUIPMENT/FURNISHINGS ¦    ¦    ¦                                       ¦

¦ 4.  Emergency Locator   C ¦ 1  ¦ 0  ¦ As required by FAR.                   ¦ ¦     Transmitter (ELT)     ¦    ¦    ¦                                       ¦ ¦                         C ¦ 1  ¦ 0  ¦ May be inoperative for published      ¦ ¦                           ¦    ¦    ¦ scheduled flights in scheduled air    ¦ ¦                           ¦    ¦    ¦ carrier service.                      ¦

¦ 5.  ELT Remote Switch   C ¦ 1  ¦ 0  ¦ (M)May be inoperative provided:       ¦ ¦                           ¦    ¦    ¦     a) Remote switch is               ¦ ¦                           ¦    ¦    ¦        disconnected from ELT, and     ¦ ¦                           ¦    ¦    ¦     b) ELT switch is placed in ARM    ¦ ¦                           ¦    ¦    ¦        position.                      ¦

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

¦ 7.  Emergency Medical   D ¦ -  ¦ -  ¦ Any in excess of those required by  | ¦ ¦     Equipment             ¦    ¦    ¦ FAR may be incomplete or missing    | ¦ ¦                           ¦    ¦    ¦ provided required distribution      | ¦ ¦                           ¦    ¦    ¦ is maintained.                      | ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 10       ¦ PAGE:    ¦ ¦      BEECH MODEL 1900/1900C SERIES       ¦                       ¦          ¦ ¦                                          ¦ DATE: 03/31/2003      ¦ 25-3     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 25  EQUIPMENT/FURNISHINGS ¦    ¦    ¦                                       ¦

¦ 8.  Forward Observer    A ¦ -  ¦ -  ¦ May be inoperative provided:          ¦ ¦     Seat (Including       ¦    ¦    ¦     a) A passenger seat in the        ¦ ¦     All Associated        ¦    ¦    ¦        passenger cabin is made        ¦ ¦     Equipment)            ¦    ¦    ¦        available to an FAA            ¦ ¦                           ¦    ¦    ¦        inspector for the              ¦ ¦                           ¦    ¦    ¦        performance of official        ¦ ¦                           ¦    ¦    ¦        duties, and                    ¦ ¦                           ¦    ¦    ¦     b) Operations are limited to      ¦ ¦                           ¦    ¦    ¦        not more than two flight       ¦ ¦                           ¦    ¦    ¦        days before repairs are        ¦ ¦                           ¦    ¦    ¦        made.                          ¦

¦ 9.  "Fasten Seat Belt   C ¦ -  ¦ -  ¦ (O) One or more signs or placards   | ¦ ¦ *** While Seated/No       ¦    ¦    ¦ may be illegible or missing         | ¦ ¦     Smoking" Sign         ¦    ¦    ¦ provided a legible sign or placard  | ¦ ¦                           ¦    ¦    ¦ is visible from each seat.          | ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 10       ¦ PAGE:    ¦ ¦      BEECH MODEL 1900/1900C SERIES       ¦                       ¦          ¦ ¦                                          ¦ DATE: 03/31/2003      ¦ 26-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 26  FIRE PROTECTION       ¦    ¦    ¦                                       ¦

¦ 1.  Portable Fire       D ¦ -  ¦ -  ¦ Any in excess of those required       ¦ ¦     Extinguisher          ¦    ¦    ¦ by 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.                    ¦

¦ 2.  Lavatory Fire       C ¦ -  ¦ -  ¦ Lavatory Fire Extinguisher System   | ¦ ¦ *** Extinguisher System   ¦    ¦    ¦ may be inoperative provided         | ¦ ¦                           ¦    ¦    ¦ Lavatory Smoke Detector system      | ¦ ¦                           ¦    ¦    ¦ operates normally.                  | ¦

¦                         C ¦ -  ¦ -  ¦ (M)(O) Lavatory Fire Extinguisher   | ¦ ¦                           ¦    ¦    ¦ System may be inoperative provided: | ¦ ¦                           ¦    ¦    ¦     a) Lavatory waste receptacle    | ¦ ¦                           ¦    ¦    ¦        is empty,                    | ¦ ¦                           ¦    ¦    ¦     b) Lavatory door is locked and  | ¦ ¦                           ¦    ¦    ¦        placarded "INOPERATIVE - DO  | ¦ ¦                           ¦    ¦    ¦        NOT USE", and                | ¦ ¦                           ¦    ¦    ¦     c) Lavatory is used only by     | ¦ ¦                           ¦    ¦    ¦        crewmembers.                 | ¦

¦                           ¦    ¦    ¦ NOTE 1: These provisos are not      | ¦ ¦                           ¦    ¦    ¦         intended to prohibit        | ¦ ¦                           ¦    ¦    ¦         lavatory use or inspections | ¦ ¦                           ¦    ¦    ¦         by crewmembers.             | ¦

¦                           ¦    ¦    ¦ NOTE 2: Lavatory fire extinguisher  | ¦ ¦                           ¦    ¦    ¦         system is not required for  | ¦ ¦                           ¦    ¦    ¦         all-cargo operations.       | ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 10       ¦ PAGE:    ¦ ¦      BEECH MODEL 1900/1900C SERIES       ¦                       ¦          ¦ ¦                                          ¦ DATE: 03/31/2003      ¦ 26-2     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 26  FIRE PROTECTION       ¦    ¦    ¦                                       ¦

¦ 3.  Lavatory Smoke      C ¦ -  ¦ -  ¦ (M)(O) Lavatory Smoke Detection     | ¦ ¦     Detection System      ¦    ¦    ¦ System may be inoperative provided: | ¦ ¦                           ¦    ¦    ¦     a) Lavatory waste receptacle    | ¦ ¦                           ¦    ¦    ¦        is empty,                    | ¦ ¦                           ¦    ¦    ¦     b) Lavatory door is locked and  | ¦ ¦                           ¦    ¦    ¦        placarded "INOPERATIVE - DO  | ¦ ¦                           ¦    ¦    ¦        NOT USE", and                | ¦ ¦                           ¦    ¦    ¦     c) Lavatory is used only by     | ¦ ¦                           ¦    ¦    ¦        crewmembers.                 | ¦

¦                           ¦    ¦    ¦ NOTE 1: These provisos are not      | ¦ ¦                           ¦    ¦    ¦         intended to prohibit        | ¦ ¦                           ¦    ¦    ¦         lavatory use or inspections | ¦ ¦                           ¦    ¦    ¦         by crewmembers.             | ¦

¦                           ¦    ¦    ¦ NOTE 2: Lavatory smoke detection    | ¦ ¦                           ¦    ¦    ¦         system is not required for  | ¦ ¦                           ¦    ¦    ¦         all-cargo operations.       | ¦

¦ 4.  Cargo Compartment   C ¦ -  ¦ 0  ¦ May be inoperative provided         | ¦ ¦     Fire Detection/       ¦    ¦    ¦ associated cargo compartment        | ¦ ¦     Suppression Systems   ¦    ¦    ¦ remains empty.                      | ¦

¦                           ¦    ¦    ¦ NOTE: Does not preclude the         | ¦ ¦                           ¦    ¦    ¦       carriage of empty cargo       | ¦ ¦                           ¦    ¦    ¦       containers, pallets,          | ¦ ¦                           ¦    ¦    ¦       ballast, etc.                 | ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 10       ¦ PAGE:    ¦ ¦      BEECH MODEL 1900/1900C SERIES       ¦                       ¦          ¦ ¦                                          ¦ DATE: 03/31/2003      ¦ 27-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 27  FLIGHT CONTROLS       ¦    ¦    ¦                                       ¦

¦ 1.  Flap Position       C ¦ 1  ¦ 0  ¦ May be inoperative provided:          ¦ ¦     Indicator             ¦    ¦    ¦     a) Flaps are visually checked     ¦ ¦                           ¦    ¦    ¦        for full travel and flap       ¦ ¦                           ¦    ¦    ¦        operation is not affected,     ¦ ¦                           ¦    ¦    ¦        and                            ¦ ¦                           ¦    ¦    ¦     b) Flaps are checked for proper   ¦ ¦                           ¦    ¦    ¦        setting prior to each          ¦ ¦                           ¦    ¦    ¦        departure and landing.         ¦

¦ 2.  Flap System         C ¦ 1  ¦ 0  ¦ (O)May be inoperative provided:       ¦ ¦                           ¦    ¦    ¦     a) Flaps are in full up           ¦ ¦                           ¦    ¦    ¦        position, and                  ¦ ¦                           ¦    ¦    ¦     b) Performance charts in AFM      ¦ ¦                           ¦    ¦    ¦        for no flap takeoff and        ¦ ¦                           ¦    ¦    ¦        landings are used.             ¦

¦                           ¦    ¦    ¦  CAUTION:  DO NOT SILENCE THE         ¦ ¦                           ¦    ¦    ¦            LANDING GEAR WARNING       ¦ ¦                           ¦    ¦    ¦            HORN.                      ¦

¦ 3.  Trim Tab Indicators C ¦ 2  ¦ 0  ¦ May be inoperative provided:          ¦ ¦     (Aileron, Rudder)     ¦    ¦    ¦     a) Tab is visually checked        ¦ ¦                           ¦    ¦    ¦        for full range of operation,   ¦ ¦                           ¦    ¦    ¦     b) Tab operation is not           ¦ ¦                           ¦    ¦    ¦        impaired, and                  ¦ ¦                           ¦    ¦    ¦     c) Tab is positioned to neutral   ¦ ¦                           ¦    ¦    ¦        prior to each departure and    ¦ ¦                           ¦    ¦    ¦        neutral position is verified   ¦ ¦                           ¦    ¦    ¦        by visual inspection.          ¦

¦ 4.  Electric Elevator   C ¦ 1  ¦ 0  ¦ (M)May be inoperative provided:       ¦ ¦ *** Trim System           ¦    ¦    ¦     a) Manual trim is operative       ¦ ¦                           ¦    ¦    ¦        and unaffected, and            ¦ ¦                           ¦    ¦    ¦     b) Autopilot is not used.         ¦

¦ 5.  ELEC TRIM OFF       C ¦ 1  ¦ 0  ¦                                       ¦ ¦ *** Annunciator System    ¦    ¦    ¦                                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 10       ¦ PAGE:    ¦ ¦      BEECH MODEL 1900/1900C SERIES       ¦                       ¦          ¦ ¦                                          ¦ DATE: 03/31/2003      ¦ 28-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 28  FUEL                  ¦    ¦    ¦                                       ¦

¦ 1.  Standby Electric    C ¦ 2  ¦ 1  ¦ One may be inoperative except         ¦ ¦     Boost Pumps           ¦    ¦    ¦ when using aviation gasoline.         ¦

¦ 2.  Engine Driven Low   C ¦ 2  ¦ 1  ¦ (M)One may be inoperative provided    ¦ ¦     Pressure Fuel Boost   ¦    ¦    ¦ standby electric fuel boost pump is   ¦ ¦     Pumps                 ¦    ¦    ¦ operative and turned on.              ¦

¦ 3.  Fuel Quantity       C ¦ 2  ¦ 1  ¦ (O)One may be inoperative provided:   ¦ ¦     Indicators            ¦    ¦    ¦     a) A reliable means is            ¦ ¦                           ¦    ¦    ¦        established to determine       ¦ ¦                           ¦    ¦    ¦        that fuel quantity on board    ¦ ¦                           ¦    ¦    ¦        meets the regulatory           ¦ ¦                           ¦    ¦    ¦        requirements for the           ¦ ¦                           ¦    ¦    ¦        intended flight,               ¦ ¦                           ¦    ¦    ¦     b) Both fuel flow indicators      ¦ ¦                           ¦    ¦    ¦        are operative,                 ¦ ¦                           ¦    ¦    ¦     c) Fuel quantity annunciators     ¦ ¦                           ¦    ¦    ¦        are operative, and             ¦ ¦                           ¦    ¦    ¦     d) Procedures are established     ¦ ¦                           ¦    ¦    ¦        to ensure fuel balance         ¦ ¦                           ¦    ¦    ¦        remains within AFM limits.     ¦

¦ 4.  L or R FUEL QTY     C ¦ 2  ¦ 1  ¦ One may be inoperative provided:      ¦ ¦     Annunciator Systems   ¦    ¦    ¦     a) Fuel quantity on board is      ¦ ¦                           ¦    ¦    ¦        adequate for intended          ¦ ¦                           ¦    ¦    ¦        flight,                        ¦ ¦                           ¦    ¦    ¦     b) Fuel quantity indicators are   ¦ ¦                           ¦    ¦    ¦        operative, and                 ¦ ¦                           ¦    ¦    ¦     c) Fuel flow indicators are       ¦ ¦                           ¦    ¦    ¦        operative.                     ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 10       ¦ PAGE:    ¦ ¦      BEECH MODEL 1900/1900C SERIES       ¦                       ¦          ¦ ¦                                          ¦ DATE: 03/31/2003      ¦ 28-2     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 28  FUEL                  ¦    ¦    ¦                                       ¦

¦ 5.  FUEL TRANSFER       C ¦ 1  ¦ 0  ¦ (O)May be inoperative provided:       ¦ ¦     Annunciator System    ¦    ¦    ¦     a) Proper operation of standby    ¦ ¦                           ¦    ¦    ¦        fuel pumps are verified        ¦ ¦                           ¦    ¦    ¦        prior to departure, and        ¦ ¦                           ¦    ¦    ¦     b) Both fuel quantity             ¦ ¦                           ¦    ¦    ¦        indicators are operative.      ¦

¦ 6.  Fuel Flow           B ¦ 2  ¦ 1  ¦ (M)One may be inoperative provided    ¦ ¦     Indicators            ¦    ¦    ¦ fuel quantity indicators are          ¦ ¦                           ¦    ¦    ¦ operative and monitored.              ¦

¦ 7.  Auxiliary Fuel      C ¦ 2  ¦ 0  ¦ (M)One or both may be inoperative     ¦ ¦     Transfer Pumps        ¦    ¦    ¦ provided:                             ¦ ¦                           ¦    ¦    ¦     a) Fuel quantity in main tank     ¦ ¦                           ¦    ¦    ¦        is adequate for the intended   ¦ ¦                           ¦    ¦    ¦        flight, and                    ¦ ¦                           ¦    ¦    ¦     b) Fuel quantity indicators are   ¦ ¦                           ¦    ¦    ¦        operative.                     ¦

¦ 8.  L or R FUEL FEED    C ¦ 2  ¦ 1  ¦ One may be inoperative provided:      ¦ ¦     Annunciator System    ¦    ¦    ¦     a) Fuel quantity on board is      ¦ ¦                           ¦    ¦    ¦        adequate for the intended      ¦ ¦                           ¦    ¦    ¦        flight,                        ¦ ¦                           ¦    ¦    ¦     b) Fuel quantity indicators are   ¦ ¦                           ¦    ¦    ¦        operative,                     ¦ ¦                           ¦    ¦    ¦     c) FUEL QTY annunciator system    ¦ ¦                           ¦    ¦    ¦        is operative, and              ¦ ¦                           ¦    ¦    ¦     d) Fuel flow indicators are       ¦ ¦                           ¦    ¦    ¦        operative.                     ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 10       ¦ PAGE:    ¦ ¦      BEECH MODEL 1900/1900C SERIES       ¦                       ¦          ¦ ¦                                          ¦ DATE: 03/31/2003      ¦ 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.  Surface Deice       C ¦ 1  ¦ 0  ¦ May be inoperative provided           ¦ ¦     System (Wing,         ¦    ¦    ¦ aircraft is not operated in known     ¦ ¦     Stabilon, and         ¦    ¦    ¦ or forecast icing conditions.         ¦ ¦     Horizontal            ¦    ¦    ¦                                       ¦ ¦     Stabilizer)           ¦    ¦    ¦                                       ¦

¦ 2.  Alternate Static    C ¦ 2  ¦ 1  ¦ One may be inoperative for VMC.       ¦ ¦     Air Source Heaters    ¦    ¦    ¦                                       ¦

¦ 3.  Engine Inertial     C ¦ 4  ¦ 2  ¦ (M)One actuator motor on each side    ¦ ¦     Ice Vane Actuator     ¦    ¦    ¦ may be inoperative.                   ¦ ¦     Motors                ¦    ¦    ¦                                       ¦ ¦                         C ¦ 4  ¦ 0  ¦ (M)Both actuator motors on each       ¦ ¦                           ¦    ¦    ¦ side may be inoperative provided:     ¦ ¦                           ¦    ¦    ¦     a) Inertial ice vanes are         ¦ ¦                           ¦    ¦    ¦        secured in the extended        ¦ ¦                           ¦    ¦    ¦        position, and                  ¦ ¦                           ¦    ¦    ¦     b) Appropriate performance        ¦ ¦                           ¦    ¦    ¦        charts are used.               ¦

¦ 4.  Engine Inertial     C ¦ 4  ¦ 2  ¦ (O)One may be inoperative on each     ¦ ¦     Ice Vane Annunciators ¦    ¦    ¦ side.                                 ¦

¦                         C ¦ 4  ¦ 0  ¦ (M)Both may be inoperative on each    ¦ ¦                           ¦    ¦    ¦ side provided:                        ¦ ¦                           ¦    ¦    ¦     a) Inertial ice vanes are         ¦ ¦                           ¦    ¦    ¦        secured in the extended        ¦ ¦                           ¦    ¦    ¦        position, and                  ¦ ¦                           ¦    ¦    ¦     b) Appropriate performance        ¦ ¦                           ¦    ¦    ¦        charts are used.               ¦

¦ 5.  Stall Warning Vane  C ¦ 1  ¦ 0  ¦ May be inoperative provided           ¦ ¦     and Mount Plate       ¦    ¦    ¦ aircraft is not operated in known     ¦ ¦     Heater System         ¦    ¦    ¦ or forecast icing conditions.         ¦

¦ 6.  Windshield Wipers   C ¦ 2  ¦ 0  ¦ May be inoperative provided           ¦ ¦                           ¦    ¦    ¦ aircraft is not operated in           ¦ ¦                           ¦    ¦    ¦ precipitation within 5 nautical       ¦ ¦                           ¦    ¦    ¦ miles of the airport of takeoff or    ¦ ¦                           ¦    ¦    ¦ intended landing.                     ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 10       ¦ PAGE:    ¦ ¦      BEECH MODEL 1900/1900C SERIES       ¦                       ¦          ¦ ¦                                          ¦ DATE: 03/31/2003      ¦ 30-2     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 30  ICE AND RAIN          ¦    ¦    ¦                                       ¦ ¦     PROTECTION            ¦    ¦    ¦                                       ¦

¦ 7.  Windshield Heaters  C ¦ 2  ¦ 0  ¦ May be inoperative provided           ¦ ¦                           ¦    ¦    ¦ aircraft is not operated in known     ¦ ¦                           ¦    ¦    ¦ or forecast icing conditions.         ¦

¦ 8.  Propeller Deicer    C ¦ 1  ¦ 0  ¦ May be inoperative provided           ¦ ¦     Ammeter               ¦    ¦    ¦ aircraft is not operated in known     ¦ ¦                           ¦    ¦    ¦ or forecast icing conditions.         ¦

¦ 9.  Propeller Deicing   C ¦ 1  ¦ 0  ¦ May be inoperative provided Manual    ¦ ¦     System (Automatic)    ¦    ¦    ¦ propeller deice system is             ¦ ¦                           ¦    ¦    ¦ operative.                            ¦

¦                         C ¦ 1  ¦ 0  ¦ May be inoperative provided           ¦ ¦                           ¦    ¦    ¦ aircraft is not operated in known     ¦ ¦                           ¦    ¦    ¦ or forecast icing conditions.         ¦

¦ 10. Propeller Deice     C ¦ 1  ¦ 0  ¦ May be inoperative provided           ¦ ¦     Systems (Manual)      ¦    ¦    ¦ Automatic propeller deice system is   ¦ ¦                           ¦    ¦    ¦ operative.                            ¦

¦                         C ¦ 1  ¦ 0  ¦ May be inoperative provided           ¦ ¦                           ¦    ¦    ¦ aircraft is not operated in known     ¦ ¦                           ¦    ¦    ¦ or forecast icing conditions.         ¦

¦ 11. Fuel Vent Heaters   C ¦ 2  ¦ 0  ¦ May be inoperative provided           ¦ ¦                           ¦    ¦    ¦ aircraft is not operated in known     ¦ ¦                           ¦    ¦    ¦ or forecast icing conditions.         ¦

¦ 12. Brake Deice System  C ¦ 1  ¦ 0  ¦ (M)May be inoperative provided        ¦ ¦ ***                       ¦    ¦    ¦ shutoff valves are in off position.   ¦

¦ 13. Pitot Heaters       B ¦ 2  ¦ 1  ¦ One may be inoperative provided:      ¦ ¦                           ¦    ¦    ¦     a) IFR passenger carrying         ¦ ¦                           ¦    ¦    ¦        operations are not             ¦ ¦                           ¦    ¦    ¦        conducted, and                 ¦ ¦                           ¦    ¦    ¦     b) Aircraft is not operated       ¦ ¦                           ¦    ¦    ¦        in known or forecast icing     ¦ ¦                           ¦    ¦    ¦        conditions.                    ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 10       ¦ PAGE:    ¦ ¦      BEECH MODEL 1900/1900C SERIES       ¦                       ¦          ¦ ¦                                          ¦ DATE: 03/31/2003      ¦ 31-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 31  INDICATING/RECORDING  ¦    ¦    ¦                                       ¦ ¦     SYSTEMS               ¦    ¦    ¦                                       ¦

¦ 1.  Clock with sweep    C ¦ 2  ¦ 0  ¦ May be inoperative for VFR.           ¦ ¦     second hand, or       ¦    ¦    ¦                                       ¦ ¦     electric digital      ¦    ¦    ¦                                       ¦ ¦     clock                 ¦    ¦    ¦                                       ¦ ¦                         C ¦ 2  ¦ 1  ¦ One may be inoperative for IFR.       ¦

¦ 2.  Flight Hour         C ¦ 1  ¦ 0  ¦ (O)                                   ¦ ¦ *** Recorder              ¦    ¦    ¦                                       ¦

¦ 3.  Flight Data         C ¦ -  ¦ -  ¦ Any in excess of those required by  | ¦ ¦ *** Recorder (FDR)        ¦    ¦    ¦ FAR may be inoperative.             | ¦

¦                         A ¦ -  ¦ 0  ¦ May be inoperative provided:        | ¦ ¦                           ¦    ¦    ¦     a) Cockpit Voice Recorder (CVR) | ¦ ¦                           ¦    ¦    ¦        operates normally,           | ¦ ¦                           ¦    ¦    ¦     b) Airplane is not dispatched   | ¦ ¦                           ¦    ¦    ¦        from a designated airport    | ¦ ¦                           ¦    ¦    ¦        as listed in the operators   | ¦ ¦                           ¦    ¦    ¦        MEL unless:                  | ¦ ¦                           ¦    ¦    ¦        1. The FDR failure occurs    | ¦ ¦                           ¦    ¦    ¦           after pushback but prior  | ¦ ¦                           ¦    ¦    ¦           to takeoff, or            | ¦ ¦                           ¦    ¦    ¦        2. The FDR repair was        | ¦ ¦                           ¦    ¦    ¦           attempted but was not     | ¦ ¦                           ¦    ¦    ¦           successful.               | ¦ ¦                           ¦    ¦    ¦     c) In those cases where repair  | ¦ ¦                           ¦    ¦    ¦        is attempted but not         | ¦ ¦                           ¦    ¦    ¦        successful, the aircraft may | ¦ ¦                           ¦    ¦    ¦        be dispatched on a flight or | ¦ ¦                           ¦    ¦    ¦        a series of flights until    | ¦ ¦                           ¦    ¦    ¦        the next designated airport  | ¦ ¦                           ¦    ¦    ¦        where repair(s) must be      | ¦ ¦                           ¦    ¦    ¦        accomplished prior to        | ¦ ¦                           ¦    ¦    ¦        dispatch, and                | ¦ ¦                           ¦    ¦    ¦     d) Repairs are made within      | ¦ ¦                           ¦    ¦    ¦        three flight days.           | ¦

¦                 (CONT.)   ¦    ¦    ¦                                     | ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 10       ¦ PAGE:    ¦ ¦      BEECH MODEL 1900/1900C SERIES       ¦                       ¦          ¦ ¦                                          ¦ DATE: 03/31/2003      ¦ 31-2     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 31  INDICATING/RECORDING  ¦    ¦    ¦                                       ¦ ¦     SYSTEMS               ¦    ¦    ¦                                       ¦

¦ 3.  Flight Data           ¦    ¦    ¦                                     | ¦ ¦ *** Recorder (FDR)        ¦    ¦    ¦                                     | ¦ ¦                 (CONT.)   ¦    ¦    ¦                                     | ¦

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

¦     2) FDR Recording    A ¦ -  ¦ -  ¦ May be inoperative provided repairs | ¦ ¦        parameters not     ¦    ¦    ¦ are made prior to the completion of | ¦ ¦        required by FAR    ¦    ¦    ¦ the next heavy maintenance visit.   | ¦

¦ 4.  Annunciator Power   C ¦ 1  ¦ 0  ¦ (O)May be illuminated provided:       ¦ ¦     Source Annunciator    ¦    ¦    ¦     a) Preflight procedures are       ¦ ¦                           ¦    ¦    ¦        conducted to check operation   ¦ ¦                           ¦    ¦    ¦        of individual annunciation     ¦ ¦                           ¦    ¦    ¦        circuits in accordance with    ¦ ¦                           ¦    ¦    ¦        Beech Minimum Equipment        ¦ ¦                           ¦    ¦    ¦        Procedures (P/N 98-30335),     ¦ ¦                           ¦    ¦    ¦     b) MEL relief is approved and     ¦ ¦                           ¦    ¦    ¦        applicable procedures and      ¦ ¦                           ¦    ¦    ¦        restrictions observed for      ¦ ¦                           ¦    ¦    ¦        all annunciator circuits       ¦ ¦                           ¦    ¦    ¦        found to be inoperative, and   ¦ ¦                           ¦    ¦    ¦     c) Operation is limited to        ¦ ¦                           ¦    ¦    ¦        12,500 feet MSL or below.      ¦

¦ 5.  Aircraft Data       D ¦ -  ¦ 0  ¦                                     | ¦ ¦ *** Acquisition System    ¦    ¦    ¦                                     | ¦ ¦     (Installed per        ¦    ¦    ¦                                     | ¦ ¦     STC SA00095BO)        ¦    ¦    ¦                                     | ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 10       ¦ PAGE:    ¦ ¦      BEECH MODEL 1900/1900C SERIES       ¦                       ¦          ¦ ¦                                          ¦ DATE: 03/31/2003      ¦ 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          ¦    ¦    ¦      Deleted, Revision 7              ¦ ¦     Handle Light Bulbs    ¦    ¦    ¦                                       ¦

¦ 2.  Landing Gear          ¦    ¦    ¦      Deleted, Revision 7              ¦ ¦     Position Indication   ¦    ¦    ¦                                       ¦ ¦     Lights                ¦    ¦    ¦                                       ¦

¦ 3.  Power Steering      C ¦ 1  ¦ 0  ¦ (M)(O)May be inoperative provided     ¦ ¦ *** System                ¦    ¦    ¦ AFM procedures are observed.          ¦

¦ 4.  PWR STEER FAIL      C ¦ 1  ¦ 0  ¦ May be inoperative provided power     ¦ ¦ *** Annunciator System    ¦    ¦    ¦ steering remains off.                 ¦

¦ 5.  MAN STEER FAIL      C ¦ 1  ¦ 0  ¦ (O)(M)May be inoperative provided:    ¦ ¦     Annunciator System    ¦    ¦    ¦     a) Power steering is disabled     ¦ ¦                           ¦    ¦    ¦        by pulling and banding         ¦ ¦                           ¦    ¦    ¦        circuit breaker, and           ¦ ¦                           ¦    ¦    ¦     b) Nose gear must be in free      ¦ ¦                           ¦    ¦    ¦        castor mode.                   ¦

¦ 6.  Manual Steering     C ¦ 1  ¦ 0  ¦ (O)(M)                                ¦ ¦     Disconnect Actuator   ¦    ¦    ¦                                       ¦

¦ 7.  HYD FLUID LOW       C ¦ 1  ¦ 0  ¦ May be inoperative provided           ¦ ¦     Annunciator System    ¦    ¦    ¦ hydraulic fluid level is verified     ¦ ¦                           ¦    ¦    ¦ prior to each departure.              ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 10       ¦ PAGE:    ¦ ¦      BEECH MODEL 1900/1900C SERIES       ¦                       ¦          ¦ ¦                                          ¦ DATE: 03/31/2003      ¦ 32-2     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 32  LANDING GEAR          ¦    ¦    ¦                                       ¦

¦ 8.  Anti-skid System    C ¦ 1  ¦ 0  ¦ May be inoperative provided:          ¦ ¦ ***                       ¦    ¦    ¦     a) The OFF-ON switch remains      ¦ ¦                           ¦    ¦    ¦        in the OFF position, and       ¦ ¦                           ¦    ¦    ¦     b) AFM performance charts for     ¦ ¦                           ¦    ¦    ¦        operation without Anti-Skid    ¦ ¦                           ¦    ¦    ¦        are used.                      ¦

¦                           ¦    ¦    ¦ NOTE: Operation from gravel runways   ¦ ¦                           ¦    ¦    ¦ requires a POH and AFM supplement     ¦ ¦                           ¦    ¦    ¦ for gravel runway operation with      ¦ ¦                           ¦    ¦    ¦ the Hydro-Aire Mark III Anti-Skid     ¦ ¦                           ¦    ¦    ¦ System.                               ¦

¦ 9.  Parking Brake       C ¦ 1  ¦ 0  ¦ (O)                                   ¦

¦ 10. Landing Gear        C ¦ 1  ¦ 0  ¦ (O)May be inoperative provided        ¦ ¦     Handle Solenoid       ¦    ¦    ¦ down lock latch is operative.         ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 10       ¦ PAGE:    ¦ ¦      BEECH MODEL 1900/1900C SERIES       ¦                       ¦          ¦ ¦                                          ¦ DATE: 03/31/2003      ¦ 33-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 33  LIGHTS                ¦    ¦    ¦                                       ¦

¦ 1. Cabin Light          C ¦ -  ¦ -  ¦ May be inoperative provided           ¦ ¦    Systems                ¦    ¦    ¦ lighting configuration is             ¦ ¦                           ¦    ¦    ¦ acceptable to the flight crew.        ¦

¦ 2. Cockpit/Flight Deck/ C ¦ -  ¦ -  ¦ Individual lights may be              ¦ ¦    Flight Compartment     ¦    ¦    ¦ inoperative provided remaining        ¦ ¦    and Instrument         ¦    ¦    ¦ lights are:                           ¦ ¦    Lighting System        ¦    ¦    ¦     a) Sufficient to clearly          ¦ ¦                           ¦    ¦    ¦        illuminate all required        ¦ ¦                           ¦    ¦    ¦        instruments, controls, and     ¦ ¦                           ¦    ¦    ¦        other devices for which it     ¦ ¦                           ¦    ¦    ¦        is provided,                   ¦ ¦                           ¦    ¦    ¦     b) Positioned so that direct      ¦ ¦                           ¦    ¦    ¦        rays are shielded from         ¦ ¦                           ¦    ¦    ¦        flight crewmembers eyes, and   ¦ ¦                           ¦    ¦    ¦     c) Lighting configuration and     ¦ ¦                           ¦    ¦    ¦        intensity is acceptable to     ¦ ¦                           ¦    ¦    ¦        the flight crew.               ¦

¦ 3.  Landing Lights      C ¦ 2  ¦ 0  ¦ May be inoperative for day            ¦ ¦                           ¦    ¦    ¦ operations.                           ¦

¦                         C ¦ 2  ¦ 1  ¦ One may be inoperative for night      ¦ ¦                           ¦    ¦    ¦ operations.                           ¦

¦ 4.  Passenger Notice      ¦    ¦    ¦ DELETED REVISION 10                 | ¦ ¦     System (Fasten Seat   ¦    ¦    ¦ (Moved to ATA 25)                   | ¦ ¦     Belt-No Smoking)      ¦    ¦    ¦                                     | ¦

¦ 5.  Position Lights     C ¦ 3  ¦ 0  ¦ May be inoperative for day            ¦ ¦                           ¦    ¦    ¦ operations.                           ¦

¦ 6.  Anti-Collision      B ¦ 1  ¦ 0  ¦ May be inoperative for day            ¦ ¦     Beacon Light System   ¦    ¦    ¦ operations.                           ¦

¦                         B ¦ 1  ¦ 0  ¦ May be inoperative for night          ¦ ¦                           ¦    ¦    ¦ operations provided Anti-Collision    ¦ ¦                           ¦    ¦    ¦ Strobe Light System is operative.     ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 10       ¦ PAGE:    ¦ ¦      BEECH MODEL 1900/1900C SERIES       ¦                       ¦          ¦ ¦                                          ¦ DATE: 03/31/2003      ¦ 33-2     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 33  LIGHTS                ¦    ¦    ¦                                       ¦

¦ 7.  Anti-Collision      C ¦ 1  ¦ 0  ¦ May be inoperative for day            ¦ ¦     Strobe Light System   ¦    ¦    ¦ operations.                           ¦

¦                         C ¦ 1  ¦ 0  ¦ May be inoperative for night          ¦ ¦                           ¦    ¦    ¦ operations provided Anti-Collision    ¦ ¦                           ¦    ¦    ¦ Beacon Light System is operative.     ¦

¦ 8.  Taxi Light          C ¦ 1  ¦ 0  ¦ May be inoperative for day            ¦ ¦                           ¦    ¦    ¦ operations.                           ¦

¦                         C ¦ 1  ¦ 0  ¦ May be inoperative for night          ¦ ¦                           ¦    ¦    ¦ operations provided both landing      ¦ ¦                           ¦    ¦    ¦ lights are operative.                 ¦

¦ 9.  Taxi Light          C ¦ 1  ¦ 0  ¦                                       ¦ ¦     Annunciator System    ¦    ¦    ¦                                       ¦

¦ 10. Recognition Lights  C ¦ 2  ¦ 0  ¦                                       ¦ ¦ ***                       ¦    ¦    ¦                                       ¦

¦ 11. Tail Flood Lights   C ¦ 2  ¦ 0  ¦                                       ¦ ¦ ***                       ¦    ¦    ¦                                       ¦

¦ 12. Wing Illumination   C ¦ -  ¦ 0  ¦ May be inoperative provided ground  | ¦ ¦     Lights                ¦    ¦    ¦ deicing procedures do not require   | ¦ ¦                           ¦    ¦    ¦ their use.                          | ¦

¦ 13. Master Caution      C ¦ 2  ¦ 1  ¦ One may be inoperative.               ¦ ¦     Lights                ¦    ¦    ¦                                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 10       ¦ PAGE:    ¦ ¦      BEECH MODEL 1900/1900C SERIES       ¦                       ¦          ¦ ¦                                          ¦ DATE: 03/31/2003      ¦ 34-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 34  NAVIGATION            ¦    ¦    ¦                                       ¦

¦ 1.  Gyroscopic Rate of  B ¦ 2  ¦ 1  ¦ Must be operative on left side for    ¦ ¦     Turn/Slip Skid        ¦    ¦    ¦ IFR, passenger carrying VFR over-     ¦ ¦     Indicators            ¦    ¦    ¦ the-top, and passenger carrying VFR   ¦ ¦                           ¦    ¦    ¦ night flights.                        ¦

¦ 2.  Vertical Speed      B ¦ 2  ¦ 1  ¦ One may be inoperative for VFR.       ¦ ¦     Indicators            ¦    ¦    ¦                                       ¦

¦ 3.  Weather Radar/      C ¦ 1  ¦ 0  ¦ As required by FAR.                   ¦ ¦     Thunderstorm          ¦    ¦    ¦                                       ¦ ¦     Detection Equipment   ¦    ¦    ¦                                       ¦

¦ 4.  Gyroscopic          B ¦ 2  ¦ 1  ¦ (O)One may be inoperative in          ¦ ¦     Directional Compass   ¦    ¦    ¦ slaved mode provided DG mode is       ¦ ¦     System                ¦    ¦    ¦ operative.                            ¦

¦ 5.  Non-Stabilized      B ¦ 1  ¦ 0  ¦ (O) May be inoperative provided any | ¦ ¦     Magnetic Compass      ¦    ¦    ¦ combination of three gyro or INS    | ¦ ¦                           ¦    ¦    ¦ (IRU) stabilized compass systems    | ¦ ¦                           ¦    ¦    ¦ are operative.                      | ¦

¦                         B ¦ 1  ¦ 0  ¦ (O) May be inoperative provided:    | ¦ ¦                           ¦    ¦    ¦     a) Any combination of two       | ¦ ¦                           ¦    ¦    ¦        stabilized Gyro or INS (IRU) | ¦ ¦                           ¦    ¦    ¦        Stabilized Compass Systems   | ¦ ¦                           ¦    ¦    ¦        are operative, and           | ¦ ¦                           ¦    ¦    ¦     b) Airplane is operated with    | ¦ ¦                           ¦    ¦    ¦        Dual Independent Navigation  | ¦ ¦                           ¦    ¦    ¦        capability and under         | ¦ ¦                           ¦    ¦    ¦        Positive Radar Control by    | ¦ ¦                           ¦    ¦    ¦        ATC on the enroute portion   | ¦ ¦                           ¦    ¦    ¦        of the flight.               | ¦

¦                (CONT.)    ¦    ¦    ¦                                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 10       ¦ PAGE:    ¦ ¦      BEECH MODEL 1900/1900C SERIES       ¦                       ¦          ¦ ¦                                          ¦ DATE: 03/31/2003      ¦ 34-2     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 34  NAVIGATION            ¦    ¦    ¦                                       ¦

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

¦ 6.  Navigation          C ¦ -  ¦ -  ¦ As required by FAR.                   ¦ ¦ *** Equipment (VOR/ILS,   ¦    ¦    ¦                                       ¦ ¦     Loran, RNAV, INS, GPS ¦    ¦    ¦                                       ¦ ¦     Omega/VLF, Doppler)   ¦    ¦    ¦                                       ¦

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

¦                         D ¦ -  ¦ 1  ¦ Any in excess of those required by  | ¦ ¦                           ¦    ¦    ¦ FAR may be inoperative.             | ¦

¦ 8.  Marker Beacon       C ¦ -  ¦ -  ¦ May be inoperative provided           ¦ ¦                           ¦    ¦    ¦ approach procedure does not require   ¦ ¦                           ¦    ¦    ¦ its use.                              ¦

¦ 9.  Altitude Encoder      ¦    ¦    ¦ Included in Item 7.                 | ¦

¦ 10. Distance Measuring  D ¦ -  ¦ -  ¦ Any in excess of those required by  | ¦ ¦     Equipment (DME)       ¦    ¦    ¦ FAR may be inoperative.             | ¦ ¦     Systems               ¦    ¦    ¦                                     | ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 10       ¦ PAGE:    ¦ ¦      BEECH MODEL 1900/1900C SERIES       ¦                       ¦          ¦ ¦                                          ¦ DATE: 03/31/2003      ¦ 34-3     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 34  NAVIGATION            ¦    ¦    ¦                                       ¦

¦ 11. ADF                 C ¦ 1  ¦ 0  ¦ As required by FAR.                   ¦

¦ 12. Radar Altimeter     C ¦ 1  ¦ 0  ¦ May be inoperative provided           ¦ ¦                           ¦    ¦    ¦ landing minimums are not based on     ¦ ¦                           ¦    ¦    ¦ its use.                              ¦

¦ 13. Flight Director     C ¦ 1  ¦ 0  ¦ May be inoperative provided           ¦ ¦ ***                       ¦    ¦    ¦ landing minimums are not based on     ¦ ¦                           ¦    ¦    ¦ its use.                              ¦

¦ 14. Altitude Alert      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.                | ¦

¦ 15. RMI                 C ¦ -  ¦ 0  ¦                                       ¦

¦ 16. Traffic Alert and   B ¦ -  ¦ 0  ¦ (M)(O)May be inoperative provided:  | ¦ ¦ *** Collision Avoidance   ¦    ¦    ¦     a)System is deactivated and     | ¦ ¦     System (TCAS I)       ¦    ¦    ¦       secured, and                  | ¦ ¦                           ¦    ¦    ¦     b)Enroute or approach           | ¦ ¦                           ¦    ¦    ¦       procedures do not require its | ¦ ¦                           ¦    ¦    ¦       use.                          | ¦

¦                         C ¦ -  ¦ 0  ¦ (M)(O)May be inoperative provided:  | ¦ ¦                           ¦    ¦    ¦     a)Not required by FAR,          | ¦ ¦                           ¦    ¦    ¦     b)System is deactivated and     | ¦ ¦                           ¦    ¦    ¦       secured, and                  | ¦ ¦                           ¦    ¦    ¦     c)Enroute or approach           | ¦ ¦                           ¦    ¦    ¦       procedures do not require its | ¦ ¦                           ¦    ¦    ¦       use.                          | ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 10       ¦ PAGE:    ¦ ¦      BEECH MODEL 1900/1900C SERIES       ¦                       ¦          ¦ ¦                                          ¦ DATE: 03/31/2003      ¦ 34-4     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 34  NAVIGATION            ¦    ¦    ¦                                       ¦

¦ 17. Traffic Alert and   B ¦ -  ¦ 0  ¦ (M)(O)May be inoperative provided:  | ¦ ¦ *** Collision Avoidance   ¦    ¦    ¦     a)System is deactivated and     | ¦ ¦     System (TCAS II)      ¦    ¦    ¦       secured, and                  | ¦ ¦                           ¦    ¦    ¦     b)Enroute or approach           | ¦ ¦                           ¦    ¦    ¦       procedures do not require     | ¦ ¦                           ¦    ¦    ¦       its use.                      | ¦

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

¦     2)Resolution        C ¦ 2  ¦ 1  ¦ May be inoperative on non-flying    | ¦ ¦       Advisory (RA)       ¦    ¦    ¦ pilot side.                         | ¦ ¦       Display System(s)   ¦    ¦    ¦                                     | ¦

¦                         C ¦ -  ¦ 0  ¦ (O)May be inoperative provided:     | ¦ ¦                           ¦    ¦    ¦     a)Traffic Alert (TA) visual     | ¦ ¦                           ¦    ¦    ¦       display and audio functions   | ¦ ¦                           ¦    ¦    ¦       are operative,                | ¦ ¦                           ¦    ¦    ¦     b)TA only mode is selected by   | ¦ ¦                           ¦    ¦    ¦       the crew, and                 | ¦ ¦                           ¦    ¦    ¦     c)Enroute or approach           | ¦ ¦                           ¦    ¦    ¦       procedures do not require     | ¦ ¦                           ¦    ¦    ¦       its use.                      | ¦

¦                 (CONT.)   ¦    ¦    ¦                                     | ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 10       ¦ PAGE:    ¦ ¦      BEECH MODEL 1900/1900C SERIES       ¦                       ¦          ¦ ¦                                          ¦ DATE: 03/31/2003      ¦ 34-5     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 34  NAVIGATION            ¦    ¦    ¦                                       ¦

¦ 17. Traffic Alert and     ¦    ¦    ¦                                     | ¦ ¦ *** Collision Avoidance   ¦    ¦    ¦                                     | ¦ ¦     System (TCAS II)      ¦    ¦    ¦                                     | ¦ ¦                 (CONT.)   ¦    ¦    ¦                                     | ¦

¦     3)Traffic Alert     C ¦ 2  ¦ 1  ¦ (O)May be inoperative provided:     | ¦ ¦       Display             ¦    ¦    ¦    a)RA visual display and audio    | ¦ ¦                           ¦    ¦    ¦      Day VMC only, and              | ¦ ¦                           ¦    ¦    ¦    b)Enroute or approach procedures | ¦ ¦                           ¦    ¦    ¦      do not require its use.        | ¦

¦ 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       | ¦ ¦                           ¦    ¦    ¦        VFR-on-Top conditions.       | ¦

¦ 19. 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.                   ¦

¦                 (CONT.)   ¦    ¦    ¦                                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 10       ¦ PAGE:    ¦ ¦      BEECH MODEL 1900/1900C SERIES       ¦                       ¦          ¦ ¦                                          ¦ DATE: 03/31/2003      ¦ 34-6     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 34  NAVIGATION            ¦    ¦    ¦                                       ¦

¦ 19. Flight Profile        ¦    ¦    ¦                                       ¦ ¦ *** Advisory System       ¦    ¦    ¦                                       ¦ ¦                 (CONT.)   ¦    ¦    ¦                                       ¦

¦    3) Radio Altitude    A ¦ 1  ¦ 0  ¦ (O)May be inoperative provided:       ¦ ¦       Mode                ¦    ¦    ¦     a) Alternate procedures are       ¦ ¦                           ¦    ¦    ¦        established and used and       ¦ ¦                           ¦    ¦    ¦     b) Repairs are made within 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  ¦                                       ¦

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

¦ 20. Ground Proximity    A ¦ -  ¦ 0  ¦ (O)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) Not required by FAR, and     | ¦ ¦                           ¦    ¦    ¦     b) Alternate procedures are     | ¦ ¦                           ¦    ¦    ¦        established and used.        | ¦

¦                (CONT.)    ¦    ¦    ¦                                     | ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 10       ¦ PAGE:    ¦ ¦      BEECH MODEL 1900/1900C SERIES       ¦                       ¦          ¦ ¦                                          ¦ DATE: 03/31/2003      ¦ 34-7     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 34  NAVIGATION            ¦    ¦    ¦                                       ¦

¦ 20. Ground Proximity      ¦    ¦    ¦                                     | ¦ ¦ *** Warning System        ¦    ¦    ¦                                     | ¦ ¦                (CONT.)    ¦    ¦    ¦                                     | ¦

¦     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) 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.                 | ¦

¦     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.            | ¦

¦                (CONT.)    ¦    ¦    ¦                                     | ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 10       ¦ PAGE:    ¦ ¦      BEECH MODEL 1900/1900C SERIES       ¦                       ¦          ¦ ¦                                          ¦ DATE: 03/31/2003      ¦ 34-8     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 34  NAVIGATION            ¦    ¦    ¦                                       ¦

¦ 20. Ground Proximity      ¦    ¦    ¦                                     | ¦ ¦ *** Warning System        ¦    ¦    ¦                                     | ¦ ¦                (CONT.)    ¦    ¦    ¦                                     | ¦

¦     5)Windshear Mode    C ¦ -  ¦ 0  ¦ (O)May be inoperative provided:     | ¦ ¦                           ¦    ¦    ¦    a)Alternate procedures are       | ¦ ¦                           ¦    ¦    ¦      established and used, and      | ¦ ¦                           ¦    ¦    ¦    b)Winshear 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 know or       | ¦ ¦                           ¦    ¦    ¦      forecast windshear conditions. | ¦

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

¦ 21. CARGO OPERATIONS ONLY ¦    ¦    ¦                                       ¦ ¦     SIC NOT REQUIRED      ¦    ¦    ¦                                       ¦

¦     1) Airspeed         B ¦ 2  ¦ 1  ¦ May be inoperative on right side      ¦ ¦        Indicator          ¦    ¦    ¦ provided:                             ¦ ¦                           ¦    ¦    ¦     a) A functioning pneumatic        ¦ ¦                           ¦    ¦    ¦        indicator is installed and     ¦ ¦                           ¦    ¦    ¦        available to the pilot, and    ¦ ¦                           ¦    ¦    ¦     b) Aircraft must be flown from    ¦ ¦                           ¦    ¦    ¦        left side by the pilot in      ¦ ¦                           ¦    ¦    ¦        command.                       ¦

¦                (CONT.)    ¦    ¦    ¦                                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 10       ¦ PAGE:    ¦ ¦      BEECH MODEL 1900/1900C SERIES       ¦                       ¦          ¦ ¦                                          ¦ DATE: 03/31/2003      ¦ 34-9     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 34  NAVIGATION            ¦    ¦    ¦                                       ¦

¦ 21. CARGO OPERATIONS ONLY ¦    ¦    ¦                                       ¦ ¦     SIC NOT REQUIRED      ¦    ¦    ¦                                       ¦ ¦                 (CONT.)   ¦    ¦    ¦                                       ¦

¦     2) Gyroscopic Bank  B ¦ 2  ¦ 1  ¦ May be inoperative on right side      ¦ ¦        and Pitch          ¦    ¦    ¦ provided:                             ¦ ¦        Indicator          ¦    ¦    ¦     a) Two independent power          ¦ ¦                           ¦    ¦    ¦        sources are available to       ¦ ¦                           ¦    ¦    ¦        drive the left side            ¦ ¦                           ¦    ¦    ¦        instruments,                   ¦ ¦                           ¦    ¦    ¦     b) Aircraft does not have an      ¦ ¦                           ¦    ¦    ¦        Electronic Attitude            ¦ ¦                           ¦    ¦    ¦        Direction Indicator (EADI)     ¦ ¦                           ¦    ¦    ¦        installed on left side, and    ¦ ¦                           ¦    ¦    ¦     c) Aircraft must be flown from    ¦ ¦                           ¦    ¦    ¦        left side by the pilot in      ¦ ¦                           ¦    ¦    ¦        command.                       ¦

¦     3) Gyroscopic       B ¦ 2  ¦ 1  ¦ May be inoperative on right side      ¦ ¦        Direction          ¦    ¦    ¦ provided:                             ¦ ¦        Indicator          ¦    ¦    ¦     a) Magnetic compass is            ¦ ¦                           ¦    ¦    ¦        operative,                     ¦ ¦                           ¦    ¦    ¦     b) Two independent power          ¦ ¦                           ¦    ¦    ¦        sources are available to       ¦ ¦                           ¦    ¦    ¦        drive the left side            ¦ ¦                           ¦    ¦    ¦        instruments, and               ¦ ¦                           ¦    ¦    ¦     c) Aircraft must be flown from    ¦ ¦                           ¦    ¦    ¦        left side by the pilot in      ¦ ¦                           ¦    ¦    ¦        command.                       ¦

¦     4) Altimeter        B ¦ 2  ¦ 1  ¦ May be inoperative on right side      ¦ ¦        Barometric         ¦    ¦    ¦ provided:                             ¦ ¦                           ¦    ¦    ¦     a) A functioning pneumatic        ¦ ¦                           ¦    ¦    ¦        altimeter, adjustable for      ¦ ¦                           ¦    ¦    ¦        barometric pressure, is        ¦ ¦                           ¦    ¦    ¦        installed and available to     ¦ ¦                           ¦    ¦    ¦        the pilot, and                 ¦ ¦                           ¦    ¦    ¦     b) Aircraft must be flown from    ¦ ¦                           ¦    ¦    ¦        left side by the pilot in      ¦ ¦                           ¦    ¦    ¦        command.                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 10       ¦ PAGE:    ¦ ¦      BEECH MODEL 1900/1900C SERIES       ¦                       ¦          ¦ ¦                                          ¦ DATE: 03/31/2003      ¦ 34-10    ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 34  NAVIGATION            ¦    ¦    ¦                                       ¦

¦ 22. Windshear Warning   C ¦ -  ¦ 0  ¦ (O) May be inoperative provided:    | ¦ ¦     and Flight Guidance   ¦    ¦    ¦     a) Alternate procedures are     | ¦ ¦     System                ¦    ¦    ¦        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.                  | ¦

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

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

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 10       ¦ PAGE:    ¦ ¦      BEECH MODEL 1900/1900C SERIES       ¦                       ¦          ¦ ¦                                          ¦ DATE: 03/31/2003      ¦ 34-11    ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 34  NAVIGATION            ¦    ¦    ¦                                       ¦

¦ 24. Flight Management   C ¦ -  ¦ -  ¦ (O) May be out of currency          | ¦ ¦     System Navigation     ¦    ¦    ¦     provided:                       | ¦ ¦     Database              ¦    ¦    ¦     a) Current Aeronautical Charts  | ¦ ¦                           ¦    ¦    ¦        are used to verify           | ¦ ¦                           ¦    ¦    ¦        navigation fixes prior to    | ¦ ¦                           ¦    ¦    ¦        dispatch,                    | ¦ ¦                           ¦    ¦    ¦     b) Procedures are established   | ¦ ¦                           ¦    ¦    ¦        and used to verify status of | ¦ ¦                           ¦    ¦    ¦        navigation facilities used   | ¦ ¦                           ¦    ¦    ¦        to define route of flight,   | ¦ ¦                           ¦    ¦    ¦        and                          | ¦ ¦                           ¦    ¦    ¦     c) Approach Navigation Radios   | ¦ ¦                           ¦    ¦    ¦        are manually tuned and       | ¦ ¦                           ¦    ¦    ¦        identified.                  | ¦

¦ 25. Navigation          C ¦ -  ¦ -  ¦ (O) May be out of currency          | ¦ ¦     Management System     ¦    ¦    ¦     provided:                       | ¦ ¦     Navigation Database   ¦    ¦    ¦     a) Current Aeronautical Charts  | ¦ ¦                           ¦    ¦    ¦        are used to verify           | ¦ ¦                           ¦    ¦    ¦        navigation fixes prior to    | ¦ ¦                           ¦    ¦    ¦        dispatch,                    | ¦ ¦                           ¦    ¦    ¦     b) Procedures are established   | ¦ ¦                           ¦    ¦    ¦        and used to verify status of | ¦ ¦                           ¦    ¦    ¦        navigation facilities used   | ¦ ¦                           ¦    ¦    ¦        to define route of flight,   | ¦ ¦                           ¦    ¦    ¦        and                          | ¦ ¦                           ¦    ¦    ¦     c) Approach Navigation Radios   | ¦ ¦                           ¦    ¦    ¦        are manually tuned and       | ¦ ¦                           ¦    ¦    ¦        identified.                  | ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 10       ¦ PAGE:    ¦ ¦      BEECH MODEL 1900/1900C SERIES       ¦                       ¦          ¦ ¦                                          ¦ DATE: 03/31/2003      ¦ 34-12    ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 34  NAVIGATION            ¦    ¦    ¦                                       ¦

¦ 26. Automatic Dependent D ¦ -  ¦ 0  ¦ May be inoperative provided not     | ¦ ¦     Surveillance-         ¦    ¦    ¦ required by 14 CFR.                 | ¦ ¦     Broadcast (ADS-B)     ¦    ¦    ¦                                     | ¦ ¦     System                ¦    ¦    ¦ NOTE: If ADS-B is installed in lieu | ¦ ¦                           ¦    ¦    ¦ of or as a replacement for 14 CFR   | ¦ ¦                           ¦    ¦    ¦ required equipment, the repair      | ¦ ¦                           ¦    ¦    ¦ category in the operator's MEL will | ¦ ¦                           ¦    ¦    ¦ be the same as that of the 14 CFR   | ¦ ¦                           ¦    ¦    ¦ required equipment.                 | ¦

¦     1) Link and Display D ¦ -  ¦ 0  ¦                                     | ¦ ¦        Processor Unit     ¦    ¦    ¦                                     | ¦ ¦        (LDPU)             ¦    ¦    ¦ NOTE: Cockpit Display Traffic       | ¦ ¦                           ¦    ¦    ¦ Information (CDTI) display of data  | ¦ ¦                           ¦    ¦    ¦ from other aircraft systems may be  | ¦ ¦                           ¦    ¦    ¦ used.                               | ¦

¦     2) Cockpit Display  D ¦ -  ¦ 0  ¦                                     | ¦ ¦        and Traffic        ¦    ¦    ¦                                     | ¦ ¦        Information (CDTI) ¦    ¦    ¦ NOTE: ADS-B data transmissions      | ¦ ¦                           ¦    ¦    ¦ may continue.                       | ¦

¦     3) CDTI Control     D ¦ -  ¦ 0  ¦ May be inoperative provided:        | ¦ ¦        Panel              ¦    ¦    ¦     a) Flight ID can be set, and    | ¦ ¦                           ¦    ¦    ¦     b) Screen display is acceptable | ¦ ¦                           ¦    ¦    ¦        to the flight crew.          | ¦

¦     4) Data Link        D ¦ -  ¦ 0  ¦                                     | ¦ ¦        Transmitter(s)     ¦    ¦    ¦                                     | ¦

¦     5) Data Link        D ¦ -  ¦ 0  ¦                                     | ¦ ¦        Receiver(s)        ¦    ¦    ¦                                     | ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 10       ¦ PAGE:    ¦ ¦      BEECH MODEL 1900/1900C SERIES       ¦                       ¦          ¦ ¦                                          ¦ DATE: 03/31/2003      ¦ 35-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 35  OXYGEN                ¦    ¦    ¦                                       ¦

¦ 1.  Oxygen System       C ¦ 1  ¦ 0  ¦ As required by FAR.                   ¦ ¦     (Passenger)           ¦    ¦    ¦                                       ¦

¦ 2.  External Oxygen     C ¦ 1  ¦ 0  ¦ May be inoperative provided a         ¦ ¦     Gauge                 ¦    ¦    ¦ maintenance or flight crewmember      ¦ ¦                           ¦    ¦    ¦ is in the cockpit and monitors the    ¦ ¦                           ¦    ¦    ¦ internal oxygen gauge during          ¦ ¦                           ¦    ¦    ¦ servicing to avoid over-servicing.    ¦

¦ 3.  Passenger Oxygen    C ¦ 19 ¦ 0  ¦ (M)May be inoperative provided:       ¦ ¦     Mask/Regulator        ¦    ¦    ¦      a)  Corresponding passenger      ¦ ¦                           ¦    ¦    ¦          seat is blocked and          ¦ ¦                           ¦    ¦    ¦          placarded "DO NOT OCCUPY".   ¦ ¦                           ¦    ¦    ¦      b)  Affected mask/regulator      ¦ ¦                           ¦    ¦    ¦          does not permit flow when    ¦ ¦                           ¦    ¦    ¦          cabin oxygen system is       ¦ ¦                           ¦    ¦    ¦          activated.                   ¦

¦ 4. Protective Breathing D ¦ -  ¦ -  ¦ Any in excess of those required by  | ¦ ¦    Equipment              ¦    ¦    ¦ FAR may be missing or inoperative.  | ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 10       ¦ PAGE:    ¦ ¦      BEECH MODEL 1900/1900C SERIES       ¦                       ¦          ¦ ¦                                          ¦ DATE: 03/31/2003      ¦ 37-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 37  VACUUM/PRESSURE       ¦    ¦    ¦                                       ¦

¦ 1.  Gyro Suction Gauge  C ¦ 1  ¦ 0  ¦ May be inoperative for day VFR.       ¦

¦                         C ¦ 1  ¦ 0  ¦ May be inoperative if all             ¦ ¦                           ¦    ¦    ¦ gyroscopic instruments except right   ¦ ¦                           ¦    ¦    ¦ side rate of turn/slip skid           ¦ ¦                           ¦    ¦    ¦ indicator is electrically powered.    ¦

¦ 2.  Instrument Air      C ¦ 2  ¦ 1  ¦ (O)One may be inoperative for         ¦ ¦     Valve                 ¦    ¦    ¦ aircraft in which all gyroscopic      ¦ ¦                           ¦    ¦    ¦ instruments except for the right      ¦ ¦                           ¦    ¦    ¦ side rate of turn/slip skid           ¦ ¦                           ¦    ¦    ¦ indicator are electrically powered    ¦ ¦                           ¦    ¦    ¦ provided:                             ¦ ¦                           ¦    ¦    ¦     a) The inoperative valve is       ¦ ¦                           ¦    ¦    ¦        verified closed, and           ¦ ¦                           ¦    ¦    ¦     b) Aircraft is not operated in    ¦ ¦                           ¦    ¦    ¦        known or forecast icing        ¦ ¦                           ¦    ¦    ¦        conditions.                    ¦

¦                         C ¦ 2  ¦ 1  ¦ (O)One may be inoperative for VFR     ¦ ¦                           ¦    ¦    ¦ flights for aircraft equipped with    ¦ ¦                           ¦    ¦    ¦ an air driven copilot's attitude      ¦ ¦                           ¦    ¦    ¦ indicator provided the inoperative    ¦ ¦                           ¦    ¦    ¦ valve is verified closed.             ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 10       ¦ PAGE:    ¦ ¦      BEECH MODEL 1900/1900C SERIES       ¦                       ¦          ¦ ¦                                          ¦ DATE: 03/31/2003      ¦ 38-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 38  WATER/WASTE           ¦    ¦    ¦                                     | ¦

¦ 1.  Potable Water       C ¦ -  ¦ -  ¦ (M) Individual components may be    | ¦ ¦     System                ¦    ¦    ¦ inoperative provided:               | ¦ ¦                           ¦    ¦    ¦     a) Associated components are    | ¦ ¦                           ¦    ¦    ¦        deactivated or isolated, and | ¦ ¦                           ¦    ¦    ¦     b) Associated system            | ¦ ¦                           ¦    ¦    ¦        components are verified not  | ¦ ¦                           ¦    ¦    ¦        to have leaks.               | ¦

¦                           ¦    ¦    ¦ NOTE: Any portion of the system     | ¦ ¦                           ¦    ¦    ¦ which operates normally may be      | ¦ ¦                           ¦    ¦    ¦ used.                               | ¦

¦                         C ¦ -  ¦ -  ¦ (M) May be inoperative provided:    | ¦ ¦                           ¦    ¦    ¦     a) System is drained, and       | ¦ ¦                           ¦    ¦    ¦     b) Procedures are established   | ¦ ¦                           ¦    ¦    ¦        to ensure the system is not  | ¦ ¦                           ¦    ¦    ¦        serviced prior to repair.    | ¦

¦ 2.  Lavatory Waste      C ¦ -  ¦ -  ¦ (M) Individual Ccomponents may be   | ¦ ¦     Systems               ¦    ¦    ¦ inoperative provided:               | ¦ ¦                           ¦    ¦    ¦     a) Associated componenets are   | ¦ ¦                           ¦    ¦    ¦        deactivated or isolated, and | ¦ ¦                           ¦    ¦    ¦     b) Associated system components | ¦ ¦                           ¦    ¦    ¦        are verified not to have     | ¦ ¦                           ¦    ¦    ¦        leaks.                       | ¦

¦                           ¦    ¦    ¦ NOTE:  Any portion of system which  | ¦ ¦                           ¦    ¦    ¦        operates normally may be     | ¦ ¦                           ¦    ¦    ¦        used.                        | ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 10       ¦ PAGE:    ¦ ¦      BEECH MODEL 1900/1900C SERIES       ¦                       ¦          ¦ ¦                                          ¦ DATE: 03/31/2003      ¦ 52-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 52  DOORS                 ¦    ¦    ¦                                       ¦

¦ 1.  Forward Cabin Door  C ¦ 1  ¦ 0  ¦ May be inoperative provided:          ¦ ¦     Warning Light         ¦    ¦    ¦     a) A flight crewmember confirms   ¦ ¦                           ¦    ¦    ¦        by visual inspection that      ¦ ¦                           ¦    ¦    ¦        the door is latched prior to   ¦ ¦                           ¦    ¦    ¦        each departure, and            ¦ ¦                           ¦    ¦    ¦     b) Fasten seat belt sign          ¦ ¦                           ¦    ¦    ¦        remains on.                    ¦

¦ 2.  Aft Cabin Door      C ¦ 1  ¦ 0  ¦ May be inoperative provided:          ¦ ¦     Warning Light         ¦    ¦    ¦     a) A flight crewmember confirms   ¦ ¦     (Cabin/Cargo)         ¦    ¦    ¦        by visual inspection that      ¦ ¦                           ¦    ¦    ¦        the door is latched prior to   ¦ ¦                           ¦    ¦    ¦        each departure, and            ¦ ¦                           ¦    ¦    ¦     b) Fasten seat belt sign          ¦ ¦                           ¦    ¦    ¦        remains on.                    ¦

¦ 3.  Air Stair Door      C ¦ 1  ¦ 0  ¦ May be inoperative provided a         ¦ ¦     Lock Observe Light(s) ¦    ¦    ¦ flashlight is used by a crewmember    ¦ ¦     System                ¦    ¦    ¦ to inspect the locking mechanism      ¦ ¦                           ¦    ¦    ¦ prior to each departure.              ¦

¦ 4.  Nose Baggage        C ¦ 1  ¦ 0  ¦ (M)(O) May be inoperative provided: | ¦ ¦     Compartment Door      ¦    ¦    ¦     a) The locking mechanism is       ¦ ¦     Warning Light System  ¦    ¦    ¦        inspected for proper           ¦ ¦                           ¦    ¦    ¦        operations, and                ¦ ¦                           ¦    ¦    ¦     b) A flight crewmember confirms   ¦ ¦                           ¦    ¦    ¦        by visual inspection that      ¦ ¦                           ¦    ¦    ¦        the compartment is empty and   ¦ ¦                           ¦    ¦    ¦        that all baggage door          ¦ ¦                           ¦    ¦    ¦        latches and fasteners are      ¦ ¦                           ¦    ¦    ¦        secured prior to each          ¦ ¦                           ¦    ¦    ¦        departure.                     ¦

¦ 5.  Entrance Door       C ¦ 1  ¦ 0  ¦ (O)                                   ¦ ¦     Snubber               ¦    ¦    ¦                                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 10       ¦ PAGE:    ¦ ¦      BEECH MODEL 1900/1900C SERIES       ¦                       ¦          ¦ ¦                                          ¦ DATE: 03/31/2003      ¦ 61-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 61  PROPELLERS            ¦    ¦    ¦                                       ¦

¦ 1.  Propeller           C ¦ 1  ¦ 0  ¦                                       ¦ ¦     Synchrophaser/        ¦    ¦    ¦                                       ¦ ¦     Synchronizer System   ¦    ¦    ¦                                       ¦

¦ 2.  Propeller           C ¦ 1  ¦ 0  ¦                                       ¦ ¦     Synchroscope          ¦    ¦    ¦                                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 10       ¦ PAGE:    ¦ ¦      BEECH MODEL 1900/1900C SERIES       ¦                       ¦          ¦ ¦                                          ¦ DATE: 03/31/2003      ¦ 79-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 79  ENGINE OIL            ¦    ¦    ¦                                       ¦

¦ 1.  Oil Low Pressure    C ¦ 2  ¦ 1  ¦ One may be inoperative provided:      ¦ ¦     Warning Lights        ¦    ¦    ¦     a) Corresponding oil pressure     ¦ ¦                           ¦    ¦    ¦        and oil temperature gauges     ¦ ¦                           ¦    ¦    ¦        are operative and              ¦ ¦                           ¦    ¦    ¦        monitored, and                 ¦ ¦                           ¦    ¦    ¦     b) Light will not be              ¦ ¦                           ¦    ¦    ¦        illuminated for flight.        ¦