DEPARTMENT OF TRANSPORTATION     Revision: 1 a

Date: 05/20/2004

FEDERAL AVIATION ADMINISTRATION

WASHINGTON, D.C.

M A S T E R   M I N I M U M   E Q U I P M E N T   L I S T

FAIRCHILD/DORNIER D-328JET

FOEB CHAIRMAN, JAMES L. MARTIN

Federal Aviation Administration Flight Standards Division AIRCRAFT EVALUATION GROUP,

1601 Lind Ave. S.W.

Renton, Washington 98055-4056

TELEPHONE: COMM: (425) 917-6627

FAX:  (425) 917-6638

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FAIRCHILD/DORNIER D-328JET

Table of Contents

SYSTEM NO.  SYSTEM                                  PAGE

--     Table of Contents                       I

--     Log of Revisions                        II

--     Control Page                            III, IV, V

--     Highlights of Change                    VI, VII, VIII

--     Definitions                             IX, X, XI, XII

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

21     Air Conditioning                        21-1, 2, 3, 4, 5 22     Auto Flight                             22-1, 2, 3, 4, 5 23     Communications                          23-1, 2, 3, 4, 5 23     Communications                          23-6

24     Electrical Power                        24-1, 2, 3, 4, 5 24     Electrical Power                        24-6, 7

25     Equipment/Furnishings                   25-1, 2, 3, 4, 5 25     Equipment/Furnishings                   25-6

26     Fire Protection                         26-1, 2, 3, 4, 5 27     Flight Controls                         27-1, 2, 3, 4

28     Fuel                                    28-1, 2, 3, 4, 5 28     Fuel                                    28-6, 7, 8, 9

29     Hydraulic Power                         29-1

30     Ice and Rain Protection                 30-1, 2, 3, 4, 5 30     Ice and Rain Protection                 30-6, 7, 8

31     Indicating/Recording Systems            31-1

32     Landing Gear                            32-1

33     Lights                                  33-1, 2, 3, 4, 5 34     Navigation                              34-1, 2, 3, 4, 5 34     Navigation                              34-6, 7, 8, 9

35     Oxygen                                  35-1, 2 36     Pneumatic                               36-1

38     Water/Waste                             38-1, 2 49     Airborne Auxiliary Power                49-1

73     Engine Fuel & Control                   73-1 77     Engine Indicating                       77-1 79     Engine Oil                              79-1

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Log of Revisions

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

¦ 1        ¦ 11/15/2001 ¦ HIGHLIGHTS OF REV.,DEFINITIONS ¦           ¦ ¦ 1        ¦ 11/15/2001 ¦ 21-1,22-1,23-2,23-3,23-4       ¦           ¦ ¦ 1        ¦ 11/15/2001 ¦ 23-5,23-6,25-6,26-1,26-2       ¦           ¦ ¦ 1        ¦ 11/15/2001 ¦ 26-3,26-4,26-5,28-7,28-8       ¦           ¦ ¦ 1        ¦ 11/15/2001 ¦ 28-9,33-5,34-5,34-9,35-1       ¦           ¦ ¦ 1        ¦ 11/15/2001 ¦ 38-1,38-2                      ¦           ¦ ¦ 1a       ¦            ¦ HIGHLIGHTS OF REV.,DEFINITIONS ¦           ¦ ¦ 1a       ¦            ¦ 28-9,34-9                      ¦           ¦

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Control Page

SYSTEM                                   PAGE  REV NO.  CURRENT DATE

Cover Page                               -       1 a      05/20/2004 Table of Contents                        I       1 a      05/20/2004 Log of Revisions                         II      1 a      05/20/2004 Control Page                             III     1 a      05/20/2004 IV      1 a      05/20/2004 V       1 a      05/20/2004 Highlights of Change                     VI      1 a      05/20/2004 VII     1        11/15/2001 VIII    1        11/15/2001 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 21                                       21-1    1         11/15/2001 21-2    ORIGINAL 07/30/1999 21-3    ORIGINAL 07/30/1999 21-4    ORIGINAL 07/30/1999 21-5    ORIGINAL 07/30/1999 22                                           22-1    1        11/15/2001 22-2       ORIGINAL 07/30/1999 22-3    ORIGINAL 07/30/1999 22-4    ORIGINAL 07/30/1999 22-5    ORIGINAL 07/30/1999 23                                        23-1    ORIGINAL 07/30/1999 23-2    1        11/15/2001 23-3    1        11/15/2001 23-4    1        11/15/2001 23-5    1        11/15/2001 23-6    1        11/15/2001 24                                               24-1    ORIGINAL 07/30/1999 24-2    ORIGINAL 07/30/1999 24-3    ORIGINAL 07/30/1999 24-4    ORIGINAL 07/30/1999                                          24-5    ORIGINAL 07/30/1999

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Control Page

SYSTEM                                   PAGE  REV NO.  CURRENT DATE

24-6    ORIGINAL 07/30/1999 24-7    ORIGINAL 07/30/1999 25                                           25-1    ORIGINAL 07/30/1999 25-2       ORIGINAL 07/30/1999 25-3    ORIGINAL 07/30/1999 25-4    ORIGINAL 07/30/1999 25-5    ORIGINAL 07/30/1999 25-6    1        11/15/2001 26                                       26-1    1        11/15/2001 26-2    1        11/15/2001 26-3    1        11/15/2001 26-4    1        11/15/2001 26-5    1        11/15/2001 27                                               27-1    ORIGINAL 07/30/1999 27-2    ORIGINAL 07/30/1999 27-3    ORIGINAL 07/30/1999 27-4    ORIGINAL 07/30/1999 28                                       28-1    ORIGINAL 07/30/1999     28-2    ORIGINAL 07/30/1999 28-3    ORIGINAL 07/30/1999 28-4       ORIGINAL 07/30/1999 28-5    ORIGINAL 07/30/1999 28-6    ORIGINAL 07/30/1999 28-7    1        11/15/2001 28-8    1        11/15/2001 28-9    1 a      05/20/2004 29                                       29-1    ORIGINAL 07/30/1999 30                                           30-1    ORIGINAL 07/30/1999 30-2    ORIGINAL 07/30/1999 30-3       ORIGINAL 07/30/1999 30-4    ORIGINAL 07/30/1999 30-5    ORIGINAL 07/30/1999 30-6    ORIGINAL 07/30/1999 30-7    ORIGINAL 07/30/1999 30-8    ORIGINAL 07/30/1999 31                                       31-1    ORIGINAL 07/30/1999 32                                       32-1    ORIGINAL 07/30/1999 33                                           33-1    ORIGINAL 07/30/1999 33-2    ORIGINAL 07/30/1999 33-3                                                     ORIGINAL 07/30/1999

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Control Page

SYSTEM                                   PAGE  REV NO.  CURRENT DATE

33-4    ORIGINAL 07/30/1999 33-5    1        11/15/2001 34                                           34-1    ORIGINAL 07/30/1999 34-2       ORIGINAL 07/30/1999 34-3    ORIGINAL 07/30/1999 34-4    ORIGINAL 07/30/1999 34-5    1        11/15/2001 34-6    ORIGINAL 07/30/1999 34-7    ORIGINAL 07/30/1999 34-8    ORIGINAL 07/30/1999 34-9    1 a      05/20/2004 35                                       35-1    1        11/15/2001 35-2    ORIGINAL 07/30/1999 36                                       36-1    ORIGINAL 07/30/1999 38                                               38-1    1        11/15/2001 38-2    1        11/15/2001 49                                       49-1    ORIGINAL 07/30/1999 73                                       73-1    ORIGINAL 07/30/1999 77                                       77-1    ORIGINAL 07/30/1999 79                                       79-1    ORIGINAL                                                           07/30/1999

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Highlights of Change

EFFECTIVE ABOVE DATE, The DO-328-300 MMEL has been revised.  The changes in this revision were made to provide relief for additional

equipment installed on the aircraft.

Retain this sheet with your MMEL until the next revision is issued.

ATA 28  FUEL

Page 28-9:  Item 40-11, EICAS Indication (Blue) L & R FUEL QTY ACCUR Illuminated - New Item.

ATA 34  NAVIGATION

Page 34-9:  Item 63-00, Cockpit Printer - New Item.

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Highlights of Change

ATA 26 FIRE PROTECTION

Item 14-00:  Changes were made to comply with Policy Letter 108.

Item 15-00: Changes were made to comply with Policy Letter 24.

Item 24-00: Changes were made to comply with Policy Letter 108.

Item 25-00: Changes were made to comply with Policy Letter 24.

ATA 28 FUEL

Item 40-04: New optional item.

Item 40-05: New optional item.

Item 40-06: New optional item.

Item 40-07: New optional item.

Item 40-08: New optional item.

Item 40-09: New optional item.

Item 40-10: New optional item.

ATA 33  LIGHTS

Item 44-00: Changed number installed from 1 to 2.

Item 52-00: New optional item.

ATA 34  NAVIGATION

Item 53-00: Change was made to comply with Policy Letter 76.

Item 62-00: New optional item.

ATA 35  OXYGEN

Item 10-00:  Editorial correction to the note.

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Highlights of Change

ATA 38  WATER/WASTE

Item 10-00:  Changes made to comply with Policy Letter 83.

Item 11-00:  Changes made to comply with Policy Letter 83.

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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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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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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

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  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

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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.

 

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FAIRCHILD/DORNIER D-328JET

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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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 1        ¦ PAGE:    ¦ ¦        FAIRCHILD/DORNIER D-328JET        ¦                       ¦          ¦ ¦                                          ¦ DATE: 11/15/2001      ¦ 21-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 21  AIR CONDITIONING      ¦    ¦    ¦                                       ¦

¦ 21-00 Avionics Fan      B ¦ 1  ¦ 0  ¦ (M)May be inoperative deactivated     ¦ ¦                           ¦    ¦    ¦ provided:                             ¦ ¦                           ¦    ¦    ¦     a) EFIS Fan is operative, and     ¦ ¦                           ¦    ¦    ¦     b) ECS Flow Mode is operated      ¦ ¦                           ¦    ¦    ¦        in HIGH.                       ¦

¦       01) "FAIL"        C ¦ 1  ¦ 0  ¦ (M)(O)May be inoperative provided:    ¦ ¦           Annunciator     ¦    ¦    ¦     a) AVIONIC Fan is operative,      ¦ ¦           Light on        ¦    ¦    ¦        and                            ¦ ¦           AVIONIC FAN     ¦    ¦    ¦     b) Light erroneously on is        ¦ ¦           Pushbutton      ¦    ¦    ¦        masked or deactivated.         ¦ ¦           (Overhead       ¦    ¦    ¦                                       ¦ ¦           Panel)          ¦    ¦    ¦                                       ¦

¦       02) "OFF"         C ¦ 1  ¦ 0  ¦ (M)(O)May be inoperative provided:    ¦ ¦           Annunciator     ¦    ¦    ¦     a) AVIONIC Fan is operative,      ¦ ¦           Light on        ¦    ¦    ¦        and                            ¦ ¦           AVIONIC FAN     ¦    ¦    ¦     b) Light erroneously on is        ¦ ¦           Pushbutton      ¦    ¦    ¦        masked or deactivated.         ¦ ¦           (Overhead       ¦    ¦    ¦                                       ¦ ¦           Panel)          ¦    ¦    ¦                                       ¦

¦ 22-00 EFIS Fan          B ¦ 1  ¦ 0  ¦ (M)May be inoperative deactivated     ¦ ¦                           ¦    ¦    ¦ provided:                             ¦ ¦                           ¦    ¦    ¦     a) AVIONIC Fan is operative,      ¦ ¦                           ¦    ¦    ¦        and                            ¦ ¦                           ¦    ¦    ¦     b) ECS Flow Mode is operated      ¦ ¦                           ¦    ¦    ¦        in HIGH.                       ¦

¦       01) "FAIL"        C ¦ 1  ¦ 0  ¦ (M)(O)May be inoperative provided:    ¦ ¦           Annunciator     ¦    ¦    ¦     a) EFIS Fan is operative, and     ¦ ¦           Light on EFIS   ¦    ¦    ¦     b) Light erroneously on is        ¦ ¦           FAN             ¦    ¦    ¦        masked or deactivated.         ¦ ¦           Pushbutton      ¦    ¦    ¦                                       ¦ ¦           (Overhead       ¦    ¦    ¦                                       ¦ ¦           Panel)          ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦ (Continued)                           ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: ORIGINAL ¦ PAGE:    ¦ ¦        FAIRCHILD/DORNIER D-328JET        ¦                       ¦          ¦ ¦                                          ¦ DATE: 07/30/1999      ¦ 21-2     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 21  AIR CONDITIONING      ¦    ¦    ¦                                       ¦

¦ 22-00 EFIS Fan            ¦    ¦    ¦                                       ¦ ¦       (Cont'd)            ¦    ¦    ¦                                       ¦

¦       02) "OFF"         C ¦ 1  ¦ 0  ¦ (M)(O)May be inoperative provided:    ¦ ¦           Annunciator     ¦    ¦    ¦     a) EFIS Fan is operative, and     ¦ ¦           Light on        ¦    ¦    ¦     b) Light erroneously on is        ¦ ¦           EFIS FAN        ¦    ¦    ¦        masked or deactivated.         ¦ ¦           Pushbutton      ¦    ¦    ¦                                       ¦ ¦           (Overhead       ¦    ¦    ¦                                       ¦ ¦           Panel)          ¦    ¦    ¦                                       ¦

¦ 23-00 Recirculation     C ¦ 2  ¦ 0  ¦ (M)May be inoperative deactivated     ¦ ¦       Fans                ¦    ¦    ¦ provided ECS Flow Mode is operated    ¦ ¦                           ¦    ¦    ¦ in HIGH.                              ¦

¦       01) "OFF"         C ¦ 1  ¦ 0  ¦ (M)(O)May be inoperative provided:    ¦ ¦           Annunciator     ¦    ¦    ¦     a) Both Recirculation Fans        ¦ ¦           Light on        ¦    ¦    ¦        are operative, and             ¦ ¦           RECIRC FAN      ¦    ¦    ¦     b) Light erroneously on is        ¦ ¦           Pushbutton      ¦    ¦    ¦        masked or deactivated.         ¦ ¦           (Overhead       ¦    ¦    ¦                                       ¦ ¦           Panel)          ¦    ¦    ¦                                       ¦

¦ 31-00 Cabin             C ¦ 1  ¦ 0  ¦ (M)(O)May be inoperative provided:    ¦ ¦       Pressurization      ¦    ¦    ¦     a) Aircraft is operated in        ¦ ¦       Control System      ¦    ¦    ¦        an unpressurized               ¦ ¦       (CPCS)              ¦    ¦    ¦        configuration, and             ¦ ¦                           ¦    ¦    ¦     b) Either outflow valve is        ¦ ¦                           ¦    ¦    ¦        secured open.                  ¦

¦       01) Automatic     C ¦ 1  ¦ 0  ¦ (M)(O)May be inoperative provided:    ¦ ¦           Mode            ¦    ¦    ¦     a) Manual Pressurization          ¦ ¦                           ¦    ¦    ¦        Mode is verified to operate    ¦ ¦                           ¦    ¦    ¦        normally, and                  ¦ ¦                           ¦    ¦    ¦     b) CPCS Automatic Controller      ¦ ¦                           ¦    ¦    ¦        is deactivated.                ¦

¦                           ¦    ¦    ¦ (Continued)                           ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: ORIGINAL ¦ PAGE:    ¦ ¦        FAIRCHILD/DORNIER D-328JET        ¦                       ¦          ¦ ¦                                          ¦ DATE: 07/30/1999      ¦ 21-3     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 21  AIR CONDITIONING      ¦    ¦    ¦                                       ¦

¦ 31-00 Cabin               ¦    ¦    ¦                                       ¦ ¦       Pressurization      ¦    ¦    ¦                                       ¦ ¦       Control System      ¦    ¦    ¦                                       ¦ ¦       (CPCS)              ¦    ¦    ¦                                       ¦ ¦       (Cont'd)            ¦    ¦    ¦                                       ¦

¦       02) Control       C ¦ 1  ¦ 0  ¦ May be inoperative provided LAND      ¦ ¦           Digital         ¦    ¦    ¦ ELEV is checked and set using the     ¦ ¦           Display         ¦    ¦    ¦ CPCS/OXYGEN System Page.              ¦ ¦           (Overhead       ¦    ¦    ¦                                       ¦ ¦           Panel)          ¦    ¦    ¦                                       ¦

¦       03) "CAB ALT"     C ¦ 1  ¦ 0  ¦ (O)May be inoperative provided:       ¦ ¦           Warning         ¦    ¦    ¦     a) Aircraft is operated within    ¦ ¦           System          ¦    ¦    ¦        the regulatory restrictions    ¦ ¦                           ¦    ¦    ¦        for unpressurized              ¦ ¦                           ¦    ¦    ¦        operations, and                ¦ ¦                           ¦    ¦    ¦     b) Lights erroneously on are      ¦ ¦                           ¦    ¦    ¦        masked or deactivated          ¦

¦       04) "MAN"         C ¦ 1  ¦ 0  ¦ (M)May be inoperative provided:       ¦ ¦           Annunciator     ¦    ¦    ¦     a) Pressurization AUTO/MAN        ¦ ¦           Light on        ¦    ¦    ¦        selection function is          ¦ ¦           Pressuriza-     ¦    ¦    ¦        operative                      ¦ ¦           tion Control    ¦    ¦    ¦     b) Lights erroneously on are      ¦ ¦           AUTO/MAN        ¦    ¦    ¦        masked or deactivated.         ¦ ¦           Pushbutton      ¦    ¦    ¦                                       ¦ ¦           (Overhead       ¦    ¦    ¦                                       ¦ ¦           Panel)          ¦    ¦    ¦                                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: ORIGINAL ¦ PAGE:    ¦ ¦        FAIRCHILD/DORNIER D-328JET        ¦                       ¦          ¦ ¦                                          ¦ DATE: 07/30/1999      ¦ 21-4     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 21  AIR CONDITIONING      ¦    ¦    ¦                                       ¦

¦ 51-00 ECS Pack            ¦    ¦    ¦                                       ¦ ¦       Pushbuttons         ¦    ¦    ¦                                       ¦ ¦       (Overhead Panel)    ¦    ¦    ¦                                       ¦

¦       01) "OFF"         C ¦ 2  ¦ 0  ¦ (M)(O)May be inoperative provided     ¦ ¦           Annuncia-       ¦    ¦    ¦ lights erroneously on are masked      ¦ ¦           tor Lights      ¦    ¦    ¦ or deactivated.                       ¦

¦       02) Vertical      C ¦ 2  ¦ 0  ¦ (M)(O)May be inoperative provided     ¦ ¦           (Pack Valve     ¦    ¦    ¦ lights erroneously on are masked      ¦ ¦           Open) Flow      ¦    ¦    ¦ or deactivated.                       ¦ ¦           Bar Lights      ¦    ¦    ¦                                       ¦

¦ 52-00 ECS ECON          C ¦ 1  ¦ 0  ¦ (O)May be inoperative provided        ¦ ¦       Flow Mode           ¦    ¦    ¦ Flight Planning is based on ECS       ¦ ¦                           ¦    ¦    ¦ HIGH Fuel Consumption.                ¦

¦ 53-00 "HIGH"            C ¦ 1  ¦ 0  ¦ (M)(O)May be inoperative provided:    ¦ ¦       Annunciator         ¦    ¦    ¦     a) ECS Flow Mode selection        ¦ ¦       Light on ECS        ¦    ¦    ¦        function is operative,         ¦ ¦       FLOW MODE           ¦    ¦    ¦        and                            ¦ ¦       Pushbutton          ¦    ¦    ¦     b) Lights erroneously on are      ¦ ¦       (Overhead Panel)    ¦    ¦    ¦        masked or deactivated.         ¦

¦ 54-00 Ground Cooling    C ¦ 2  ¦ 1  ¦ (M)(O)One may be inoperative          ¦ ¦       (HX) Fans           ¦    ¦    ¦ deactivated provided:                 ¦ ¦                           ¦    ¦    ¦     a) Single ECS Pack Takeoff        ¦ ¦                           ¦    ¦    ¦        and Landing procedures are     ¦ ¦                           ¦    ¦    ¦        are developed and used,        ¦ ¦                           ¦    ¦    ¦     b) Associated Pack is not         ¦ ¦                           ¦    ¦    ¦        operated on the ground,        ¦ ¦                           ¦    ¦    ¦     c) Associated Pack is not         ¦ ¦                           ¦    ¦    ¦        operated inflight at           ¦ ¦                           ¦    ¦    ¦        airspeeds below                ¦ ¦                           ¦    ¦    ¦        120 KIAS, and                  ¦ ¦                           ¦    ¦    ¦     d) During single pack             ¦ ¦                           ¦    ¦    ¦        operations, ECS Flow Mode      ¦ ¦                           ¦    ¦    ¦        is operated in HIGH.           ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: ORIGINAL ¦ PAGE:    ¦ ¦        FAIRCHILD/DORNIER D-328JET        ¦                       ¦          ¦ ¦                                          ¦ DATE: 07/30/1999      ¦ 21-5     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 21  AIR CONDITIONING      ¦    ¦    ¦                                       ¦

¦ 61-00 Cabin               ¦    ¦    ¦                                       ¦ ¦       Temperature         ¦    ¦    ¦                                       ¦ ¦       Control System      ¦    ¦    ¦                                       ¦

¦       01) Automatic     C ¦ 1  ¦ 0  ¦ May be inoperative provided           ¦ ¦           Mode            ¦    ¦    ¦ Manual Mode is operative.             ¦

¦       02) Manual        C ¦ 1  ¦ 0  ¦ May be inoperative provided           ¦ ¦           Mode            ¦    ¦    ¦ Automatic Mode is operative.          ¦

¦       03) "MAN"         C ¦ 2  ¦ 0  ¦ (M)(O)May be inoperative provided     ¦ ¦           Annunciator     ¦    ¦    ¦ lights erroneously on are masked      ¦ ¦           Pushbutton      ¦    ¦    ¦ or deactivated.                       ¦ ¦           Light           ¦    ¦    ¦                                       ¦ ¦           (Overhead       ¦    ¦    ¦                                       ¦ ¦           Panel)          ¦    ¦    ¦                                       ¦

¦ 62-00 Flight              ¦    ¦    ¦                                       ¦ ¦       Compartment         ¦    ¦    ¦                                       ¦ ¦       Temperature         ¦    ¦    ¦                                       ¦ ¦       Control System      ¦    ¦    ¦                                       ¦

¦       01) Automatic     C ¦ 1  ¦ 0  ¦ May be inoperative provided           ¦ ¦           Mode            ¦    ¦    ¦ Manual Mode is operative.             ¦

¦       02) Manual        C ¦ 1  ¦ 0  ¦ May be inoperative provided           ¦ ¦           Mode            ¦    ¦    ¦ Automatic Mode is operative.          ¦

¦       03) "MAN"         C ¦ 1  ¦ 0  ¦ (M)(O)May be inoperative provided     ¦ ¦           Annunciator     ¦    ¦    ¦ lights erroneously on are masked      ¦ ¦           Pushbutton      ¦    ¦    ¦ or deactivated.                       ¦ ¦           Light           ¦    ¦    ¦                                       ¦ ¦           (Overhead       ¦    ¦    ¦                                       ¦ ¦           Panel)          ¦    ¦    ¦                                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 1        ¦ PAGE:    ¦ ¦        FAIRCHILD/DORNIER D-328JET        ¦                       ¦          ¦ ¦                                          ¦ DATE: 11/15/2001      ¦ 22-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 22  AUTO FLIGHT           ¦    ¦    ¦                                       ¦

¦ 10-00 Autopilot         B ¦ 1  ¦ 0  ¦ May be inoperative provided           ¦ ¦       System              ¦    ¦    ¦ approach minimums do not require      ¦ ¦                           ¦    ¦    ¦ it's use.                             ¦

¦       01) Disconnect    C ¦ 1  ¦ 0  ¦ May be inoperative provided           ¦ ¦           Warning         ¦    ¦    ¦ Autopilot is not used.                ¦ ¦           System          ¦    ¦    ¦                                       ¦ ¦           (Aural and      ¦    ¦    ¦                                       ¦ ¦           PFD Visual      ¦    ¦    ¦                                       ¦ ¦           Warnings)       ¦    ¦    ¦                                       ¦

¦       02) Control       C ¦ 2  ¦ 1  ¦ One may be inoperative provided       ¦ ¦           Wheel           ¦    ¦    ¦ the autopilot is not utilized         ¦ ¦           Disconnect      ¦    ¦    ¦ at less than the initial              ¦ ¦           Switches        ¦    ¦    ¦ approach altitude.                    ¦

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

¦       03) Yaw Damper    C ¦ 1  ¦ 0  ¦ May be inoperative provided           ¦ ¦                           ¦    ¦    ¦ Autopilot is not used.                ¦

¦ 11-00 Touch Control     C ¦ 2  ¦ 0  ¦                                       ¦ ¦       Steering (TCS)      ¦    ¦    ¦                                       ¦ ¦       Switches            ¦    ¦    ¦                                       ¦

¦ 12-00 Go Around (GA)    C ¦ 2  ¦ 0  ¦ (O)May be inoperative provided        ¦ ¦       Switches (on        ¦    ¦    ¦ alternate Go Around Procedures        ¦ ¦       Thrust Levers)      ¦    ¦    ¦ are established and used.             ¦

¦ 13-00 Flight Guidance   C ¦ 1  ¦ 0  ¦ May be inoperative provided           ¦ ¦       Control Unit        ¦    ¦    ¦ Autopilot and Flight Director         ¦ ¦                           ¦    ¦    ¦ are not used.                         ¦

¦       01) Flight        C ¦ 1  ¦ 0  ¦ May be inoperative provided           ¦ ¦           Director        ¦    ¦    ¦ Takeoff Minimums and/or Approach      ¦ ¦                           ¦    ¦    ¦ Minimums do not require its use.      ¦

¦                           ¦    ¦    ¦ (Continued)                           ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: ORIGINAL ¦ PAGE:    ¦ ¦        FAIRCHILD/DORNIER D-328JET        ¦                       ¦          ¦ ¦                                          ¦ DATE: 07/30/1999      ¦ 22-2     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 22  AUTO FLIGHT           ¦    ¦    ¦                                       ¦

¦ 13-00 Flight Guidance     ¦    ¦    ¦                                       ¦ ¦       Control Unit        ¦    ¦    ¦                                       ¦ ¦       (Cont'd)            ¦    ¦    ¦                                       ¦

¦       02) Reduced Bank  C ¦ 1  ¦ 0  ¦ May be inoperative provided:          ¦ ¦           Angle (BANK)    ¦    ¦    ¦     a) BANK Mode is not used, and     ¦ ¦           Mode            ¦    ¦    ¦     b) Auto Pilot and Flight          ¦ ¦                           ¦    ¦    ¦        Director are not engaged       ¦ ¦                           ¦    ¦    ¦        in Heading (HDG) Mode if       ¦ ¦                           ¦    ¦    ¦        Reduced Bank Angle             ¦ ¦                           ¦    ¦    ¦        Synoptic is displayed on       ¦ ¦                           ¦    ¦    ¦        either Primary Flight          ¦ ¦                           ¦    ¦    ¦        Display (PFD).                 ¦

¦       03) Navigation    C ¦ 1  ¦ 0  ¦ May be inoperative provided:          ¦ ¦           (NAV) Mode      ¦    ¦    ¦     a) NAV Mode is not engaged,       ¦ ¦                           ¦    ¦    ¦        and                            ¦ ¦                           ¦    ¦    ¦     b) Auto Pilot and Flight          ¦ ¦                           ¦    ¦    ¦        Director are not engaged       ¦ ¦                           ¦    ¦    ¦        if "LNAV", "VOR", "LOC" or     ¦ ¦                           ¦    ¦    ¦        "AZ" Mode Annunciations        ¦ ¦                           ¦    ¦    ¦        are displayed on either        ¦ ¦                           ¦    ¦    ¦        Primary Flight Display         ¦ ¦                           ¦    ¦    ¦        (PFD).                         ¦

¦       04) Approach      C ¦ 1  ¦ 0  ¦ May be inoperative provided:          ¦ ¦           (APP) Mode      ¦    ¦    ¦     a) Approach Minimums do not       ¦ ¦                           ¦    ¦    ¦        require its use,               ¦ ¦                           ¦    ¦    ¦     b) APP Mode is not engaged,       ¦ ¦                           ¦    ¦    ¦        and                            ¦ ¦                           ¦    ¦    ¦     c) Auto Pilot and Flight          ¦ ¦                           ¦    ¦    ¦        Director are not engaged       ¦ ¦                           ¦    ¦    ¦        if "LOC", "VOR" or "AZ"        ¦ ¦                           ¦    ¦    ¦        Mode Annunciations are         ¦ ¦                           ¦    ¦    ¦        displayed on either            ¦ ¦                           ¦    ¦    ¦        Primary Flight Display         ¦ ¦                           ¦    ¦    ¦        (PFD).                         ¦

¦                           ¦    ¦    ¦        (Continued)                    ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: ORIGINAL ¦ PAGE:    ¦ ¦        FAIRCHILD/DORNIER D-328JET        ¦                       ¦          ¦ ¦                                          ¦ DATE: 07/30/1999      ¦ 22-3     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 22  AUTO FLIGHT           ¦    ¦    ¦                                       ¦

¦ 13-00 Flight Guidance     ¦    ¦    ¦                                       ¦ ¦       Control Unit        ¦    ¦    ¦                                       ¦ ¦       (Cont'd)            ¦    ¦    ¦                                       ¦

¦       05) Back Course   C ¦ 1  ¦ 0  ¦ May be inoperative provided:          ¦ ¦           (BC) Mode       ¦    ¦    ¦     a) BC Mode is not engaged,        ¦ ¦                           ¦    ¦    ¦        and                            ¦ ¦                           ¦    ¦    ¦     b) Auto Pilot and Flight          ¦ ¦                           ¦    ¦    ¦        Director are not engaged       ¦ ¦                           ¦    ¦    ¦        if "BC" Mode Annunciation      ¦ ¦                           ¦    ¦    ¦        is displayed on either         ¦ ¦                           ¦    ¦    ¦        Primary Flight Display         ¦ ¦                           ¦    ¦    ¦        (PFD).                         ¦

¦       06) Flight Level  B ¦ 1  ¦ 0  ¦ May be inoperative provided:          ¦ ¦           Change          ¦    ¦    ¦     a) FLCH Mode is not engaged,      ¦ ¦           (FLCH) Mode     ¦    ¦    ¦        and                            ¦ ¦                           ¦    ¦    ¦     b) Auto Pilot and Flight          ¦ ¦                           ¦    ¦    ¦        Director are not engaged       ¦ ¦                           ¦    ¦    ¦        if "FLCH" Mode                 ¦ ¦                           ¦    ¦    ¦        Annunciation is displayed      ¦ ¦                           ¦    ¦    ¦        on either Primary Flight       ¦ ¦                           ¦    ¦    ¦        Display (PFD).                 ¦

¦       07) Vertical      B ¦ 1  ¦ 0  ¦ May be inoperative provided:          ¦ ¦           Speed (VS)      ¦    ¦    ¦     a) VS Mode is not engaged,        ¦ ¦           Mode            ¦    ¦    ¦        and                            ¦ ¦                           ¦    ¦    ¦     b) Auto Pilot and Flight          ¦ ¦                           ¦    ¦    ¦        Director are not engaged if    ¦ ¦                           ¦    ¦    ¦        "VS" Mode Annunciation is      ¦ ¦                           ¦    ¦    ¦        displayed on either            ¦ ¦                           ¦    ¦    ¦        Primary Fight Display          ¦ ¦                           ¦    ¦    ¦        (PFD).                         ¦

¦                           ¦    ¦    ¦        (Continued)                    ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: ORIGINAL ¦ PAGE:    ¦ ¦        FAIRCHILD/DORNIER D-328JET        ¦                       ¦          ¦ ¦                                          ¦ DATE: 07/30/1999      ¦ 22-4     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 22  AUTO FLIGHT           ¦    ¦    ¦                                       ¦

¦ 13-00 Flight Guidance     ¦    ¦    ¦                                       ¦ ¦       Control Unit        ¦    ¦    ¦                                       ¦ ¦       (Cont'd)            ¦    ¦    ¦                                       ¦

¦       08) Vertical      C ¦ 1  ¦ 0  ¦ May be inoperative provided:          ¦ ¦           Navigation      ¦    ¦    ¦     a) VNAV is not engaged, and       ¦ ¦           (VNAV) Mode     ¦    ¦    ¦     b) Auto Pilot and Flight          ¦ ¦                           ¦    ¦    ¦        Director are not engaged       ¦ ¦                           ¦    ¦    ¦        if "VALT", "VFLCH" or          ¦ ¦                           ¦    ¦    ¦        "VPATH" Mode Annunciations     ¦ ¦                           ¦    ¦    ¦        are displayed on either        ¦ ¦                           ¦    ¦    ¦        Primary Flight Display         ¦ ¦                           ¦    ¦    ¦        (PFD).                         ¦

¦       09) "BANK"        C ¦ 1  ¦ 0  ¦ May be inoperative provided           ¦ ¦           Pushbutton      ¦    ¦    ¦ Reduced Bank Angle Synoptic           ¦ ¦           Annunciator     ¦    ¦    ¦ is operative on both                  ¦ ¦           Light           ¦    ¦    ¦ Primary Flight Displays (PFD).        ¦

¦       10) "NAV"         C ¦ 1  ¦ 0  ¦ May be inoperative provided           ¦ ¦           Pushbutton      ¦    ¦    ¦ "NAV" Mode Annunciations              ¦ ¦           Annunciator     ¦    ¦    ¦ are operative on both                 ¦ ¦           Light           ¦    ¦    ¦ Primary Flight Displays (PFD).        ¦

¦       11) "APP"         C ¦ 1  ¦ 0  ¦ May be inoperative provided           ¦ ¦           Pushbutton      ¦    ¦    ¦ "LOC" and "VOR" Mode                  ¦ ¦           Annunciator     ¦    ¦    ¦ Annunciations are operative           ¦ ¦           Light           ¦    ¦    ¦ on both Primary                       ¦ ¦                           ¦    ¦    ¦ Flight Displays (PFD).                ¦

¦       12) "BC"          C ¦ 1  ¦ 0  ¦ May be inoperative provided           ¦ ¦           Pushbutton      ¦    ¦    ¦ "BC" Mode Annunciations               ¦ ¦           Annunciator     ¦    ¦    ¦ are operative on both                 ¦ ¦           Light           ¦    ¦    ¦ Primary Flight Displays (PFD).        ¦

¦                           ¦    ¦    ¦ (Continued)                           ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: ORIGINAL ¦ PAGE:    ¦ ¦        FAIRCHILD/DORNIER D-328JET        ¦                       ¦          ¦ ¦                                          ¦ DATE: 07/30/1999      ¦ 22-5     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 22  AUTO FLIGHT           ¦    ¦    ¦                                       ¦

¦ 13-00 Flight Guidance     ¦    ¦    ¦                                       ¦ ¦       Control Unit        ¦    ¦    ¦                                       ¦ ¦       (Cont'd)            ¦    ¦    ¦                                       ¦

¦       13) "FLCH"        C ¦ 1  ¦ 0  ¦ May be inoperative provided           ¦ ¦           Pushbutton      ¦    ¦    ¦ "FLCH" Mode Annunciations             ¦ ¦           Annunciator     ¦    ¦    ¦ are operative on both                 ¦ ¦           Light           ¦    ¦    ¦ Primary Flight Displays (PFD).        ¦

¦       14) "VS"          C ¦ 1  ¦ 0  ¦ May be inoperative provided           ¦ ¦           Pushbutton      ¦    ¦    ¦ "VS" Mode Annunciations               ¦ ¦           Annunciator     ¦    ¦    ¦ are operative on both                 ¦ ¦           Light           ¦    ¦    ¦ Primary Flight Displays (PFD).        ¦

¦       15) "VNAV"        C ¦ 1  ¦ 0  ¦ May be inoperative provided           ¦ ¦           Pushbutton      ¦    ¦    ¦ "VNAV" Mode Annunciations             ¦ ¦           Annunciator     ¦    ¦    ¦ are operative on both                 ¦ ¦           Light           ¦    ¦    ¦ Primary Flight Displays (PFD).        ¦

¦       16) "ALT"         C ¦ 1  ¦ 0  ¦ May be inoperative provided           ¦ ¦           Pushbutton      ¦    ¦    ¦ "ALT" Mode Annunciations              ¦ ¦           Annunciator     ¦    ¦    ¦ are operative on both                 ¦ ¦           Light           ¦    ¦    ¦ Primary Flight Displays (PFD).        ¦

¦       17) "CPL"         C ¦ 2  ¦ 0  ¦ May be inoperative provided           ¦ ¦           Pushbutton      ¦    ¦    ¦ Flight Director Couple                ¦ ¦           Annunciator     ¦    ¦    ¦ Annunciator Arrows are operative      ¦ ¦           Lights          ¦    ¦    ¦ on both Primary Flight Displays       ¦ ¦                           ¦    ¦    ¦ (PFD).                                ¦

¦       18) "AP"          C ¦ 2  ¦ 0  ¦ May be inoperative provided           ¦ ¦           Pushbutton      ¦    ¦    ¦ Autopilot Status ("AP" & "TCS")       ¦ ¦           Annunciator     ¦    ¦    ¦ Annunciations are operative           ¦ ¦           Lights          ¦    ¦    ¦ on both Primary Flight Displays       ¦ ¦                           ¦    ¦    ¦ (PFD).                                ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: ORIGINAL ¦ PAGE:    ¦ ¦        FAIRCHILD/DORNIER D-328JET        ¦                       ¦          ¦ ¦                                          ¦ DATE: 07/30/1999      ¦ 23-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 23  COMMUNICATIONS        ¦    ¦    ¦                                       ¦

¦ 11-00 Clearance         C ¦ 1  ¦ 0  ¦ May be inoperative provided           ¦ ¦       Delivery Head       ¦    ¦    ¦ Radio Management Units (RMU's)        ¦ ¦       (CDH)               ¦    ¦    ¦ are operative.                        ¦

¦ 12-00 Communications    D ¦ -  ¦ -  ¦ Any in excess of those required       ¦ ¦       Systems (VHF        ¦    ¦    ¦ by FAR may be inoperative             ¦ ¦       HF, UHF)            ¦    ¦    ¦ provided it is not powered by         ¦ ¦                           ¦    ¦    ¦ the Hot Battery Bus or Essential      ¦ ¦                           ¦    ¦    ¦ Bus.                                  ¦

¦ 13-00 Radio Management  C ¦ 2  ¦ 1  ¦ (O)May be inoperative on one          ¦ ¦       Units (RMU's)       ¦    ¦    ¦ RMU provided:                         ¦ ¦       Nav/Comm Tuning     ¦    ¦    ¦     a) Back-up Engine and             ¦ ¦       Function            ¦    ¦    ¦        Navigation Displays on         ¦ ¦                           ¦    ¦    ¦        both RMU's are operative,      ¦ ¦                           ¦    ¦    ¦     b) Clearance Delivery Head        ¦ ¦                           ¦    ¦    ¦        (CDH) operates normally,       ¦ ¦                           ¦    ¦    ¦        and                            ¦ ¦                           ¦    ¦    ¦     c) Cross-side and FMS radio       ¦ ¦                           ¦    ¦    ¦        tuning is operative.           ¦

¦ 20-00 Microphones         ¦    ¦    ¦                                       ¦

¦       01) Headset/      A ¦ -  ¦ 0  ¦ May be inoperative provided:          ¦ ¦           Boom            ¦    ¦    ¦     a) Hand microphones and           ¦ ¦           Microphones     ¦    ¦    ¦        Headsets are installed and     ¦ ¦                           ¦    ¦    ¦        are operative,                 ¦ ¦                           ¦    ¦    ¦     b) Flight Data Recorder (FDR)     ¦ ¦                           ¦    ¦    ¦        is operative, and              ¦ ¦                           ¦    ¦    ¦     c) Repairs are made within        ¦ ¦                           ¦    ¦    ¦        three flight days.             ¦

¦  ***  02) Hand          C ¦ -  ¦ -  ¦                                       ¦ ¦           Microphones     ¦    ¦    ¦                                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 1        ¦ PAGE:    ¦ ¦        FAIRCHILD/DORNIER D-328JET        ¦                       ¦          ¦ ¦                                          ¦ DATE: 11/15/2001      ¦ 23-2     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 23  COMMUNICATIONS        ¦    ¦    ¦                                       ¦

¦ 21-00 SELCAL System     C ¦ -  ¦ 0  ¦ May be inoperative provided           ¦ ¦ ***                       ¦    ¦    ¦ alternate procedures are              ¦ ¦                           ¦    ¦    ¦ established and used.                 ¦

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

¦ 22-00 ACARS System      C ¦ -  ¦ 0  ¦ (O)May be inoperative provided        ¦ ¦ ***                       ¦    ¦    ¦ alternate procedures are              ¦ ¦                           ¦    ¦    ¦ established and used.                 ¦

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

¦ 30-00 Passenger           ¦    ¦    ¦                                       ¦ ¦       Address System      ¦    ¦    ¦                                       ¦

¦       01) Passenger     B ¦ 1  ¦ 0  ¦ (O)May be inoperative provided:       ¦ ¦           Configura-      ¦    ¦    ¦     a) Alternate, normal and          ¦ ¦           tion            ¦    ¦    ¦        emergency procedures           ¦ ¦                           ¦    ¦    ¦        and/or operating               ¦ ¦                           ¦    ¦    ¦        restrictions are               ¦ ¦                           ¦    ¦    ¦        established and used, and      ¦ ¦                           ¦    ¦    ¦     b) Flight attendant chime         ¦ ¦                           ¦    ¦    ¦        operates normally.             ¦

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

¦                           ¦    ¦    ¦ NOTE:  Any station that operates      ¦ ¦                           ¦    ¦    ¦        normally may be used.          ¦

¦      02) Cargo          D ¦ 1  ¦ 0  ¦ May be inoperative unless             ¦ ¦          Configura-       ¦    ¦    ¦ procedures require its use.           ¦ ¦          tion (Courier/   ¦    ¦    ¦                                       ¦ ¦          Supernumerary    ¦    ¦    ¦                                       ¦ ¦          Address System)  ¦    ¦    ¦                                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 1        ¦ PAGE:    ¦ ¦        FAIRCHILD/DORNIER D-328JET        ¦                       ¦          ¦ ¦                                          ¦ DATE: 11/15/2001      ¦ 23-3     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 23  COMMUNICATIONS        ¦    ¦    ¦                                       ¦

¦ 31-00 Alerting System     ¦    ¦    ¦                                       ¦ ¦       (Chime/Light)       ¦    ¦    ¦                                       ¦

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

¦        a) Flight Deck   B ¦ 1  ¦ 0  ¦ May be inoperative provided           ¦ ¦           Call Light      ¦    ¦    ¦ the flight deck chime is              ¦ ¦                           ¦    ¦    ¦ operative.                            ¦

¦                           ¦    ¦    ¦ NOTE: The flight deck chime           ¦ ¦                           ¦    ¦    ¦       must always be operative.       ¦

¦        b) Flight        B ¦ 1  ¦ 0  ¦ May be inoperative provided:          ¦ ¦           Attendant       ¦    ¦    ¦     a) PA system operates normally,   ¦ ¦           Call Light      ¦    ¦    ¦        and                            ¦ ¦                           ¦    ¦    ¦     b) Affected light is not used     ¦ ¦                           ¦    ¦    ¦        for Lavatory Smoke Detector    ¦ ¦                           ¦    ¦    ¦        alerting.                      ¦

¦                           ¦    ¦    ¦ NOTE:  Passenger to attendant call    ¦ ¦                           ¦    ¦    ¦        system is considered a         ¦ ¦                           ¦    ¦    ¦        passenger convenience item.    ¦

¦        c) Flight        B ¦ 1  ¦ 0  ¦ May be inoperative provided:          ¦ ¦           Attendant       ¦    ¦    ¦     a) PA system operates normally,   ¦ ¦           Chime           ¦    ¦    ¦     b) Affected chime is not used     ¦ ¦                           ¦    ¦    ¦        for lavatory smoke detector    ¦ ¦                           ¦    ¦    ¦        alerting, and                  ¦ ¦                           ¦    ¦    ¦     c) Alternate procedures for       ¦ ¦                           ¦    ¦    ¦        contacting flight attendants   ¦ ¦                           ¦    ¦    ¦        are established and used.      ¦

¦                           ¦    ¦    ¦ NOTE:  Passenger to attendant call    ¦ ¦                           ¦    ¦    ¦        system is considered a         ¦ ¦                           ¦    ¦    ¦        passenger conveience item.     ¦

¦ 32-00 Prerecorded       C ¦ 1  ¦ 0  ¦ (O)May be inoperative provided        ¦ ¦ ***   Passenger           ¦    ¦    ¦ alternate procedures are              ¦ ¦       Announcement        ¦    ¦    ¦ established and used.                 ¦ ¦       System              ¦    ¦    ¦                                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 1        ¦ PAGE:    ¦ ¦        FAIRCHILD/DORNIER D-328JET        ¦                       ¦          ¦ ¦                                          ¦ DATE: 11/15/2001      ¦ 23-4     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 23  COMMUNICATIONS        ¦    ¦    ¦                                       ¦

¦ 40-00 Crewmember        C ¦ 2  ¦ 1  ¦                                       ¦ ¦       Interphone          ¦    ¦    ¦                                       ¦ ¦       System              ¦    ¦    ¦                                       ¦

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

¦        a) Flight Deck   B ¦ -  ¦ 1  ¦ (O)May be inoperative provided:       ¦ ¦           to Cabin,       ¦    ¦    ¦     a) Operative station has an       ¦ ¦           Cabin to        ¦    ¦    ¦        operative flight attendant     ¦ ¦           Flight Deck,    ¦    ¦    ¦        seat, and                      ¦ ¦           Cabin to Cabin  ¦    ¦    ¦     b) Alternate communications       ¦ ¦           Station         ¦    ¦    ¦        procedures between the         ¦ ¦                           ¦    ¦    ¦        affected Flight Attendants     ¦ ¦                           ¦    ¦    ¦        station(s) and the flight      ¦ ¦                           ¦    ¦    ¦        deck are established and       ¦ ¦                           ¦    ¦    ¦        used.                          ¦

¦                           ¦    ¦    ¦ NOTE:  Any station that operates      ¦ ¦                           ¦    ¦    ¦        normally may be used.          ¦

¦        b) Flight       C  ¦ 2  ¦ 0  ¦ (O)May be inoperative provided        ¦ ¦           Deck to         ¦    ¦    ¦ alternate procedures are              ¦ ¦           Ground          ¦    ¦    ¦ established and used.                 ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 1        ¦ PAGE:    ¦ ¦        FAIRCHILD/DORNIER D-328JET        ¦                       ¦          ¦ ¦                                          ¦ DATE: 11/15/2001      ¦ 23-5     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 23  COMMUNICATIONS        ¦    ¦    ¦                                       ¦

¦ 41-00 Passenger-To-     B ¦ -  ¦ -  ¦ (M)Individual Call Buttons may be     ¦ ¦       Flight Attendant    ¦    ¦    ¦ inoperative provided:                 ¦ ¦       Call Buttons        ¦    ¦    ¦     a) Associated Seat(s) is          ¦ ¦       (Lights and         ¦    ¦    ¦        Blocked and Placarded          ¦ ¦       Aural Tones)        ¦    ¦    ¦        "DO NOT OCCUPY",               ¦ ¦                           ¦    ¦    ¦     b) Inoperative Call Button        ¦ ¦                           ¦    ¦    ¦        Light(s), and associated       ¦ ¦                           ¦    ¦    ¦        Aural Tones, failed ON are     ¦ ¦                           ¦    ¦    ¦        deactivated, and               ¦ ¦                           ¦    ¦    ¦     c) If Lavatory Call Buttons       ¦ ¦                           ¦    ¦    ¦        are inoperative, Lavatory      ¦ ¦                           ¦    ¦    ¦        is not used for any            ¦ ¦                           ¦    ¦    ¦        purpose, and affected          ¦ ¦                           ¦    ¦    ¦        Lavatory Door is locked        ¦ ¦                           ¦    ¦    ¦        closed and Placarded           ¦ ¦                           ¦    ¦    ¦        "INOPERATIVE-                  ¦ ¦                           ¦    ¦    ¦        DO NOT ENTER".                 ¦

¦ 42-00 Airborne Flight   D ¦ -  ¦ 0  ¦                                       ¦ ¦       Information         ¦    ¦    ¦                                       ¦ ¦       Services (AFIS)     ¦    ¦    ¦                                       ¦

¦ 43-00 Flightphone       D ¦ 1  ¦ 0  ¦                                       ¦ ¦       System              ¦    ¦    ¦                                       ¦

¦ 44-00 Heads Up          D ¦ 1  ¦ 0  ¦ (O)May be inoperative provided        ¦ ¦       Checklist System    ¦    ¦    ¦ alternate procedures are              ¦ ¦                           ¦    ¦    ¦ established and used.                 ¦

¦                           ¦    ¦    ¦ NOTE:  Any activation switch which    ¦ ¦                           ¦    ¦    ¦        functions normally may be      ¦ ¦                           ¦    ¦    ¦        used.                          ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 1        ¦ PAGE:    ¦ ¦        FAIRCHILD/DORNIER D-328JET        ¦                       ¦          ¦ ¦                                          ¦ DATE: 11/15/2001      ¦ 23-6     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 23  COMMUNICATIONS        ¦    ¦    ¦                                       ¦

¦ 71-00 Cockpit Voice     A ¦ 1  ¦ 0  ¦ May be inoperative provided:          ¦ ¦       Recorder System     ¦    ¦    ¦     a) Flight Data Recorder (FDR)     ¦ ¦       (CVR)               ¦    ¦    ¦        is operative, and              ¦ ¦                           ¦    ¦    ¦     b) Repairs are made within        ¦ ¦                           ¦    ¦    ¦        three flight days.             ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: ORIGINAL ¦ PAGE:    ¦ ¦        FAIRCHILD/DORNIER D-328JET        ¦                       ¦          ¦ ¦                                          ¦ DATE: 07/30/1999      ¦ 24-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 24  ELECTRICAL POWER      ¦    ¦    ¦                                       ¦

¦ 20-00 Inverters         A ¦ 2  ¦ 1  ¦ One may be inoperative provided:      ¦ ¦                           ¦    ¦    ¦     a) Inverter Failure               ¦ ¦                           ¦    ¦    ¦        Indication(s) on Overhead      ¦ ¦                           ¦    ¦    ¦        Panel for operative            ¦ ¦                           ¦    ¦    ¦        Inverter are operative,        ¦ ¦                           ¦    ¦    ¦     b) Takeoff, Approach and          ¦ ¦                           ¦    ¦    ¦        Landing Minimums do not        ¦ ¦                           ¦    ¦    ¦        require its use, and           ¦ ¦                           ¦    ¦    ¦     c) Operations are limited to      ¦ ¦                           ¦    ¦    ¦        two flight days before         ¦ ¦                           ¦    ¦    ¦        repairs are made.              ¦

¦       01) "FAIL"        C ¦ 2  ¦ 0  ¦ (M)(O)Light(s) may fail provided:     ¦ ¦           Annunciator     ¦    ¦    ¦     a) Associated Inverter(s)         ¦ ¦           Lights on       ¦    ¦    ¦        are operative, and             ¦ ¦           Inverter        ¦    ¦    ¦     b) Lights erroneously on are      ¦ ¦           Pushbuttons     ¦    ¦    ¦        masked or deactivated.         ¦ ¦           (Overhead       ¦    ¦    ¦                                       ¦ ¦           Panel)          ¦    ¦    ¦                                       ¦

¦       02) "OFF"         C ¦ 2  ¦ 0  ¦ (M)(O)Light(s) may fail provided:     ¦ ¦           Annunciator     ¦    ¦    ¦     a) Associated Inverter(s)         ¦ ¦           Lights on       ¦    ¦    ¦        are operative, and             ¦ ¦           Inverter        ¦    ¦    ¦     b) Lights erroneously on are      ¦ ¦           Pushbuttons     ¦    ¦    ¦        masked or deactivated.         ¦ ¦           (Overhead       ¦    ¦    ¦                                       ¦ ¦           Panel)          ¦    ¦    ¦                                       ¦

¦ 30-00 Transformer       B ¦ 1  ¦ 0  ¦ May be inoperative provided:          ¦ ¦       Rectifier Unit      ¦    ¦    ¦     a) DC Voltmeters are              ¦ ¦       (TRU)               ¦    ¦    ¦        operative, and                 ¦ ¦                           ¦    ¦    ¦     b) All three DC generators        ¦ ¦                           ¦    ¦    ¦        are operative.                 ¦

¦ 31-00 DC Voltmeters     C ¦  2 ¦ 1  ¦ One may be inoperative provided       ¦ ¦       (Overhead Panel)    ¦    ¦    ¦ TRU is operative.                     ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: ORIGINAL ¦ PAGE:    ¦ ¦        FAIRCHILD/DORNIER D-328JET        ¦                       ¦          ¦ ¦                                          ¦ DATE: 07/30/1999      ¦ 24-2     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 24  ELECTRICAL POWER      ¦    ¦    ¦                                       ¦

¦ 32-00 DC Generators     B ¦ 2  ¦ 1  ¦ (M)(O)Right DC Generator              ¦ ¦                           ¦    ¦    ¦ may be inoperative provided:          ¦ ¦                           ¦    ¦    ¦     a) The APU generator is           ¦ ¦                           ¦    ¦    ¦        operated continuously,         ¦ ¦                           ¦    ¦    ¦     b) The aircraft is limited        ¦ ¦                           ¦    ¦    ¦        to operations at or below      ¦ ¦                           ¦    ¦    ¦        FL300, and                     ¦ ¦                           ¦    ¦    ¦     c) DC Generator Annunciators,     ¦ ¦                           ¦    ¦    ¦        DC TIE Annunciators, TRU,      ¦ ¦                           ¦    ¦    ¦        NON-ESS Bus Annunciators       ¦ ¦                           ¦    ¦    ¦        are operative.                 ¦

¦       01) "FAIL"        C ¦ 3  ¦ 0  ¦ (M)(O)May be inoperative provided:    ¦ ¦           Annunciator     ¦    ¦    ¦     a) Associated Generator(s)        ¦ ¦           Light(s) on     ¦    ¦    ¦        are operative, and             ¦ ¦           DC Generator    ¦    ¦    ¦     b) Lights erroneously on are      ¦ ¦           Pushbuttons     ¦    ¦    ¦        masked or deactivated.         ¦ ¦           (Overhead       ¦    ¦    ¦                                       ¦ ¦           Panel)          ¦    ¦    ¦                                       ¦

¦       02) "OFF"         C ¦ 3  ¦ 0  ¦ (M)(O)May be inoperative provided:    ¦ ¦           Annunciator     ¦    ¦    ¦     a) Associated Generator(s)        ¦ ¦           Light(s) on     ¦    ¦    ¦        are operative, and             ¦ ¦           DC Generator    ¦    ¦    ¦     b) Lights erroneously on are      ¦ ¦           Pushbuttons     ¦    ¦    ¦        masked or deactivated.         ¦ ¦           (Overhead       ¦    ¦    ¦                                       ¦ ¦           Panel)          ¦    ¦    ¦                                       ¦

¦ 33-00 APU DC Generator  C ¦ 1  ¦ 0  ¦ (M)The APU DC Generator may be        ¦ ¦                           ¦    ¦    ¦ inoperative provided it is            ¦ ¦                           ¦    ¦    ¦ selected off.                         ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: ORIGINAL ¦ PAGE:    ¦ ¦        FAIRCHILD/DORNIER D-328JET        ¦                       ¦          ¦ ¦                                          ¦ DATE: 07/30/1999      ¦ 24-3     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 24  ELECTRICAL POWER      ¦    ¦    ¦                                       ¦

¦ 40-00 AC External       C ¦ 1  ¦ 0  ¦                                       ¦ ¦       Power System        ¦    ¦    ¦                                       ¦

¦       01) "AVAIL"       C ¦ 2  ¦ 0  ¦ May be inoperative provided           ¦ ¦           and "ON"        ¦    ¦    ¦ procedures do not require their       ¦ ¦           Annunciator     ¦    ¦    ¦ use.                                  ¦ ¦           Pushbutton      ¦    ¦    ¦                                       ¦ ¦           Lights          ¦    ¦    ¦                                       ¦ ¦           (Overhead       ¦    ¦    ¦                                       ¦ ¦           Panel)          ¦    ¦    ¦                                       ¦ ¦                         C ¦ 2  ¦ 0  ¦ (O)May be inoperative provided        ¦ ¦                           ¦    ¦    ¦ alternate procedures for              ¦ ¦                           ¦    ¦    ¦ determining availability and          ¦ ¦                           ¦    ¦    ¦ operational status of AC External     ¦ ¦                           ¦    ¦    ¦ Power are established and used.       ¦

¦ 41-00 DC External       C ¦ 1  ¦ 0  ¦                                       ¦ ¦       Power System        ¦    ¦    ¦                                       ¦

¦       01) "AVAIL"       C ¦ 2  ¦ 1  ¦ (O)May be inoperative provided:       ¦ ¦           and "ON"        ¦    ¦    ¦     a) "ON" and "NOT USED"            ¦ ¦           Annunciator     ¦    ¦    ¦        External Power                 ¦ ¦           Pushbutton      ¦    ¦    ¦        Annunciator Lights on          ¦ ¦           Lights          ¦    ¦    ¦        Exterior Panel are             ¦ ¦           (Overhead       ¦    ¦    ¦        operative,                     ¦ ¦           Panel)          ¦    ¦    ¦     b) Alternate Procedures for       ¦ ¦                           ¦    ¦    ¦        determining External           ¦ ¦                           ¦    ¦    ¦        Power availability and         ¦ ¦                           ¦    ¦    ¦        operation status are           ¦ ¦                           ¦    ¦    ¦        established and used, and      ¦ ¦                           ¦    ¦    ¦     c) Lights erroneously on are      ¦ ¦                           ¦    ¦    ¦        masked or deactivated.         ¦

¦                           ¦    ¦    ¦ (Continued)                           ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: ORIGINAL ¦ PAGE:    ¦ ¦        FAIRCHILD/DORNIER D-328JET        ¦                       ¦          ¦ ¦                                          ¦ DATE: 07/30/1999      ¦ 24-4     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 24  ELECTRICAL POWER      ¦    ¦    ¦                                       ¦

¦ 41-00 DC External         ¦    ¦    ¦                                       ¦ ¦       Power System        ¦    ¦    ¦                                       ¦ ¦       (Cont'd)            ¦    ¦    ¦                                       ¦

¦       02) "NOT USED"    C ¦ 2  ¦ 1  ¦ (O)May be inoperative provided:       ¦ ¦           and "ON"        ¦    ¦    ¦     a) "ON" and "AVAIL"               ¦ ¦           Annunciator     ¦    ¦    ¦        External Power                 ¦ ¦           Pushbutton      ¦    ¦    ¦        Annunciator Lights on          ¦ ¦           Lights          ¦    ¦    ¦        Overhead Panel are             ¦ ¦           (Exterior       ¦    ¦    ¦        operative,                     ¦ ¦           Panel)          ¦    ¦    ¦     b) Alternate Procedures for       ¦ ¦                           ¦    ¦    ¦        determining External           ¦ ¦                           ¦    ¦    ¦        Power availability and         ¦ ¦                           ¦    ¦    ¦        operation status are           ¦ ¦                           ¦    ¦    ¦        established and used, and      ¦ ¦                           ¦    ¦    ¦     c) Lights erroneously on are      ¦ ¦                           ¦    ¦    ¦        masked or deactivated.         ¦

¦ 50-00 Alternator          ¦    ¦    ¦                                       ¦ ¦       Pushbuttons         ¦    ¦    ¦                                       ¦ ¦       (Overhead Panel)    ¦    ¦    ¦                                       ¦

¦       01) "FAIL"        C ¦ 2  ¦ 0  ¦ (M)(O)May be inoperative provided:    ¦ ¦           Annunciator     ¦    ¦    ¦     a) Associated Alternator(s)       ¦ ¦           Lights          ¦    ¦    ¦        are operative, and             ¦ ¦                           ¦    ¦    ¦     b) Lights erroneously on are      ¦ ¦                           ¦    ¦    ¦        masked or deactivated.         ¦

¦       02) "OFF"         C ¦ 2  ¦ 0  ¦ (M)(O)May be inoperative provided:    ¦ ¦           Annunciator     ¦    ¦    ¦     a) Associated Alternator(s)       ¦ ¦           Lights          ¦    ¦    ¦        are operative, and             ¦ ¦                           ¦    ¦    ¦     b) Lights erroneously on are      ¦ ¦                           ¦    ¦    ¦        masked or deactivated.         ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: ORIGINAL ¦ PAGE:    ¦ ¦        FAIRCHILD/DORNIER D-328JET        ¦                       ¦          ¦ ¦                                          ¦ DATE: 07/30/1999      ¦ 24-5     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 24  ELECTRICAL POWER      ¦    ¦    ¦                                       ¦

¦ 51-00 AC TIE              ¦    ¦    ¦                                       ¦ ¦       Pushbutton          ¦    ¦    ¦                                       ¦ ¦       (Overhead Panel)    ¦    ¦    ¦                                       ¦

¦       01) Vertical      C ¦ 1  ¦ 0  ¦ (M)(O)Light may fail provided:        ¦ ¦           (Bus Un-)       ¦    ¦    ¦  a) AC Bus Tie function               ¦ ¦           Tied) Flow      ¦    ¦    ¦     is operative,                     ¦ ¦           Bar Light       ¦    ¦    ¦  b) AC Alternator (ALT LH/RH)         ¦ ¦                           ¦    ¦    ¦     Pushbutton "FAIL" and             ¦ ¦                           ¦    ¦    ¦     "OFF" Annunciator Lights          ¦ ¦                           ¦    ¦    ¦     are operative, and                ¦ ¦                           ¦    ¦    ¦  c) Lights erroneously on are         ¦ ¦                           ¦    ¦    ¦     masked or deactivated.            ¦

¦       02) Horizontal    C ¦ 1  ¦ 0  ¦ (M)(O)Light may fail provided:        ¦ ¦           (Bus Tied)      ¦    ¦    ¦     a) AC Bus Tie function            ¦ ¦           Flow Bar        ¦    ¦    ¦        is operative,                  ¦ ¦           Light           ¦    ¦    ¦     b) AC Alternator (ALT LH/RH)      ¦ ¦                           ¦    ¦    ¦        Pushbutton "FAIL" and          ¦ ¦                           ¦    ¦    ¦        "OFF" Annunciator Lights       ¦ ¦                           ¦    ¦    ¦        are operative, and             ¦ ¦                           ¦    ¦    ¦     c) Lights erroneously on are      ¦ ¦                           ¦    ¦    ¦        masked or deactivated.         ¦

¦ 60-00 NON-ESS Bus         ¦    ¦    ¦                                       ¦ ¦       Pushbuttons         ¦    ¦    ¦                                       ¦ ¦       (Overhead Panel)    ¦    ¦    ¦                                       ¦

¦       01) Vertical      C ¦ 2  ¦ 0  ¦ (M)(O) May be inoperative provided:   ¦ ¦           (Bus Tied)      ¦    ¦    ¦     a) Associated NON-ESS             ¦ ¦           Flow Bar        ¦    ¦    ¦        Pushbutton(s) are              ¦ ¦           Lights          ¦    ¦    ¦        operative,                     ¦ ¦                           ¦    ¦    ¦     b) DC Generator (LH/RH/APU)       ¦ ¦                           ¦    ¦    ¦        Pushbutton "FAIL" and          ¦ ¦                           ¦    ¦    ¦        "OFF" Annunciator Lights       ¦ ¦                           ¦    ¦    ¦        are operative, and             ¦ ¦                           ¦    ¦    ¦     c) Lights erroneously on are      ¦ ¦                           ¦    ¦    ¦        masked or deactivated.         ¦

¦                           ¦    ¦    ¦  (Continued)                          ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: ORIGINAL ¦ PAGE:    ¦ ¦        FAIRCHILD/DORNIER D-328JET        ¦                       ¦          ¦ ¦                                          ¦ DATE: 07/30/1999      ¦ 24-6     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 24  ELECTRICAL POWER      ¦    ¦    ¦                                       ¦

¦ 60-00 NON-ESS Bus         ¦    ¦    ¦                                       ¦ ¦       Pushbuttons         ¦    ¦    ¦                                       ¦ ¦       (Overhead Panel)    ¦    ¦    ¦                                       ¦ ¦       (Cont'd)            ¦    ¦    ¦                                       ¦

¦       02) "OFF"         C ¦ 2  ¦ 0  ¦ (M)(O) May be inoperative provided:   ¦ ¦           Annunciator     ¦    ¦    ¦     a) Associated NON-ESS             ¦ ¦           Lights          ¦    ¦    ¦        Pushbutton(s) are              ¦ ¦                           ¦    ¦    ¦        operative,                     ¦ ¦                           ¦    ¦    ¦     b) DC Generator (LH/RH/APU)       ¦ ¦                           ¦    ¦    ¦        Pushbutton "FAIL" and          ¦ ¦                           ¦    ¦    ¦        "OFF" Annunciator Lights       ¦ ¦                           ¦    ¦    ¦        are operative, and             ¦ ¦                           ¦    ¦    ¦     c) Lights erroneously on are      ¦ ¦                           ¦    ¦    ¦        masked or deactivated.         ¦

¦ 61-00 DC TIE              ¦    ¦    ¦                                       ¦ ¦       Pushbutton          ¦    ¦    ¦                                       ¦ ¦       (Overhead Panel)    ¦    ¦    ¦                                       ¦

¦       01) Vertical      B ¦ 1  ¦ 0  ¦ (M)(O) May be inoperative provided:   ¦ ¦           (Bus Un-        ¦    ¦    ¦     a) DC Bus TIE Pushbutton          ¦ ¦           Tied) Flow      ¦    ¦    ¦        is operative,                  ¦ ¦           Bar Light       ¦    ¦    ¦     b) DC Generator (LH/RH/APU)       ¦ ¦                           ¦    ¦    ¦        Pushbutton "FAIL" and          ¦ ¦                           ¦    ¦    ¦        "OFF" Annunciator Lights       ¦ ¦                           ¦    ¦    ¦        are operative, and             ¦ ¦                           ¦    ¦    ¦     c) Lights erroneously on are      ¦ ¦                           ¦    ¦    ¦        masked or deactivated.         ¦

¦       02) Horizontal    B ¦ 1  ¦ 0  ¦ (M)(O) May be inoperative provided:   ¦ ¦           (Bus Tied)      ¦    ¦    ¦     a) DC Bus TIE Pushbutton          ¦ ¦           Flow Bar        ¦    ¦    ¦        is operative,                  ¦ ¦           Light           ¦    ¦    ¦     b) DC Generator (LH/RH/APU)       ¦ ¦                           ¦    ¦    ¦        Pushbutton "FAIL" and          ¦ ¦                           ¦    ¦    ¦        "OFF" Annunciator Lights       ¦ ¦                           ¦    ¦    ¦        are operative, and             ¦ ¦                           ¦    ¦    ¦     c) Lights erroneously on are      ¦ ¦                           ¦    ¦    ¦        masked or deactivated.         ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: ORIGINAL ¦ PAGE:    ¦ ¦        FAIRCHILD/DORNIER D-328JET        ¦                       ¦          ¦ ¦                                          ¦ DATE: 07/30/1999      ¦ 24-7     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 24  ELECTRICAL POWER      ¦    ¦    ¦                                       ¦

¦ 62-00 Essential Bus     C ¦ 2  ¦ 1  ¦                                       ¦ ¦       LED(s) (Bus         ¦    ¦    ¦                                       ¦ ¦       Powered) Lights     ¦    ¦    ¦                                       ¦ ¦       (Overhead Panel)    ¦    ¦    ¦                                       ¦

¦ 63-00 Battery 1 / 2       ¦    ¦    ¦                                       ¦ ¦       Pushbuttons         ¦    ¦    ¦                                       ¦ ¦       (Overhead Panel)    ¦    ¦    ¦                                       ¦

¦       01) "FAIL"        C ¦ 2  ¦ 0  ¦ (M)(O)May be inoperative provided:    ¦ ¦           Annunciator     ¦    ¦    ¦     a) Associated Battery(s)          ¦ ¦           Light(s)        ¦    ¦    ¦        are operative,                 ¦ ¦                           ¦    ¦    ¦     b) Lights erroneously on are      ¦ ¦                           ¦    ¦    ¦        masked or deactivated.         ¦

¦       02) "OFF"         C ¦ 2  ¦ 0  ¦ (M)(O)May be inoperative provided:    ¦ ¦           Annunciator     ¦    ¦    ¦     a) Associated Battery(s)          ¦ ¦           Light(s)        ¦    ¦    ¦        are operative, and             ¦ ¦                           ¦    ¦    ¦     b) Lights erroneously on are      ¦ ¦                           ¦    ¦    ¦        masked or deactivated.         ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: ORIGINAL ¦ PAGE:    ¦ ¦        FAIRCHILD/DORNIER D-328JET        ¦                       ¦          ¦ ¦                                          ¦ DATE: 07/30/1999      ¦ 25-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 25  EQUIPMENT/FURNISHINGS ¦    ¦    ¦                                       ¦

¦ 00-00 Passenger         D ¦ -  ¦ -  ¦ Passenger Convenience Items as        ¦ ¦ ***   Convenience         ¦    ¦    ¦ expressed in the MMEL, are 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.  Items            ¦ ¦                           ¦    ¦    ¦ addressed elsewhere in this           ¦ ¦                           ¦    ¦    ¦ document shall not be included.(M)    ¦ ¦                           ¦    ¦    ¦ and (O) procedures may be required    ¦ ¦                           ¦    ¦    ¦ and included in the air carrier's     ¦ ¦                           ¦    ¦    ¦ appropriate document.                 ¦

¦                           ¦    ¦    ¦ NOTE: Lavatory Door Ash Tray(s) is    ¦ ¦                           ¦    ¦    ¦       not considered a Passenger      ¦ ¦                           ¦    ¦    ¦       Convenience Item.               ¦

¦ 01-00 Operator          C ¦ -  ¦ -  ¦ Any or all may be inoperative or      ¦ ¦ ***   Initiated           ¦    ¦    ¦ missing.                              ¦ ¦       Placards            ¦    ¦    ¦                                       ¦ ¦       (Internal and       ¦    ¦    ¦                                       ¦ ¦       External)           ¦    ¦    ¦                                       ¦

¦ 10-01 Cockpit Sunvisor  C ¦ 2  ¦ 0  ¦ May be inoperative provided:          ¦ ¦                           ¦    ¦    ¦      a) No visual restrictions to     ¦ ¦                           ¦    ¦    ¦         the flight crew,              ¦ ¦                           ¦    ¦    ¦      b) Acceptable to flight crew,    ¦ ¦                           ¦    ¦    ¦         and                           ¦ ¦                           ¦    ¦    ¦      c) Affected sunvisor is          ¦ ¦                           ¦    ¦    ¦         removed or stowed.            ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: ORIGINAL ¦ PAGE:    ¦ ¦        FAIRCHILD/DORNIER D-328JET        ¦                       ¦          ¦ ¦                                          ¦ DATE: 07/30/1999      ¦ 25-2     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 25  EQUIPMENT/FURNISHINGS ¦    ¦    ¦                                       ¦

¦ 11-00 Observer Seat     A ¦ 1  ¦ 0  ¦ May be inoperative provided:          ¦ ¦       (Including          ¦    ¦    ¦     a) A Passenger Seat in the        ¦ ¦       Associated          ¦    ¦    ¦        Passenger Cabin is made        ¦ ¦       Equipment)          ¦    ¦    ¦        available to an FAA            ¦ ¦                           ¦    ¦    ¦        Inspector for the              ¦ ¦                           ¦    ¦    ¦        performance of official        ¦ ¦                           ¦    ¦    ¦        duties, and                    ¦ ¦                           ¦    ¦    ¦     b) Repairs are made within        ¦ ¦                           ¦    ¦    ¦        two flight days.               ¦

¦                         A ¦ 1  ¦ 0  ¦ May be inoperative provided:          ¦ ¦                           ¦    ¦    ¦     a) The primary observer seat      ¦ ¦                           ¦    ¦    ¦        is available with the          ¦ ¦                           ¦    ¦    ¦        required minimum safety        ¦ ¦                           ¦    ¦    ¦        equipment(safety belt and      ¦ ¦                           ¦    ¦    ¦        oxygen) and acceptable to      ¦ ¦                           ¦    ¦    ¦        the FAA inspector for the      ¦ ¦                           ¦    ¦    ¦        performance of official        ¦ ¦                           ¦    ¦    ¦        duties, and                    ¦ ¦                           ¦    ¦    ¦     b) Repairs are made within        ¦ ¦                           ¦    ¦    ¦        two flight days.               ¦

¦                           ¦    ¦    ¦ NOTE 1: These provisions are          ¦ ¦                           ¦    ¦    ¦         intended to provide for       ¦ ¦                           ¦    ¦    ¦         occupancy of the above        ¦ ¦                           ¦    ¦    ¦         seats by an FAA Inspector     ¦ ¦                           ¦    ¦    ¦         when minimum safety           ¦ ¦                           ¦    ¦    ¦         equipment (safety belt,       ¦ ¦                           ¦    ¦    ¦         shoulder harness, flotation   ¦ ¦                           ¦    ¦    ¦         device, audio panel and       ¦ ¦                           ¦    ¦    ¦         oxygen mask with somke        ¦ ¦                           ¦    ¦    ¦         goggles) is functional and    ¦ ¦                           ¦    ¦    ¦         the inspector  detemines      ¦ ¦                           ¦    ¦    ¦         the conditions to be          ¦ ¦                           ¦    ¦    ¦         acceptable.                   ¦ ¦                           ¦    ¦    ¦ NOTE 2: The Pilot-In-Command will     ¦ ¦                           ¦    ¦    ¦         determine if the minimum      ¦ ¦                           ¦    ¦    ¦         Safety Equipment is           ¦ ¦                           ¦    ¦    ¦         functional for other          ¦ ¦                           ¦    ¦    ¦         persons authorized to         ¦ ¦                           ¦    ¦    ¦         occupy Observer Seat.         ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: ORIGINAL ¦ PAGE:    ¦ ¦        FAIRCHILD/DORNIER D-328JET        ¦                       ¦          ¦ ¦                                          ¦ DATE: 07/30/1999      ¦ 25-3     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 25  EQUIPMENT/FURNISHINGS ¦    ¦    ¦                                       ¦

¦ 13-00 Crewmember        C ¦ -  ¦ 0  ¦ May be inoperative or missing         ¦ ¦       Flashlight/         ¦    ¦    ¦ provided Crewmember(s)                ¦ ¦       Holder              ¦    ¦    ¦ assigned to associated Seat(s)        ¦ ¦       Assembly(s)         ¦    ¦    ¦ has an equivalent, operating          ¦ ¦                           ¦    ¦    ¦ Flashlight readily available.         ¦

¦ 20-00 Flight Attendant  A ¦ 1  ¦ 0  ¦ (M)(O)Flight Attendant seat           ¦ ¦       Seat Assembly       ¦    ¦    ¦  may be inoperative provided:         ¦ ¦                           ¦    ¦    ¦     a) Affected Seat or seat          ¦ ¦                           ¦    ¦    ¦        assembly is not occupied,      ¦ ¦                           ¦    ¦    ¦     b) Flight Attendant displaced     ¦ ¦                           ¦    ¦    ¦        by inoperative seat            ¦ ¦                           ¦    ¦    ¦        position occupies the          ¦ ¦                           ¦    ¦    ¦        passenger Seat most            ¦ ¦                           ¦    ¦    ¦        accessible to the              ¦ ¦                           ¦    ¦    ¦        inoperative seat,              ¦ ¦                           ¦    ¦    ¦     c) Alternate procedures are       ¦ ¦                           ¦    ¦    ¦        established and used as        ¦ ¦                           ¦    ¦    ¦        published in the crew          ¦ ¦                           ¦    ¦    ¦        members manuals,               ¦ ¦                           ¦    ¦    ¦     d) Folding type Seat is           ¦ ¦                           ¦    ¦    ¦        stowed or secured in the       ¦ ¦                           ¦    ¦    ¦        retracted position,            ¦ ¦                           ¦    ¦    ¦     e) Passenger Seat assigned        ¦ ¦                           ¦    ¦    ¦        to the Flight Attendant        ¦ ¦                           ¦    ¦    ¦        is placarded "FOR FLIGHT       ¦ ¦                           ¦    ¦    ¦        ATTENDANT USE ONLY", and       ¦ ¦                           ¦    ¦    ¦     f) Repairs are made within        ¦ ¦                           ¦    ¦    ¦        two flight days.               ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: ORIGINAL ¦ PAGE:    ¦ ¦        FAIRCHILD/DORNIER D-328JET        ¦                       ¦          ¦ ¦                                          ¦ DATE: 07/30/1999      ¦ 25-4     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 25  EQUIPMENT/FURNISHINGS ¦    ¦    ¦                                       ¦

¦ 21-00 Passenger Seat(s) D ¦ -  ¦ -  ¦ May be inoperative provided:          ¦ ¦                           ¦    ¦    ¦     a) Seat does not block an         ¦ ¦                           ¦    ¦    ¦        Emergency Exit,                ¦ ¦                           ¦    ¦    ¦     b) Seat does not restrict         ¦ ¦                           ¦    ¦    ¦        any passenger from access      ¦ ¦                           ¦    ¦    ¦        to the main aisle, and         ¦ ¦                           ¦    ¦    ¦     c) The affected seat(s) are       ¦ ¦                           ¦    ¦    ¦        blocked and placarded          ¦ ¦                           ¦    ¦    ¦        "DO NOT OCCUPY".               ¦

¦                           ¦    ¦    ¦ NOTE:                                 ¦ ¦                           ¦    ¦    ¦     1) A seat with an inoperative     ¦ ¦                           ¦    ¦    ¦        seat belt (or shoulder harn-   ¦ ¦                           ¦    ¦    ¦        ess, for front row seat) is    ¦ ¦                           ¦    ¦    ¦        considered inopeative.         ¦ ¦                           ¦    ¦    ¦     2) Inoperative seats do not       ¦ ¦                           ¦    ¦    ¦        affect the required number     ¦ ¦                           ¦    ¦    ¦        of Flight Attendants.          ¦ ¦                           ¦    ¦    ¦     3) Affected seat(s) may           ¦ ¦                           ¦    ¦    ¦        include the seat(s) behind     ¦ ¦                           ¦    ¦    ¦        and/or adjacent outboard       ¦ ¦                           ¦    ¦    ¦        seats.                         ¦

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

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

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: ORIGINAL ¦ PAGE:    ¦ ¦        FAIRCHILD/DORNIER D-328JET        ¦                       ¦          ¦ ¦                                          ¦ DATE: 07/30/1999      ¦ 25-5     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 25  EQUIPMENT/FURNISHINGS ¦    ¦    ¦                                       ¦

¦ 30-00 Galley Waste      C ¦ -  ¦ 0  ¦ (M)May be inoperative provided        ¦ ¦       Receptacles         ¦    ¦    ¦ the container is empty                ¦ ¦       Access Doors/       ¦    ¦    ¦ and the access is secured to          ¦ ¦       Covers              ¦    ¦    ¦ prevent waste introduction into       ¦ ¦                           ¦    ¦    ¦ the compartment.                      ¦

¦ 40-00 Lavatory Area       ¦    ¦    ¦                                       ¦ ¦       Ashtrays-           ¦    ¦    ¦                                       ¦

¦       01) Airplanes     A ¦ -  ¦ -  ¦ One may be missing provided           ¦ ¦           with more       ¦    ¦    ¦ it is replaced within 10              ¦ ¦           than one        ¦    ¦    ¦ calendar days.                        ¦ ¦           lavatory        ¦    ¦    ¦                                       ¦ ¦           area ashtray    ¦    ¦    ¦                                       ¦ ¦           installed.      ¦    ¦    ¦                                       ¦

¦       02) Airplanes     A ¦ 1  ¦ 0  ¦ May be missing provided               ¦ ¦           with only       ¦    ¦    ¦ it is replaced within                 ¦ ¦           one lavatory    ¦    ¦    ¦ 3 calendar days.                      ¦ ¦           area ashtray    ¦    ¦    ¦                                       ¦ ¦           installed.      ¦    ¦    ¦                                       ¦

¦ 51-00 Cargo Restraint   C ¦ -  ¦ 0  ¦ May be inoperative or missing         ¦ ¦ ***   System              ¦    ¦    ¦ provided acceptable cargo             ¦ ¦                           ¦    ¦    ¦ loading limits from an approved       ¦ ¦                           ¦    ¦    ¦ source i.e.; Handling manual, or      ¦ ¦                           ¦    ¦    ¦ Weight and Balance document are       ¦ ¦                           ¦    ¦    ¦ observed.                             ¦

¦                         C ¦ -  ¦ 0  ¦ May be inoperative or missing         ¦ ¦                           ¦    ¦    ¦ provided cargo compartment            ¦ ¦                           ¦    ¦    ¦ remains empty.                        ¦

¦ 60-00 Emergency         D ¦ -  ¦ -  ¦ Any in excess of those required       ¦ ¦ ***   Locator             ¦    ¦    ¦ by FAR may be inoperative or          ¦ ¦       Transmitter         ¦    ¦    ¦ missing.                              ¦ ¦       (ELT)               ¦    ¦    ¦                                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 1        ¦ PAGE:    ¦ ¦        FAIRCHILD/DORNIER D-328JET        ¦                       ¦          ¦ ¦                                          ¦ DATE: 11/15/2001      ¦ 25-6     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 25  EQUIPMENT/FURNISHINGS ¦    ¦    ¦                                       ¦

¦ 61-00 "Fasten Seat      C ¦ -  ¦ -  ¦ One or more Signs or                  ¦ ¦       Belt While          ¦    ¦    ¦ Placards may be illegible             ¦ ¦       Seated" Signs       ¦    ¦    ¦ or missing provided a legible         ¦ ¦                           ¦    ¦    ¦ Sign or Placard is readable from      ¦ ¦                           ¦    ¦    ¦ each occupied Passenger Seat.         ¦

¦ 62-00 Megaphones        D ¦ -  ¦ -  ¦ Any in excess of those required by    ¦ ¦ ***                       ¦    ¦    ¦ FAR may be missing or inoperative.    ¦

¦ 63-00 First Aid Kits    D ¦ -  ¦ -  ¦ Any in excess of those required by    ¦ ¦                           ¦    ¦    ¦ FAR may be incomplete or              ¦ ¦                           ¦    ¦    ¦ missing, provided required            ¦ ¦                           ¦    ¦    ¦ distribution is maintained.           ¦

¦ 64-00 Emergency         D ¦ -  ¦ -  ¦ Any in excess of those required by    ¦ ¦ ***   Medical Kits        ¦    ¦    ¦ FAR may be opened or                  ¦ ¦                           ¦    ¦    ¦ missing provided required             ¦ ¦                           ¦    ¦    ¦ distribution of remaining Kit(s)      ¦ ¦                           ¦    ¦    ¦ is maintained.                        ¦

¦ 65-00 Over-Water        C ¦ -  ¦ -  ¦ Any items in excess of those          ¦ ¦ ***   Equipment           ¦    ¦    ¦ required by FAR may be                ¦ ¦                           ¦    ¦    ¦ inoperative or missing provided       ¦ ¦                           ¦    ¦    ¦ required distribution of operative    ¦ ¦                           ¦    ¦    ¦ equipment is maintained.              ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 1        ¦ PAGE:    ¦ ¦        FAIRCHILD/DORNIER D-328JET        ¦                       ¦          ¦ ¦                                          ¦ DATE: 11/15/2001      ¦ 26-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 26  FIRE PROTECTION       ¦    ¦    ¦                                       ¦

¦ 14-00 Cargo             C ¦ -  ¦ -  ¦ (O)May be inoperative provided        ¦ ¦ ***   Compartment         ¦    ¦    ¦ procedures are established and used   ¦ ¦       Smoke Detection     ¦    ¦    ¦ to ensure the associated compart-     ¦ ¦       System              ¦    ¦    ¦ ment remains empty, or is verified    ¦ ¦                           ¦    ¦    ¦ to contain only empty cargo handl-    ¦ ¦                           ¦    ¦    ¦ ing equipment, ballast (ballast       ¦ ¦                           ¦    ¦    ¦ may be loaded in ULDs), and/or Fly    ¦ ¦                           ¦    ¦    ¦ Away kits.                            ¦

¦                           ¦    ¦    ¦ NOTE:  Operators MELs must define     ¦ ¦                           ¦    ¦    ¦        which items are approved for   ¦ ¦                           ¦    ¦    ¦        inclusion in the Fly Away      ¦ ¦                           ¦    ¦    ¦        Kits, and which materials      ¦ ¦                           ¦    ¦    ¦        can be used as ballast.        ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 1        ¦ PAGE:    ¦ ¦        FAIRCHILD/DORNIER D-328JET        ¦                       ¦          ¦ ¦                                          ¦ DATE: 11/15/2001      ¦ 26-2     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 26  FIRE PROTECTION       ¦    ¦    ¦                                       ¦

¦ 15-00 Lavatory Smoke    C ¦ -  ¦ -  ¦ (M)(O)For each lavatory, the          ¦ ¦       Detection           ¦    ¦    ¦ lavatory smoke detection system may   ¦ ¦       System              ¦    ¦    ¦ be inoperate provided:                ¦ ¦                           ¦    ¦    ¦     a) Lavatory waste receptacle      ¦ ¦                           ¦    ¦    ¦        is empty,                      ¦ ¦                           ¦    ¦    ¦     b) Assocated lavatory door is     ¦ ¦                           ¦    ¦    ¦        locked closed and placarded    ¦ ¦                           ¦    ¦    ¦        "INOPERATIVE - DO NOT          ¦ ¦                           ¦    ¦    ¦        ENTER", and                    ¦ ¦                           ¦    ¦    ¦     c) Lavatory is used only by       ¦ ¦                           ¦    ¦    ¦        crewmembers.                   ¦

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

¦                           ¦    ¦    ¦     2) Lavatory smoke detection       ¦ ¦                           ¦    ¦    ¦        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: 1        ¦ PAGE:    ¦ ¦        FAIRCHILD/DORNIER D-328JET        ¦                       ¦          ¦ ¦                                          ¦ DATE: 11/15/2001      ¦ 26-3     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 26  FIRE PROTECTION       ¦    ¦    ¦                                       ¦

¦ 21-00 Fire              C ¦ 5  ¦ 0  ¦ (M)(O)May be inoperative or           ¦ ¦       Extinguisher        ¦    ¦    ¦ missing provided:                     ¦ ¦       Thermal             ¦    ¦    ¦     a) Adequate charge of             ¦ ¦       Discharge Discs     ¦    ¦    ¦        associated extinguisher        ¦ ¦                           ¦    ¦    ¦        is verified each flight        ¦ ¦                           ¦    ¦    ¦        day, and                       ¦ ¦                           ¦    ¦    ¦     b) Associated Engine Fire         ¦ ¦                           ¦    ¦    ¦        Protection Discharge (DIS)     ¦ ¦                           ¦    ¦    ¦        Bottle Lights are tested       ¦ ¦                           ¦    ¦    ¦        each flight day.               ¦

¦ 24-00 Cargo             C ¦ -  ¦ -  ¦ (O)May be inoperative provided        ¦ ¦ ***   Compartment Fire    ¦    ¦    ¦ procedures are established and        ¦ ¦       Extinguisher        ¦    ¦    ¦ used to ensure the associated         ¦ ¦       System              ¦    ¦    ¦ compartment remains empty, or is      ¦ ¦                           ¦    ¦    ¦ verified to contain only empty        ¦ ¦                           ¦    ¦    ¦ cargo handling equipment, ballast     ¦ ¦                           ¦    ¦    ¦ (ballast may be loaded in ULDs),      ¦ ¦                           ¦    ¦    ¦ and/or Fly Away Kits.                 ¦

¦                           ¦    ¦    ¦ NOTE:  Operator MELs must define      ¦ ¦                           ¦    ¦    ¦        which items are approved for   ¦ ¦                           ¦    ¦    ¦        inclusion in the Fly Away      ¦ ¦                           ¦    ¦    ¦        Kits, and which materials      ¦ ¦                           ¦    ¦    ¦        can be used as ballast.        ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 1        ¦ PAGE:    ¦ ¦        FAIRCHILD/DORNIER D-328JET        ¦                       ¦          ¦ ¦                                          ¦ DATE: 11/15/2001      ¦ 26-4     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 26  FIRE PROTECTION       ¦    ¦    ¦                                       ¦

¦ 25-00 Lavatory Fire     C ¦ -  ¦ -  ¦ For each lavatory, the lavatory       ¦ ¦       Extinguisher        ¦    ¦    ¦ fire extinguisher system may be       ¦ ¦       Systems             ¦    ¦    ¦ inoperative provided Lavatory Smoke   ¦ ¦                           ¦    ¦    ¦ Detector system operates normally.    ¦

¦                         C ¦ -  ¦ -  ¦ (M)(O)For each lavatory, the          ¦ ¦                           ¦    ¦    ¦ lavatory fire extinguisher system     ¦ ¦                           ¦    ¦    ¦ may be inoperative provided:          ¦ ¦                           ¦    ¦    ¦     a) Lavatory Waste Receptacle      ¦ ¦                           ¦    ¦    ¦        is empty,                      ¦ ¦                           ¦    ¦    ¦     b) Associated lavatory door is    ¦ ¦                           ¦    ¦    ¦        locked closed and placarded    ¦ ¦                           ¦    ¦    ¦        "INOPERATIVE - DO NOT          ¦ ¦                           ¦    ¦    ¦        ENTER", and                    ¦ ¦                           ¦    ¦    ¦     c) Lavatory is used only by       ¦ ¦                           ¦    ¦    ¦        crewmembers.                   ¦

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

¦                           ¦    ¦    ¦     2) A 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: 1        ¦ PAGE:    ¦ ¦        FAIRCHILD/DORNIER D-328JET        ¦                       ¦          ¦ ¦                                          ¦ DATE: 11/15/2001      ¦ 26-5     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 26  FIRE PROTECTION       ¦    ¦    ¦                                       ¦

¦ 27-00 Portable Fire     D ¦ -  ¦ -  ¦ Any in excess of those required by    ¦ ¦       Extinguisher        ¦    ¦    ¦ FAR may be inoperative or missing     ¦ ¦                           ¦    ¦    ¦ provided:                             ¦ ¦                           ¦    ¦    ¦      a) The inoperative Fire          ¦ ¦                           ¦    ¦    ¦         Extinguisher is tagged        ¦ ¦                           ¦    ¦    ¦         "INOPERATIVE," removed        ¦ ¦                           ¦    ¦    ¦         from the installed            ¦ ¦                           ¦    ¦    ¦         position, and placed out      ¦ ¦                           ¦    ¦    ¦         of sight so it can not be     ¦ ¦                           ¦    ¦    ¦         mistaken for a functional     ¦ ¦                           ¦    ¦    ¦         unit, and                     ¦ ¦                           ¦    ¦    ¦      b) Required distribution is      ¦ ¦                           ¦    ¦    ¦         maintained.                   ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: ORIGINAL ¦ PAGE:    ¦ ¦        FAIRCHILD/DORNIER D-328JET        ¦                       ¦          ¦ ¦                                          ¦ DATE: 07/30/1999      ¦ 27-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 27  FLIGHT CONTROLS       ¦    ¦    ¦                                       ¦

¦ 12-00 Normal Aileron    B ¦ 1  ¦ 0  ¦ (O)May be inoperative provided:       ¦ ¦       Trim System         ¦    ¦    ¦     a) Aileron Trim Indication        ¦ ¦                           ¦    ¦    ¦        System is operative,           ¦ ¦                           ¦    ¦    ¦     b) Standby Aileron Trim           ¦ ¦                           ¦    ¦    ¦        System is operated             ¦ ¦                           ¦    ¦    ¦        through full travel            ¦ ¦                           ¦    ¦    ¦        before each departure,         ¦ ¦                           ¦    ¦    ¦        and                            ¦ ¦                           ¦    ¦    ¦     c) Standby Aileron Trim           ¦ ¦                           ¦    ¦    ¦        System is selected and         ¦ ¦                           ¦    ¦    ¦        used throughout flight.        ¦

¦ 13-00 Standby Aileron   B ¦ 1  ¦ 0  ¦ (O)May be inoperative provided:       ¦ ¦       Trim System         ¦    ¦    ¦     a) Aileron Trim Indication        ¦ ¦                           ¦    ¦    ¦        System is operative,           ¦ ¦                           ¦    ¦    ¦     b) Normal Aileron Trim System     ¦ ¦                           ¦    ¦    ¦        is operated through            ¦ ¦                           ¦    ¦    ¦        full travel before             ¦ ¦                           ¦    ¦    ¦        each departure, and            ¦ ¦                           ¦    ¦    ¦     c) Normal Aileron Trim System     ¦ ¦                           ¦    ¦    ¦        is selected and used           ¦ ¦                           ¦    ¦    ¦        throughout flight.             ¦

¦ 15-00 Aileron Trim      B ¦ 1  ¦ 0  ¦ (M)(O)May be inoperative:             ¦ ¦       Indication          ¦    ¦    ¦ provided:                             ¦ ¦       System              ¦    ¦    ¦     a) Normal and Standby Aileron     ¦ ¦                           ¦    ¦    ¦        Trim Systems are               ¦ ¦                           ¦    ¦    ¦        operative,                     ¦ ¦                           ¦    ¦    ¦     b) Aileron Trim Systems are       ¦ ¦                           ¦    ¦    ¦        operated through full          ¦ ¦                           ¦    ¦    ¦        travel before each             ¦ ¦                           ¦    ¦    ¦        departure, and                 ¦ ¦                           ¦    ¦    ¦     c) At completion of Trim          ¦ ¦                           ¦    ¦    ¦        check, Aileron Trim Tab is     ¦ ¦                           ¦    ¦    ¦        visually verified in the       ¦ ¦                           ¦    ¦    ¦        neutral position, and          ¦ ¦                           ¦    ¦    ¦        Aileron Trim is not            ¦ ¦                           ¦    ¦    ¦        repositioned unless            ¦ ¦                           ¦    ¦    ¦        required in flight.            ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: ORIGINAL ¦ PAGE:    ¦ ¦        FAIRCHILD/DORNIER D-328JET        ¦                       ¦          ¦ ¦                                          ¦ DATE: 07/30/1999      ¦ 27-2     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 27  FLIGHT CONTROLS       ¦    ¦    ¦                                       ¦

¦ 16-00 Aileron Position  C ¦ 2  ¦ 0  ¦ (O)May be inoperative provided,       ¦ ¦       Indications         ¦    ¦    ¦ before each takeoff, normal           ¦ ¦       (FLT CTRL Page)     ¦    ¦    ¦ Aileron control movement is           ¦ ¦                           ¦    ¦    ¦ verified by an acceptable             ¦ ¦                           ¦    ¦    ¦ alternate means.                      ¦

¦ 23-00 Rudder Limiter    A ¦ 1  ¦ 0  ¦ (O)May be inoperative in the          ¦ ¦       System              ¦    ¦    ¦ Disengaged Mode provided:             ¦ ¦                           ¦    ¦    ¦     a) Airspeed is limited to a       ¦ ¦                           ¦    ¦    ¦        maximum of 160 KIAS,           ¦ ¦                           ¦    ¦    ¦     b) Aircraft is not operated       ¦ ¦                           ¦    ¦    ¦        in known or forecast           ¦ ¦                           ¦    ¦    ¦        icing conditions,              ¦ ¦                           ¦    ¦    ¦     c) Maximum allowable takeoff      ¦ ¦                           ¦    ¦    ¦        weight is limited to at or     ¦ ¦                           ¦    ¦    ¦        below 31,000 pounds, and       ¦ ¦                           ¦    ¦    ¦     b) Operations are limited to      ¦ ¦                           ¦    ¦    ¦        two flight days before         ¦ ¦                           ¦    ¦    ¦        repairs are made.              ¦

¦       01) "UN-LIMIT"    C ¦ 1  ¦ 0  ¦ (M)(O)May be inoperative provided:    ¦ ¦           Annunciator     ¦    ¦    ¦     a) RUD LIMIT Pushbutton is        ¦ ¦           Pushbutton      ¦    ¦    ¦        operative, and                 ¦ ¦           Light           ¦    ¦    ¦     b) Lights erroneously on are      ¦ ¦                           ¦    ¦    ¦        masked or deactivated.         ¦

¦ 25-00 Rudder Trim       B ¦ 1  ¦ 0  ¦ (M)(O)May be inoperative provided:    ¦ ¦       Indication          ¦    ¦    ¦     a) Rudder Trim System is          ¦ ¦       System              ¦    ¦    ¦        operated through               ¦ ¦                           ¦    ¦    ¦        full travel before             ¦ ¦                           ¦    ¦    ¦        each departure, and            ¦ ¦                           ¦    ¦    ¦     b) At completion of Trim          ¦ ¦                           ¦    ¦    ¦        check, Rudder Trim Tab is      ¦ ¦                           ¦    ¦    ¦        visually verified in the       ¦ ¦                           ¦    ¦    ¦        neutral position, and          ¦ ¦                           ¦    ¦    ¦        Rudder Trim is not             ¦ ¦                           ¦    ¦    ¦        repositioned unless            ¦ ¦                           ¦    ¦    ¦        required in flight.            ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: ORIGINAL ¦ PAGE:    ¦ ¦        FAIRCHILD/DORNIER D-328JET        ¦                       ¦          ¦ ¦                                          ¦ DATE: 07/30/1999      ¦ 27-3     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 27  FLIGHT CONTROLS       ¦    ¦    ¦                                       ¦

¦ 26-00 Rudder Position   C ¦ 1  ¦ 0  ¦ (O)May be inoperative provided,       ¦ ¦       Indication          ¦    ¦    ¦ before each takeoff, normal           ¦ ¦       (FLT CTRL Page)     ¦    ¦    ¦ Rudder control movement is            ¦ ¦                           ¦    ¦    ¦ verified by an acceptable             ¦ ¦                           ¦    ¦    ¦ alternate means.                      ¦

¦ 33-00 Stick Shaker      B ¦ 2  ¦ 1  ¦ (M)(O)One may be inoperative          ¦ ¦                           ¦    ¦    ¦ provided:                             ¦ ¦                           ¦    ¦    ¦     a) Inoperative Stick Shaker       ¦ ¦                           ¦    ¦    ¦        is deactivated, and            ¦ ¦                           ¦    ¦    ¦     b) Before each departure,         ¦ ¦                           ¦    ¦    ¦        Stick Pusher and remaining     ¦ ¦                           ¦    ¦    ¦        Stick Shaker are verified      ¦ ¦                           ¦    ¦    ¦        to operate normally.           ¦

¦ 34-00 "OFF"             C ¦ 1  ¦ 0  ¦ (M)(O)Light may fail provided:        ¦ ¦       Annunciator         ¦    ¦    ¦     a) PUSHER Pushbutton              ¦ ¦       Light on Stick      ¦    ¦    ¦        is operative,                  ¦ ¦       Pusher(PUSHER)      ¦    ¦    ¦     b) Before each departure          ¦ ¦       Pushbutton          ¦    ¦    ¦        Stick Pusher is verified       ¦ ¦       (Center Pedestal)   ¦    ¦    ¦        to operate normally, and       ¦ ¦                           ¦    ¦    ¦     c) Lights erroneously on are      ¦ ¦                           ¦    ¦    ¦        masked or deactivated.         ¦

¦ 35-00 Elevator          C ¦ 1  ¦ 0  ¦ (O)May be inoperative provided,       ¦ ¦       Position            ¦    ¦    ¦ before each takeoff, normal           ¦ ¦       Indication(FLT      ¦    ¦    ¦ Elevator control movement             ¦ ¦       CTRL Page)          ¦    ¦    ¦ is verified by an acceptable          ¦ ¦                           ¦    ¦    ¦ alternate means.                      ¦

¦ 60-00 Roll Spoiler      C ¦ 2  ¦ 0  ¦ (O)May be inoperative provided,       ¦ ¦       Position            ¦    ¦    ¦ before each takeoff, normal           ¦ ¦       Indications(FLT     ¦    ¦    ¦ Roll Spoiler control movement         ¦ ¦       CTRL Page)          ¦    ¦    ¦ is verified by an acceptable          ¦ ¦                           ¦    ¦    ¦ alternate means.                      ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: ORIGINAL ¦ PAGE:    ¦ ¦        FAIRCHILD/DORNIER D-328JET        ¦                       ¦          ¦ ¦                                          ¦ DATE: 07/30/1999      ¦ 27-4     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 27  FLIGHT CONTROLS       ¦    ¦    ¦                                       ¦

¦ 61-00 Ground Spoiler    C ¦ 1  ¦ 0  ¦ (M)(O)May be inoperative              ¦ ¦       System              ¦    ¦    ¦ provided:                             ¦ ¦                           ¦    ¦    ¦     a) System is deactivated,         ¦ ¦                           ¦    ¦    ¦        and                            ¦ ¦                           ¦    ¦    ¦     b) Performance limitations        ¦ ¦                           ¦    ¦    ¦        are applied.                   ¦

¦       01) "TEST"        C ¦ 2  ¦ 0  ¦ (O)Light(s) may fail provided:        ¦ ¦           Annunciator     ¦    ¦    ¦     a) Ground Spoiler Test            ¦ ¦           Light on GND    ¦    ¦    ¦        pushbuttons are                ¦ ¦           SPOIL Test      ¦    ¦    ¦        operative, and                 ¦ ¦           A and Test B    ¦    ¦    ¦     b) Lights erroneously on          ¦ ¦           Pushbuttons     ¦    ¦    ¦        are masked or deactivated.     ¦ ¦           (Center         ¦    ¦    ¦                                       ¦ ¦           Pedestal)       ¦    ¦    ¦                                       ¦

¦ 71-00 Gust Lock System  C ¦ 1  ¦ 0  ¦ (M)May be inoperative provided:       ¦ ¦                           ¦    ¦    ¦     a) An acceptable alternate        ¦ ¦                           ¦    ¦    ¦        method of securing the         ¦ ¦                           ¦    ¦    ¦        affected Flight Controls       ¦ ¦                           ¦    ¦    ¦        is developed and used, and     ¦ ¦                           ¦    ¦    ¦     b) Full and free movement of      ¦ ¦                           ¦    ¦    ¦        associated Flight Controls     ¦ ¦                           ¦    ¦    ¦        is verified before takeoff.    ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: ORIGINAL ¦ PAGE:    ¦ ¦        FAIRCHILD/DORNIER D-328JET        ¦                       ¦          ¦ ¦                                          ¦ DATE: 07/30/1999      ¦ 28-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 28  FUEL                  ¦    ¦    ¦                                       ¦

¦ 10-00 Magnetic          C ¦ 4  ¦ 0  ¦                                       ¦ ¦       Dipsticks           ¦    ¦    ¦                                       ¦ ¦       (Magna Sticks)      ¦    ¦    ¦                                       ¦

¦ 20-00 Fuel Pump           ¦    ¦    ¦                                       ¦ ¦       System              ¦    ¦    ¦                                       ¦

¦       01) ELPMP "FAIL"  C ¦ 2  ¦ 0  ¦ (M)May be inoperative provided:       ¦ ¦           Pushbutton      ¦    ¦    ¦     a) Associated Electric Boost      ¦ ¦           Annunciator     ¦    ¦    ¦        Pump(s) is operative,          ¦ ¦           Lights          ¦    ¦    ¦     b) Associated Jet Pump            ¦ ¦           (Overhead       ¦    ¦    ¦        System(s), and Jet Pump        ¦ ¦           Panel)          ¦    ¦    ¦        Pushbutton Annunciator         ¦ ¦                           ¦    ¦    ¦        Lights are operative,          ¦ ¦                           ¦    ¦    ¦        and                            ¦ ¦                           ¦    ¦    ¦     c) Lights erroneously on are      ¦ ¦                           ¦    ¦    ¦        masked or deactivated.         ¦

¦       02) ELPMP "ON"    C ¦ 2  ¦ 0  ¦ (M)(O)May be inoperative provided:    ¦ ¦           Pushbutton      ¦    ¦    ¦     a) Associated Electric Boost      ¦ ¦           Annunciator     ¦    ¦    ¦        Pump(s) is operative,          ¦ ¦           Lights          ¦    ¦    ¦     b) Associated Jet Pump            ¦ ¦           (Overhead       ¦    ¦    ¦        System(s), and Jet Pump        ¦ ¦           Panel)          ¦    ¦    ¦        Pushbutton Annunciator         ¦ ¦                           ¦    ¦    ¦        Lights are operative,          ¦ ¦                           ¦    ¦    ¦        and                            ¦ ¦                           ¦    ¦    ¦     c) Lights erroneously on are      ¦ ¦                           ¦    ¦    ¦        masked or deactivated.         ¦

¦                           ¦    ¦    ¦ (Continued)                           ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: ORIGINAL ¦ PAGE:    ¦ ¦        FAIRCHILD/DORNIER D-328JET        ¦                       ¦          ¦ ¦                                          ¦ DATE: 07/30/1999      ¦ 28-2     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 28  FUEL                  ¦    ¦    ¦                                       ¦

¦ 20-00 Fuel Pump           ¦    ¦    ¦                                       ¦ ¦       System              ¦    ¦    ¦                                       ¦ ¦       (Cont'd)            ¦    ¦    ¦                                       ¦

¦       03) Jet Pumps     C ¦ 4  ¦ 2  ¦ (M)(O)Any two may be inoperative      ¦ ¦                           ¦    ¦    ¦ provided:                             ¦ ¦                           ¦    ¦    ¦     a) Both Electric Fuel Pumps       ¦ ¦                           ¦    ¦    ¦        operate normally,              ¦ ¦                           ¦    ¦    ¦     b) Fuel Quantity Indications      ¦ ¦                           ¦    ¦    ¦        operate normally,              ¦ ¦                           ¦    ¦    ¦     c) Only Jet A or Jet A1 Fuel      ¦ ¦                           ¦    ¦    ¦        is used, and                   ¦ ¦                           ¦    ¦    ¦     d) Unusable Fuel Quantity in      ¦ ¦                           ¦    ¦    ¦        affected Wing Tank Group       ¦ ¦                           ¦    ¦    ¦        (Inner, Outer, and Feeder      ¦ ¦                           ¦    ¦    ¦        Tanks) is increased by         ¦ ¦                           ¦    ¦    ¦        30 lbs.                        ¦

¦       04) JETPMP        C ¦ 2  ¦ 0  ¦ (M)May be inoperative provided:       ¦ ¦           "FAIL"          ¦    ¦    ¦     a) Associated Jet Pump(s)         ¦ ¦           Pushbutton      ¦    ¦    ¦        are operative,                 ¦ ¦           Annunciator     ¦    ¦    ¦     b) Associated Automatic           ¦ ¦           Lights          ¦    ¦    ¦        Electric Boost Pump(ELPMP      ¦ ¦           (Overhead       ¦    ¦    ¦        AUTO) System(s), and           ¦ ¦           Panel)          ¦    ¦    ¦        Pushbutton                     ¦ ¦                           ¦    ¦    ¦        Annunciator Lights             ¦ ¦                           ¦    ¦    ¦        are operative, and             ¦ ¦                           ¦    ¦    ¦     c) Lights erroneously on are      ¦ ¦                           ¦    ¦    ¦        masked or deactivated.         ¦

¦                           ¦    ¦    ¦ (Continued)                           ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: ORIGINAL ¦ PAGE:    ¦ ¦        FAIRCHILD/DORNIER D-328JET        ¦                       ¦          ¦ ¦                                          ¦ DATE: 07/30/1999      ¦ 28-3     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 28  FUEL                  ¦    ¦    ¦                                       ¦

¦ 20-00 Fuel Pump           ¦    ¦    ¦                                       ¦ ¦       System              ¦    ¦    ¦                                       ¦ ¦       (Cont'd)            ¦    ¦    ¦                                       ¦

¦       05) JETPMP        C ¦ 2  ¦ 0  ¦ (M)(O)May be inoperative provided:    ¦ ¦           "OFF"           ¦    ¦    ¦     a) Associated Jet Pump(s)         ¦ ¦           Pushbutton      ¦    ¦    ¦        are operative,                 ¦ ¦           Annunciator     ¦    ¦    ¦     b) Associated Electric Boost      ¦ ¦           Lights          ¦    ¦    ¦        Pump (ELPMP) System(s),        ¦ ¦           (Overhead       ¦    ¦    ¦        and its associated             ¦ ¦           Panel)          ¦    ¦    ¦        Pushbutton                     ¦ ¦                           ¦    ¦    ¦        Annunciation Lights            ¦ ¦                           ¦    ¦    ¦        operate normally, and          ¦ ¦                           ¦    ¦    ¦     c) Lights erroneously on are      ¦ ¦                           ¦    ¦    ¦        masked or deactivated.         ¦

¦       06) ELPMP Auto    C ¦ 2  ¦ 0  ¦ (M)(O)May be inoperative provided:    ¦ ¦           Boost Pump      ¦    ¦    ¦     a) Associated Electric Boost      ¦ ¦           Function        ¦    ¦    ¦        Pump (ELPMP) is operative,     ¦ ¦                           ¦    ¦    ¦     b) "FAIL" Annunciator Lights      ¦ ¦                           ¦    ¦    ¦        on ELPMP and JETPMP            ¦ ¦                           ¦    ¦    ¦        Pushbuttons are operative,     ¦ ¦                           ¦    ¦    ¦        and                            ¦ ¦                           ¦    ¦    ¦     d) Associated ELPMP remains       ¦ ¦                           ¦    ¦    ¦        ON continuously from           ¦ ¦                           ¦    ¦    ¦        Takeoff to Landing unless      ¦ ¦                           ¦    ¦    ¦        otherwise directed by          ¦ ¦                           ¦    ¦    ¦        Abnormal or Emergency          ¦ ¦                           ¦    ¦    ¦        Procedures.                    ¦

¦                           ¦    ¦    ¦ (Continued)                           ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: ORIGINAL ¦ PAGE:    ¦ ¦        FAIRCHILD/DORNIER D-328JET        ¦                       ¦          ¦ ¦                                          ¦ DATE: 07/30/1999      ¦ 28-4     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 28  FUEL                  ¦    ¦    ¦                                       ¦

¦ 20-00 Fuel Pump           ¦    ¦    ¦                                       ¦ ¦       System              ¦    ¦    ¦                                       ¦ ¦       (Cont'd)            ¦    ¦    ¦                                       ¦

¦       07) ELPMP AUTO    C ¦ 2  ¦ 0  ¦ (M)May be inoperative provided:       ¦ ¦           "FAIL"          ¦    ¦    ¦     a) Associated Electric Boost      ¦ ¦           Pushbutton      ¦    ¦    ¦        Pump is operative,             ¦ ¦           Annunciator     ¦    ¦    ¦     b) Associated Jet Pump            ¦ ¦           Lights          ¦    ¦    ¦        System(s) and Pushbutton       ¦ ¦           (Overhead       ¦    ¦    ¦        Annunciator Lights are         ¦ ¦           Panel)          ¦    ¦    ¦        operative, and                 ¦ ¦                           ¦    ¦    ¦     c) Lights erroneously on are      ¦ ¦                           ¦    ¦    ¦        masked or deactivated.         ¦

¦       08) ELPMP AUTO    C ¦ 2  ¦ 0  ¦ (M)May be inoperative provided:       ¦ ¦           "OFF"           ¦    ¦    ¦     a) Associated Electric Boost      ¦ ¦           Pushbutton      ¦    ¦    ¦        Pump is operative,             ¦ ¦           Annunciator     ¦    ¦    ¦     b) Associated Jet Pump            ¦ ¦           Lights          ¦    ¦    ¦        System(s), and Pushbutton      ¦ ¦           (Overhead       ¦    ¦    ¦        Annunciation Lights are        ¦ ¦           Panel)          ¦    ¦    ¦        operative, and                 ¦ ¦                           ¦    ¦    ¦     c) Lights erroneously on are      ¦ ¦                           ¦    ¦    ¦        masked or deactivated.         ¦

¦ 21-00 Fuel Crossfeed      ¦    ¦    ¦                                       ¦ ¦       Indications         ¦    ¦    ¦                                       ¦ ¦       (Overhead Panel)    ¦    ¦    ¦                                       ¦

¦       01) Horizontal    C ¦ 1  ¦ 0  ¦ (M)(O)Light may fail provided:        ¦ ¦           (Valve Open)    ¦    ¦    ¦     a) Fuel Cross Feed System         ¦ ¦           Flow Bar        ¦    ¦    ¦        is operative, and              ¦ ¦           Annunciator     ¦    ¦    ¦     b) Lights erroneously on are      ¦ ¦           Light           ¦    ¦    ¦        masked or deactivated.         ¦

¦       02) Vertical      C ¦ 1  ¦ 0  ¦ (M)(O)Light may fail provided:        ¦ ¦           (Valve          ¦    ¦    ¦     a) Fuel Cross Feed System         ¦ ¦           Closed) Flow    ¦    ¦    ¦        is operative, and              ¦ ¦           Bar             ¦    ¦    ¦     b) Lights erroneously on are      ¦ ¦           Annunciator     ¦    ¦    ¦        masked or deactivated.         ¦ ¦           Light           ¦    ¦    ¦                                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: ORIGINAL ¦ PAGE:    ¦ ¦        FAIRCHILD/DORNIER D-328JET        ¦                       ¦          ¦ ¦                                          ¦ DATE: 07/30/1999      ¦ 28-5     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 28  FUEL                  ¦    ¦    ¦                                       ¦

¦ 22-00 Fuel Shut           ¦    ¦    ¦                                       ¦ ¦       Off Valve           ¦    ¦    ¦                                       ¦ ¦       Indications         ¦    ¦    ¦                                       ¦ ¦       (Overhead Panel)    ¦    ¦    ¦                                       ¦

¦       01) Horizontal    C ¦ 2  ¦ 0  ¦ (M)(O)May be inoperative provided:    ¦ ¦           (Valve          ¦    ¦    ¦     a) Associated Engine Fuel         ¦ ¦           Closed)         ¦    ¦    ¦        Shut Off Valve(s)              ¦ ¦           Flow Bar        ¦    ¦    ¦        operate normally,              ¦ ¦           Annunciator     ¦    ¦    ¦     b) Lights erroneously on are      ¦ ¦           Light           ¦    ¦    ¦        masked or deactivated.         ¦

¦       02) Vertical      C ¦ 2  ¦ 0  ¦ (M)(O)May be inoperative provided:    ¦ ¦           (Valve Open)    ¦    ¦    ¦     a) Associated Engine Fuel         ¦ ¦           Flow Bar        ¦    ¦    ¦        Shut Off Valve(s) are          ¦ ¦           Annunciator     ¦    ¦    ¦        operative, and                 ¦ ¦           Lights          ¦    ¦    ¦     b) Lights erroneously on are      ¦ ¦                           ¦    ¦    ¦        masked or deactivated.         ¦

¦ 23-00 Pressure          C ¦ 1  ¦ 0  ¦ May be inoperative provided           ¦ ¦       Refueling System    ¦    ¦    ¦ acceptable alternate refueling        ¦ ¦                           ¦    ¦    ¦ procedures are established            ¦ ¦                           ¦    ¦    ¦ and used.                             ¦

¦       01) Automatic     C ¦ 1  ¦ 0  ¦ May be inoperative provided           ¦ ¦           Function        ¦    ¦    ¦ Manual Pressure Refueling             ¦ ¦                           ¦    ¦    ¦ Function operates normally.           ¦

¦       02) Manual        C ¦ 1  ¦ 0  ¦ May be inoperative provided           ¦ ¦           Function        ¦    ¦    ¦ Automatic Pressure Refueling          ¦ ¦                           ¦    ¦    ¦ Function operates normally.           ¦

¦       03) Pressure      C ¦ 1  ¦ 0  ¦ May be missing.                       ¦ ¦           Refueling       ¦    ¦    ¦                                       ¦ ¦           Cap             ¦    ¦    ¦                                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: ORIGINAL ¦ PAGE:    ¦ ¦        FAIRCHILD/DORNIER D-328JET        ¦                       ¦          ¦ ¦                                          ¦ DATE: 07/30/1999      ¦ 28-6     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 28  FUEL                  ¦    ¦    ¦                                       ¦

¦ 40-01 EICAS "FUEL       C ¦ 2  ¦ 0  ¦ (O)May be inoperative provided        ¦ ¦       LEVEL LOW"          ¦    ¦    ¦ associated EICAS Fuel Quantity        ¦ ¦       Cautions            ¦    ¦    ¦ indications operate normally.         ¦

¦ 40-02 EICAS "FUEL       C ¦ 2  ¦ 0  ¦ (O)May be inoperative provided:       ¦ ¦       TANK TEMP"          ¦    ¦    ¦     a) Static Air Temperature         ¦ ¦       Cautions            ¦    ¦    ¦        (SAT) Indications operate      ¦ ¦                           ¦    ¦    ¦        normally, and                  ¦ ¦                           ¦    ¦    ¦     b) Appropriate AFM                ¦ ¦                           ¦    ¦    ¦        Limitations, Procedures,       ¦ ¦                           ¦    ¦    ¦        and Performance                ¦ ¦                           ¦    ¦    ¦        adjustments are applied.       ¦

¦ 40-03 EICAS Fuel       C  ¦ 6  ¦ 5  ¦ (M)(O)One may be inoperative          ¦ ¦       Quantity            ¦    ¦    ¦ provided:                             ¦ ¦       Indications         ¦    ¦    ¦     a) Fuel Quantity in               ¦ ¦                           ¦    ¦    ¦        associated Fuel Tank(s)        ¦ ¦                           ¦    ¦    ¦        is verified by an              ¦ ¦                           ¦    ¦    ¦        acceptable alternate           ¦ ¦                           ¦    ¦    ¦        means,                         ¦ ¦                           ¦    ¦    ¦     b) Associated Fuel Flow           ¦ ¦                           ¦    ¦    ¦        and Fuel Remaining             ¦ ¦                           ¦    ¦    ¦        Indications operate            ¦ ¦                           ¦    ¦    ¦        normally,                      ¦ ¦                           ¦    ¦    ¦     c) All Fuel Pumps (Electric       ¦ ¦                           ¦    ¦    ¦        and Jet) operate normally,     ¦ ¦                           ¦    ¦    ¦     d) Fuel Quantity of affected      ¦ ¦                           ¦    ¦    ¦        Wing Tank Group is             ¦ ¦                           ¦    ¦    ¦        manually entered in the        ¦ ¦                           ¦    ¦    ¦        EICAS Fuel System Page         ¦ ¦                           ¦    ¦    ¦        prior to engine start          ¦ ¦                           ¦    ¦    ¦        and,                           ¦ ¦                           ¦    ¦    ¦     e) 300 pounds remaining fuel      ¦ ¦                           ¦    ¦    ¦        in the affected tank is        ¦ ¦                           ¦    ¦    ¦        considered to be unusable.     ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 1        ¦ PAGE:    ¦ ¦        FAIRCHILD/DORNIER D-328JET        ¦                       ¦          ¦ ¦                                          ¦ DATE: 11/15/2001      ¦ 28-7     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 28  FUEL                  ¦    ¦    ¦                                       ¦

¦ 40-04 "ON" Annunciator  C ¦ 3  ¦ 0  ¦ Light(s) may fail to illuminate       ¦ ¦       Lights on Auxiliary ¦    ¦    ¦ provided:                             ¦ ¦       Transfer pumps      ¦    ¦    ¦     a) Associated Electric Transfer   ¦ ¦       (AUXPMP) Push-      ¦    ¦    ¦        pump(s)is verified to          ¦ ¦       buttons             ¦    ¦    ¦        operate normally,              ¦ ¦                           ¦    ¦    ¦     b) EICAS FUEL System page         ¦ ¦                           ¦    ¦    ¦        operates normally,             ¦ ¦                           ¦    ¦    ¦     c) Remaining Annunciator Lights   ¦ ¦                           ¦    ¦    ¦        on affected pushbuttons(s)     ¦ ¦                           ¦    ¦    ¦        operate normally,              ¦ ¦                           ¦    ¦    ¦     d) EICAS FUEL System page         ¦ ¦                           ¦    ¦    ¦        for determining Electric       ¦ ¦                           ¦    ¦    ¦        Boost Pump(s) status is        ¦ ¦                           ¦    ¦    ¦        used, and                      ¦ ¦                           ¦    ¦    ¦     e) Auxiliary fuel system AUTO     ¦ ¦                           ¦    ¦    ¦        mode active and operate.       ¦

¦ 40-05 "Fail"            C ¦ 3  ¦ 0  ¦ Light(s) may fail to illuminate       ¦ ¦       Annunciator Lights  ¦    ¦    ¦ provided:                             ¦ ¦       On Auxiliary        ¦    ¦    ¦     a) Associated Electric Transfer   ¦ ¦       Transfer pumps      ¦    ¦    ¦        pumps is verified to operate   ¦ ¦       (AUXPMP) Push-      ¦    ¦    ¦        normally,                      ¦ ¦       buttons             ¦    ¦    ¦     b) EICAS FUEL System Page         ¦ ¦                           ¦    ¦    ¦        operates normally,             ¦ ¦                           ¦    ¦    ¦     c) Remaining Annunciator Lights   ¦ ¦                           ¦    ¦    ¦        on affected pushbuttons        ¦ ¦                           ¦    ¦    ¦        operate normally, and          ¦ ¦                           ¦    ¦    ¦     d) Auxiliary fuel system AUTO     ¦ ¦                           ¦    ¦    ¦        mode active and operate.       ¦

¦ 40-06 "MAN" Annunciator C ¦ 1  ¦ 0  ¦ Light may fail to illuminate          ¦ ¦       Light on MAN        ¦    ¦    ¦ provided indication on EICAS FUEL     ¦ ¦       Pushbutton          ¦    ¦    ¦ System Page operates normally.        ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 1        ¦ PAGE:    ¦ ¦        FAIRCHILD/DORNIER D-328JET        ¦                       ¦          ¦ ¦                                          ¦ DATE: 11/15/2001      ¦ 28-8     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 28  FUEL                  ¦    ¦    ¦                                       ¦

¦ 40-07 Auxiliary         C ¦ 3  ¦ 0  ¦ Auxiliary transfer pumps may be       ¦ ¦       Transfer pumps      ¦    ¦    ¦ inoperative provided:                 ¦ ¦       (AUXPMP)            ¦    ¦    ¦     a) Auxiliary fuel system is in    ¦ ¦                           ¦    ¦    ¦        MAN mode,                      ¦ ¦                           ¦    ¦    ¦     b) All three auxiliary transfer   ¦ ¦                           ¦    ¦    ¦        pumps are selected OFF,        ¦ ¦                           ¦    ¦    ¦     c) EICAS FUEL System Page         ¦ ¦                           ¦    ¦    ¦        operates normally,             ¦ ¦                           ¦    ¦    ¦     d) Auxiliary Fuel Quantity        ¦ ¦                           ¦    ¦    ¦        operate                        ¦ ¦                           ¦    ¦    ¦     e) Auxiliary Fuel Quantities      ¦ ¦                           ¦    ¦    ¦        are within CG limits, and      ¦ ¦                           ¦    ¦    ¦     f) Indicated Auxiliary Fuel       ¦ ¦                           ¦    ¦    ¦        is considered unusable.        ¦

¦ 40-08 Auxiliary Refuel  C ¦ 3  ¦ 0  ¦ Auiliary refuel valves may be         ¦ ¦       Valves (AUXSOV)     ¦    ¦    ¦ inoperative provided:                 ¦ ¦                           ¦    ¦    ¦     a) Associated auxiliary refuel    ¦ ¦                           ¦    ¦    ¦        valve is verified to be        ¦ ¦                           ¦    ¦    ¦        closed, and                    ¦ ¦                           ¦    ¦    ¦     b) EICAS Fuel System page         ¦ ¦                           ¦    ¦    ¦        operates normally.             ¦

¦ 40-09 Auxiliary         C ¦ 2  ¦ 0  ¦ Auxiliary transfer valve may be       ¦ ¦       Transfer Valves     ¦    ¦    ¦ inoperative provided:                 ¦ ¦       (XFERSOV)           ¦    ¦    ¦     a) Associated auxiliary           ¦ ¦                           ¦    ¦    ¦        transfer valves are verified   ¦ ¦                           ¦    ¦    ¦        to be closed,                  ¦ ¦                           ¦    ¦    ¦     b) EICAS Fuel System page         ¦ ¦                           ¦    ¦    ¦        operates normally,             ¦ ¦                           ¦    ¦    ¦     c) Auxiliary fuel system is in    ¦ ¦                           ¦    ¦    ¦        MAN mode,                      ¦ ¦                           ¦    ¦    ¦     d) All three auxiliary pumps      ¦ ¦                           ¦    ¦    ¦        are selected OFF,              ¦ ¦                           ¦    ¦    ¦     e) Auxiliary fuel quantities      ¦ ¦                           ¦    ¦    ¦        are within CG limits, and      ¦ ¦                           ¦    ¦    ¦     f) Indicated auxiliary fuel is    ¦ ¦                           ¦    ¦    ¦        considered unuable.            ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 1 a      ¦ PAGE:    ¦ ¦        FAIRCHILD/DORNIER D-328JET        ¦                       ¦          ¦ ¦                                          ¦ DATE: 05/20/2004      ¦ 28-9     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 28  FUEL                  ¦    ¦    ¦                                       ¦

¦ 40-10 EICAS Fuel        C ¦ 3  ¦ 0  ¦ Auxiliary fuel quantity indication    ¦ ¦       Quantity            ¦    ¦    ¦ may be inoperative provided:          ¦ ¦       Indication          ¦    ¦    ¦     a) Auxiliary fuel tanks are       ¦ ¦       Auxiliary Fuel      ¦    ¦    ¦        verified to be empty,          ¦ ¦       Tanks               ¦    ¦    ¦     b) Auxiliary fuel system is in    ¦ ¦                           ¦    ¦    ¦        MAN mode,                      ¦ ¦                           ¦    ¦    ¦     c) All three auxiliary transfer   ¦ ¦                           ¦    ¦    ¦        pumps are selected OFF         ¦ ¦                           ¦    ¦    ¦     d) EICAS fuel system page         ¦ ¦                           ¦    ¦    ¦        operates normally,             ¦ ¦                           ¦    ¦    ¦     e) Auxiliary transfer pumps       ¦ ¦                           ¦    ¦    ¦        operate normally (OFF), and    ¦ ¦                           ¦    ¦    ¦     f) Auxiliary refuel valves        ¦ ¦                           ¦    ¦    ¦        operate normally (Closed).     ¦

¦ 40-11 EICAS Indication  C ¦ -  ¦ 0  ¦ (O)May be inoperative provided:     | ¦ ¦       (Blue) L & R FUEL   ¦    ¦    ¦     a) Fuel Quantity is associated  | ¦ ¦       QTY ACCUR           ¦    ¦    ¦        fuel tank(s) is verified by  | ¦ ¦       Illuminated         ¦    ¦    ¦        by an acceptable means,      | ¦ ¦                           ¦    ¦    ¦     b) Associated Fuel Flow and     | ¦ ¦                           ¦    ¦    ¦        Fuel Remaining indications   | ¦ ¦                           ¦    ¦    ¦        operate normally, and        | ¦ ¦                           ¦    ¦    ¦     c) All Fuel Pumps (Electric and | ¦ ¦                           ¦    ¦    ¦        Jet) operate normally.       | ¦

¦                           ¦    ¦    ¦ NOTE: Aircraft with Option          | ¦ ¦                           ¦    ¦    ¦       # 0330F003A will lose the     | ¦ ¦                           ¦    ¦    ¦       ability to Refuel the         | ¦ ¦                           ¦    ¦    ¦       Auxiliary Fuel Tanks.         | ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: ORIGINAL ¦ PAGE:    ¦ ¦        FAIRCHILD/DORNIER D-328JET        ¦                       ¦          ¦ ¦                                          ¦ DATE: 07/30/1999      ¦ 29-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 29  HYDRAULIC POWER       ¦    ¦    ¦                                       ¦

¦ 31-00 "OFF"             C ¦ 1  ¦ 0  ¦ (M)(O)May be inoperative provided:    ¦ ¦       Annunciator         ¦    ¦    ¦     a) Hydraulic System "A" pump      ¦ ¦       Light on            ¦    ¦    ¦        Pushbutton is operative,       ¦ ¦       Hydraulic Power     ¦    ¦    ¦        and,                           ¦ ¦       (HYD PWR)           ¦    ¦    ¦     b) Lights erroneously on are      ¦ ¦       System "A"          ¦    ¦    ¦        masked or deactivated.         ¦ ¦       Pushbutton          ¦    ¦    ¦                                       ¦ ¦       (Overhead Panel)    ¦    ¦    ¦                                       ¦

¦ 32-00 "OFF"             C ¦ 1  ¦ 0  ¦ (M)(O)May be inoperative provided:    ¦ ¦       Annunciator         ¦    ¦    ¦     a) Hydraulic System "B" pump      ¦ ¦       Light on            ¦    ¦    ¦        Pushbutton is operative,       ¦ ¦       Hydraulic Power     ¦    ¦    ¦        and,                           ¦ ¦       (HYD PWR)           ¦    ¦    ¦     b) Lights erroneously on are      ¦ ¦       System "B"          ¦    ¦    ¦        masked or deactivated.         ¦ ¦       Pushbutton          ¦    ¦    ¦                                       ¦ ¦       (Overhead Panel)    ¦    ¦    ¦                                       ¦

¦ 33-00 "ALT BRK"         C ¦ 1  ¦ 0  ¦ (M)(O)May be inoperative provided:    ¦ ¦       Annunciator         ¦    ¦    ¦     a) ALT BRK COV pushbutton         ¦ ¦       Light on            ¦    ¦    ¦        is operative, and              ¦ ¦       Brake Change        ¦    ¦    ¦     b) Lights erroneously on are,     ¦ ¦       Over Valve          ¦    ¦    ¦        masked or deactivated.         ¦ ¦       (COV)               ¦    ¦    ¦                                       ¦ ¦       Pushbutton          ¦    ¦    ¦                                       ¦ ¦       (Overhead Panel)    ¦    ¦    ¦                                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: ORIGINAL ¦ PAGE:    ¦ ¦        FAIRCHILD/DORNIER D-328JET        ¦                       ¦          ¦ ¦                                          ¦ DATE: 07/30/1999      ¦ 30-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 30  ICE AND RAIN          ¦    ¦    ¦                                       ¦ ¦     PROTECTION            ¦    ¦    ¦                                       ¦

¦ 10-00 Elevator/Rudder   B ¦ 2  ¦ 0  ¦ May be inoperative provided:          ¦ ¦       Horn Heater         ¦    ¦    ¦     a) Both Elevator/Rudder Horn      ¦ ¦       Systems             ¦    ¦    ¦        Heater Selector Switches       ¦ ¦                           ¦    ¦    ¦        remain in the OFF              ¦ ¦                           ¦    ¦    ¦        Position, and                  ¦ ¦                           ¦    ¦    ¦     b) Aircraft is not operated       ¦ ¦                           ¦    ¦    ¦        in known or forecast           ¦ ¦                           ¦    ¦    ¦        icing conditions.              ¦

¦       01) "FAIL"        B ¦ 2  ¦ 0  ¦ (M)(O)May be inoperative provided:    ¦ ¦           Annunciator     ¦    ¦    ¦     a) Associated Horn De-ice         ¦ ¦           Pushbutton      ¦    ¦    ¦        System is operative, and       ¦ ¦           Lights          ¦    ¦    ¦     b) Lights erroneously on are      ¦ ¦                           ¦    ¦    ¦        masked or deactivated.         ¦

¦       02) "ON"          B ¦ 2  ¦ 0  ¦ (M)(O)May be inoperative provided:    ¦ ¦           Annunicator     ¦    ¦    ¦     a) Associated Horn De-ice         ¦ ¦           Pushbutton      ¦    ¦    ¦        System is operative, and       ¦ ¦           Lights          ¦    ¦    ¦     b) Lights erroneously on are      ¦ ¦                           ¦    ¦    ¦        masked or deactivated.         ¦

¦ 11-00 Airfoil De-ice      ¦    ¦    ¦                                       ¦ ¦       Bleed System        ¦    ¦    ¦                                       ¦

¦       01) "OFF"         C ¦ 2  ¦ 0  ¦ (M)(O)May be inoperative provided:    ¦ ¦           Annunciator     ¦    ¦    ¦     a) Affected De-ice Airfoil        ¦ ¦           Pushbutton      ¦    ¦    ¦        Bleed System(s) are            ¦ ¦           Lights          ¦    ¦    ¦        operative, and                 ¦ ¦                           ¦    ¦    ¦     b) Lights erroneously on are      ¦ ¦                           ¦    ¦    ¦        masked or deactivated.         ¦

¦       02) Horizontal    C ¦ 2  ¦ 0  ¦ (M)(O)May be inoperative provided:    ¦ ¦           (Valve Open)    ¦    ¦    ¦     a) Affected Airfoil De-ice        ¦ ¦           Flow Bars       ¦    ¦    ¦        Bleed System(s) are            ¦ ¦           Annunciator     ¦    ¦    ¦        operative, and                 ¦ ¦           Pushbutton      ¦    ¦    ¦     b) Lights erroneously on are      ¦ ¦           Lights          ¦    ¦    ¦        masked or deactivated.         ¦

¦                           ¦    ¦    ¦ (Continued)                           ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

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