DEPARTMENT OF TRANSPORTATION     Revision: 10 a

Date: 06/25/2004

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

FAN JET FALCON (Falcon 20)

SERIES C, D, E, F

/S/

JAMES M. EITEL, CHAIRMAN DA-20

FLIGHT OPERATIONS EVALUATION BOARD

Federal Aviation Administration

Flight Standards Division

AIRCRAFT EVALUATION GROUP, SEA-AEG

1601 Lind Ave. S.W.

RENTON, WASHINGTON 98055-4056

TELEPHONE: COMM: (425) 917-6600

FAX:  (425) 917-6638

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Table of Contents

SYSTEM NO.  SYSTEM                                  PAGE

--     Table of Contents                       I, II

--     Log of Revisions                        III

--     Control Page                            IV, V, VI

--     Highlights of Change                    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

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

24     Electrical Power                        24-1

25     Equipment/Furnishings                   25-1, 2

26     Fire Protection                         26-1

27     Flight Controls                         27-1, 2, 3

28     Fuel                                    28-1, 2

29     Hydraulic Power                         29-1, 2

30     Ice and Rain Protection                 30-1, 2

31     Indicating/Recording Systems            31-1, 2

32     Landing Gear                            32-1, 2

33     Lights                                  33-1, 2, 3

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

34     Navigation                              34-11  THRU 15 34     Navigation                              34-16

35     Oxygen                                  35-1

36     Pneumatic                               36-1

49     Airborne Auxiliary Power                49-1

52     Doors                                   52-1

73     Engine Fuel & Control                   73-1

74     Ignition                                74-1

76     Engine Controls                         76-1

77     Engine Indicating                       77-1, 2 78     Engine Exhaust                          78-1

79     Engine Oil                              79-1

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Table of Contents

SYSTEM NO.  SYSTEM                                  PAGE

80     Starting                                80-1

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Log of Revisions

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

¦ 8        ¦ 02/27/1990 ¦ ALL PAGES                      ¦           ¦ ¦ 9        ¦ 10/12/1993 ¦ HIGHLIGHTS OF REV.,DEFINITIONS ¦           ¦ ¦ 9        ¦ 10/12/1993 ¦ 21-1,21-2,21-3,21-4,22-1       ¦           ¦ ¦ 9        ¦ 10/12/1993 ¦ 23-1,23-2,24-1,25-1,25-2       ¦           ¦ ¦ 9        ¦ 10/12/1993 ¦ 26-1,27-1,27-2,27-3,28-1       ¦           ¦ ¦ 9        ¦ 10/12/1993 ¦ 28-2,29-1,29-2,30-1,30-2       ¦           ¦ ¦ 9        ¦ 10/12/1993 ¦ 31-1,32-1,33-1,33-2,33-3       ¦           ¦ ¦ 9        ¦ 10/12/1993 ¦ 34-1,34-2,34-3,34-4,34-5       ¦           ¦ ¦ 9        ¦ 10/12/1993 ¦ 34-6,34-7,34-8,34-9,34-10      ¦           ¦ ¦ 9        ¦ 10/12/1993 ¦ 34-11,35-1,36-1,49-1,52-1      ¦           ¦ ¦ 9        ¦ 10/12/1993 ¦ 73-1,74-1,77-1,77-2,78-1       ¦           ¦ ¦ 9        ¦ 10/12/1993 ¦ 79-1,80-1                      ¦           ¦ ¦ 9a       ¦ 07/07/1998 ¦ HIGHLIGHTS OF REV.,DEFINITIONS ¦           ¦ ¦ 9a       ¦ 07/07/1998 ¦ 22-1,23-1,23-2,25-2,26-1       ¦           ¦ ¦ 9a       ¦ 07/07/1998 ¦ 31-1,33-1,33-3,34-2,34-3       ¦           ¦ ¦ 9a       ¦ 07/07/1998 ¦ 34-4,34-5,34-10,34-11          ¦           ¦ ¦ 9b       ¦ 02/22/1999 ¦ HIGHLIGHTS OF REV.,DEFINITIONS ¦           ¦ ¦ 9b       ¦ 02/22/1999 ¦ 21-4,22-1,23-2,23-3,28-1       ¦           ¦ ¦ 9b       ¦ 02/22/1999 ¦ 76-1                           ¦           ¦ ¦ 10       ¦ 08/12/2002 ¦ HIGHLIGHTS OF REV.,DEFINITIONS ¦           ¦ ¦ 10       ¦ 08/12/2002 ¦ 21-5,22-1,22-2,22-3,22-4       ¦           ¦ ¦ 10       ¦ 08/12/2002 ¦ 23-1,23-2,23-3,23-4,23-5       ¦           ¦ ¦ 10       ¦ 08/12/2002 ¦ 23-6,25-1,31-1,31-2,34-3       ¦           ¦ ¦ 10       ¦ 08/12/2002 ¦ 34-4,34-5,34-6,34-7,34-8       ¦           ¦ ¦ 10       ¦ 08/12/2002 ¦ 34-9,34-10,34-11,34-12,34-13   ¦           ¦ ¦ 10       ¦ 08/12/2002 ¦ 34-14,34-15,34-16              ¦           ¦ ¦ 10a      ¦            ¦ HIGHLIGHTS OF REV.,DEFINITIONS ¦           ¦ ¦ 10a      ¦            ¦ 21-4,23-1,23-2,23-3,23-4       ¦           ¦ ¦ 10a      ¦            ¦ 23-5,23-6,23-7,25-1,27-1       ¦           ¦ ¦ 10a      ¦            ¦ 32-1,32-2,34-5,34-6,34-16      ¦           ¦ ¦ 10a      ¦            ¦ 49-1,52-1                      ¦           ¦

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Control Page

SYSTEM                                   PAGE  REV NO.  CURRENT DATE

Cover Page                               -       10 a     06/25/2004 Table of Contents                        I       10 a     06/25/2004 II      10 a     06/25/2004 Log of Revisions                         III     10 a     06/25/2004 Control Page                             IV      10 a     06/25/2004 V       10 a     06/25/2004 VI      10 a     06/25/2004 Highlights of Change                     VII     10 a     06/25/2004 VIII    10 a     06/25/2004 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    9         10/12/1993 21-2    9        10/12/1993 21-3    9        10/12/1993 21-4    10 a     06/25/2004 21-5    10       08/12/2002 22                                       22-1    10       08/12/2002 22-2    10               08/12/2002 22-3    10       08/12/2002 22-4    10       08/12/2002 23                                       23-1    10 a     06/25/2004 23-2    10 a     06/25/2004 23-3    10 a     06/25/2004 23-4    10 a     06/25/2004 23-5    10 a     06/25/2004 23-6    10 a     06/25/2004 23-7    10 a     06/25/2004 24                                       24-1    9        10/12/1993 25                                               25-1    10 a     06/25/2004 25-2    9 a      07/07/1998 26                                       26-1    9 a      07/07/1998 27                                       27-1    10 a                                                               06/25/2004

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Control Page

SYSTEM                                   PAGE  REV NO.  CURRENT DATE

27-2    9        10/12/1993 27-3    9        10/12/1993 28                                       28-1    9 b      02/22/1999 28-2    9        10/12/1993 29                                       29-1    9        10/12/1993 29-2    9        10/12/1993 30                                               30-1    9        10/12/1993 30-2    9        10/12/1993 31                                       31-1    10       08/12/2002 31-2    10       08/12/2002 32                                        32-1    10 a     06/25/2004 32-2    10 a     06/25/2004 33                                       33-1    9 a      07/07/1998 33-2    9        10/12/1993 33-3    9 a      07/07/1998 34                                       34-1    9        10/12/1993 34-2    9 a              07/07/1998 34-3    10       08/12/2002 34-4    10       08/12/2002 34-5    10 a     06/25/2004 34-6    10 a     06/25/2004 34-7    10       08/12/2002 34-8    10       08/12/2002 34-9    10               08/12/2002 34-10   10       08/12/2002 34-11   10       08/12/2002 34-12   10       08/12/2002 34-13   10       08/12/2002 34-14   10       08/12/2002 34-15   10       08/12/2002 34-16   10 a     06/25/2004 35                                       35-1    9        10/12/1993 36                                       36-1    9        10/12/1993 49                                       49-1    10 a     06/25/2004 52                                       52-1    10 a     06/25/2004 73                                       73-1    9        10/12/1993 74                                       74-1    9        10/12/1993 76                                       76-1    9 b      02/22/1999 77                                       77-1    9                                  10/12/1993 77-2    9        10/12/1993

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Control Page

SYSTEM                                   PAGE  REV NO.  CURRENT DATE

78                                       78-1    9        10/12/1993 79                                       79-1    9        10/12/1993 80                                       80-1    9        10/12/1993

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Highlights of Change

EFFECTIVE ABOVE DATE, The Falcon 20 Master Minimum Equipment List has been revised.  Please replace affected pages of the previous list with Revision 10a for a complete up-to-date MMEL.  Change bars have been included to aid the user in identifying any changes as a result of this revision.

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

ATA 21  AIR CONDITIONING

Item 14, Electrical Rack Blowers: Deleted, no reference in AFM to allow operation with inoperative Electrical Rack Blowers.

ATA 23  COMMUNICATIONS

Item 1,  Passenger Address System: Amended to comply with PL 9.

Item 2,  Communications Systems (VHF, UHF): Deleted "HF" from title to comply with PL 95.

Item 4,  Crewmember Interphone System(s): Amended to comply with PL 9.

Item 17, High Frequency Communication System: New item to comply with PL 106.

ATA 25  EQUIPMENT/FURNISHINGS

Item 2,  Emergency Locator Transmitter:  Deleted, relief already provided in item 23-16.

ATA 27  FLIGHT CONTROLS

Item 1,  Arthur Q Units: Added second proviso to clarify F20-5 airspeed limits.

Item 2,  Arthur Q Unit Warning Light Systems: Added second proviso to clarify F20-5 airspeed limits.

ATA 32  LANDING GEAR

Item 1,  Anti-Skid System: Amended to comply with PL 113.

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Highlights of Change

ATA 34  NAVIGATION

Item 17, ATC Transponders and Automatic Reporting Systems: Amended category from "C" to "B", reference PL 76.

Item 19, Standby Attitude Indicator: Amended to comply with PL 111.

Item 22, Flight Management System: Deleted, duplicate with item 34-55.

Item 55, Flight Management System: Incorporated relief from item 34-22.

ATA 52  DOORS

Item 1,  Door Warning Light System: Added "(M)" procedure to proviso, complies with PL 69.

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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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Preamble

(Effective 6/14/89)

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

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

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

 

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

DA-20

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: 9        ¦ PAGE:    ¦ ¦                  DA-20                   ¦                       ¦          ¦ ¦                                          ¦ DATE: 10/12/1993      ¦ 21-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦

¦ 21  AIR CONDITIONING      ¦    ¦    ¦                                       ¦

¦ 1.  Out-Flow/Safety     C ¦ 2  ¦ 0  ¦ (M)May be inoperative provided:       ¦ ¦     Valves                ¦    ¦    ¦     a) Flight is conducted in an      ¦ ¦                           ¦    ¦    ¦        unpressurized configuration,   ¦ ¦                           ¦    ¦    ¦     b) Flight remains at or below     ¦ ¦                           ¦    ¦    ¦        10,000 feet MSL, and           ¦ ¦                           ¦    ¦    ¦     c) Extended overwater flights     ¦ ¦                           ¦    ¦    ¦        are prohibited.                ¦

¦ 2.  Cabin Altitude/     C ¦ 1  ¦ 0  ¦ May be inoperative provided:          ¦ ¦     Overpressure (CAB)    ¦    ¦    ¦     a) Cabin altimeter operates       ¦ ¦     Warning Light         ¦    ¦    ¦        normally,                      ¦ ¦                           ¦    ¦    ¦     b) Cabin altitude warning horn    ¦ ¦                           ¦    ¦    ¦        operates normally, and         ¦ ¦                           ¦    ¦    ¦     c) Cabin pressure indicator       ¦ ¦                           ¦    ¦    ¦        operates normally.             ¦

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

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

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 9        ¦ PAGE:    ¦ ¦                  DA-20                   ¦                       ¦          ¦ ¦                                          ¦ DATE: 10/12/1993      ¦ 21-2     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 21. AIR CONDITIONING      ¦    ¦    ¦                                       ¦

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

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

¦ 7.  Electronic          C ¦ 2  ¦ 1  ¦ (O)Automatic control may be           ¦ ¦     Temperature Control   ¦    ¦    ¦ inoperative provided manual           ¦ ¦     Systems               ¦    ¦    ¦ electric temperature control          ¦ ¦                           ¦    ¦    ¦ operates normally.                    ¦

¦                         C ¦ 2  ¦ 0  ¦ (O)Automatic and manual electric      ¦ ¦                           ¦    ¦    ¦ temperature controls may be           ¦ ¦                           ¦    ¦    ¦ inoperative provided manual           ¦ ¦                           ¦    ¦    ¦ temperature control (located in aft   ¦ ¦                           ¦    ¦    ¦ cabin)operates normally and is set    ¦ ¦                           ¦    ¦    ¦ before departure in accordance        ¦ ¦                           ¦    ¦    ¦ with an approved procedure.           ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 9        ¦ PAGE:    ¦ ¦                  DA-20                   ¦                       ¦          ¦ ¦                                          ¦ DATE: 10/12/1993      ¦ 21-3     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 21. AIR CONDITIONING      ¦    ¦    ¦                                       ¦

¦ 8.  Cabin Pressurization  ¦    ¦    ¦                                       ¦ ¦     Control System        ¦    ¦    ¦                                       ¦

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

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

¦ 9.  Cabin Temperature   C ¦ 1  ¦ 0  ¦                                       ¦ ¦     Remote Control        ¦    ¦    ¦                                       ¦

¦ 10. Temperature         C ¦ 1  ¦ 0  ¦                                       ¦ ¦     Control Valve         ¦    ¦    ¦                                       ¦ ¦     Position Indicator    ¦    ¦    ¦                                       ¦

¦ 11. Cabin Temperature   C ¦ 1  ¦ 0  ¦                                       ¦ ¦     Indicator             ¦    ¦    ¦                                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 10 a     ¦ PAGE:    ¦ ¦                  DA-20                   ¦                       ¦          ¦ ¦                                          ¦ DATE: 06/25/2004      ¦ 21-4     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 21. AIR CONDITIONING      ¦    ¦    ¦                                       ¦

¦ 12. Cabin Air           C ¦ 1  ¦ 0  ¦ (M)(O)May be inoperative in the       ¦ ¦     Conditioning Valve    ¦    ¦    ¦ CLOSED position provided:             ¦ ¦                           ¦    ¦    ¦     a) Flight is conducted in an      ¦ ¦                           ¦    ¦    ¦        unpressurized configuration,   ¦ ¦                           ¦    ¦    ¦        and                            ¦ ¦                           ¦    ¦    ¦     b) Cabin ram air scoop is OPEN.   ¦

¦                         C ¦ 1  ¦ 0  ¦ (M)(O)May be inoperative in the       ¦ ¦                           ¦    ¦    ¦ full OPEN position provided:          ¦ ¦                           ¦    ¦    ¦     a) Both bleed valves operate      ¦ ¦                           ¦    ¦    ¦        normally,                      ¦ ¦                           ¦    ¦    ¦     b) Both bleed valves are          ¦ ¦                           ¦    ¦    ¦        selected OFF for takeoff,      ¦ ¦                           ¦    ¦    ¦     c) Cabin Altitude/Overpressure    ¦ ¦                           ¦    ¦    ¦        Warning Light operates         ¦ ¦                           ¦    ¦    ¦        normally, and                  ¦ ¦                           ¦    ¦    ¦     d) Cabin Altitude/Overpressure    ¦ ¦                           ¦    ¦    ¦        Warning Horn operates          ¦ ¦                           ¦    ¦    ¦        normally.                      ¦

¦ 13. Cockpit Gasper      C ¦ 2  ¦ 1  ¦                                       ¦ ¦     Outlets               ¦    ¦    ¦                                       ¦

¦ 14. Electrical Rack       ¦    ¦    ¦ Deleted, revision 10a.              | ¦ ¦     Blowers               ¦    ¦    ¦                                       ¦

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

¦ 16. Ram Air Scoop       C ¦ 1  ¦ 0  ¦ (O)May be inoperative in the OPEN     ¦ ¦                           ¦    ¦    ¦ position.                             ¦

¦ 17. Pilot Foot Warmer   C ¦ 1  ¦ 0  ¦ May be inoperative CLOSED (Bleed      ¦ ¦                           ¦    ¦    ¦ Air) or OFF (Electric).               ¦

¦ 18. Cockpit Cooling     C ¦ 1  ¦ 0  ¦                                       ¦ ¦ *** Fan                   ¦    ¦    ¦                                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 10       ¦ PAGE:    ¦ ¦                  DA-20                   ¦                       ¦          ¦ ¦                                          ¦ DATE: 08/12/2002      ¦ 21-5     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 21  AIR CONDITIONING      ¦    ¦    ¦                                       ¦

¦ 19. EFIS Blowers        C ¦ 4  ¦ 3  ¦ (M)One may be inoperative provided:   ¦ ¦     (Pro Line 4, STC      ¦    ¦    ¦     a) Both PFD blowers operate       ¦ ¦     ST00600WI-D)          ¦    ¦    ¦        normally, and                  ¦ ¦                           ¦    ¦    ¦     b) The cold air supply system     ¦ ¦                           ¦    ¦    ¦        is verified to provide an      ¦ ¦                           ¦    ¦    ¦        adequate air flow to the       ¦ ¦                           ¦    ¦    ¦        EFIS.                          ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 10       ¦ PAGE:    ¦ ¦                  DA-20                   ¦                       ¦          ¦ ¦                                          ¦ DATE: 08/12/2002      ¦ 22-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 22. AUTO FLIGHT           ¦    ¦    ¦                                       ¦

¦ 1.  Autopilot Systems   C ¦ -  ¦ 1  ¦                                       ¦

¦                         B ¦ -  ¦ 0  ¦ Except for ER operations, may be      ¦ ¦                           ¦    ¦    ¦ inoperative provided:                 ¦ ¦                           ¦    ¦    ¦     a) Approach minimums do not       ¦ ¦                           ¦    ¦    ¦        require autopilot use,         ¦ ¦                           ¦    ¦    ¦     b) Enroute operations do not      ¦ ¦                           ¦    ¦    ¦        require autopilot use, and     ¦ ¦                           ¦    ¦    ¦     c) Number of flight segments      ¦ ¦                           ¦    ¦    ¦        and segment duration is        ¦ ¦                           ¦    ¦    ¦        acceptable to the flight       ¦ ¦                           ¦    ¦    ¦        crew.                          ¦

¦                           ¦    ¦    ¦ NOTE 1: Operators should make every   ¦ ¦                           ¦    ¦    ¦         effort to repair the          ¦ ¦                           ¦    ¦    ¦         autopilot early in the        ¦ ¦                           ¦    ¦    ¦         repair interval, as           ¦ ¦                           ¦    ¦    ¦         provided by this relief       ¦ ¦                           ¦    ¦    ¦         statement, in consideration   ¦ ¦                           ¦    ¦    ¦         of such factors as weather,   ¦ ¦                           ¦    ¦    ¦         traffic density and the       ¦ ¦                           ¦    ¦    ¦         effects of other              ¦ ¦                           ¦    ¦    ¦         inoperative systems.          ¦

¦                           ¦    ¦    ¦ NOTE 2: Any mode which functions      ¦ ¦                           ¦    ¦    ¦         normally may be used.         ¦

¦ 2.  AUTOPILOT           C ¦ -  ¦ 1  ¦                                       ¦ ¦     DISENGAGE Lights      ¦    ¦    ¦                                       ¦

¦                         B ¦ -  ¦ 0  ¦ May be inoperative provided           ¦ ¦                           ¦    ¦    ¦ autopilot is not used.                ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 10       ¦ PAGE:    ¦ ¦                  DA-20                   ¦                       ¦          ¦ ¦                                          ¦ DATE: 08/12/2002      ¦ 22-2     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 22  AUTO FLIGHT           ¦    ¦    ¦                                       ¦

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

¦                         C ¦ 2  ¦ 0  ¦ May be inoperative provided           ¦ ¦                           ¦    ¦    ¦ autopilot is not used below           ¦ ¦                           ¦    ¦    ¦ 10,000 feet AGL.                      ¦

¦ 4.  Yaw Damper          C ¦ 1  ¦ 0  ¦                                       ¦

¦ 5.  Autopilot Computer    ¦    ¦    ¦                                       ¦ ¦     (Pro Line 4, STC      ¦    ¦    ¦                                       ¦ ¦     ST00600WI-D)          ¦    ¦    ¦                                       ¦

¦     1) AP Function      B ¦ 1  ¦ 0  ¦ Except for ER operations, may be      ¦ ¦                           ¦    ¦    ¦ inoperative provided:                 ¦ ¦                           ¦    ¦    ¦     a) Approach minimums do not       ¦ ¦                           ¦    ¦    ¦        require autopilot use,         ¦ ¦                           ¦    ¦    ¦     b) Enroute operations do not      ¦ ¦                           ¦    ¦    ¦        require autopilot use, and     ¦ ¦                           ¦    ¦    ¦     c) Number of flight segments      ¦ ¦                           ¦    ¦    ¦        and segment duration is        ¦ ¦                           ¦    ¦    ¦        acceptable to the flight       ¦ ¦                           ¦    ¦    ¦        crew.                          ¦

¦                           ¦    ¦    ¦ NOTE 1: Operators should make every   ¦ ¦                           ¦    ¦    ¦         effort to repair the          ¦ ¦                           ¦    ¦    ¦         autopilot early in the        ¦ ¦                           ¦    ¦    ¦         repair interval, as           ¦ ¦                           ¦    ¦    ¦         provided by this relief       ¦ ¦                           ¦    ¦    ¦         statement, in consideration   ¦ ¦                           ¦    ¦    ¦         of such factors as weather,   ¦ ¦                           ¦    ¦    ¦         traffic density and the       ¦ ¦                           ¦    ¦    ¦         effects of other              ¦ ¦                           ¦    ¦    ¦         inoperative systems.          ¦

¦                           ¦    ¦    ¦ NOTE 2: Any mode which functions      ¦ ¦                           ¦    ¦    ¦         normally may be used.         ¦

¦                           ¦    ¦    ¦ (Continued)                           ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 10       ¦ PAGE:    ¦ ¦                  DA-20                   ¦                       ¦          ¦ ¦                                          ¦ DATE: 08/12/2002      ¦ 22-3     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 22  AUTO FLIGHT           ¦    ¦    ¦                                       ¦

¦ 5.  Autopilot Computer    ¦    ¦    ¦                                       ¦ ¦     (Pro Line 4, STC      ¦    ¦    ¦                                       ¦ ¦     ST00600WI-D)          ¦    ¦    ¦                                       ¦ ¦     (Cont'd)              ¦    ¦    ¦                                       ¦

¦     2) FD Function      C ¦ 2  ¦ 0  ¦ May be inoperative provided           ¦ ¦                           ¦    ¦    ¦ approach minimums do not require      ¦ ¦                           ¦    ¦    ¦ their use.                            ¦

¦     3) AP Warning       C ¦ 1  ¦ 0  ¦ May be inoperative provided           ¦ ¦        Light              ¦    ¦    ¦ annunciation on EFIS and aural        ¦ ¦                           ¦    ¦    ¦ warning operate normally.             ¦

¦ 6.  Autopilot           C ¦ 3  ¦ 2  ¦                                       ¦ ¦     Interlock Switches    ¦    ¦    ¦                                       ¦ ¦     (Pro Line 4, STC      ¦    ¦    ¦                                       ¦ ¦     ST00600WI-D)          ¦    ¦    ¦                                       ¦ ¦                         C ¦ 3  ¦ 1  ¦ Two may be inoperative provided       ¦ ¦                           ¦    ¦    ¦ autopilot is not utlized at less      ¦ ¦                           ¦    ¦    ¦ than initial approach altitude.       ¦

¦                         C ¦ 3  ¦ 0  ¦ May be inoperative provided           ¦ ¦                           ¦    ¦    ¦ autopilot is not used below           ¦ ¦                           ¦    ¦    ¦ 10,000 feet AGL.                      ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 10       ¦ PAGE:    ¦ ¦                  DA-20                   ¦                       ¦          ¦ ¦                                          ¦ DATE: 08/12/2002      ¦ 22-4     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 22  AUTO FLIGHT           ¦    ¦    ¦                                       ¦

¦ 7.  Go-Around Buttons   C ¦ 2  ¦ 1  ¦ (O)Copilot's button may be            ¦ ¦     (Pro Line 4, STC      ¦    ¦    ¦ inoperative.                          ¦ ¦     ST00600WI-D)          ¦    ¦    ¦                                       ¦ ¦                         C ¦ 2  ¦ 0  ¦ May be inoperative provided           ¦ ¦                           ¦    ¦    ¦ autopilot or flight director is       ¦ ¦                           ¦    ¦    ¦ not utilized at less than initial     ¦ ¦                           ¦    ¦    ¦ approach altitude.                    ¦

¦ 8.  Flight Control      B ¦ 1  ¦ 0  ¦ (O)Except where enroute operations    ¦ ¦     Panel (FCP)           ¦    ¦    ¦ require the use of ALT AP function    ¦ ¦     (Pro Line 4, STC      ¦    ¦    ¦ may be inoperative provided:          ¦ ¦     ST00600WI-D)          ¦    ¦    ¦     a) ASEL and course functions      ¦ ¦                           ¦    ¦    ¦        are verified to operate        ¦ ¦                           ¦    ¦    ¦        normally before takeoff, and   ¦ ¦                           ¦    ¦    ¦     b) Autopilot and flight           ¦ ¦                           ¦    ¦    ¦        director are considered        ¦ ¦                           ¦    ¦    ¦        inoperative and not used.      ¦

¦ 9.  Pitch and Roll      B ¦ 2  ¦ 0  ¦ May be inoperative provided           ¦ ¦ *** Servomotors           ¦    ¦    ¦ autopilot is considered               ¦ ¦     (Pro Line 4, STC      ¦    ¦    ¦ inoperative and not used.             ¦ ¦     ST00600WI-D)          ¦    ¦    ¦                                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 10 a     ¦ PAGE:    ¦ ¦                  DA-20                   ¦                       ¦          ¦ ¦                                          ¦ DATE: 06/25/2004      ¦ 23-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦

¦ 23  COMMUNICATIONS        ¦    ¦    ¦                                       ¦

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

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

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

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

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

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

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

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

¦                           ¦    ¦    ¦ (Continued)                           ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 10 a     ¦ PAGE:    ¦ ¦                  DA-20                   ¦                       ¦          ¦ ¦                                          ¦ DATE: 06/25/2004      ¦ 23-2     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 23  COMMUNICATIONS        ¦    ¦    ¦                                       ¦

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

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

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

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

¦ 2.  Communications      D ¦ -  ¦ -  ¦ Any in excess of those required by    ¦ ¦     Systems (VHF,         ¦    ¦    ¦ FAR may be inoperative provided it  | ¦ ¦     UHF)                  ¦    ¦    ¦ is not powered by the Emergency AC    ¦ ¦                           ¦    ¦    ¦ Bus, Emergency DC Bus, Battery Bus,   ¦ ¦                           ¦    ¦    ¦ Battery Direct Bus, or the DC         ¦ ¦                           ¦    ¦    ¦ Transfer Bus and not required for     ¦ ¦                           ¦    ¦    ¦ emergency procedures.                 ¦

¦     1) VHF Comm           ¦    ¦    ¦                                       ¦ ¦        Control Panels     ¦    ¦    ¦                                     | ¦

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

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

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

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

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 10 a     ¦ PAGE:    ¦ ¦                  DA-20                   ¦                       ¦          ¦ ¦                                          ¦ DATE: 06/25/2004      ¦ 23-3     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 23  COMMUNICATIONS        ¦    ¦    ¦                                       ¦

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

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

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

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

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

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

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

¦                           ¦    ¦    ¦ (Continued)                           ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 10 a     ¦ PAGE:    ¦ ¦                  DA-20                   ¦                       ¦          ¦ ¦                                          ¦ DATE: 06/25/2004      ¦ 23-4     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 23  COMMUNICATIONS        ¦    ¦    ¦                                       ¦

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

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

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

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

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

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

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

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

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

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

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

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 10 a     ¦ PAGE:    ¦ ¦                  DA-20                   ¦                       ¦          ¦ ¦                                          ¦ DATE: 06/25/2004      ¦ 23-5     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 23  COMMUNICATIONS        ¦    ¦    ¦                                       ¦

¦ 6.  Telephone System    D ¦ 1  ¦ 0  ¦                                       ¦ ¦ ***                       ¦    ¦    ¦                                       ¦

¦ 7.  SELCAL              C ¦ 1  ¦ 0  ¦                                       ¦ ¦ ***                       ¦    ¦    ¦                                       ¦

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

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

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

¦ 11. Boom Microphones      ¦    ¦    ¦                                       ¦

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

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

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

¦                           ¦    ¦    ¦ (Continued)                           ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 10 a     ¦ PAGE:    ¦ ¦                  DA-20                   ¦                       ¦          ¦ ¦                                          ¦ DATE: 06/25/2004      ¦ 23-6     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 23  COMMUNICATIONS        ¦    ¦    ¦                                       ¦

¦ 11. Boom Microphones      ¦    ¦    ¦                                       ¦ ¦     (Cont'd)              ¦    ¦    ¦                                       ¦

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

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

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

¦ 12. Radio Tuning Unit   C ¦ 2  ¦ 1  ¦ (O)One may be inoperative provided    ¦ ¦     (RTU)(Pro Line 4,     ¦    ¦    ¦ radio tuning function of the FMS      ¦ ¦     STC ST00600WI-D)      ¦    ¦    ¦ operates normally.                    ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 10 a     ¦ PAGE:    ¦ ¦                  DA-20                   ¦                       ¦          ¦ ¦                                          ¦ DATE: 06/25/2004      ¦ 23-7     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 23  COMMUNICATIONS        ¦    ¦    ¦                                       ¦

¦ 13. Headsets            C ¦ -  ¦ 0  ¦ May be inoperative provided:          ¦ ¦                           ¦    ¦    ¦     a) Procedures do not require      ¦ ¦                           ¦    ¦    ¦        their use, and                 ¦ ¦                           ¦    ¦    ¦     b) Flight Deck Speakers           ¦ ¦                           ¦    ¦    ¦        operate normally.              ¦

¦ 14. Satellite           C ¦ -  ¦ 0  ¦ (O)May be inoperative provided        ¦ ¦ *** Communication         ¦    ¦    ¦ alternate procedures are              ¦ ¦     System (SATCOM)       ¦    ¦    ¦ established and used.                 ¦

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

¦ 15. Aiborne Flight      C ¦ -  ¦ 0  ¦ (O)May be inoperative provided        ¦ ¦ *** Information System    ¦    ¦    ¦ alternate procedures are              ¦ ¦     (AFIS) (VHF and       ¦    ¦    ¦ established and used.                 ¦ ¦     Satellite)            ¦    ¦    ¦                                       ¦ ¦                         D ¦ -  ¦ 0  ¦ May be inoperative provided           ¦ ¦                           ¦    ¦    ¦ procedures do not require its use.    ¦

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

¦ 17. High Frequency      C ¦ -  ¦ 1  ¦ (O)May be inoperative while         | ¦ ¦     (HF) Communication    ¦    ¦    ¦ conducting operations that require  | ¦ ¦     System                ¦    ¦    ¦ two LRCS provided:                  | ¦ ¦                           ¦    ¦    ¦     a) SATCOM (High or Low Gain)    | ¦ ¦                           ¦    ¦    ¦        Data Link system operates    | ¦ ¦                           ¦    ¦    ¦        normally, and                | ¦ ¦                           ¦    ¦    ¦     b) SATCOM Data Link             | ¦ ¦                           ¦    ¦    ¦        communication operates       | ¦ ¦                           ¦    ¦    ¦        normally over the intended   | ¦ ¦                           ¦    ¦    ¦        route of flight.             | ¦

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

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 9        ¦ PAGE:    ¦ ¦                  DA-20                   ¦                       ¦          ¦ ¦                                          ¦ DATE: 10/12/1993      ¦ 24-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦

¦ 24  ELECTRICAL POWER      ¦    ¦    ¦                                       ¦

¦ 1.  Inverters           B ¦ 3  ¦ 2  ¦ (O)One may be inoperative provided    ¦ ¦                           ¦    ¦    ¦ the remaining two operate normally.   ¦

¦ 2.  DC Voltmeter        C ¦ 1  ¦ 0  ¦ May be inoperative provided all       ¦ ¦                           ¦    ¦    ¦ other generator system components     ¦ ¦                           ¦    ¦    ¦ operate normally.                     ¦

¦ 3.  Batteries           C ¦ 2  ¦ 1  ¦ (M)(O)One may be inoperative          ¦ ¦                           ¦    ¦    ¦ provided:                             ¦ ¦                           ¦    ¦    ¦     a) Both generators operate        ¦ ¦                           ¦    ¦    ¦        normally,                      ¦ ¦                           ¦    ¦    ¦     b) Inoperative battery is         ¦ ¦                           ¦    ¦    ¦        disconnected in accordance     ¦ ¦                           ¦    ¦    ¦        with an acceptable             ¦ ¦                           ¦    ¦    ¦        maintenance procedure, and     ¦ ¦                           ¦    ¦    ¦     c) A ground power unit is used    ¦ ¦                           ¦    ¦    ¦        for engine start.              ¦

¦ 4.  Battery Tempera-    C ¦ -  ¦ 0  ¦ May be inoperative provided battery   ¦ ¦     ture Indicator        ¦    ¦    ¦ temperature warning light operates    ¦ ¦     System                ¦    ¦    ¦ normally.                             ¦

¦ 5.  Generator Warning   C ¦ 2  ¦ 1  ¦ (O)One may be inoperative provided    ¦ ¦     Lights                ¦    ¦    ¦ the D.C. voltmeter operates           ¦ ¦                           ¦    ¦    ¦ normally.                             ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 10 a     ¦ PAGE:    ¦ ¦                  DA-20                   ¦                       ¦          ¦ ¦                                          ¦ DATE: 06/25/2004      ¦ 25-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦

¦ 25  EQUIPMENT/FURNISHINGS ¦    ¦    ¦                                       ¦

¦ 1.  Crewmember            ¦    ¦    ¦ Deleted, Rev. 8.                      ¦ ¦     Shoulder Harness      ¦    ¦    ¦                                       ¦

¦ 2.  Emergency Locator     ¦    ¦    ¦ Deleted, Rev. 10a.  Relief          | ¦ ¦     Transmitter (ELT)     ¦    ¦    ¦ incorporated into Item 23-16.       | ¦

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

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

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

¦                           ¦    ¦    ¦ NOTE 3: Affected seat(s) may          ¦ ¦                           ¦    ¦    ¦         include the seat(s) behind    ¦ ¦                           ¦    ¦    ¦         and/or adjacent outboard      ¦ ¦                           ¦    ¦    ¦         seats.                        ¦

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

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 9 a      ¦ PAGE:    ¦ ¦                  DA-20                   ¦                       ¦          ¦ ¦                                          ¦ DATE: 07/07/1998      ¦ 25-2     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 25  EQUIPMENT/FURNISHINGS ¦    ¦    ¦                                       ¦

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

¦ 5.  Drag Chute          C ¦ 1  ¦ 0  ¦ (M)May be inoperative or removed      ¦ ¦                           ¦    ¦    ¦ provided weight and balance are       ¦ ¦                           ¦    ¦    ¦ verified in accordance with an        ¦ ¦                           ¦    ¦    ¦ acceptable procedure.                 ¦

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

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

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

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

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 9 a      ¦ PAGE:    ¦ ¦                  DA-20                   ¦                       ¦          ¦ ¦                                          ¦ DATE: 07/07/1998      ¦ 26-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦

¦ 26  FIRE PROTECTION       ¦    ¦    ¦                                       ¦

¦ 1.  Fire Extinguisher   C ¦ 2  ¦ 0  ¦ (M)May be missing provided pressure   ¦ ¦     Thermal Discharge     ¦    ¦    ¦ indicators are checked once each      ¦ ¦     Discs                 ¦    ¦    ¦ flight day to verify adequate         ¦ ¦                           ¦    ¦    ¦ charge.                               ¦

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

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

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

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 10 a     ¦ PAGE:    ¦ ¦                  DA-20                   ¦                       ¦          ¦ ¦                                          ¦ DATE: 06/25/2004      ¦ 27-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦

¦ 27  FLIGHT CONTROLS       ¦    ¦    ¦                                       ¦

¦ 1.  Arthur Q Units      C ¦ 2  ¦ 0  ¦ (M)(O)May be inoperative provided:    ¦ ¦     (Aileron and          ¦    ¦    ¦     a) Arthur Q units are in the      ¦ ¦     Elevator)             ¦    ¦    ¦        low speed position, and        ¦ ¦                           ¦    ¦    ¦     b) Airspeed remains at or below   ¦ ¦                           ¦    ¦    ¦        250 KIAS - .8 Mach.            ¦

¦     a) Retrofit         C ¦ 2  ¦ 0  ¦ (M)(O)May be inoperative provided:  | ¦ ¦        (F20-5)            ¦    ¦    ¦     a) Arthur Q units are in the    | ¦ ¦                           ¦    ¦    ¦        low speed position, and      | ¦ ¦                           ¦    ¦    ¦     b) Airspeed remains at or below | ¦ ¦                           ¦    ¦    ¦        260 KIAS - .76 Mach.         | ¦

¦ 2.  Arthur Q Unit       C ¦ 2  ¦ 0  ¦ (M)(O)May be inoperative provided:    ¦ ¦     Warning Light         ¦    ¦    ¦     a) Associated Arthur Q unit(s)    ¦ ¦     Systems               ¦    ¦    ¦        are in the low speed           ¦ ¦                           ¦    ¦    ¦        position, and                  ¦ ¦                           ¦    ¦    ¦     b) Airspeed remains at or         ¦ ¦                           ¦    ¦    ¦        below 250 KIAS - .8 Mach.      ¦

¦     a) Retrofit         C ¦ 2  ¦ 0  ¦ (M)(O)May be inoperative provided:  | ¦ ¦        (F20-5)            ¦    ¦    ¦     a) Associated Arthur Q unit(s)  | ¦ ¦                           ¦    ¦    ¦        are in the low speed         | ¦ ¦                           ¦    ¦    ¦        position, and                | ¦ ¦                           ¦    ¦    ¦     b) Airspeed remains at or       | ¦ ¦                           ¦    ¦    ¦        below 260 KIAS - .76 Mach.   | ¦

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

¦ 4.  Trailing Edge       C ¦ 1  ¦ 0  ¦ May be inoperative provided flap      ¦ ¦     Flap Indicator        ¦    ¦    ¦ position indicator operates           ¦ ¦     Light                 ¦    ¦    ¦ normally.                             ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 9        ¦ PAGE:    ¦ ¦                  DA-20                   ¦                       ¦          ¦ ¦                                          ¦ DATE: 10/12/1993      ¦ 27-2     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦

¦ 27  FLIGHT CONTROLS       ¦    ¦    ¦                                       ¦

¦ 5.  Leading Edge        C ¦ 1  ¦ 0  ¦ (O)May be inoperative provided:       ¦ ¦     Device Indicator      ¦    ¦    ¦     a) Position of leading edge       ¦ ¦     Light                 ¦    ¦    ¦        devices is visually checked    ¦ ¦                           ¦    ¦    ¦        before each departure and      ¦ ¦                           ¦    ¦    ¦        after each commanded move-     ¦ ¦                           ¦    ¦    ¦        ment of the leading edge       ¦ ¦                           ¦    ¦    ¦        devices in flight,             ¦ ¦                           ¦    ¦    ¦     b) All other flap position        ¦ ¦                           ¦    ¦    ¦        indicators and lights          ¦ ¦                           ¦    ¦    ¦        operate normally, and          ¦ ¦                           ¦    ¦    ¦     c) For night flight, wing ice     ¦ ¦                           ¦    ¦    ¦        detection lights operate       ¦ ¦                           ¦    ¦    ¦        normally.                      ¦

¦ 6.  Stall Warning       C ¦ 1  ¦ 0  ¦ (M)(O)May be inoperative provided     ¦ ¦     Horn Test System      ¦    ¦    ¦ the stall warning system is           ¦ ¦                           ¦    ¦    ¦ verified to operate normally before   ¦ ¦                           ¦    ¦    ¦ each departure.                       ¦

¦ 7.  Flap Bypass         C ¦ 1  ¦ 0  ¦ (O)May be inoperative provided:       ¦ ¦     System                ¦    ¦    ¦     a) AMD SB 537 is installed,       ¦ ¦                           ¦    ¦    ¦     b) Manual flap system operates    ¦ ¦                           ¦    ¦    ¦        normally, and                  ¦ ¦                           ¦    ¦    ¦     c) Standby pump operates          ¦ ¦                           ¦    ¦    ¦        normally.                      ¦

¦ 8.  Horizontal          C ¦ 1  ¦ 0  ¦ (O)May be inoperative provided:       ¦ ¦     Stabilizer Trim       ¦    ¦    ¦     a) Takeoff trim system is         ¦ ¦     Indicator             ¦    ¦    ¦        visually checked using the     ¦ ¦                           ¦    ¦    ¦        reference marks on the         ¦ ¦                           ¦    ¦    ¦        vertical stabilizer before     ¦ ¦                           ¦    ¦    ¦        each departure, and            ¦ ¦                           ¦    ¦    ¦     b) Audio trim in motion warning   ¦ ¦                           ¦    ¦    ¦        system is installed and        ¦ ¦                           ¦    ¦    ¦        operates normally.             ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 9        ¦ PAGE:    ¦ ¦                  DA-20                   ¦                       ¦          ¦ ¦                                          ¦ DATE: 10/12/1993      ¦ 27-3     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦

¦ 27. FLIGHT CONTROLS       ¦    ¦    ¦                                       ¦

¦ 9.  Horizontal Stabi-   C ¦ 1  ¦ 0  ¦ (O)May be inoperative provided:       ¦ ¦     lizer Trim Takeoff    ¦    ¦    ¦     a) Stabilizer trim is checked     ¦ ¦     Warning Light         ¦    ¦    ¦        to be in proper position       ¦ ¦                           ¦    ¦    ¦        before each departure, and     ¦ ¦                           ¦    ¦    ¦     b) Horizontal stabilizer trim     ¦ ¦                           ¦    ¦    ¦        position indicator operates    ¦ ¦                           ¦    ¦    ¦        normally.                      ¦

¦ 10. Horizontal          C ¦ 1  ¦ 0  ¦ (O)May be inoperative provided:       ¦ ¦     Stabilizer Trim       ¦    ¦    ¦     a) Horizontal stabilizer trim     ¦ ¦     Operating Aural       ¦    ¦    ¦        position indicator operates    ¦ ¦     Alert (Clacker)       ¦    ¦    ¦        normally,                      ¦ ¦                           ¦    ¦    ¦     b) Trim is monitored during       ¦ ¦                           ¦    ¦    ¦        takeoff, and                   ¦ ¦                           ¦    ¦    ¦     c) Autopilot is not used.         ¦

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

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

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

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 9 b      ¦ PAGE:    ¦ ¦                  DA-20                   ¦                       ¦          ¦ ¦                                          ¦ DATE: 02/22/1999      ¦ 28-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 28  FUEL                  ¦    ¦    ¦                                       ¦

¦ 1.  Booster Pumps       C ¦ 2  ¦ 1  ¦ (M)(O)One may be inoperative          ¦ ¦                           ¦    ¦    ¦ provided:                             ¦ ¦                           ¦    ¦    ¦     a) Both transfer pumps operate    ¦ ¦                           ¦    ¦    ¦        normally,                      ¦ ¦                           ¦    ¦    ¦     b) Feeder tank pressurization     ¦ ¦                           ¦    ¦    ¦        is normal and is checked       ¦ ¦                           ¦    ¦    ¦        before each departure,         ¦ ¦                           ¦    ¦    ¦     c) Crossfeed valve operates       ¦ ¦                           ¦    ¦    ¦        normally, and                  ¦ ¦                           ¦    ¦    ¦     d) AFM provisions for engine      ¦ ¦                           ¦    ¦    ¦        operation without assistance   ¦ ¦                           ¦    ¦    ¦        of any booster pump are        ¦ ¦                           ¦    ¦    ¦        observed.                      ¦

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

¦ 3.  Low Fuel Pressure   C ¦ 2  ¦ 0  ¦ (O)May be inoperative provided the    ¦ ¦     Warning Lights        ¦    ¦    ¦ associated fuel pressure indicators   ¦ ¦     (CF 700 Engines       ¦    ¦    ¦ operate normally.                     ¦ ¦     Only)                 ¦    ¦    ¦                                       ¦

¦ 4.  Fuel Pressure       C ¦ 2  ¦ 0  ¦ (O)May be inoperative provided        ¦ ¦     Indicators            ¦    ¦    ¦ the associated fuel low pressure      ¦ ¦     (CF 700 Engines)      ¦    ¦    ¦ warning light(s) operates normally.   ¦

¦ 5.  Wing Interconnect   C ¦ 1  ¦ 0  ¦ (M)(O)May be inoperative provided:    ¦ ¦     System                ¦    ¦    ¦     a) All other fuel system          ¦ ¦                           ¦    ¦    ¦        components operate normally,   ¦ ¦                           ¦    ¦    ¦        and                            ¦ ¦                           ¦    ¦    ¦     b) Wing interconnect valve is     ¦ ¦                           ¦    ¦    ¦        secured closed.                ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 9        ¦ PAGE:    ¦ ¦                  DA-20                   ¦                       ¦          ¦ ¦                                          ¦ DATE: 10/12/1993      ¦ 28-2     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦

¦ 28  FUEL                  ¦    ¦    ¦                                       ¦

¦ 6.  Wing Tank Fuel      C ¦ 1  ¦ 0  ¦ (M)One tank indication may be         ¦ ¦     Quantity Indicators   ¦    ¦    ¦ inoperative provided:                 ¦ ¦                           ¦    ¦    ¦     a) Alternate procedures are       ¦ ¦                           ¦    ¦    ¦        established and used to        ¦ ¦                           ¦    ¦    ¦        ensure fuel is adequate for    ¦ ¦                           ¦    ¦    ¦        operations being conducted,    ¦ ¦                           ¦    ¦    ¦        and                            ¦ ¦                           ¦    ¦    ¦     b) Both Fuel Flow/Fuel Used       ¦ ¦                           ¦    ¦    ¦        indicators operate normally.   ¦

¦ 7.  Wing Fuel Tank      C ¦ 2  ¦ 0  ¦ (M)May be inoperative provided they   ¦ ¦     Dip Sticks            ¦    ¦    ¦ are verified in the locked CLOSED     ¦ ¦                           ¦    ¦    ¦ position.                             ¦

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

¦ 9.  Fuel Temperature    C ¦ 1  ¦ 0  ¦ (O)May be inoperative provided:       ¦ ¦ *** Indicator             ¦    ¦    ¦     a) Boost pumps, transfer          ¦ ¦                           ¦    ¦    ¦        systems and engine crossfeed   ¦ ¦                           ¦    ¦    ¦        operate normally, and          ¦ ¦                           ¦    ¦    ¦     b) Operations are not conducted   ¦ ¦                           ¦    ¦    ¦        at an RAT below the fuel       ¦ ¦                           ¦    ¦    ¦        freeze point.                  ¦

¦ 10. Fuel Used System    C ¦ 1  ¦ 0  ¦ May be inoperative provided all       ¦ ¦                           ¦    ¦    ¦ fuel quantity systems operate         ¦ ¦                           ¦    ¦    ¦ normally.                             ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 9        ¦ PAGE:    ¦ ¦                  DA-20                   ¦                       ¦          ¦ ¦                                          ¦ DATE: 10/12/1993      ¦ 29-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦

¦ 29  HYDRAULIC POWER       ¦    ¦    ¦                                       ¦

¦ 1.  Hydraulic Quantity  C ¦ 2  ¦ 0  ¦ (M)(O)Hydraulic quantity indica-      ¦ ¦     Indicators (Dual      ¦    ¦    ¦ tions may be inoperative provided:    ¦ ¦     Indicating)           ¦    ¦    ¦     a) Hydraulic quantity in the      ¦ ¦                           ¦    ¦    ¦        associated reservoir(s) is     ¦ ¦                           ¦    ¦    ¦        verified adequate using an     ¦ ¦                           ¦    ¦    ¦        acceptable procedure before    ¦ ¦                           ¦    ¦    ¦        each departure, and            ¦ ¦                           ¦    ¦    ¦     b) All other hydraulic system     ¦ ¦                           ¦    ¦    ¦        indicators and warning         ¦ ¦                           ¦    ¦    ¦        lights operate normally.       ¦

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

¦ 3.  Standby Pump        C ¦ 2  ¦ 0  ¦ (O)May be inoperative provided all    ¦ ¦     Warning Lights        ¦    ¦    ¦ other hydraulic system pressure       ¦ ¦     (Arrows)              ¦    ¦    ¦ indications and warning lights        ¦ ¦                           ¦    ¦    ¦ operate normally.                     ¦

¦ 4.  System Pressure     C ¦ 2  ¦ 0  ¦ (O)May be inoperative provided all    ¦ ¦     Warning Lights        ¦    ¦    ¦ other hydraulic system pressure       ¦ ¦     (Flight Control       ¦    ¦    ¦ indications and warning lights        ¦ ¦     Circuit Red Light     ¦    ¦    ¦ operate normally.                     ¦ ¦     1 and 2)              ¦    ¦    ¦                                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 9        ¦ PAGE:    ¦ ¦                  DA-20                   ¦                       ¦          ¦ ¦                                          ¦ DATE: 10/12/1993      ¦ 29-2     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 29  HYDRAULIC POWER       ¦    ¦    ¦                                       ¦

¦ 5.  Hydraulic Pressure    ¦    ¦    ¦                                       ¦ ¦     Indicators (Triple    ¦    ¦    ¦                                       ¦ ¦     Indicating)           ¦    ¦    ¦                                       ¦

¦     1) Main Pressure    C ¦ 2  ¦ 0  ¦ Main system pressure functions may    ¦ ¦        Systems            ¦    ¦    ¦ be inoperative provided the asso-     ¦ ¦                           ¦    ¦    ¦ ciated main system warning light(s)   ¦ ¦                           ¦    ¦    ¦ operate normally.                     ¦

¦     2) Standby Pres-    C ¦ 1  ¦ 0  ¦ May be inoperative provided all       ¦ ¦        sure System        ¦    ¦    ¦ other main and standby system         ¦ ¦                           ¦    ¦    ¦ warning lights and pressure gauge     ¦ ¦                           ¦    ¦    ¦ indications operate normally.         ¦

¦ 6.  Hydraulic           B ¦ 1  ¦ 0  ¦ (M)(O)May be inoperative provided:    ¦ ¦     Reservoir             ¦    ¦    ¦     a) Reservoir pressurization is    ¦ ¦     Pressurization        ¦    ¦    ¦        determined to operate          ¦ ¦     Warning Light         ¦    ¦    ¦        normally using an acceptable   ¦ ¦                           ¦    ¦    ¦        procedure before each          ¦ ¦                           ¦    ¦    ¦        departure.                     ¦ ¦                           ¦    ¦    ¦           OR                          ¦ ¦                         B ¦    ¦    ¦     b) Flight is operated at or       ¦ ¦                           ¦    ¦    ¦        below 12,000 feet MSL.         ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 9        ¦ PAGE:    ¦ ¦                  DA-20                   ¦                       ¦          ¦ ¦                                          ¦ DATE: 10/12/1993      ¦ 30-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦

¦ 30  ICE AND RAIN          ¦    ¦    ¦                                       ¦ ¦     PROTECTION            ¦    ¦    ¦                                       ¦

¦ 1.  Airframe Anti-      C ¦ 1  ¦ 0  ¦ (O)May be inoperative CLOSED          ¦ ¦     Icing System          ¦    ¦    ¦ provided the airplane is not          ¦ ¦                           ¦    ¦    ¦ operated in known or forecast         ¦ ¦                           ¦    ¦    ¦ icing conditions.                     ¦

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

¦ 3.  Pitot Heater        B ¦ 2  ¦ 1  ¦ (O)One may be inoperative provided    ¦ ¦     Systems               ¦    ¦    ¦ flight is conducted in day VMC        ¦ ¦                           ¦    ¦    ¦ flight conditions only.               ¦

¦ 4.  Pitot Heater        B ¦ 2  ¦ 1  ¦ (O)One may be inoperative provided:   ¦ ¦     Light Systems         ¦    ¦    ¦     a) Remaining elements of the      ¦ ¦                           ¦    ¦    ¦        pitot heat system are veri-    ¦ ¦                           ¦    ¦    ¦        fied to operate normally,      ¦ ¦                           ¦    ¦    ¦        and                            ¦ ¦                           ¦    ¦    ¦     b) Airplane is not operated       ¦ ¦                           ¦    ¦    ¦        in known or forecast icing     ¦ ¦                           ¦    ¦    ¦        conditions.                    ¦

¦ 5.  Static Heater       C ¦ 2  ¦ 1  ¦ (O)One may be inoperative provided:   ¦ ¦     Systems               ¦    ¦    ¦     a) Airplane is not operated       ¦ ¦                           ¦    ¦    ¦        in known or forecast icing     ¦ ¦                           ¦    ¦    ¦        conditions, and                ¦ ¦                           ¦    ¦    ¦     b) Taxiway or runway is not       ¦ ¦                           ¦    ¦    ¦        covered with standing          ¦ ¦                           ¦    ¦    ¦        water or slush.                ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 9        ¦ PAGE:    ¦ ¦                  DA-20                   ¦                       ¦          ¦ ¦                                          ¦ DATE: 10/12/1993      ¦ 30-2     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦

¦ 30  ICE AND RAIN          ¦    ¦    ¦                                       ¦ ¦     PROTECTION            ¦    ¦    ¦                                       ¦

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

¦ 7.  Side Window         C ¦ 1  ¦ 0  ¦                                       ¦ ¦     Heating System        ¦    ¦    ¦                                       ¦

¦ 8.  Windshield Wipers   C ¦ 2  ¦ 0  ¦ (O)May be inoperative provided the    ¦ ¦                           ¦    ¦    ¦ airplane is not flown in precipita-   ¦ ¦                           ¦    ¦    ¦ tion within 5 nautical miles of the   ¦ ¦                           ¦    ¦    ¦ airport of takeoff or intended        ¦ ¦                           ¦    ¦    ¦ landing.                              ¦

¦ 9.  Rain Repellent      C ¦ 2  ¦ 0  ¦                                       ¦ ¦     Systems               ¦    ¦    ¦                                       ¦

¦ 10. Defog System        C ¦ 1  ¦ 0  ¦ May be inoperative provided           ¦ ¦                           ¦    ¦    ¦ windshield heating systems operate    ¦ ¦                           ¦    ¦    ¦ normally.                             ¦

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

¦ 12. Stall Warning       C ¦ 1  ¦ 0  ¦ (O)May be inoperative provided the    ¦ ¦     Sensor Heating        ¦    ¦    ¦ airplane is not operated in known     ¦ ¦     System                ¦    ¦    ¦ or forecast icing conditions.         ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 10       ¦ PAGE:    ¦ ¦                  DA-20                   ¦                       ¦          ¦ ¦                                          ¦ DATE: 08/12/2002      ¦ 31-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 31  INDICATING/RECORDING  ¦    ¦    ¦                                       ¦ ¦     SYSTEMS               ¦    ¦    ¦                                       ¦

¦ 1.  Clocks              C ¦ -  ¦ 1  ¦ One may be inoperative at either      ¦ ¦                           ¦    ¦    ¦ the pilot's or copilot's station.     ¦

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

¦                           ¦    ¦    ¦ (Continued)                           ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 10       ¦ PAGE:    ¦ ¦                  DA-20                   ¦                       ¦          ¦ ¦                                          ¦ DATE: 08/12/2002      ¦ 31-2     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 31  INDICATING/RECORDING  ¦    ¦    ¦                                       ¦ ¦     SYSTEMS               ¦    ¦    ¦                                       ¦

¦ 2.  Flight Data           ¦    ¦    ¦                                       ¦ ¦     Recorder (FDR)        ¦    ¦    ¦                                       ¦ ¦     System                ¦    ¦    ¦                                       ¦ ¦     (Cont'd)              ¦    ¦    ¦                                       ¦

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

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

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

¦ 4.  SAT/TAT/TAS         C ¦ 1  ¦ 0  ¦ (O)May be inoperative provided RAT    ¦ ¦     Indicator             ¦    ¦    ¦ indicator operates normally.          ¦

¦ 5.  RAT Indicator       C ¦ 1  ¦ 0  ¦ (O)May be inoperative provided air    ¦ ¦                           ¦    ¦    ¦ data computer and associated SAT/     ¦ ¦                           ¦    ¦    ¦ TAT indicator system are installed    ¦ ¦                           ¦    ¦    ¦ and operate normally.                 ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 10 a     ¦ PAGE:    ¦ ¦                  DA-20                   ¦                       ¦          ¦ ¦                                          ¦ DATE: 06/25/2004      ¦ 32-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦

¦ 32  LANDING GEAR          ¦    ¦    ¦                                       ¦

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

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

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

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 10 a     ¦ PAGE:    ¦ ¦                  DA-20                   ¦                       ¦          ¦ ¦                                          ¦ DATE: 06/25/2004      ¦ 32-2     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 32  LANDING GEAR          ¦    ¦    ¦                                       ¦

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

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

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 9 a      ¦ PAGE:    ¦ ¦                  DA-20                   ¦                       ¦          ¦ ¦                                          ¦ DATE: 07/07/1998      ¦ 33-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦

¦ 33  LIGHTS                ¦    ¦    ¦                                       ¦

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

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

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

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 9        ¦ PAGE:    ¦ ¦                  DA-20                   ¦                       ¦          ¦ ¦                                          ¦ DATE: 10/12/1993      ¦ 33-2     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 33  LIGHTS                ¦    ¦    ¦                                       ¦

¦ 4.  Landing Lights      C ¦ 2  ¦ 1  ¦ One may be inoperative for night      ¦ ¦     (Wing Root or         ¦    ¦    ¦ operations provided taxi light        ¦ ¦      Retractable)         ¦    ¦    ¦ operates normally.                    ¦

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

¦ 5.  Landing Light       C ¦ 2  ¦ 1  ¦ (O)One may be inoperative in the      ¦ ¦     Retraction Systems    ¦    ¦    ¦ retracted position for night          ¦ ¦                           ¦    ¦    ¦ operations provided taxi light        ¦ ¦                           ¦    ¦    ¦ operates normally.                    ¦

¦                         C ¦ 2  ¦ 0  ¦ (O)May be inoperative in the          ¦ ¦                           ¦    ¦    ¦ extended position provided AFM        ¦ ¦                           ¦    ¦    ¦ speed restrictions are observed.      ¦

¦ 6.  Wing Root           C ¦ 2  ¦ 0  ¦                                       ¦ ¦     Recognition Lights    ¦    ¦    ¦                                       ¦

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

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

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 9 a      ¦ PAGE:    ¦ ¦                  DA-20                   ¦                       ¦          ¦ ¦                                          ¦ DATE: 07/07/1998      ¦ 33-3     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 33  LIGHTS                ¦    ¦    ¦                                       ¦

¦ 8.  Position Lights     C ¦ 1  ¦ 0  ¦ May be inoperative for day            ¦ ¦     System                ¦    ¦    ¦ operations.                           ¦

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

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

¦ 10. Wing Ice            C ¦ 2  ¦ 0  ¦ May be inoperative for night          ¦ ¦     Detection Lights      ¦    ¦    ¦ operations provided:                  ¦ ¦                           ¦    ¦    ¦     a) A portable light/lamp of       ¦ ¦                           ¦    ¦    ¦        adequate capacity is           ¦ ¦                           ¦    ¦    ¦        available for use in icing     ¦ ¦                           ¦    ¦    ¦        conditions.                    ¦ ¦                           ¦    ¦    ¦           OR                          ¦ ¦                         C ¦    ¦    ¦     b) Airplane is not operated in    ¦ ¦                           ¦    ¦    ¦        known or forecast icing        ¦ ¦                           ¦    ¦    ¦        conditions.                    ¦

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

¦ 11. Strobe Light        C ¦ 1  ¦ 0  ¦ May be inoperative for night          ¦ ¦     System                ¦    ¦    ¦ operations provided anti-collision    ¦ ¦                           ¦    ¦    ¦ lights operate normally.              ¦

¦ 12. Exterior Emergency  C ¦ 1  ¦ 0  ¦ May be inoperative for day            ¦ ¦     Lighting System       ¦    ¦    ¦ operations.                           ¦

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

¦ 14. Baggage Compartment C ¦ -  ¦ 0  ¦                                       ¦ ¦     Lights                ¦    ¦    ¦                                       ¦

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

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 9        ¦ PAGE:    ¦ ¦                  DA-20                   ¦                       ¦          ¦ ¦                                          ¦ DATE: 10/12/1993      ¦ 34-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦

¦ 34  NAVIGATION            ¦    ¦    ¦                                       ¦

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

¦ 2.  Angle of Attack     C ¦ -  ¦ 0  ¦ (O)May be inoperative provided        ¦ ¦     Systems               ¦    ¦    ¦ stall warning systems operate         ¦ ¦                           ¦    ¦    ¦ normally.                             ¦

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

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

¦ 4.  Stabilized Heading    ¦    ¦    ¦ Deleted, Rev. 8.                      ¦ ¦     Indication Systems    ¦    ¦    ¦                                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 9 a      ¦ PAGE:    ¦ ¦                  DA-20                   ¦                       ¦          ¦ ¦                                          ¦ DATE: 07/07/1998      ¦ 34-2     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦

¦ 34  NAVIGATION            ¦    ¦    ¦                                       ¦

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

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

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

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

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 10       ¦ PAGE:    ¦ ¦                  DA-20                   ¦                       ¦          ¦ ¦                                          ¦ DATE: 08/12/2002      ¦ 34-3     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦

¦ 34  NAVIGATION            ¦    ¦    ¦                                       ¦

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

¦ 8.  Weather Radar/      C ¦ -  ¦ -  ¦ As required by FAR.                   ¦ ¦     Lighting Detection    ¦    ¦    ¦                                       ¦ ¦     System                ¦    ¦    ¦                                       ¦

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

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

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

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

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

¦                           ¦    ¦    ¦ (Continued)                           ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 10       ¦ PAGE:    ¦ ¦                  DA-20                   ¦                       ¦          ¦ ¦                                          ¦ DATE: 08/12/2002      ¦ 34-4     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 34  NAVIGATION            ¦    ¦    ¦                                       ¦

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

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

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

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

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

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

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

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

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 10 a     ¦ PAGE:    ¦ ¦                  DA-20                   ¦                       ¦          ¦ ¦                                          ¦ DATE: 06/25/2004      ¦ 34-5     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 34  NAVIGATION            ¦    ¦    ¦                                       ¦

¦ 11. Radio Altimeter     A ¦ -  ¦ -  ¦ (M)(O)May be inoperative provided:    ¦ ¦     System                ¦    ¦    ¦     a) Dispatch deviation for GPWS    ¦ ¦                           ¦    ¦    ¦        is observed,                   ¦ ¦                           ¦    ¦    ¦     b) Approach minimums or           ¦ ¦                           ¦    ¦    ¦        operating procedures do not    ¦ ¦                           ¦    ¦    ¦        require its use, and           ¦ ¦                           ¦    ¦    ¦     c) Repairs are made within        ¦ ¦                           ¦    ¦    ¦        two flight days.               ¦

¦ 12. Instrument          C ¦ 1  ¦ 0  ¦ May be inoperative provided           ¦ ¦     Comparator            ¦    ¦    ¦ approach minimums do not require      ¦ ¦                           ¦    ¦    ¦ their use.                            ¦

¦ 13. Marker Beacon       C ¦ -  ¦ -  ¦ May be inoperative provided           ¦ ¦                           ¦    ¦    ¦ approach minimums do not require      ¦ ¦                           ¦    ¦    ¦ their use.                            ¦

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

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

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

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

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

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 10 a     ¦ PAGE:    ¦ ¦                  DA-20                   ¦                       ¦          ¦ ¦                                          ¦ DATE: 06/25/2004      ¦ 34-6     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦

¦ 34  NAVIGATION            ¦    ¦    ¦                                       ¦

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

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

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

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

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

¦ 20. Remote Magnetic     C ¦ -  ¦ -  ¦                                       ¦ ¦     Indicator (RMI)       ¦    ¦    ¦                                       ¦

¦ 21. Inertial            C ¦ -  ¦ -  ¦ As required by FAR.                   ¦ ¦     Navigation System     ¦    ¦    ¦                                       ¦ ¦     (INS)                 ¦    ¦    ¦                                       ¦

¦ 22. Flight Management   C ¦ -  ¦ -  ¦ May be inoperative provided re-       ¦ ¦     System (FMS)          ¦    ¦    ¦ quired navigation and communication   ¦ ¦                           ¦    ¦    ¦ systems are not affected.             ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 10       ¦ PAGE:    ¦ ¦                  DA-20                   ¦                       ¦          ¦ ¦                                          ¦ DATE: 08/12/2002      ¦ 34-7     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦

¦ 34  NAVIGATION            ¦    ¦    ¦                                       ¦

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

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

¦ 25. Microwave Landing   C ¦ -  ¦ -  ¦ As required by FAR.                   ¦ ¦     Systems (MLS)         ¦    ¦    ¦                                       ¦

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

¦ 27. RNAV System         C ¦ -  ¦ -  ¦ As required by FAR.                   ¦

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

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

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

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 10       ¦ PAGE:    ¦ ¦                  DA-20                   ¦                       ¦          ¦ ¦                                          ¦ DATE: 08/12/2002      ¦ 34-8     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦

¦ 34  NAVIGATION            ¦    ¦    ¦                                       ¦

¦ 31. EADI Annunciators/    ¦    ¦    ¦                                       ¦ ¦     Displays              ¦    ¦    ¦                                       ¦

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

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

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

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

¦     5) Marker           C ¦ 2  ¦ 0  ¦ As required by FAR.                   ¦ ¦        Indications        ¦    ¦    ¦                                       ¦

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

¦     7) Airspeed         C ¦ 2  ¦ 0  ¦ May be inoperative provided           ¦ ¦                           ¦    ¦    ¦ airspeed information is removed       ¦ ¦                           ¦    ¦    ¦ from display.                         ¦

¦     8) Speed Trend      C ¦ 2  ¦ 0  ¦ May be inoperative provided trend     ¦ ¦                           ¦    ¦    ¦ information is removed from           ¦ ¦                           ¦    ¦    ¦ display.                              ¦

¦     9) Mach Indication  C ¦ 2  ¦ 0  ¦ May be inoperative provided Mach      ¦ ¦                           ¦    ¦    ¦ information is removed from           ¦ ¦                           ¦    ¦    ¦ display.                              ¦

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

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

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 10       ¦ PAGE:    ¦ ¦                  DA-20                   ¦                       ¦          ¦ ¦                                          ¦ DATE: 08/12/2002      ¦ 34-9     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦

¦ 34  NAVIGATION            ¦    ¦    ¦                                       ¦

¦ 32. EHSI Annunciator/     ¦    ¦    ¦                                       ¦ ¦     Displays              ¦    ¦    ¦                                       ¦

¦     1) Selected         C ¦ 2  ¦ 0  ¦                                       ¦ ¦        Headings           ¦    ¦    ¦                                       ¦

¦     2) Selected         C ¦ 2  ¦ 0  ¦ (O)May be in operative provided       ¦ ¦        Course             ¦    ¦    ¦ navigation does not require their     ¦ ¦                           ¦    ¦    ¦ use.                                  ¦

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

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

¦     5) Groundspeed/     C ¦ 2  ¦ 0  ¦                                       ¦ ¦        Time to go         ¦    ¦    ¦                                       ¦

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

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

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

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

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 10       ¦ PAGE:    ¦ ¦                  DA-20                   ¦                       ¦          ¦ ¦                                          ¦ DATE: 08/12/2002      ¦ 34-10    ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦

¦ 34  NAVIGATION            ¦    ¦    ¦                                       ¦

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

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

¦ 35. Storm Scope         C ¦ 1  ¦ 0  ¦ As required by FAR.                   ¦

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

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

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

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

¦ 40. Compass Transfer    C ¦ 2  ¦ 0  ¦ May be inoperative provided compass   ¦ ¦                           ¦    ¦    ¦ information remains in the            ¦ ¦                           ¦    ¦    ¦ (onside) selection.                   ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 10       ¦ PAGE:    ¦ ¦                  DA-20                   ¦                       ¦          ¦ ¦                                          ¦ DATE: 08/12/2002      ¦ 34-11    ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 34  NAVIGATION            ¦    ¦    ¦                                       ¦

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

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

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

¦ 44. Airborne Flight     C ¦ 1  ¦ 0  ¦                                       ¦ ¦     Information           ¦    ¦    ¦                                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 10       ¦ PAGE:    ¦ ¦                  DA-20                   ¦                       ¦          ¦ ¦                                          ¦ DATE: 08/12/2002      ¦ 34-12    ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 34  NAVIGATION            ¦    ¦    ¦                                       ¦

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

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

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

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

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

¦                           ¦    ¦    ¦ (Continued)                           ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 10       ¦ PAGE:    ¦ ¦                  DA-20                   ¦                       ¦          ¦ ¦                                          ¦ DATE: 08/12/2002      ¦ 34-13    ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 34  NAVIGATION            ¦    ¦    ¦                                       ¦

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

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

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

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

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

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 10       ¦ PAGE:    ¦ ¦                  DA-20                   ¦                       ¦          ¦ ¦                                          ¦ DATE: 08/12/2002      ¦ 34-14    ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 34  NAVIGATION            ¦    ¦    ¦                                       ¦

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

¦                         C ¦ -  ¦ 0  ¦ (O)May be inoperative provided:       ¦ ¦                           ¦    ¦    ¦     a) Alternate procedures are       ¦ ¦                           ¦    ¦    ¦        established and used, and      ¦