DEPARTMENT OF TRANSPORTATION     Revision: 14 a

Date: 06/17/1999

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

DE HAVILLAND DHC-7

Federal Aviation Administration

Flight Standards Division

AIRCRAFT EVALUATION GROUP, ANM-270S

1601 Lind Ave. S.W.

RENTON, WASHINGTON 98055-4056

Telephone: Comm: (206) 227-2280 FTS:  (206) 227-2280 FAX:  (206)                         227-1270



FEDERAL AVIATION ADMINISTRATION     Page: I

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Table of Contents

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SYSTEM NO.  SYSTEM                                  PAGE

--     Table of Contents                       I

--     Log of Revisions                        II

--     Control Page                            III, IV

--     Highlights of Change                    V

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

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

22     Auto Flight                             22-1

23     Communications                          23-1, 2, 3, 4

24     Electrical Power                        24-1, 2, 3, 4

25     Equipment/Furnishings                   25-1, 2, 3, 4, 5 26     Fire Protection                         26-1, 2, 3, 4, 5 27     Flight Controls                         27-1, 2, 3, 4

28     Fuel                                    28-1, 2, 3

29     Hydraulic Power                         29-1

30     Ice and Rain Protection                 30-1, 2

31     Indicating/Recording Systems            31-1

32     Landing Gear                            32-1

33     Lights                                  33-1, 2, 3, 4, 5 33     Lights                                  33-6

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

35     Oxygen                                  35-1 49     Airborne Auxiliary Power                49-1 52     Doors                                   52-1 61     Propellers                              61-1 73     Engine Fuel & Control                   73-1 77     Engine Indicating                       77-1 79     Engine Oil                              79-1 82     Water Injection                         82-1



FEDERAL AVIATION ADMINISTRATION   Page: II

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MASTER MINIMUM EQUIPMENT LIST    Date: 06/17/1999

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Log of Revisions

| REV.NO.  |  DATE      | PAGE NUMBERS                   | INITIALS  |

| 9        | 04/13/1990 | ALL PAGES                      |           | | 10       | 11/05/1990 | HIGHLIGHTS OF REV.             |           | | 10       | 11/05/1990 | 21-4,23-3,24-3,25-1,25-2       |           | | 10       | 11/05/1990 | 25-3,26-5,31-1,34-3,34-4       |           | | 10       | 11/05/1990 | 34-5,34-6                      |           | | 11       | 06/05/1991 | HIGHLIGHTS OF REV.             |           | | 11       | 06/05/1991 | 23-3,31-1,34-4,34-5,34-6       |           | | 12       | 03/24/1992 | HIGHLIGHTS OF REV.             |           | | 12       | 03/24/1992 | 23-1,23-3,24-2,24-3,24-4       |           | | 12       | 03/24/1992 | 25-2,25-3,25-4,33-3,33-4       |           | | 12       | 03/24/1992 | 33-5,35-1                      |           | | 13       | 07/15/1992 | HIGHLIGHTS OF REV.             |           | Page 2

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| 13       | 07/15/1992 | 21-4,24-1,24-2,25-3,26-1       |           | | 13       | 07/15/1992 | 27-1,28-1,28-2,33-1,33-2       |           | | 13       | 07/15/1992 | 33-5,34-4,52-1,79-1            |           | | 14       | 06/16/1994 | HIGHLIGHTS OF REV.,DEFINITIONS |           | | 14       | 06/16/1994 | 21-1,21-2,21-3,21-4,22-1       |           | | 14       | 06/16/1994 | 23-1,23-2,23-3,23-4,24-1       |           | | 14       | 06/16/1994 | 24-2,24-3,24-4,25-1,25-2       |           | | 14       | 06/16/1994 | 25-3,25-4,25-5,26-1,26-2       |           | | 14       | 06/16/1994 | 26-3,26-4,26-5,27-1,27-2       |           | | 14       | 06/16/1994 | 27-3,27-4,28-1,28-2,28-3       |           | | 14       | 06/16/1994 | 29-1,30-1,30-2,31-1,32-1       |           | | 14       | 06/16/1994 | 33-1,33-2,33-3,33-4,33-5       |           | | 14       | 06/16/1994 | 33-6,34-1,34-2,34-3,34-4       |           | | 14       | 06/16/1994 | 34-5,34-6,34-7,34-8,35-1       |           | | 14       | 06/16/1994 | 49-1,52-1,61-1,73-1,77-1       |           | | 14       | 06/16/1994 | 79-1,82-1                      |           | | 14a      |            | HIGHLIGHTS OF REV.,DEFINITIONS |           | | 14a      |            | 27-1,27-2,27-3,27-4            |           | |          |            |                                |           | |          |            |                                |           | |          |            |                                |           | |          |            |                                |           | |          |            |                                |           | |          |            |                                |           | |          |            |                                |           | |          |            |                                |           | |          |            |                                |           | |          |            |                                |           | |          |            |                                |           | |          |            |                                |           | |          |            |                                |           |



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Control Page

SYSTEM                                   PAGE  REV NO.  CURRENT DATE

Cover Page                               -       14 a     06/17/1999 Table of Contents                        I       14 a     06/17/1999 Log of Revisions                         II      14 a     06/17/1999 Control Page                             III     14 a     06/17/1999 IV      14 a     06/17/1999 Highlights of Change                     V       14 a     06/17/1999 Definitions                              VI      6        01/31/1995 VII     6        01/31/1995 VIII    6        01/31/1995 IX      6        01/31/1995 X       6        01/31/1995 XI      6        01/31/1995 XII     6        01/31/1995 XIII    6        01/31/1995 Preamble                                 XIV     2        06/14/1989 Page 3

 

                                         XV      2        06/14/1989 21                                       21-1    14       06/16/1994 21-2    14       06/16/1994 21-3    14       06/16/1994 21-4    14       06/16/1994 22                                       22-1    14       06/16/1994 23                                       23-1    14       06/16/1994 23-2    14       06/16/1994 23-3    14       06/16/1994 23-4    14       06/16/1994 24                                       24-1    14       06/16/1994 24-2    14       06/16/1994 24-3    14       06/16/1994 24-4    14       06/16/1994 25                                       25-1    14       06/16/1994 25-2    14       06/16/1994 25-3    14       06/16/1994 25-4    14       06/16/1994 25-5    14       06/16/1994 26                                       26-1    14       06/16/1994 26-2    14       06/16/1994 26-3    14       06/16/1994 26-4    14       06/16/1994 26-5    14       06/16/1994 27                                       27-1    14 a     06/17/1999



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Control Page

SYSTEM                                   PAGE  REV NO.  CURRENT DATE

27-2    14 a     06/17/1999 27-3    14 a     06/17/1999 27-4    14 a     06/17/1999 28                                       28-1    14       06/16/1994 28-2    14       06/16/1994 28-3    14       06/16/1994 29                                       29-1    14       06/16/1994 30                                       30-1    14       06/16/1994 30-2    14       06/16/1994 31                                       31-1    14       06/16/1994 32                                       32-1    14       06/16/1994 33                                       33-1    14       06/16/1994 33-2    14       06/16/1994 33-3    14       06/16/1994 33-4    14       06/16/1994 33-5    14       06/16/1994 33-6    14       06/16/1994 34                                       34-1    14       06/16/1994 34-2    14       06/16/1994 34-3    14                                   06/16/1994 34-4    14       06/16/1994

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34-5    14       06/16/1994 34-6    14       06/16/1994 34-7    14       06/16/1994 34-8    14       06/16/1994 35                                       35-1    14       06/16/1994 49                                       49-1    14       06/16/1994 52                                       52-1    14       06/16/1994 61                                       61-1    14       06/16/1994 73                                       73-1    14       06/16/1994 77                                       77-1    14       06/16/1994 79                                       79-1    14       06/16/1994 82                                                                           82-1    14       06/16/1994



FEDERAL AVIATION ADMINISTRATION   Page: V

Revision: 14 a

MASTER MINIMUM EQUIPMENT LIST    Date: 06/17/1999

DHC-7

Highlights of Change

EFFECTIVE ABOVE DATE, the deHavilland DHC-7 Master Minimum Equipment List has been revised.  Please replace revised pages of previous lists with revision 14a for a complete and up-to-date MMEL.

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

27.  FLIGHT CONTROLS

Item 5. Flap Position Indicator.

Item 5 was deleted from a previous revision due to AEG policy of denying relief for an item that would require a Flightdeck crewmember to leave their seat during a critical phase of flight. The new proviso will provide for another crewmember to verify the flap position.

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FEDERAL AVIATION ADMINISTRATION     Page: VI

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MASTER MINIMUM EQUIPMENT LIST      Date: 01/31/1995

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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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MASTER MINIMUM EQUIPMENT LIST      Date: 01/31/1995

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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

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operation with the  listed item inoperative.

12.  "Inoperative" means a system and/or component malfunction to the extent that it does not accomplish its intended purpose and/or is not consistently functioning normally within its approved operating limit(s) or tolerance(s).

13.  "Notes:" in Column 4 provides additional information for crewmember or maintenance consideration.  Notes are used to identify applicable material which is intended to assist with compliance, but do not relieve the operator of the responsibility for compliance with all applicable requirements.  Notes are not a part of the provisos.

14.  Inoperative components of an inoperative system:

Inoperative items which are components of a system which is inoperative are usually considered components directly associated with and having no other function than to support that system. (Warning/caution systems associated with the inoperative system must be operative unless relief is specifically authorized per the MMEL).

15.  "(M)" symbol indicates a requirement for a specific maintenance procedure which must be accomplished prior to operation with the listed item inoperative.  Normally these procedures are accomplished by maintenance personnel;  however, other personnel may be qualified and authorized to perform certain functions.  Procedures requiring specialized knowledge or skill, or requiring the use of tools or test equipment should be accomplished by maintenance personnel.  The satisfactory accomplishment of all maintenance procedures, regardless of

who performs them, is the responsibility of the operator. Appropriate procedures are required to be published as part of the operator's manual or MEL.

16.  "(O)" symbol indicates a requirement for a specific operations procedure which must be accomplished in planning for and/or operating with the listed item inoperative.  Normally these procedures are accomplished by the flight crew; however, other personnel may be qualified and authorized to perform certain functions.  The satisfactory accomplishment of all procedures, regardless of who performs them, is the responsibility of the operator.  Appropriate procedures are



FEDERAL AVIATION ADMINISTRATION     Page: IX

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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 Page 8

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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.

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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                                                                   | |

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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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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 Page 11

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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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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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FEDERAL AVIATION ADMINISTRATION   Page: XIV

Revision: 2

MASTER MINIMUM EQUIPMENT LIST    Date: 06/14/1989

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Preamble

(Effective 6/14/89)

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

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

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



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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.



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 14       | PAGE:    | |                  DHC-7                   |                       |          | |                                          | DATE: 06/16/1994      | 21-1     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 21  AIR CONDITIONING      |    |    |                                       | |                           |    |    |                                       | Page 14

DHC7R14A.txt

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|                           |    |    |                                       | | 1.  Air Conditioning      |    |    |                                       | |     Packs                 |    |    |                                       | |                           |    |    |                                       | |     1) (With Mod        C | 2  | 1  | (O)One may be inoperative provided    | |        7/1493             |    |    | Emergency Ram Air System operates     | |        installed)         |    |    | normally.                             | |                           |    |    |                                       | | 2.  Nacelle Flow        C | 4  | 2  | (M)(O)One may be inoperative on       | |     Control Valves        |    |    | each side provided:                   | |                           |    |    |     a) Both air conditioning          | |                           |    |    |        packs operate normally,        | |                           |    |    |     b) Inoperative valves are         | |                           |    |    |        deactivated closed, and        | |                           |    |    |     c) Operations are conducted       | |                           |    |    |        in compliance with AFM.        | |                           |    |    |                                       | | 3.  BLEED AIR           B | 1  | 0  | (O)May be inoperative provided:       | |     Caution Light         |    |    |     a) Engine Bleed switches are      | |                           |    |    |        verified either OFF or LOW,    | |                           |    |    |        and                            | |                           |    |    |     b) Operations comply with AFM.    | |                           |    |    |                                       | | 4.  Cabin Pressure        |    |    |                                       | |     Control               |    |    |                                       | |                           |    |    |                                       | |     1) Automatic        C | 1  | 0  | (O)May be inoperative provided        | |                           |    |    | manual control operates normally.     | |                           |    |    |                                       | |     2) Manual           C | 1  | 0  | May be inoperative provided           | |                           |    |    | automatic control operates            | |                           |    |    | normally.                             | |                           |    |    |                                       | |     3) Automatic and    C | 2  | 0  | May be inoperative provided flight    | |        Manual             |    |    | is conducted in an unpressurized      | |                           |    |    | configuration.                        | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 14       | PAGE:    | |                  DHC-7                   |                       |          | |                                          | DATE: 06/16/1994      | 21-2     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 21  AIR CONDITIONING      |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | | 5.  Rear Outflow        C | 2  | 1  | (O)One may be inoperative provided    | Page 15

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|     Valves                |    |    | flight is conducted in an             | |                           |    |    | unpressurized configuration.          | |                           |    |    |                                       | | 6.  Differential        C | 1  | 0  | (O)May be inoperative provided:       | |     Pressure Indicator    |    |    |     a) Cabin altitude indicator       | |                           |    |    |        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.   | |                           |    |    |                                       | | 7.  Cabin Altitude      C | 1  | 0  | (O)May be inoperative provided:       | |     Indicator             |    |    |     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.   | |                           |    |    |                                       | | 8.  Cabin Rate of       C | 1  | 0  | May be inoperative provided:          | |     Climb Indicator       |    |    |     a) All other instruments and      | |                           |    |    |        functions of the pressuriza-   | |                           |    |    |        tion system operate            | |                           |    |    |        normally.                      | |                           |    |    |           OR                          | |                         C |    |    |     b) Flight is conducted in an      | |                           |    |    |        unpressurized configuration.   | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 14       | PAGE:    | |                  DHC-7                   |                       |          | |                                          | DATE: 06/16/1994      | 21-3     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 21  AIR CONDITIONING      |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | | 9.  CABIN PRESS         C | 1  | 0  | May be inoperative provided flight    | |     Caution Light         |    |    | remains at or below 10,000 ft. MSL.   | |                           |    |    |                                       | Page 16

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| 10. Flight Compartment    |    |    |                                       | |     Temperature Control   |    |    |                                       | |                           |    |    |                                       | |     1) Automatic        C | 1  | 0  | May be inoperative provided:          | |                           |    |    |     a) Manual control operates        | |                           |    |    |        normally, and                  | |                           |    |    |     b) Associated overheat caution    | |                           |    |    |        lights operate normally.       | |                           |    |    |                                       | |     2) Manual           C | 1  | 0  | May be inoperative provided auto-     | |                           |    |    | matic control operates normally.      | |                           |    |    |                                       | | 11. Cabin Temperature     |    |    |                                       | |     Control               |    |    |                                       | |                           |    |    |                                       | |     1) Automatic        C | 1  | 0  | May be inoperative provided manual    | |                           |    |    | control operates normally.            | |                           |    |    |                                       | |     2) Manual           C | 1  | 0  | May be inoperative provided auto-     | |                           |    |    | matic control operates normally.      | |                           |    |    |                                       | | 12. Temperature         C | 1  | 0  | May be inoperative provided:          | |     Monitoring Indicator  |    |    |     a) Associated overheat caution    | |                           |    |    |        lights operate normally, and   | |                           |    |    |     b) Both the Flight Compartment    | |                           |    |    |        and Cabin Automatic Temp-      | |                           |    |    |        erature Control operate        | |                           |    |    |        normally.                      | |                           |    |    |                                       | | 13. Ground Gasper       C | 2  | 0  |                                       | | *** Fans                  |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 14       | PAGE:    | |                  DHC-7                   |                       |          | |                                          | DATE: 06/16/1994      | 21-4     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 21  AIR CONDITIONING      |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | | 14. BLEED HOT           C | 4  | 2  | (M)(O)One may be inoperative on       | |     Caution Lights        |    |    | each side provided:                   | |                           |    |    |     a) Both air conditioning          | |                           |    |    |        packs operate normally,        | |                           |    |    |     b) Associated bleed air valve     | Page 17

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|                           |    |    |        is deactivated closed, and     | |                           |    |    |     c) Operations are conducted       | |                           |    |    |        in compliance with the AFM.    | |                           |    |    |                                       | | 15. Freon Air           D | -  | 0  |                                       | | *** Conditioning System   |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 14       | PAGE:    | |                  DHC-7                   |                       |          | |                                          | DATE: 06/16/1994      | 22-1     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 22  AUTO FLIGHT           |    |    |                                       | |                           |    |    |                                       | | 1.  Autopilot System    C | 1  | 0  |                                       | | ***                       |    |    |                                       | |                           |    |    | NOTE: Any mode which functions        | |                           |    |    |       normally may be used.           | |                           |    |    |                                       | | 2.  Yaw Damper System   C | 1  | 0  |                                       | |                           |    |    |                                       | | 3.  Control Wheel       C | 2  | 1  | (O)One control wheel disengage        | |     Autopilot/Yaw Damper  |    |    | switch may be inoperative provided:   | Page 18

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|     Disengage Switches    |    |    |     a) Autopilot is not used below    | |                           |    |    |        1,500 ft. AGL, and             | |                           |    |    |     b) Center glareshield panel       | |                           |    |    |        guarded YAW DAMPER switch      | |                           |    |    |        is OFF.                        | |                           |    |    |                                       | | 4.  AUTOPILOT           C | 1  | 0  | May be inoperative provided           | |     DISENGAGED  Caution   |    |    | autopilot is not used.                | |     Light                 |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 14       | PAGE:    | |                  DHC-7                   |                       |          | |                                          | DATE: 06/16/1994      | 23-1     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 23  COMMUNICATIONS        |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | | 1.  Flight              C | 2  | 0  | May be inoperative provided:          | |     Compartment Speakers  |    |    |     a) Procedures do not require      | |                           |    |    |        their use, and                 | |                           |    |    |     b) Headsets are installed and     | |                           |    |    |        operate normally.              | |                           |    |    |           OR                          | |                         D | 2  | 1  | One may be inoperative provided:      | |                           |    |    |     a) Procedures do not require      | |                           |    |    |        its use,                       | |                           |    |    |     b) Headsets are installed and     | |                           |    |    |        operate normally, and          | Page 19

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|                           |    |    |     c) A spare operable headset is    | |                           |    |    |        available.                     | |                           |    |    |                                       | | 2.  Passenger             |    |    |                                       | |     Address System        |    |    |                                       | |                           |    |    |                                       | |     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 Deck-Cabin Interphone   | |                           |    |    |        function (two-way) operates    | |                           |    |    |        normally.                      | |                           |    |    |                                       | |     2) Cargo            D | 1  | 0  |                                       | |        Configuration      |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 14       | PAGE:    | |                  DHC-7                   |                       |          | |                                          | DATE: 06/16/1994      | 23-2     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 23  COMMUNICATIONS        |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | | 3.  Cabin/Service         |    |    |                                       | |     Interphone System     |    |    |                                       | |                           |    |    |                                       | |     1) Flight Deck to   C | 1  | 0  | (O)May be inoperative provided:       | |        Cabin/Cabin to     |    |    |     a) Procedures do not require      | |        Flight Deck        |    |    |        its use.                       | |                           |    |    |           OR                          | |                         C | 1  | 0  |     b) PA system operates             | |                           |    |    |        normally, and                  | |                           |    |    |     c) Alternate, normal and          | |                           |    |    |        emergency procedures are       | |                           |    |    |        established and used.          | |                           |    |    |                                       | Page 20

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|     2) Crew Call        C | 1  | 0  | Both visual and aural signals may     | |        System             |    |    | be inoperative in the cabin, pro-     | |                           |    |    | vided PA system operates normally     | |                           |    |    | from the flight deck.                 | |                           |    |    |                                       | |     3) Flight Deck      C | 1  | 0  |                                       | |        ATTEND'T           |    |    |                                       | |        Annunciator Light  |    |    |                                       | |                           |    |    |                                       | | 4.  Communication       D | -  | -  | Any in excess of those required by    | |     Systems               |    |    | FAR may be inoperative.               | |     (HF, VHF, UHF)        |    |    |                                       | |                           |    |    |                                       | |     1) VHF Communi-     A | -  | 3  | (M)(O)One may be inoperative          | |        cation Frequency   |    |    | provided:                             | |        Selectors          |    |    |     a) Remaining Selector on          | |                           |    |    |        affected control panel         | |                           |    |    |        operates normally, and         | |                           |    |    |     b) Repairs are made within two    | |                           |    |    |        flight days.                   | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 14       | PAGE:    | |                  DHC-7                   |                       |          | |                                          | DATE: 06/16/1994      | 23-3     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 23  COMMUNICATIONS        |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | | 5.  Static              C | 16 | 12 | A maximum of four may be missing      | |     Dischargers           |    |    | provided not more than one is         | |                           |    |    | missing from each siting group.       | |                           |    |    |                                       | | 6.  Flight Deck           |    |    |                                       | |     Interphone System     |    |    |                                       | |                           |    |    |                                       | |     1) Flight Deck      C | 1  | 0  | (O)May be inoperative provided:       | |        to Ground          |    |    |     a) Procedures do not require      | |                           |    |    |        its use.                       | |                           |    |    |           OR                          | |                         C | 1  | 0  |     b) Alternate procedures are       | |                           |    |    |        established and used.          | |                           |    |    |                                       | | 7.  Cockpit Voice       A | 1  | 0  | May be inoperative provided:          | Page 21

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|     Recorder System       |    |    |     a) Flight Data Recorder (FDR)     | |     (CVR)                 |    |    |        operates normally, and         | |                           |    |    |     b) Repairs are made within        | |                           |    |    |        three flight days              | |                           |    |    |                                       | | 8.  Headsets/           C | -  | -  | Any in excess of those required       | |     Microphones           |    |    | for flight deck crewmembers           | |                           |    |    | (including official observer in       | |                           |    |    | observer's seat) may be               | |                           |    |    | inoperative.                          | |                           |    |    |                                       | | 9.  Microphones           |    |    | Incorporated into 23-8, REV. 12.      | |                           |    |    |                                       | | 10. Audio Panels          |    |    | DELETED REV. 14.                      | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 14       | PAGE:    | |                  DHC-7                   |                       |          | |                                          | DATE: 06/16/1994      | 23-4     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 23  COMMUNICATIONS        |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | | 11. Boom Microphones      |    |    |                                       | |                           |    |    |                                       | |     1) Input To         A | -  | 0  | May be inoperative provided:          | |        Cockpit Voice      |    |    |     a) Flight Data Recorder (FDR)     | |        Recorder Required  |    |    |        operates normally, and         | |                           |    |    |     b) Repairs are made within        | |                           |    |    |        three flight days.             | |                           |    |    |                                       | | *** 2) Input To         C | -  | 0  |                                       | |        Cockpit Voice      |    |    |                                       | |        Recorder Not       |    |    |                                       | |        Required           |    |    |                                       | |                           |    |    |                                       | | 12. Selective Calling   C | 1  | 0  | May be inoperative provided:          | | *** System (SELCAL or     |    |    |     a) Alternate procedures are       | |     CALSEL)               |    |    |        established and used.          | |                           |    |    |           OR                          | Page 22

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|                         D |    |    |     b) Procedures do not require      | |                           |    |    |        its use.                       | |                           |    |    |                                       | | 13. ACARS System        C | 1  | 0  | May be inoperative provided:          | |                           |    |    |     a) Alternate procedures are       | |                           |    |    |        established and used.          | |                           |    |    |           OR                          | |                         D |    |    |     b) Procedures do not require      | |                           |    |    |        its use.                       | |                           |    |    |                                       | |     1) ACARS            C | 1  | 0  | May be inoperative provided:          | |        Printer            |    |    |     a) Alternate procedures are       | |                           |    |    |        established and used.          | |                           |    |    |           OR                          | |                         D |    |    |     b) Procedures do not require      | |                           |    |    |        its use.                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 14       | PAGE:    | |                  DHC-7                   |                       |          | |                                          | DATE: 06/16/1994      | 24-1     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 24  ELECTRICAL POWER      |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | | 1.  AC Generator        C | 4  | 3  | (M)One may be inoperative provided:   | |     System (Generator     |    |    |     a) Cause of malfunction is        | |     & Related GCU)        |    |    |        determined, and                | |                           |    |    |     b) Appropriate action is taken    | |                           |    |    |        to assure that no hazard       | |                           |    |    |        exists.                        | |                           |    |    |                                       | |                         B | 4  | 2  | (M)(O)Two may be inoperative          | |                           |    |    | provided:                             | |                           |    |    |     a) Cause of malfunction is        | |                           |    |    |        determined,                    | |                           |    |    |     b) Appropriate action is taken    | |                           |    |    |        to assure that no hazard       | |                           |    |    |        exits,                         | |                           |    |    |     c) Airplane is not operated       | |                           |    |    |        in known or forecast icing     | |                           |    |    |        conditions,                    | |                           |    |    |     d) Dispatching does not require   | |                           |    |    |        fuel transfer, and             | |                           |    |    |     e) Dispatch does not require      | Page 23

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|                           |    |    |        use of water methanol          | |                           |    |    |        system.                        | |                           |    |    |                                       | | 2.  AC GEN Caution      C | 4  | 3  | (M)(O)One may be inoperative          | |     Lights                |    |    | provided:                             | |                           |    |    |     a) All generators are verified    | |                           |    |    |        to operate normally, and       | |                           |    |    |     b) Generators are monitored       | |                           |    |    |        throughout flight.             | |                           |    |    |                                       | |                           |    |    | (Continued)                           | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 14       | PAGE:    | |                  DHC-7                   |                       |          | |                                          | DATE: 06/16/1994      | 24-2     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 24  ELECTRICAL POWER      |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | | 2.  AC GEN Caution      B | 4  | 2  | (M)(O)Two may be inoperative          | |     Lights (Cont'd)       |    |    | provided:                             | |                           |    |    |     a) All generators are verified    | |                           |    |    |        to operate normally, and are   | |                           |    |    |        monitored throughout flight,   | |                           |    |    |     b) Airplane is not operated       | |                           |    |    |        in known or forecast icing     | |                           |    |    |        conditions,                    | |                           |    |    |     c) Dispatching does not require   | |                           |    |    |        fuel transfer, and             | |                           |    |    |     d) Dispatching does not require   | |                           |    |    |        use of water methanol          | |                           |    |    |        system.                        | |                           |    |    |                                       | | 3.  AC GEN HOT          C | 4  | 3  | (M)One may be inoperative provided    | |     Caution Lights        |    |    | associated generator is removed and   | |                           |    |    | secured by an acceptable procedure.   | |                           |    |    |                                       | |                         B | 4  | 2  | (M)(O)Two may be inoperative          | |                           |    |    | provided:                             | |                           |    |    |     a) Associated generators are      | |                           |    |    |        removed and secured by an      | Page 24

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|                           |    |    |        acceptable procedure,          | |                           |    |    |     b) Airplane is not operated       | |                           |    |    |        in known or forecast icing     | |                           |    |    |        conditions,                    | |                           |    |    |     c) Dispatching does not require   | |                           |    |    |        fuel transfer, and             | |                           |    |    |     d) Dispatching does not require   | |                           |    |    |        use of water methanol          | |                           |    |    |        system.                        | |                           |    |    |                                       | |                           |    |    | (Continued)                           | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 14       | PAGE:    | |                  DHC-7                   |                       |          | |                                          | DATE: 06/16/1994      | 24-3     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 24  ELECTRICAL POWER      |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | | 3.  AC GEN HOT            |    |    |                                       | |     Caution Lights        |    |    |                                       | |     (Cont'd)              |    |    |                                       | |                           |    |    |                                       | |     1) With Mod         A | 4  | 3  | (M)(O)One may be inoperative          | |        7/2097             |    |    | provided:                             | |        Installed          |    |    |     a) Inoperative caution light is   | |                           |    |    |        caused by associated bearing   | |                           |    |    |        wear indicator,                | |                           |    |    |     b) Associated AC generator is     | |                           |    |    |        verified OFF, and              | |                           |    |    |     c) Operations are limited to      | |                           |    |    |        not more than one flight       | |                           |    |    |        day.                           | |                           |    |    |                                       | | 4.  Static Inverters    B | 3  | 2  | (M)One may be inoperative provided    | |                           |    |    | the inoperative inverter is           | |                           |    |    | deactivated.                          | |                           |    |    |                                       | | 5.  Inverter Caution    C | 3  | 2  | (M)One may be inoperative provided    | |     Lights                |    |    | associated inverter is verified       | |                           |    |    | to operate normally.                  | |                           |    |    |                                       | Page 25

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| 6.  DC Voltmeter          |    |    | Deleted REV. 9.                       | |                           |    |    |                                       | | 7.  DC Starter-         C | 4  | 3  | (M)One generator control system       | |     Generator Control     |    |    | may be inoperative in generator       | |     System                |    |    | mode only provided:                   | |                           |    |    |     a) Failed generator is            | |                           |    |    |        verified OFF,                  | |                           |    |    |     b) Load shedding procedures are   | |                           |    |    |        used,                          | |                           |    |    |     c) Associated DC Generator        | |                           |    |    |        Caution light is deactiv-      | |                           |    |    |        ated, and                      | |                           |    |    |     d) Freon Air Conditioning         | |                           |    |    |        system is verified OFF.        | |                           |    |    |                                       | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 14       | PAGE:    | |                  DHC-7                   |                       |          | |                                          | DATE: 06/16/1994      | 24-4     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 24  ELECTRICAL POWER      |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | | 8.  Batteries           C | -  | 2  | (M)May be inoperative provided one    | |                           |    |    | normal battery is connected to        | |                           |    |    | the left main bus, and another of     | |                           |    |    | the same capacity is connected to     | |                           |    |    | the right main bus.                   | |                           |    |    |                                       | | 9.  Battery             C | -  | 2  | (M)May be inoperative provided:       | |     Temperature Monitor   |    |    |     a) One system operates normally   | |     System (Indicator &   |    |    |        for each operating battery,    | |     Caution Lights)       |    |    |        and                            | |                           |    |    |     b) Batteries with inoperative     | |                           |    |    |        monitor systems are            | |                           |    |    |        disconnected.                  | |                           |    |    |                                       | | 10. AC External         C | 1  | 0  |                                       | |     Power System          |    |    |                                       | |                           |    |    |                                       | | 11. DC External         C | 1  | 0  |                                       | |     Power System          |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | Page 26

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|                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 14       | PAGE:    | |                  DHC-7                   |                       |          | |                                          | DATE: 06/16/1994      | 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. 14.                      | |     Shoulder Harness      |    |    |                                       | |     (Flight Deck)         |    |    |                                       | |                           |    |    |                                       | | 2.  Emergency Locator   C | -  | -  | As required by FAR.                   | |     Transmitter (ELT)     |    |    |                                       | |                           |    |    |                                       | | *** Excess Items        D | -  | 0  |                                       | |                           |    |    |                                       | | 3.  Passenger Seats       |    |    |                                       | |                           |    |    |                                       | |     1) Seat Backs       C | -  | -  | (M)May be inoperative secured in      | |                           |    |    | the upright position.                 | |                           |    |    |                                       | |                         C | -  | -  | (M)May be inoperative in other        | |                           |    |    | than the upright position provided:   | |                           |    |    |     a) Does not block an Emergency    | |                           |    |    |        Exit,                          | |                           |    |    |     b) Does not restrict any pas-     | |                           |    |    |        senger from access to the      | |                           |    |    |        main aircraft aisle, and       | |                           |    |    |     c) The associated seat(s) is      | |                           |    |    |        blocked and placarded "DO      | |                           |    |    |        NOT OCCUPY".                   | |                           |    |    |                                       | |                           |    |    | NOTE 1: A seat with an inoperative    | |                           |    |    |         seat belt is considered       | |                           |    |    |         inoperative.                  | |                           |    |    |                                       | Page 27

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|                           |    |    | NOTE 2: Inoperative seats do not      | |                           |    |    |         affect the required number    | |                           |    |    |         of Flight Attendants.         | |                           |    |    |                                       | | 4.  "Fasten Seat Belt   C | -  | -  | One or more signs or placards may     | |     While Seated" Signs   |    |    | be illegible or missing provided a    | |     or Placards           |    |    | legible sign or placard is readable   | |                           |    |    | from each occupied passenger seat.    | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 14       | PAGE:    | |                  DHC-7                   |                       |          | |                                          | DATE: 06/16/1994      | 25-2     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 25  EQUIPMENT/FURNISHINGS |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | | 5.  Pilot's Seat          |    |    |                                       | |     Adjustment            |    |    |                                       | |                           |    |    |                                       | |     1) Vertical         C | 2  | 0  | (M)Vertical mode adjustment may be    | |        Mode               |    |    | inoperative provided:                 | |                           |    |    |     a) Seat is secured at the         | |                           |    |    |        individual crewmembers         | |                           |    |    |        requirements, and              | |                           |    |    |     b) Fore-aft adjustment operates   | |                           |    |    |        normally.                      | |                           |    |    |                                       | | 6.  Flight Attendant    C | -  | -  | (M)(O)One single or one dual          | |     Seat Assembly         |    |    | position seat may be inoperative      | |     (Single or Dual       |    |    | provided:                             | |     Position)             |    |    |     a) Affected seat position(s) is   | |                           |    |    |        not occupied,                  | |                           |    |    |     b) Flight attendant(s)            | |                           |    |    |        displaced by inoperative       | |                           |    |    |        seat(s) occupies the           | |                           |    |    |        passenger seat(s) most         | |                           |    |    |        accessible to his or her       | |                           |    |    |        assigned exit,                 | |                           |    |    |     c) Alternate procedures are       | |                           |    |    |        established for displaced      | |                           |    |    |        flight attendant(s),           | |                           |    |    |     d) Folding type seat is stowed    | |                           |    |    |        or secured in the retracted    | |                           |    |    |        position, and                  | |                           |    |    |     e) Passenger seat(s) assigned     | |                           |    |    |        to flight attendant(s) is      | |                           |    |    |        placarded "FOR FLIGHT          | Page 28

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|                           |    |    |        ATTENDANT USE ONLY".           | |                           |    |    |                                       | |                           |    |    | NOTE 1: A folding seat that will      | |                           |    |    |         not stow is considered        | |                           |    |    |         inoperative.                  | |                           |    |    |                                       | |                           |    |    | (Continued)                           | |                           |    |    |                                       | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 14       | PAGE:    | |                  DHC-7                   |                       |          | |                                          | DATE: 06/16/1994      | 25-3     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 25  EQUIPMENT/FURNISHINGS |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | | 6. Flight Attendant       |    |    | NOTE 2: A seat position with an       | |    Seat Assembly          |    |    |         inoperative or missing lap    | |    (Single or Dual        |    |    |         belt is considered            | |    Positions)             |    |    |         inoperative.                  | |    (Cont'd)               |    |    |                                       | |                           |    |    | NOTE 3: The above provisos apply      | |                           |    |    |         only to required flight       | |                           |    |    |         attendant seats.  Seat        | |                           |    |    |         positions in excess of        | |                           |    |    |         those required may be         | |                           |    |    |         inoperative provided they     | |                           |    |    |         are properly stowed or        | |                           |    |    |         secured in the retracted      | |                           |    |    |         position.  Individual         | |                           |    |    |         operators, when operating     | |                           |    |    |         with inoperative seats,       | |                           |    |    |         will consider the locations   | |                           |    |    |         and combinations of seats     | |                           |    |    |         to ensure that the            | |                           |    |    |         proximity to exits and        | |                           |    |    |         distribution requirements     | |                           |    |    |         of the applicable FAR         | |                           |    |    |         are met.                      | |                           |    |    |                                       | | 7.  Passenger             | -  | -  | Passenger convenience items, as       | |     Convenience Items     |    |    | expressed in this 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   | Page 29

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|                           |    |    | included.  (M) and (O) procedures     | |                           |    |    | may be required and included in the   | |                           |    |    | air carrier's appropriate document.   | |                           |    |    |                                       | |                           |    |    | NOTE: Lavatory door ash tray is not   | |                           |    |    |       considered a passenger          | |                           |    |    |       convenience item.               |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 14       | PAGE:    | |                  DHC-7                   |                       |          | |                                          | DATE: 06/16/1994      | 25-4     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 25  EQUIPMENT/FURNISHINGS |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | | 8.  Forward Observer    A | 1  | 0  | May be inoperative provided:          | |     Seat (Including       |    |    |     a) A passenger seat in the        | |     Associated Equip-     |    |    |        passenger cabin is made        | |     ment)                 |    |    |        available to an FAA            | |                           |    |    |        inspector for the              | |                           |    |    |        performance of official        | |                           |    |    |        duties, and                    | |                           |    |    |     b) Operations are limited to      | |                           |    |    |        not more than two flight       | |                           |    |    |        days before repairs are        | |                           |    |    |        made.                          | |                           |    |    |                                       | |     1) Forward          A | 1  | 0  | May be inoperative provided:          | |        Observer's         |    |    |     a) Occupant of seat is not        | |        Audio Selector     |    |    |        required to perform official   | |        Panel              |    |    |        duties,                        | |                           |    |    |     b) An FAA Inspector may, after    | |                           |    |    |        being briefed on the nature    | |                           |    |    |        of the discrepancy, elect to   | |                           |    |    |        utilize the seat,              | |                           |    |    |     c) Alternate communications       | |                           |    |    |        procedures are established     | |                           |    |    |        and used, and                  | |                           |    |    |     d) Operations are limited to      | |                           |    |    |        not more than two flight       | |                           |    |    |        days before repair is made.    | |                           |    |    |                                       | | 9.  Megaphones          D | -  | 0  | Any in excess of those required by    | |                           |    |    | FAR may be inoperative or missing     | |                           |    |    | provided:                             | |                           |    |    |     a) Inoperative megaphone is       | |                           |    |    |        removed from the passenger     | |                           |    |    |        cabin, and                     | |                           |    |    |     b) Required distribution is       | |                           |    |    |        maintained.                    | Page 30

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|                           |    |    |                                       | |     1) Cargo            D | -  | 0  |                                       | |        Operations         |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 14       | PAGE:    | |                  DHC-7                   |                       |          | |                                          | DATE: 06/16/1994      | 25-5     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 25  EQUIPMENT/FURNISHINGS |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | | 10. First Aid Kits      D | -  | -  | Any in excess of those required by    | |                           |    |    | FAR may be incomplete or missing      | |                           |    |    | provided required distribution is     | |                           |    |    | maintained.                           | |                           |    |    |                                       | | 11. Cabin Emergency       |    |    |                                       | |     Flashlight Holders/   |    |    |                                       | |     Flashlights           |    |    |                                       | |                           |    |    |                                       | |     1) Passenger And    C | -  | -  | May be inoperative or missing         | |        Mixed              |    |    | provided the crewmember assigned to   | |        Configurations     |    |    | the associated position has a         | |                           |    |    | normally operating flashlight         | |                           |    |    | readily available.                    | |                           |    |    |                                       | |     2) Cargo            D | -  | 0  |                                       | |        Operations         |    |    |                                       | |                           |    |    |                                       | | 12. Overhead Storage    D | -  | -  | (M)May be inoperative provided:       | |     Bin Latches           |    |    |     a) Affected storage bin lid(s)    | |                           |    |    |        is secured closed,             | |                           |    |    |     b) Affected bin is not used       | |                           |    |    |        for storage of any items,      | |                           |    |    |        and                            | |                           |    |    |     c) Affected bin is placarded      | |                           |    |    |        "INOPERATIVE-DO NOT USE".      | |                           |    |    |                                       | |                           |    |    | NOTE: If partitions are not           | |                           |    |    |       installed, the entire           | |                           |    |    |       overhead storage compartment    | |                           |    |    |       is considered to be one bin.    | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | Page 31

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|                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 14       | PAGE:    | |                  DHC-7                   |                       |          | |                                          | DATE: 06/16/1994      | 26-1     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 26  FIRE PROTECTION       |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | | 1.  Engine Fire         C | 8  | 4  | (M)(O)Either Loop A or Loop B may     | |     Detection Systems     |    |    | be inoperative on each engine pro-    | |     (With Mod 7/1302      |    |    | vided short discrimination cir-       | |     installed)            |    |    | cuitry is installed and operates      | |                           |    |    | normally.                             | |                           |    |    |                                       | | 2.  Baggage             C | 2  | 1  |                                       | |     Compartment Smoke     |    |    |                                       | |     Detectors           C | 2  | 0  | (O)May be inoperative provided:       | |                           |    |    |     a) Inner baggage door remains     | |                           |    |    |        open,                          | |                           |    |    |     b) Compartment contents are       | |                           |    |    |        properly restrained, and       | |                           |    |    |     c) Flight attendant is advised    | |                           |    |    |        of the condition.              | |                           |    |    |                                       | |                         C | 2  | 0  | May be inoperative provided only      | |                           |    |    | non-combustible materials are         | |                           |    |    | carried.                              | |                           |    |    |                                       | | 3.  DELETED               |    |    | Deleted prior to REV. 9.              | |                           |    |    |                                       | | 4.  Fire Extinguisher   C | 4  | 0  | (M)May be missing provided indi-      | |     Thermal and           |    |    | cator readings are checked once       | |     Discharge Discs       |    |    | each flight day to verify adequate    | |                           |    |    | charge.                               | |                           |    |    |                                       | | 5.  DELETED               |    |    | Deleted prior to REV. 9.              | |                           |    |    |                                       | | 6.  DELETED               |    |    | Deleted prior to REV. 9.              | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | Page 32

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| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 14       | PAGE:    | |                  DHC-7                   |                       |          | |                                          | DATE: 06/16/1994      | 26-2     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 26  FIRE PROTECTION       |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | | 7.  Fire Warning Bell   A | 1  | 0  | (O)May be inoperative provided:       | | ***                       |    |    |     a) All Fire Warning lights        | |                           |    |    |        operate normally, and          | |                           |    |    |     b) Repairs are made within        | |                           |    |    |        three flight days.             | |                           |    |    |                                       | | 8.  Cargo Compartment   C | 3  | 2  |                                       | |     Smoke Detectors       |    |    |                                       | |                         C | 3  | 0  | (O)May be inoperative provided:       | |                           |    |    |     a) Cargo compartment is           | |                           |    |    |        occupied and monitored, and    | |                           |    |    |     b) Flight deck-to-cabin and       | |                           |    |    |        cabin-to-flight deck           | |                           |    |    |        interphone system is           | |                           |    |    |        operating normally.            | |                           |    |    |                                       | |                         C | 2  | 0  | May be inoperative provided only      | |                           |    |    | non-combustible materials are         | |                           |    |    | carried.                              | |                           |    |    |                                       | |                         C | 2  | 0  | May be inoperative for all            | |                           |    |    | passenger configuration.              | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       |



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| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 14       | PAGE:    | |                  DHC-7                   |                       |          | |                                          | DATE: 06/16/1994      | 26-3     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 26  FIRE PROTECTION       |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | | 9.  Lavatory Fire       C | -  | -  | (M)For each lavatory, the lavatory    | |     Extinguisher Systems  |    |    | fire extinguisher system may be       | |                           |    |    | inoperative provided:                 | |                           |    |    |     a) Lavatory Smoke Detector        | |                           |    |    |        System operates normally.      | |                           |    |    |           OR                          | |                         C | -  | -  |     b) Lavatory waste receptacle is   | |                           |    |    |        empty,                         | |                           |    |    |     c) Lavatory door is locked        | |                           |    |    |        closed and placarded           | |                           |    |    |        "INOPERATIVE-DO NOT ENTER",    | |                           |    |    |        and                            | |                           |    |    |     d) Lavatory is not used for any   | |                           |    |    |        purpose.                       | |                           |    |    |                                       | |                           |    |    | NOTE 1: These provisos are not        | |                           |    |    |         intended to prohibit          | |                           |    |    |         lavatory inspections by       | |                           |    |    |         crewmembers.                  | |                           |    |    |                                       | |                           |    |    | NOTE 2: A lavatory fire               | |                           |    |    |         extinguisher system is not    | |                           |    |    |         required for all-cargo        | |                           |    |    |         operations.                   | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       |



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| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 14       | PAGE:    | |                  DHC-7                   |                       |          | |                                          | DATE: 06/16/1994      | 26-4     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 26  FIRE PROTECTION       |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | | 10. Lavatory Smoke      C | -  | -  | (M)For each lavatory, the lavatory    | |     Detection Systems     |    |    | smoke detection system may be         | |                           |    |    | inoperative provided:                 | |                           |    |    |     a) Lavatory fire extinguisher     | |                           |    |    |        system operates normally.      | |                           |    |    |           OR                          | |                         C | -  | -  |     b) The lavatory waste             | |                           |    |    |        receptacle is empty,           | |                           |    |    |     c) Lavatory door is locked        | |                           |    |    |        closed and placarded           | |                           |    |    |        "INOPERATIVE-DO NOT ENTER",    | |                           |    |    |        and                            | |                           |    |    |     d) Lavatory is not used for any   | |                           |    |    |        purpose.                       | |                           |    |    |                                       | |                           |    |    | NOTE 1: These provisos are not        | |                           |    |    |         intended to prohibit          | |                           |    |    |         lavatory inspections by       | |                           |    |    |         crewmembers.                  | |                           |    |    |                                       | |                           |    |    | NOTE 2: A lavatory smoke detection    | |                           |    |    |         system is not required for    | |                           |    |    |         all-cargo operations.         | |                           |    |    |                                       | | 11. APU Fire            D | 1  | 0  | (M)May be inoperative provided APU    | | *** Detection System      |    |    | is considered inoperative and not     | |                           |    |    | used.                                 | |                           |    |    |                                       | | 12. APU Fire            D | 1  | 0  | (M)May be inoperative provided APU    | | *** Extinguishing System  |    |    | is considered inoperative and not     | |                           |    |    | used.                                 | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | Page 35

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DHC7R14A.txt

|                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 14       | PAGE:    | |                  DHC-7                   |                       |          | |                                          | DATE: 06/16/1994      | 26-5     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 26  FIRE PROTECTION       |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | | 13. Aft Cargo Compart-  C | 2  | 1  |                                       | | *** ment (Class C) Smoke  |    |    |                                       | |     Detection System      |    |    |                                       | |                         C | 2  | 0  | Both may be inoperative provided:     | |                           |    |    |     a) No combustible cargo is        | |                           |    |    |        carried in the associated      | |                           |    |    |        compartment.                   | |                           |    |    |                OR                     | |                         C |    |    |     b) Associated compartment         | |                           |    |    |        remains empty.                 | |                           |    |    |                                       | | 14.  Aft Cargo Compart- C | 1  | 0  | May be inoperative provided:          | | ***  ment (Class C)       |    |    |     a) No combustible cargo is        | |      Extinguisher System  |    |    |        carried in the assoc-          | |                           |    |    |        iated compartment.             | |                           |    |    |                 OR                    | |                         C |    |    |     b) Associated compartment         | |                           |    |    |        remains empty.                 | |                           |    |    |                                       | | 15. Portable Fire       D | -  | -  | (M)Any in excess of those required    | |     Extinguishers         |    |    | by FAR may be inoperative or          | |                           |    |    | missing provided:                     | |                           |    |    |     a) Inoperative fire extin-        | |                           |    |    |        guisher is removed from the    | |                           |    |    |        passenger compartment, and     | |                           |    |    |     b) Required distribution is       | |                           |    |    |        maintained.                    | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | Page 36

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DHC7R14A.txt

| AIRCRAFT:                                | REVISION NO: 14 a     | PAGE:    | |                  DHC-7                   |                       |          | |                                          | DATE: 06/17/1999      | 27-1     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 27  FLIGHT CONTROLS       |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | | 1.  Aileron Trim        C | 1  | 0  | (O)May be inoperative provided the    | |     Indicator             |    |    | aileron trim tab is verified          | |                           |    |    | neutral before each departure.        | |                           |    |    |                                       | | 2.  Stall Warning       B | 2  | 1  | (M)One may be inoperative provided    | |     Systems               |    |    | the associated system is              | |                           |    |    | deactivated.                          | |                           |    |    |                                       | |                           |    |    | NOTE: Deactivating a stall warning    | |                           |    |    |       system will also deactivate     | |                           |    |    |       the associated speed control    | |                           |    |    |       indicator.                      | |                           |    |    |                                       | | 3.  Rudder Trim         C | 1  | 0  | (M)May be inoperative provided:       | |     Indicator             |    |    |     a) Rudder Trim is verified to     | |                           |    |    |        have full and free movement    | |                           |    |    |        and,                           | |                           |    |    |     b) Rudder Trim is verified        | |                           |    |    |        neutral before each            | |                           |    |    |        departure.                     | |                           |    |    |                                       | | 4.  Trailing Flap       C | 1  | 0  | (M)(O)May be inoperative provided:    | |     System                |    |    |     a) System is secured, and         | |                           |    |    |     b) Operations are conducted in    | |                           |    |    |        compliance with the AFM.       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 14 a     | PAGE:    | |                  DHC-7                   |                       |          | Page 37

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DHC7R14A.txt

|                                          | DATE: 06/17/1999      | 27-2     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 27  FLIGHT CONTROLS       |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | | 5.  Flap Position       B | 1  | 0  | (M)(O)May be inoperative provided:  ] | |     Indicator             |    |    |     a) Flap position markings are   ] | |                           |    |    |        legible on inboard nacelles, ] | |                           |    |    |     b) Flaps operate normally       ] | |                           |    |    |        through 25 degrees travel,   ] | |                           |    |    |     c) Seat row adjacent to Flap    ] | |                           |    |    |        Position markings is plac-   ] | |                           |    |    |        arded "DO NOT OCCUPY",       ] | |                           |    |    |     d) Proper flap position is      ] | |                           |    |    |        visually verified by a       ] | |                           |    |    |        qualified person other than  ] | |                           |    |    |        a flight deck crewmember,and ] | |                           |    |    |     e) Flaps are limited to 25      ] | |                           |    |    |        degrees maximum.             ] | |                           |    |    |                                       | | 6.  Spoilers Advisory     |    |    |                                       | |     Lights                |    |    |                                       | |                           |    |    |                                       | |     1) ROLL INBD        C | 1  | 0  | (O)May be inoperative provided        | |                           |    |    | all PFCS SPOILERS indicators          | |                           |    |    | operate normally, and monitored       | |                           |    |    | closely.                              | |                           |    |    |                                       | |     2) ROLL OUTBD       C | 1  | 0  | (O)May be inoperative provided        | |                           |    |    | all PFCS SPOILERS indicators          | |                           |    |    | operate normally, and are monitored   | |                           |    |    | closely.                              | |                           |    |    |                                       | |     3) GROUND           C | 1  | 0  | (M)May be inoperative provided the    | |                           |    |    | ground spoiler system is              | |                           |    |    | deactivated.                          | |                           |    |    |                                       | | 7.  Ground Spoiler      C | 1  | 0  | (O)May be inoperative in the DOWN     | |     System                |    |    | position provided:                    | |                           |    |    |     a) System is deactivated, and     | |                           |    |    |     b) Appropriate AFM performance    | |                           |    |    |        decrements are applied.        | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 14 a     | PAGE:    | |                  DHC-7                   |                       |          | |                                          | DATE: 06/17/1999      | 27-3     | | --------------------------------------------------------------------------- | Page 38

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DHC7R14A.txt

|                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 27  FLIGHT CONTROLS       |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | | 8.  Powered Flight        |    |    |                                       | |     Control System        |    |    |                                       | |     (PFCS) Indicators     |    |    |                                       | |                           |    |    |                                       | |     1) RUDDER (RUD)     B | 1  | 0  | (M)May be inoperative provided a      | |                           |    |    | visual flight control check is ac-    | |                           |    |    | complished before each departure.     | |                           |    |    |                                       | |     2) SPOILERS         B | 4  | 0  | (M)May be inoperative provided:       | |        (LO, LI, RI, RO)   |    |    |     a) ROLL INBD and ROLL OUTBD       | |                           |    |    |        spoilers advisory lights       | |                           |    |    |        operate normally, and          | |                           |    |    |     b) A visual flight control        | |                           |    |    |        check is accomplished before   | |                           |    |    |        each departure.                | |                           |    |    |                                       | | 9.  Rudder Hydraulic    C | 2  | 1  | (M)One may be inoperative provided    | |     Pressure Caution      |    |    | RUD 1 and RUD 2 actuators are         | |     Lights (#1 RUD HYD,   |    |    | verified to operate normally before   | |     #2 RUD HYD)           |    |    | each departure.                       | |                           |    |    |                                       | | 10. Rudder Pedal        C | 2  | 0  | (M)May be inoperative provided        | |     Adjustment            |    |    | rudder pedals can be secured in a     | |                           |    |    | position which meets individual       | |                           |    |    | pilot requirements.                   | |                           |    |    |                                       | | 11. Control Lock        C | 1  | 0  | (M)May be inoperative provided:       | |                           |    |    |     a) An acceptable procedure is     | |                           |    |    |        established and used to        | |                           |    |    |        verify Control Lock is         | |                           |    |    |        secured in the unlocked        | |                           |    |    |        position, and                  | |                           |    |    |     b) Procedures are established     | |                           |    |    |        to restrain control movement   | |                           |    |    |        on the ground.                 | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 14 a     | PAGE:    | |                  DHC-7                   |                       |          | |                                          | DATE: 06/17/1999      | 27-4     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | Page 39

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DHC7R14A.txt

| SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 27  FLIGHT CONTROLS       |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | | 12. Trailing Flap         |    |    |                                       | |     Actuator Locking      |    |    |                                       | |     System                |    |    |                                       | |                           |    |    |                                       | |     1) With Mod         C | 1  | 0  |                                       | |        7/2067 Installed   |    |    |                                       | |                           |    |    |                                       | | 13. Rudder Trim Switch    |    |    |                                       | |                           |    |    |                                       | |     1) Return to        B | 1  | 0  | (O)May be inoperative provided:       | |        Center Spring      |    |    |     a) Rudder Trim Indicator          | |                           |    |    |        operates normally, and         | |                           |    |    |     b) Rudder Trim Switch is          | |                           |    |    |        manually returned to center    | |                           |    |    |        detent position after each     | |                           |    |    |        selection of Rudder Trim.      | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 14       | PAGE:    | |                  DHC-7                   |                       |          | |                                          | DATE: 06/16/1994      | 28-1     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | Page 40

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| 28  FUEL                  |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | | 1.  AC Auxiliary        B | 4  | 3  | (M)(O)One may be inoperative          | |     Fuel Pumps            |    |    | provided:                             | |                           |    |    |     a) Flight compartment fuel        | |                           |    |    |        quantity indicators operate    | |                           |    |    |        normally, and                  | |                           |    |    |     b) Airplane is dispatched so      | |                           |    |    |        that fuel transfer is not      | |                           |    |    |        required.                      | |                           |    |    |                                       | | 2.  Fuel Quantity       C | 4  | 3  | (M)(O)One may be inoperative          | |     Indicators            |    |    | provided:                             | |                           |    |    |     a) Fuel quantity in associated    | |                           |    |    |        tank is verified by an         | |                           |    |    |        acceptable means,              | |                           |    |    |     b) All Fuel Flow Meters operate   | |                           |    |    |        normally,                      | |                           |    |    |     c) Fuel flow is monitored         | |                           |    |    |        during flight, and             | |                           |    |    |     d) Fuel consumption is            | |                           |    |    |        recorded.                      | |                           |    |    |                                       | | 3.  Fuel Tank           C | 4  | 0  | (M)May be inoperative provided fuel   | |     Indication System     |    |    | quantity is verified by an accept-    | |     (Refueling Panel)     |    |    | able means at each refueling.         | |                           |    |    |                                       | | 4.  Pressure            C | 1  | 0  |                                       | |     Refueling System      |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 14       | PAGE:    | |                  DHC-7                   |                       |          | |                                          | DATE: 06/16/1994      | 28-2     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 28  FUEL                  |    |    |                                       | |                           |    |    |                                       | Page 41

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|                           |    |    |                                       | | 5.  TANK FUEL LOW       C | 4  | 3  | (O)One may be inoperative provided    | |     Caution Lights        |    |    | associated fuel quantity indicator    | |                           |    |    | operates normally, and is monitored   | |                           |    |    | during flight.                        | |                           |    |    |                                       | |                         C | 4  | 0  | (O)May be inoperative provided:       | |                           |    |    |     a) Associated fuel quantity       | |                           |    |    |        indicator(s) operates          | |                           |    |    |        normally,                      | |                           |    |    |     b) Airplane is dispatched so as   | |                           |    |    |        to assure flight completion    | |                           |    |    |        with a minimum of 700 lb.      | |                           |    |    |        fuel in related tank(s), and   | |                           |    |    |     c) Dispatching does not require   | |                           |    |    |        fuel transfer.                 | |                           |    |    |                                       | | 6.  FUEL XFR System       |    |    |                                       | |                           |    |    |                                       | |     1) Caution Light    A | 1  | 0  | (O)May be inoperative provided:       | |                           |    |    |     a) Dispatching does not           | |                           |    |    |        require fuel transfer, and     | |                           |    |    |     b) Repair is made within three    | |                           |    |    |        flight days.                   | |                           |    |    |                                       | | 7.  FUELING ON          C | 1  | 0  | (M)May be inoperative provided        | |     Caution Light         |    |    | Refuel/Defuel POWER ON light oper-    | |                           |    |    | ates normally, and is verified        | |                           |    |    | extinguished after each refueling.    | |                           |    |    |                                       | | 8.  ENG FUEL PRESS      B | 4  | 3  | (O)One may be inoperative provided:   | |     Caution Lights        |    |    |     a) Associated Fuel Flow Meter     | |                           |    |    |        operates normally, and         | |                           |    |    |     b) Associated auxiliary pump      | |                           |    |    |        operates normally, is          | |                           |    |    |        selected ON before             | |                           |    |    |        departure, and remains ON      | |                           |    |    |        throughout the flight.         | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 14       | PAGE:    | |                  DHC-7                   |                       |          | |                                          | DATE: 06/16/1994      | 28-3     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 28  FUEL                  |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | | 9.  Aux Pump            C | 4  | 0  | (M)May be inoperative provided:       | Page 42

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|     Advisory Lights       |    |    |     a) Associated auxiliary pump(s)   | |                           |    |    |        and ENG FUEL PRESS caution     | |                           |    |    |        light(s) operates normally,    | |                           |    |    |        and                            | |                           |    |    |     b) Dispatching does not require   | |                           |    |    |        fuel transfer.                 | |                           |    |    |                                       | | 10. Fuel Tank           C | 4  | 0  | (M)May be inoperative provided fuel   | |     Magnasticks           |    |    | quantity is verified by other         | |                           |    |    | acceptable means.                     | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 14       | PAGE:    | |                  DHC-7                   |                       |          | |                                          | DATE: 06/16/1994      | 29-1     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 29  HYDRAULIC POWER       |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | | 1.  DELETED               |    |    | Deleted prior to REV. 9.              | |                           |    |    |                                       | | 2.  System Quantity     C | 2  | 1  | (M)May be inoperative provided:       | |     Indicators            |    |    |     a) Quantity is verified ade-      | Page 43

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|                           |    |    |        quate before each departure,   | |                           |    |    |        and                            | |                           |    |    |     b) Associated ENG HYD PUMP        | |                           |    |    |        caution lights and pressure    | |                           |    |    |        indicator(s) operates          | |                           |    |    |        normally.                      | |                           |    |    |                                       | | 3.  System Pressure     C | 2  | 0  | (M)(O)May be inoperative provided     | |     Indicators            |    |    | associated ENG HYD PUMP caution       | |                           |    |    | lights and quantity indicator(s)      | |                           |    |    | operates normally.                    | |                           |    |    |                                       | | 4.  ENG HYD PUMP        C | 4  | 2  | (M)(O)One may be inoperative for      | |     Caution Lights        |    |    | each hydraulic system provided the    | |                           |    |    | associated pressure indicator and     | |                           |    |    | associated pump are verified to       | |                           |    |    | operate normally before each          | |                           |    |    | departure.                            | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 14       | PAGE:    | |                  DHC-7                   |                       |          | |                                          | DATE: 06/16/1994      | 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            C | 1  | 0  | (O)May be inoperative provided        | |     De-Icing System       |    |    | airplane is not operated in known     | |     (Wing, Tail and       |    |    | or forecast icing conditions.         | |     Engine Intake)        |    |    |                                       | |                           |    |    |                                       | | 2.  Elevator            C | 1  | 0  | (O)May be inoperative provided        | |     Anti-icing System     |    |    | airplane is not operated in known     | Page 44

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|                           |    |    | or forecast icing conditions.         | |                           |    |    |                                       | | 3.  Engine Intake       C | 4  | 0  | (O)May be inoperative retracted       | |     Deflectors            |    |    | provided airplane is not operated     | |                           |    |    | in known or forecast icing condi-     | |                           |    |    | tions, or in visible precipitation    | |                           |    |    | with temperatures below +5            | |                           |    |    | degrees C.                            | |                           |    |    |                                       | |                         C | 4  | 0  | (O)May be inoperative deployed        | |                           |    |    | provided operations comply with       | |                           |    |    | AFM.                                  | |                           |    |    |                                       | | 4.  Engine Intake       C | 4  | 0  | (O)May be inoperative provided:       | |     Deflector Indicators  |    |    |     a) Associated Deflector is        | |                           |    |    |        verified in proper position    | |                           |    |    |        before each departure, and     | |                           |    |    |     b) Operations comply with AFM.    | |                           |    |    |                                       | | 5.  Propeller           C | 4  | 0  | (O)May be inoperative provided        | |     De-icing Systems      |    |    | airplane is not operated in known     | |                           |    |    | or forecast icing conditions.         | |                           |    |    |                                       | | 6.  Windshield          C | 2  | 0  | (O)May be inoperative provided        | |     Wipers                |    |    | the airplane is not operated in       | |                           |    |    | precipitation within 5 nautical       | |                           |    |    | miles of the airport of takeoff or    | |                           |    |    | intended landing.                     | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 14       | PAGE:    | |                  DHC-7                   |                       |          | |                                          | DATE: 06/16/1994      | 30-2     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 30  ICE AND RAIN          |    |    |                                       | |     PROTECTION            |    |    |                                       | |                           |    |    |                                       | | 7.  Windshield          C | 2  | 0  | (O)May be inoperative provided        | |     Heating Systems       |    |    | airplane is not operated in known     | |                           |    |    | or forecast icing conditions, or in   | |                           |    |    | visible precipitation with tempera-   | |                           |    |    | tures below +5 degrees C.             | |                           |    |    |                                       | | 8.  Pitot Static        B | 3  | 2  | (O)One may be inoperative provided    | |     Heater Systems        |    |    | airplane is not operated in known     | |                           |    |    | or forecast icing conditions.         | Page 45

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|                           |    |    |                                       | | 9.  Wing Deicer Boot    C | 8  | 0  | (O)May be inoperative provided:       | |     Advisory Lights       |    |    |     a) Boot operation is visually     | |                           |    |    |        monitored when in use, and     | |                           |    |    |     b) Appropriate wing inspection    | |                           |    |    |        light(s) operates normally     | |                           |    |    |        for night operations.          | |                           |    |    |                                       | | 10. Tail Deicer Boot    C | 4  | 0  | (O)May be inoperative provided        | |     Advisory Lights       |    |    | airplane is not operated in known     | |                           |    |    | or forecast icing conditions.         | |                           |    |    |                                       | | 11. DE-ICE PRESS        C | 1  | 0  | May be inoperative provided wing      | |     Indicator             |    |    | and tail deicer boot advisory         | |                           |    |    | lights operate normally.              | |                           |    |    |                                       | | 12. Engine PX-PY        C | 4  | 0  | (O)May be inoperative provided        | |     Heaters               |    |    | airplane is not operated in known     | |                           |    |    | or forecast icing conditions.         | |                           |    |    |                                       | | 13. Pitot Heat          B | 1  | 0  | (M)May be inoperative provided:       | |     Caution Light         |    |    |     a) Both heaters are verified to   | |                           |    |    |        operate normally before each   | |                           |    |    |        departure, and                 | |                           |    |    |     b) Airplane is not operated in    | |                           |    |    |        known or forecast icing        | |                           |    |    |        conditions.                    | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       |



| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 14       | PAGE:    | |                  DHC-7                   |                       |          | |                                          | DATE: 06/16/1994      | 31-1     | | --------------------------------------------------------------------------- | |                        1. | 2. NUMBER INSTALLED                             | | SYSTEM &                  |    -------------------------------------------- | | SEQUENCE          ITEM    |    | 3. NUMBER REQUIRED FOR DISPATCH            | | NUMBERS                   |    |    --------------------------------------- | | ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              | | 31  INDICATING/RECORDING  |    |    |                                       | |     SYSTEMS               |    |    |                                       | |                           |    |    |                                       | | 1.  Flight Data         A | 1  | 0  | May be inoperative provided:          | |     Recorder (FDR)        |    |    |     a) Cockpit Voice Recorder (CVR)   | |                           |    |    |        operates normally, and         | |                           |    |    |     b) Repairs are made within        | |                           |    |    |        three flight days.             | |                           |    |    |                                       | | 2.  Clocks              C | 2  | 1  | One may be inoperative at either      | |                           |    |    | the pilot's or co-pilot's station.    | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | |                           |    |    |                                       | Page 46

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| U.S. DEPARTMENT OF TRANSPORTATION                                           | |                                                                             | |                                            MASTER MINIMUM EQUIPMENT LIST    | | FEDERAL AVIATION ADMINISTRATION                                             | | --------------------------------------------------------------------------- | | AIRCRAFT:                                | REVISION NO: 14       | PAGE:    | |                  DHC-7                   |                       |          | |                                          | DATE: 06/16/1994      | 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           C | 1  | 0  | (O)May be inoperative provided:       | |     System                |    |    |     a) Operations are limited to      | |                           |    |    |        dry hard surfaced runways,     | |                           |    |    |     c) Operations are conducted in    | |                           |    |    |        compliance with the AFM, and   | |                           |    |    |     d) Anti-Skid system remains       | |                           |    |    |        OFF.                           | |                           |    |    |                                       | | 2.  Parking Brake       C | 2  | 1  | (O)Either the flight deck indicator   | |     Pressure Indicators   |    |    | or the nacelle mounted indicator      | |                           |    |    | may be inoperative provided brake     | |                           |    |    | pressure is verified adequate for     | |                           |    |    | the associated system before          | |                           |    |    | engine start.                         | |                           |    |    |                                       | Page 47