Microsoft Word - BE-99 R7.doc

Date: 01/25/2007

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

BEECHCRAFT MODEL 99 SERIES

FEDERAL AVIATION ADMINISTRATION AIRCRAFT EVALUATION GROUP, MKC-AEG 901 LOCUST STREET, ROOM 332

KANSAS CITY, MISSOURI 64106-2641

TELEPHONE: (816) 329-3233

FAX: (816) 329-3241

DEPARTMENT OF TRANSPORTATION Revision: 7

Revision: 7

MASTER MINIMUM EQUIPMENT LIST Date: 01/25/2007

BEECHCRAFT MODEL 99 SERIES

Table of Contents

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

-- Guidelines for (O) & (M) Procedures XVI, XVII, XVIII, XIX 21 Air Conditioning 21-1, 2, 3

22 Auto Flight 22-1

23 Communications 23-1, 2, 3

24 Electrical Power 24-1

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

26 Fire Protection 26-1

27 Flight Controls 27-1, 2

28 Fuel 28-1, 2, 3

30 Ice and Rain Protection 30-1, 2

31 Indicating/Recording Systems 31-1, 2

32 Landing Gear 32-1

33 Lights 33-1, 2

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

35 Oxygen 35-1 36 Pneumatic 36-1 37 Vacuum/Pressure 37-1 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

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Log of Revisions

� REV.NO. � DATE � PAGE NUMBERS � INITIALS �

� ORIGINAL � 12/18/1981 � � � � 1 � 08/30/1984 � 34-1, 34-2, 82-1 � � � 2 � 03/14/1985 � All Pages � � � 3 � 03/16/1989 � All Pages � � � 4 � 06/22/1989 � HIGHLIGHTS OF REV.,DEFINITIONS � � � 4 � 06/22/1989 � PREAMBLE � � � 5 � 05/24/1991 � HIGHLIGHTS OF REV.,DEFINITIONS � � � 5 � 05/24/1991 � GUIDELINES � � � 5 � 05/24/1991 � 21-1,21-2,23-1,24-1,25-1 � � � 5 � 05/24/1991 � 25-2,26-1,27-1,28-1,28-3 � � � 5 � 05/24/1991 � 30-1,30-2,31-1,32-1,33-1 � � � 5 � 05/24/1991 � 33-2,34-1,34-2,34-3,34-4 � � � 5 � 05/24/1991 � 34-5,35-1,36-1,52-1,61-1 � � � 5 � 05/24/1991 � 73-1,77-1,79-1 � � � 6 � 06/13/1994 � HIGHLIGHTS OF REV.,DEFINITIONS � � � 6 � 06/13/1994 � GUIDELINES � � � 6 � 06/13/1994 � 21-1,21-2,22-1,23-1,23-2 � � � 6 � 06/13/1994 � 24-1,25-1,25-2,26-1,27-1 � � � 6 � 06/13/1994 � 28-1,28-2,28-3,30-1,30-2 � � � 6 � 06/13/1994 � 31-1,32-1,33-1,33-2,34-1 � � � 6 � 06/13/1994 � 34-2,34-3,34-4,34-5,35-1 � � � 6 � 06/13/1994 � 36-1,37-1,52-1,61-1,73-1 � � � 6 � 06/13/1994 � 77-1,79-1,82-1 � � � 7 � 01/25/2007 � HIGHLIGHTS OF REV.,DEFINITIONS � � � 7 � 01/25/2007 � GUIDELINES � � � 7 � 01/25/2007 � 21-1,21-2,21-3,22-1,23-1 � � � 7 � 01/25/2007 � 23-2,23-3,24-1,25-1,25-2 � � � 7 � 01/25/2007 � 25-3,25-4,26-1,27-1,27-2 � � � 7 � 01/25/2007 � 28-1,28-2,28-3,30-1,30-2 � � � 7 � 01/25/2007 � 31-1,31-2,32-1,33-1,33-2 � � � 7 � 01/25/2007 � 34-1,34-2,34-3,34-4,34-5 � � � 7 � 01/25/2007 � 34-6,34-7,34-8,36-1,52-1 � � � 7 � 01/25/2007 � 79-1 � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � �

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Control Page

SYSTEM PAGE REV NO. CURRENT DATE

Cover Page - 7 01/25/2007 Table of Contents I 7 01/25/2007 Log of Revisions II 7 01/25/2007 Control Page III 7 01/25/2007 IV 7 01/25/2007 Highlights of Change V 7 01/25/2007 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 XV 2 06/14/1989 Guidelines for (O) & (M) Procedures XVI 7 01/25/2007 XVII 7 01/25/2007 XVIII 7 01/25/2007 XIX 7 01/25/2007 21 21-1 7 01/25/2007 21-2 7 01/25/2007 21-3 7 01/25/2007 22 22-1 7 01/25/2007 23 23-1 7 01/25/2007 23-2 7 01/25/2007 23-3 7 01/25/2007 24 24-1 7 01/25/2007 25 25-1 7 01/25/2007 25-2 7 01/25/2007 25-3 7 01/25/2007 25-4 7 01/25/2007 26 26-1 7 01/25/2007 27 27-1 7 01/25/2007 27-2 7 01/25/2007 28 28-1 7 01/25/2007 28-2 7 01/25/2007 28-3 7 01/25/2007 30 30-1 7 01/25/2007 30-2 7 01/25/2007

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Control Page

SYSTEM PAGE REV NO. CURRENT DATE

31 31-1 7 01/25/2007 31-2 7 01/25/2007 32 32-1 7 01/25/2007 33 33-1 7 01/25/2007 33-2 7 01/25/2007 34 34-1 7 01/25/2007 34-2 7 01/25/2007 34-3 7 01/25/2007 34-4 7 01/25/2007 34-5 7 01/25/2007 34-6 7 01/25/2007 34-7 7 01/25/2007 34-8 7 01/25/2007 35 35-1 6 06/13/1994 36 36-1 7 01/25/2007 37 37-1 6 06/13/1994 52 52-1 7 01/25/2007 61 61-1 6 06/13/1994 73 73-1 6 06/13/1994 77 77-1 6 06/13/1994 79 79-1 7 01/25/2007 82 82-1 6 06/13/1994

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Highlights of Change

Revision 7 changes are marked with change bars on each page with revised items of MMEL relief. Many new items of relief have been added based on numerous requests for additional relief. Many items have

been updated in accordance with current Policy Letters. Revision 7 changes affect most of the BE-99 MMEL.

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BEECHCRAFT MODEL 99 SERIES

Definitions

1. System Definitions.

System numbers are based on the Air Transport Association (ATA) Specification Number 100 and items are numbered sequentially.

a. "Item" (Column 1) means the equipment, system, component, or function listed in the "Item" column.

b. "Number Installed" (Column 2) is the number

(quantity) of items normally installed in the aircraft. This number represents the aircraft configuration considered in developing this MMEL. Should the number be a variable (e.g., passenger cabin items) a number is not required.

�

c. "Number Required for Dispatch" (Column 3) is the minimum number (quantity) of items required for operation provided the conditions specified in Column 4 are met.

NOTE: Where the MMEL shows a variable number required for dispatch, the MEL must reflect the actual number required for dispatch or an alternate means of configuration control approved by the Administrator.

d. "Remarks or Exceptions" (Column 4) in this column includes a statement either prohibiting or permitting operation with a specific number of items inoperative, provisos (conditions and limitations) for such operation, and appropriate notes.

e. A vertical bar (change bar) in the margin

indicates a change, addition or deletion in the adjacent text for the current revision of that page only. The change bar is dropped at the next revision of that page.

2. "Airplane/Rotorcraft Flight Manual" (AFM/RFM) is the document required for type certification and approved by the responsible FAA Aircraft Certification Office. The FAA approved AFM/RFM for the specific aircraft is listed on the applicable Type

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Definitions

Certificate Data Sheet.

3. "As required by FAR" means that the listed item is subject to certain provisions (restrictive or permissive) expressed in the Federal Aviation Regulations operating rules. The number of items required by the FAR must be operative. When the listed item is not required by FAR it may be inoperative for time specified by repair category.

4. Each inoperative item must be placarded to inform and remind the crewmembers and maintenance personnel of the equipment condition.

NOTE: To the extent practical, placards should be located adjacent to the control or indicator for the item affected; however, unless otherwise specified, placard wording and location will be determined by the operator.

5. "-" symbol in Column 2 and/or Column 3 indicates a variable number (quantity) of the item installed.

�

6. "Deleted" in the remarks column after a sequence item indicates that the item was previously listed but is now required to be operative if installed in the aircraft.

7. "ER" refers to extended range operations of a two-engine

airplane which has a type design approval for ER operations and complies with the provisions of Advisory Circular 120-42A. �

8. "Federal Aviation Regulations" (FAR) means the applicable portions of the Federal Aviation Act and Federal Aviation Regulations.

9. "Flight Day" means a 24 hour period (from midnight to midnight) either Universal Coordinated Time (UCT) or local time, as established by the operator, during which at least one flight is initiated for the affected aircraft.

10. "Icing Conditions" means an atmospheric environment that may cause ice to form on the aircraft or in the engine(s).

11. Alphabetical symbol in Column 4 indicates a proviso (condition or limitation) that must be complied with for

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Definitions

operation with the listed item inoperative.

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

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

14. Inoperative components of an inoperative system:

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

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

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

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

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Definitions

required to be published as a part of the operator's manual or MEL.

NOTE: The (M) and (O) symbols are required in the operator's MEL unless otherwise authorized by the Administrator.

17. "Deactivated" and "Secured" means that the specified component must be put into an acceptable condition for safe flight. An acceptable method of securing or deactivating will be established by the operator.

18. "Visual Flight Rules" (VFR) is as defined in FAR Part 91. This precludes a pilot from filing an Instrument Flight Rules (IFR) flight plan.

19. "Visual Meteorological Conditions" (VMC) means the atmospheric environment is such that would allow a flight to proceed under the visual flight rules applicable to the flight. This does not preclude operating under Instrument Flight Rules.

20. "Visible Moisture" means an atmospheric environment containing water in any form that can be seen in natural or artificial light; for example, clouds, fog, rain, sleet, hail, or snow.

21. "Passenger Convenience Items" means those items related to passenger convenience, comfort or entertainment such as, but not limited to, galley equipment, movie equipment, ash trays, stereo equipment, overhead reading lamps, etc.

22. Repair Intervals: All users of an MEL approved under FAR 121, 125, 129 and 135 must effect repairs of inoperative systems or components, deferred in accordance with the MEL, at or prior to the repair times established by the following letter designators:

Category A. Items in this category shall be repaired within the time interval specified in the remarks column of the operator's approved MEL.

Category B. Items in this category shall be repaired within three (3) consecutive calendar days (72 hours), excluding the day the malfunction was recorded in the aircraft maintenance

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Definitions

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

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

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

The letter designators are inserted adjacent to Column 2.

23. Electronic fault alerting system - General � � New generation aircraft display system fault indications to the � flight crew by use of computerized display systems. Each � aircraft manufacturer has incorporated individual design � philosophies in determining the data that would be � represented. The following are customized definitions (specific� to each manufacturer) to help determine the level of messages � affecting the aircraft's dispatch status. When preparing the � MEL document, operators are to select the proper Definition No. � 23 for their aircraft, if appropriate. � � a. BOEING (B-757/767, B-747-400, B-777) � � Boeing airplanes equipped with Engine Indicating and Crew � Alerting Systems (EICAS), provide different priority levels of � system messages (WARNING, CAUTION, ADVISORY, STATUS and � MAINTENANCE). Any messages that affects airplane dispatch � status will be displayed at a STATUS message level or higher. � The absence of an EICAS STATUS or higher level (WARNING, � CAUTION, ADVISORY) indicates that the system/component is � operating within its approved operating limits or tolerances. � � System conditions that result only in a maintenance level � message, i.e. no correlation with a higher level EICAS message, �

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do not affect dispatch and do not require action other than as � addressed within an operators standard maintenance program. � � b. DOUGLAS (MD-11) � � Some Douglas aircraft are equipped with an alerting function � which is a subsystem within the Electronic Instrument System � (EIS). The alerting function provides various levels of system � condition alerts (WARNING, CAUTION, ADVISORY, MAINTENANCE and � STATUS). � � Alerts that affect aircraft dispatch will include WARNING, � CAUTION, STATUS or MAINTENANCE level. MAINTENANCE alerts are � displayed on the status page of the EIS display panel under the � maintenance heading. � � A MAINTENANCE alert on the EIS indicates the presence of a � system fault which can be identified by the Central Fault � Display System (CFDS) interrogation. The systems are designed � to be fault tolerant, however, for any MAINTENANCE alert, the � MEL must be verified for dispatch purposes. � � c. AIRBUS (A-300-600, A-310, A-320/319/321, A-330, A-340 � � Airbus aircraft equipped with Electronic Centralized Aircraft � Monitoring (ECAM) provide different levels of system condition � messages (WARNING, CAUTION, STATUS, and ADVISORY). A-320/319/ � 321, A-330, and A-340 also provide MAINTENANCE status messages. � � Any message that effects airplane dispatchability will normally � be at the WARNING, CAUTION or STATUS level. MAINTENANCE � messages (A-320/319/321, A-330, and A-340 only) are also � indicated on ECAM Status Page below the white Maintenance label.� � A MAINTENANCE status (Class II) message on ECAM indicates the � presence of a system fault which can be identified by CFDS � (A-320/319/321) or CMS (A-330/A-340) interrogation. The systems � are designed to be fault tolerant, however for any MAINTENANCE � status (Class II) message, the A-320/319/321 MEL must be � verified for dispatch capability. For the A-330 and A-340, � MAINTENANCE status messages do not affect dispatch. �

d. FOKKER (FK-100) �

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Definitions

�

Fokker aircraft are equipped with Multi Function Display System � (MFDS) which provides electronic message referring to the � different priority levels of system information (WARNING (red), � CAUTION (amber), AWARENESS (cyan) AND STATUS (white). Any � messages that affects aircraft dispatch will be at the WARNING, � CAUTION or AWARENESS level. In these cases the MEL must be � verified for dispatch capability and maintenance may be � required. � � System conditions that only require maintenance are not � presented on the flight deck. These maintenance � indications/messages may be presented on the Maintenance & Test � Panel (MAP) or the Centralized Fault Display Unit (CFDU) and by � dedicated Built In Test Evaluation (BITE) of systems. �

24. "Administrative control item" means an item listed by the operator in the MEL for tracking and informational purposes. It may be added to an operator's MEL by approval of the Principal Operations Inspector provided no relief is granted, or provided conditions and limitations are contained in an approved document (i.e. Structural Repair Manual, airworthiness directive, etc.). If relief other than that granted by an approved document is sought for an administrative control item, a request must be submitted to the Administrator. If the request results in review and approval by the FOEB, the item becomes an MMEL item rather than an administrative control item.

25. "***" symbol in Column 1 indicates an item which is not required by regulation but which may have been installed on some models of aircraft covered by this MMEL. This item may be included on the operator's MEL after the approving office has determined that the item has been installed on one or more of the operator's aircraft. The symbol, however, shall not be carried forward into the operator's MEL. It should be noted that neither this policy nor the use of this symbol provide authority to install or remove an item from an aircraft.

26. "Excess Items" means those items that have been installed that are redundant to the requirements of the FARs.

27. "Day of Discovery" is the calendar day an equipment/instrument malfunction was recorded in the aircraft

D."

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Definitions

maintenance log and or record. This day is excluded from the calendar days or flight days specified in the MMEL for the repair of an inoperative item of equipment. This provision is applicable to all MMEL items, i.e., categories "A, B, C, and

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BEECHCRAFT MODEL 99 SERIES

Preamble

(Effective 6/14/89)

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

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

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

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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.

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21-1-3

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Guidelines for (O) & (M) Procedures

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

21-1-1(M) Maintenance procedure to ensure no fuel leak or

mechanical/electrical fault exists and deactivate heater.

21-1-1(O) Operations procedure to identify acceptable conditions 21-1-2 to operate without affected heat in the aircraft.

21-6 (M) Maintenance procedure to secure air conditioner to ensure fault will not affect other system.

21-12 (M) Maintenance procedure to ensure bleed air shutoff valve(s) 21-13 are in the closed position.

21-13 (O) Operations procedure to identify acceptable conditions to operate without heat in the aircraft.

22-1 (M) Maintenance procedure to ensure no electrical or

mechanical fault exists that will have an adverse affect on any flight control function.

22-1-1(M) Maintenance procedure to verify remaining autopilot

functions to maintain constant altitude and direction are available and placard for crew awareness.

(O) Establish alternate procedures for autopilot use with inoperative autopilot functions.

22-2 (M) Maintenance procedure to ensure no electrical or

mechanical fault exists that will have an adverse affect on any flight control function.

23-1-1(O) Operations procedure for briefing the passengers.

24-4 (M) Maintenance procedure to verify items on the now single fed buss are operative.

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Guidelines for (O) & (M) Procedures

24-8 (M) Maintenance procedure to verify the External Power Solinoid is not powered.

24-8-1(O) Operations procedure for crew to verify correct external

power is used and verify external power is disconnect and recepticle door is closed prior to flight.

25-2-2(O) Operations procedure for crew awareness of inoperative

baggage stowage area and alternate procedures for baggage.

25-4-1(M) Maintenance procedure disconnect ELT Remote Switch and verify ELT is operative in the ARMED mode.

25-8 (M) Maintenance procedure to secure and placard compartment.

25-9 (M) Maintenance procedure to determine acceptable cargo loading limits with inoperative restraints.

26-2 (M) Maintenance procedure to deactivate system and ensure Engine Fire Lights are extinguished prior to operation of aircraft.

27-4 (O) Operations procedure for crew to verify operation of

Main and Standby Pitch Trim, Trim in Motion warning,

Out of Trim warning, and to visually verify the Stabilizer Pitch Trim Position, prior to each takeoff.

28-1-2(O) Procedure to verify crossfeed is operative prior to each flight.

28-3 (O) Operations procedure to ensure the quantity and balance

of fuel on board meets the regulatory requirements for the intended flight.

28-4 (O) Operations procedure to verify NO MTV FLOW annunciator is operative and nacelle fuel quantify is monitored.

28-7-1(O) Operations procedure to verify both the Primary and Secondary fuel boost pumps are operative and both are operated for the entire flight.

28-7-2(O) Operations procedure to verify the NO MTV FLOW annunciator and standby boost pump are both operative prior to flight.

30-9 (M) Maintenance procedure to secure valves in off position.

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Guidelines for (O) & (M) Procedures

31-2 (O) Operations procedure for recording flight time.

31-3 (O) Operations procedure for recording combustion heater use time.

32-1 (O) Operator must use procedure published by Raytheon Aircraft Company to verify the landing gear is down and locked with an inoperative gear indicator.

32-3 (M) Maintenance procedure to ensure nose steering is disconnected.

32-4 (O) Operations procedure to prevent movement of aircraft when stopped or parked.

32-6 (O) Operations procedure for crew awareness and procedure to

manually release gear handle downlock to retract landing gear

33-3 (O) Operations procedure to specify passenger briefing.

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

34-17 (M) Maintenance procedure to deactivate and secure the system.

34-17-2(O) Operations procedure for crew awareness of inoperative RA

mode and procedures to select and operate in TA model only.

34-17-3(O) Operations procedure to verify RA mode is operative and procedures to select and operate in RA mode only.

34-19 (O) Operations procedure for crew awareness and flight planning for aircraft altitude, performance and terrain clearance.

34-19-1-a(O) Operations procedure to ensure alternatives are

established and used for the appropriate inoperative mode(s).

34-19-1-d(O) Operations procedure to ensure alternatives are established for inoperative Advisory Callouts.

34-19-1-e(O) Operations procedure to ensure alternatives are

established and used for windshear avoidance and recovery procedures.

Revision: 7

MASTER MINIMUM EQUIPMENT LIST Date: 01/25/2007

BEECHCRAFT MODEL 99 SERIES

Guidelines for (O) & (M) Procedures

34-19-2(O) Operations procedure for crew awareness and flight planning for terrain avoidance with inoperative FLTA/PDA.

36-1 (M) Maintenance procedure to determine bleed air shutoff valve(s) are in closed position..

52-1 (O) Operations procedure to brief the passengers to remain seated with their seatbelt fasten for entire duration

of the flight and except for an emergency, only the crew will operate the cabin door.

61-2 (O) Operations procedure to ensure prop levers are full forward prior to landing.

FEDERAL AVIATION ADMINISTRATION Page XIX

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� U.S. DEPARTMENT OF TRANSPORTATION �

� MASTER MINIMUM EQUIPMENT LIST � � FEDERAL AVIATION ADMINISTRATION � � --------------------------------------------------------------------------- � � AIRCRAFT: � REVISION NO: 7 � PAGE: � � � � � � BEECHCRAFT MODEL 99 SERIES � DATE: 01/25/2007 � 21-1 � � --------------------------------------------------------------------------- � � 1. � 2. NUMBER INSTALLED � � SYSTEM & � -------------------------------------------- � � SEQUENCE ITEM � � 3. NUMBER REQUIRED FOR DISPATCH � � NUMBERS � � --------------------------------------- � � ------------------------- � � � 4. REMARKS OR EXCEPTIONS � � 21 AIR CONDITIONING � � � � � � � � � � � � � � � 1. Heater � � � � � 1)Combustion C � 1 � 0 � (O)(M)May be inoperative provided | � � (Except C-99) � � � heater is deactivated. | � � � � � � � 2)Bleed Air Heat C � 1 � 0 � (O)May be inoperative provided: | � � (C-99 only) � � � a)Operating conditions are | � � � � � acceptable without heat, and | � � � � � b)Both Environmental Bleed Air | � � � � � Valves remain ENVIR OFF. | � � � � � � � *** 3)Auxilary Bleed C � 1 � 0 � (O)May be inoperative provided: | � � Air Heat System � � � a)Operating conditions are | � � (Except C-99) � � � acceptable without heat, and | � � � � � b)Left Engine Bleed Air Shutoff | � � � � � Valve remains OFF and closed. | � � � � � � � 2. Forward C � 1 � 0 � May be inoperative provided: � � Ventilation � � � a) Cumbustion Heater is not � � Blower � � � operated on the ground, � � � � � b) Combustion Heater in turned � � � � � off prior to landing, � � � � � c) Electric Heater is not � � � � � operated, and � � � � � d) Windshield defrost air is � � � � � not required. � � 3. Aft Ventilation C � 1 � 0 � � � Blower � � � � � � � � � � 4. Automatic C � 1 � 0 � May be inoperative provided Manual � � Temperature Control � � � Temperature Control is operative. � � � � � � � 5. Manual Temperature C � 1 � 0 � May be inoperative provided | � � Control � � � Automatic Temperature Control | � � � � � is operative. | � � � � � � � C � 1 � 0 � May be inoperative provided: | � � � � � a)Heater is considered | � � � � � inoperative, and | � � � � � b)Item 21-1, Heater, | � � � � � is complied with. | �

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� U.S. DEPARTMENT OF TRANSPORTATION � � MASTER MINIMUM EQUIPMENT LIST � � FEDERAL AVIATION ADMINISTRATION � � --------------------------------------------------------------------------- � � AIRCRAFT: � REVISION NO: 7 � PAGE: � � � � � � BEECHCRAFT MODEL 99 SERIES � DATE: 01/25/2007 � 21-2 � � --------------------------------------------------------------------------- � � 1. � 2. NUMBER INSTALLED � � SYSTEM & � -------------------------------------------- � � SEQUENCE ITEM � � 3. NUMBER REQUIRED FOR DISPATCH � � NUMBERS � � --------------------------------------- � � ------------------------- � � � 4. REMARKS OR EXCEPTIONS � � 21 AIR CONDITIONING � � � � � � � � � � � � � � � 6. Air Conditioning C � 1 � 0 � (M) � � System � � � � � � � � � � 7. Windshield Defrost C � 1 � 0 � May be inoperative provided one of � � � � � the following is operative: � � � � � a) Ventilation Blower � � � � � b) Windshield Heat (electric) � � � � � c) Bleed Air Heat and � � � � � Ventilation Blower � � � � � d) Electric Heater and � � � � � Ventilation Blower � � � � � � � 8. Duct Over C � 1 � 0 � May be inoperative provided: � � Temperature � � � a) Both Environmental Valves � � Annunciator � � � are closed, and � � (C-99 only) � � � b) Ventilation Blower is � � � � � operative. � � � � � � � 9. Electric Heater C � 1 � 0 � May be inoperative provided | � � *** � � � Electric Heater remains OFF. | � � � � � � � 10. Auxiliary Bleed � � � Moved to Item 21-1 Revision 7. | � � *** Air Heat System � � � | � � � � � � � 11. Ram Air Vent C � 1 � 0 � � � (C-99 only) � � � � � � � � � � 12. Bleed Air Fail C � 2 � 1 � (M)May be inoperative provided: | � � Annunciator Lights � � � a)Affected side Environmental | � � (Fails to illuminate) � � � Bleed Air Valve remains | � � (C-99 only) � � � ENVIR OFF, and | � � � � � b)Affected side Environmental | � � � � � Bleed Air Valve is verified | � � � � � closed. | � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � �

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� U.S. DEPARTMENT OF TRANSPORTATION � � MASTER MINIMUM EQUIPMENT LIST � � FEDERAL AVIATION ADMINISTRATION � � --------------------------------------------------------------------------- � � AIRCRAFT: � REVISION NO: 7 � PAGE: � � � � � � BEECHCRAFT MODEL 99 SERIES � DATE: 01/25/2007 � 21-3 � � --------------------------------------------------------------------------- � � 1. � 2. NUMBER INSTALLED � � SYSTEM & � -------------------------------------------- � � SEQUENCE ITEM � � 3. NUMBER REQUIRED FOR DISPATCH � � NUMBERS � � --------------------------------------- � � ------------------------- � � � 4. REMARKS OR EXCEPTIONS � � 21 AIR CONDITIONING � � � � � � � � � � � � � � � 13. Environmental Bleed C � 2 � 1 � (M)One may be inoperative provided: | � � Air Shutoff Valve(s) � � � a)Affected valve remains OFF, | � � (C-99 Only) � � � and | � � � � � b)Affected Valve is verified | � � � � � closed. | � � � � � � � � 2 � 0 � (O)(M)Both may be inoperative | � � � � � provided: | � � � � � a)Both valves remain OFF, | � � � � � b)Both valves are verified | � � � � � closed, and | � � � � � c)Operating conditions are | � � � � � acceptable without heat. | � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � �

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� U.S. DEPARTMENT OF TRANSPORTATION � � MASTER MINIMUM EQUIPMENT LIST � � FEDERAL AVIATION ADMINISTRATION � � --------------------------------------------------------------------------- � � AIRCRAFT: � REVISION NO: 7 � PAGE: � � � � � � BEECHCRAFT MODEL 99 SERIES � DATE: 01/25/2007 � 22-1 � � --------------------------------------------------------------------------- � � 1. � 2. NUMBER INSTALLED � � SYSTEM & � -------------------------------------------- � � SEQUENCE ITEM � � 3. NUMBER REQUIRED FOR DISPATCH � � NUMBERS � � --------------------------------------- � � ------------------------- � � � 4. REMARKS OR EXCEPTIONS � � 22 AUTO FLIGHT � � � � � � � � � � � � � � � 1. Autopilot C � - � 0 � (M)May be inoperative provided | � � *** � � � operations do not require its use. | � � � � � � � C � 2 � 1 � One may be inoperative provided | � � � � � approach procedures do not require | � � � � � dual autopilot operation. | � � � � � � � 1)Autopilot Modes C � - � 2 � (M)(O)Individual Autopilot Modes | � � � � � may be inoperative provided: | � � � � � a)Operations do not require | � � � � � use of the affected mode(s), | � � � � � b)Remaining modes are capable | � � � � � of maintaining a constant | � � � � � altitude and direction, and | � � � � � c)Autopilot is not used for | � � � � � any segment of an approach. | � � � � � � � 2. Yaw Damper C � - � 0 � (M) | � � *** � � � � � � � � � � 3. Autopilot C � - � 0 � May be inoperative provided | � � Disconnect � � � autopilot is not utilized at less | � � � � � than initial approach altitude. | � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � �

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� U.S. DEPARTMENT OF TRANSPORTATION � � MASTER MINIMUM EQUIPMENT LIST � � FEDERAL AVIATION ADMINISTRATION � � --------------------------------------------------------------------------- � � AIRCRAFT: � REVISION NO: 7 � PAGE: � � � � � � BEECHCRAFT MODEL 99 SERIES � DATE: 01/25/2007 � 23-1 � � --------------------------------------------------------------------------- � � 1. � 2. NUMBER INSTALLED � � SYSTEM & � -------------------------------------------- � � SEQUENCE ITEM � � 3. NUMBER REQUIRED FOR DISPATCH � � NUMBERS � � --------------------------------------- � � ------------------------- � � � 4. REMARKS OR EXCEPTIONS � � 23 COMMUNICATIONS � � � � � � � � � � � � � � � 1. Passenger Address � � � � � System � � � � � � � � � � 1) Passenger C � 1 � 0 � (O)May be inoperative provided: | � � Configuration � � � a) PA not required by FAR, and | � � � � � b) Alternate, normal and | � � � � � emergency procedures, and/or | � � � � � operating restrictions are | � � � � � established and used. | � � � � � � � � � � NOTE: Any station that operates | � � � � � normally may be used. | � � � � � � � 2)Cargo D � 1 � 0 � May be inoperative provided | � � Configuration � � � procedures do not require its use. | � � � � � � � 2. Communications D � - � - � Any in excess of those required by | � � Equipment � � � FAR may be inoperative provided it | � � (VHF, UHF) � � � is not powered by an emergency | � � � � � power source and is not required | � � � � � for emergency operations. | � � � � � � � 3. Cockpit Speakers C � 2 � 0 � May be inoperative provided an � � � � � operative headset is used by each � � � � � flight crew member. � � � � � � � 4. Audio Amplifier C � 1 � 0 � May be inoperative provided an � � � � � operative headset is used by each � � � � � flight crew member. � � � � � � � � � � � � 5. Static Discharge C � - � - � No more than one wick may be � � Wicks � � � missing on any one surface. � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � �

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� U.S. DEPARTMENT OF TRANSPORTATION � � MASTER MINIMUM EQUIPMENT LIST � � FEDERAL AVIATION ADMINISTRATION � � --------------------------------------------------------------------------- � � AIRCRAFT: � REVISION NO: 7 � PAGE: � � � � � � BEECHCRAFT MODEL 99 SERIES � DATE: 01/25/2007 � 23-2 � � --------------------------------------------------------------------------- � � 1. � 2. NUMBER INSTALLED � � SYSTEM & � -------------------------------------------- � � SEQUENCE ITEM � � 3. NUMBER REQUIRED FOR DISPATCH � � NUMBERS � � --------------------------------------- � � ------------------------- � � � 4. REMARKS OR EXCEPTIONS � � 23 COMMUNICATIONS � � � � � � � � � � � � � � � 6. Cockpit Voice A � 1 � 0 � May be inoperative provided: | � � Recorder (CVR) � � � a) Flight Data Recorder (FDR) | � � (With Flight Data � � � operates normally, and | � � Recorder) � � � b) Repairs are made within | � � � � � three flight days. | � � � � � � � D � - � - � Any in excess of those required by | � � � � � FAR may be inoperative. | � � � � � � � Cockpit Voice A � 1 � 0 � May be inoperative provided | � � Recorder (CVR) � � � repairs are made within | � � (Without Flight Data � � � three flight days. | � � Recorder) � � � | � � D � - � - � Any in excess of those required by | � � � � � FAR may be inoperative. | � � � � � � � Cockpit Voice A � 1 � 0 � May be inoperative provided | � � Recorder (CVR) � � � repairs are made in accordance | � � (Non-Certificated � � � with applicable FARs. | � � operator) � � � | � � � � � � � 7. Boom Microphones � � � � � COCKPIT VOICE � � � � � RECORDER (CVR) WITH � � � � � FLIGHT DATA RECORDER � � � � � (FDR) INSTALLED � � � | � � � � � � � 1) Cockpit Voice A � - � 0 � May be inoperative provided: � � Recorder equipped � � � a) Flight Data Recorder (FDR) � � to record Boom � � � operates normally and � � Microphone per � � � b) Repairs are made within � � FAR 135.151(d) � � � three flight days. � � � � � � � *** 2) Cockpit Voice D � - � 0 � Any in excess of those required by | � � Recorder not � � � FAR may be inoperative. | � � equipped to record � � � � � Boom Microphone � � � � � � � � � � � � � � � (continued) � � � �

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� U.S. DEPARTMENT OF TRANSPORTATION � � MASTER MINIMUM EQUIPMENT LIST � � FEDERAL AVIATION ADMINISTRATION � � --------------------------------------------------------------------------- � � AIRCRAFT: � REVISION NO: 7 � PAGE: � � � � � � BEECHCRAFT MODEL 99 SERIES � DATE: 01/25/2007 � 23-3 � � --------------------------------------------------------------------------- � � 1. � 2. NUMBER INSTALLED � � SYSTEM & � -------------------------------------------- � � SEQUENCE ITEM � � 3. NUMBER REQUIRED FOR DISPATCH � � NUMBERS � � --------------------------------------- � � ------------------------- � � � 4. REMARKS OR EXCEPTIONS � � 23 COMMUNICATIONS � � � � � � � � � � � � � � � 7. Boom Microphone(CONT) � � � � � CVR WITHOUT FDR � � � � � INSTALLED. � � � � � � � � � � 1) Cockpit Voice A � - � 0 � May be inoperative provided � � Recorder Equipped � � � repairs are made within three � � to record boom � � � flight days. � � microphone per � � � � � FAR 135.151(d) � � � � � � � � � � *** 2) Cockpit Voice D � - � 0 � Any in excess of those required by | � � Recorder not � � � FAR may be inoperative. | � � Equipped to record � � � � � Boom Microphone � � � � � � � � � � 8. High Frequency D � - � 0 � Any in excess of those required by | � � (HF) Communication � � � FAR may be inoperative. | � � System � � � | � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � �

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� U.S. DEPARTMENT OF TRANSPORTATION � � MASTER MINIMUM EQUIPMENT LIST � � FEDERAL AVIATION ADMINISTRATION � � --------------------------------------------------------------------------- � � AIRCRAFT: � REVISION NO: 7 � PAGE: � � � � � � BEECHCRAFT MODEL 99 SERIES � DATE: 01/25/2007 � 24-1 � � --------------------------------------------------------------------------- � � 1. � 2. NUMBER INSTALLED � � SYSTEM & � -------------------------------------------- � � SEQUENCE ITEM � � 3. NUMBER REQUIRED FOR DISPATCH � � NUMBERS � � --------------------------------------- � � ------------------------- � � � 4. REMARKS OR EXCEPTIONS � � 24 ELECTRICAL POWER � � � � � � � � � � � � � � � 1. DC Loadmeters � � � DELETED, REVISION 5. � � � � � � � 2. Generator Warning B � 2 � 0 � May be inoperative provided both � � Lights � � � DC Loadmeters are monitored. � � � � � � � 3. Inverter Warning B � 1 � 0 � May be inoperative provided an AC � � Light � � � Volt/Frequency meter is installed � � � � � and operative. � � � � � � � 4. Bus Feeder Limiter B � 4 � 3 � (M)One limiter may be open for VFR | � � (60 Amp) � � � day operations provided all bus � � (except C-99) � � � functions are operating properly. � � � � � � � � � � NOTE: For U-80 and after, the bus | � � � � � fault light ON indicates an | � � � � � open current limiter. | � � � � � � � 5. Inverter B � 2 � 1 � One may be inoperative for day � � � � � VMC operations. � � � � � � � 6. AC Volt/Frequency B � 1 � 0 � May be inoperative provided � � Meter � � � Inverter Warning Light is | � � (C-99 Only) � � � operative. | � � � � � � � 7. Nicad Battery C � 1 � 0 � May be inoperative provided the � � *** Temperature � � � Beech Battery Monitor System � � Indicator � � � is installed. � � � � � | � � C � 1 � 0 � May be inoperative provided NICAD � � � � � batteries are not installed. � � � � � � � 8. External Power C � 1 � 0 � (M) | � � System � � � � � � � � � � 1)External Power C � 1 � 0 � (O) | � � Annunciator System � � � | � � � � � � � � � � � � � � � � � � � � �

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� U.S. DEPARTMENT OF TRANSPORTATION � � MASTER MINIMUM EQUIPMENT LIST � � FEDERAL AVIATION ADMINISTRATION � � --------------------------------------------------------------------------- � � AIRCRAFT: � REVISION NO: 7 � PAGE: � � � � � � BEECHCRAFT MODEL 99 SERIES � DATE: 01/25/2007 � 25-1 � � --------------------------------------------------------------------------- � � 1. � 2. NUMBER INSTALLED � � SYSTEM & � -------------------------------------------- � � SEQUENCE ITEM � � 3. NUMBER REQUIRED FOR DISPATCH � � NUMBERS � � --------------------------------------- � � ------------------------- � � � 4. REMARKS OR EXCEPTIONS � � 25 EQUIPMENT/FURNISHINGS � � � � � � � � � � � � � � � 1. Cockpit Shoulder B � 2 � 1 � Right side may be inoperative � � Harness � � � provided seat is not occupied. � � � � � � � 2. Passenger Seat C � - � - � May be inoperative provided: | � � � � � a)Seat does not block an � � � � � Emergency Exit, � � � � � b)Seat does not restrict any | � � � � � passenger from access to the | � � � � � main aircraft aisle, and | � � � � � c)Affected seat(s) are blocked | � � � � � and placarded "DO NOT OCCUPY" | � � � � � � � � � � NOTE 1: A seat with an inoperative � � � � � seat belt is considered � � � � � inoperative. � � � � � NOTE 2: Affected seat(s) may � � � � � include the seat(s) behind � � � � � and/or adjacent outboard � � � � � seats. � � � � � � � 1) Recline C � - � - � May be inoperative and seat � � Mechanism � � � occupied provided seat is secure � � � � � in the upright position. � � � � � � � 2) Underseat C � - � - � (O)May be inoperative provided: | � � Baggage � � � a)Baggage is not stowed under | � � Restraint Bars � � � seat with inopeative | � � � � � restraining bar, | � � � � � b)Associated seat is placarded | � � � � � "DO NOT STOW BAGGAGE UNDER | � � � � � THIS SEAT", and | � � � � � c)Procedures are established to | � � � � � alert crew of inoperative | � � � � � restraining bar. | � � � � � � � � � � � � � � � � � � � � � � � � � � � (continued) � � � �

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� U.S. DEPARTMENT OF TRANSPORTATION � � MASTER MINIMUM EQUIPMENT LIST � � FEDERAL AVIATION ADMINISTRATION � � --------------------------------------------------------------------------- � � AIRCRAFT: � REVISION NO: 7 � PAGE: � � � � � � BEECHCRAFT MODEL 99 SERIES � DATE: 01/25/2007 � 25-2 � � --------------------------------------------------------------------------- � � 1. � 2. NUMBER INSTALLED � � SYSTEM & � -------------------------------------------- � � SEQUENCE ITEM � � 3. NUMBER REQUIRED FOR DISPATCH � � NUMBERS � � --------------------------------------- � � ------------------------- � � � 4. REMARKS OR EXCEPTIONS � � 25 EQUIPMENT/FURNISHINGS � � � � � � � � � � � � � � � 2. Passenger Seat (cont) � � � � � � � � � � 3) Armrest C � - � - � May be inoperative or missing and | � � � � � seat occupied provided: | � � � � � a)Armrest does not block an | � � � � � Emergency Exit, | � � � � � b)Armrest does nor restrict any | � � � � � passenger from access to the | � � � � � main aircraft aisle, and | � � � � � c)For an armrest with a recline | � � � � � mechanism, seat is secure | � � � � � in the upright position. | � � � � � � � 3. Flotation D � - � - � Any in excess of those required by | � � *** Equipment � � � FAR may be missing provided | � � � � � required distribution is maintained | � � � � � � � 4. Emergency Locator C � 1 � 0 � As required by FAR. � � Transmitter (ELT) � � � � � � � � | � � 1) Remote Switch C � 1 � 0 � (M) May be inoperative provided: | � � � � � a) Remote switch is | � � � � � disconnected from the ELT, | � � � � � and | � � � � � b) ELT switch is placed in the | � � � � � ARMED position. | � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � �

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� U.S. DEPARTMENT OF TRANSPORTATION � � MASTER MINIMUM EQUIPMENT LIST � � FEDERAL AVIATION ADMINISTRATION � � --------------------------------------------------------------------------- � � AIRCRAFT: � REVISION NO: 7 � PAGE: � � � � � � BEECHCRAFT MODEL 99 SERIES � DATE: 01/25/2007 � 25-3 � � --------------------------------------------------------------------------- � � 1. � 2. NUMBER INSTALLED � � SYSTEM & � -------------------------------------------- � � SEQUENCE ITEM � � 3. NUMBER REQUIRED FOR DISPATCH � � NUMBERS � � --------------------------------------- � � ------------------------- � � � 4. REMARKS OR EXCEPTIONS � � 25 EQUIPMENT/FURNISHINGS � � � � � � � � � � � � � � � 5. Non-Essential � � � � � Equipment and � � � � � Furnishings (NEF) � � � � � � � � � � *** 1)Passenger � - � 0 � Passenger convenience items, as � � Convenience Items � � � expressed in this MMEL are those � � (Expires 12/31/2007) � � � related to passenger convenience, | � � � � � comfort or entertainment such as � � � � � but not limited to, galley � � � � � equipment, movie equipment, ash � � � � � trays, stereo equipment, overhead � � � � � reading lamps, etc. Items � � � � � addressed elsewhere in this � � � � � document shall not be included. � � � � � (M) and (O) procedures may be � � � � � required and included in the air � � � � � carrier's appropriate document. � � � � � � � *** 2)Non-Essential � - � 0 � May be inopertive, damaged or | � � Equipment & � � � missing provided that the item(s) | � � Furnishings � � � is deferred in accordance with the | � � (NEF) � � � operator's NEF deferral program. | � � � � � The NEF program, procedures and | � � � � � processes are outlined in the | � � � � � operator's (insert name) Manual. | � � � � � (M) and (O) procedures, if | � � � � � required, must be available to the | � � � � � flight crew and included in the | � � � � � operator's appropriate document. | � � � � � � � � � � NOTE: Exterior Lavatory Door | � � � � � Ash Trays are not considered | � � � � � NEF items. | � � � � � � � 6. Emergency Medical D � - � - � Any in excess of those required by | � � *** Equipment � � � FAR may be incomplete or missing | � � � � � provided required distribution is | � � � � � maintained. | � � � � � � � � � � �

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� U.S. DEPARTMENT OF TRANSPORTATION � � MASTER MINIMUM EQUIPMENT LIST � � FEDERAL AVIATION ADMINISTRATION � � --------------------------------------------------------------------------- � � AIRCRAFT: � REVISION NO: 7 � PAGE: � � � � � � BEECHCRAFT MODEL 99 SERIES � DATE: 01/25/2007 � 25-4 � � --------------------------------------------------------------------------- � � 1. � 2. NUMBER INSTALLED � � SYSTEM & � -------------------------------------------- � � SEQUENCE ITEM � � 3. NUMBER REQUIRED FOR DISPATCH � � NUMBERS � � --------------------------------------- � � ------------------------- � � � 4. REMARKS OR EXCEPTIONS � � 25 EQUIPMENT/FURNISHINGS � � � � � � � � � � � � � � � 7. "Fasten Seat Belt C � - � - � One or more signs may be illegible | � � While Seated" � � � or missing provided a legible sign | � � Sign or Placard � � � or placard is visible from each | � � � � � occupied passenger seat. | � � � � � � � 8. Galley Storage C � - � - � (M) May be inoperative provided: | � � *** Compartment(s) � � � a) Procedures are established | � � � � � to secure compartment | � � � � � CLOSED, | � � � � � b) Compartment is not used for | � � � � � storage of emergency | � � � � � equipment, and | � � � � � c) Affected compartment is not | � � � � � used for storage of any | � � � � � item(s) except for those | � � � � � permanently affixed. | � � � � � � � 9. Cargo Restraint C � - � - � (M)May be inoperative or missing | � � *** Systems � � � provided acceptable cargo loading | � � � � � limits from an approved source, | � � � � � i.e. Approved Cargo Loading Manual | � � � � � or Weight and Balance Manual are | � � � � � observed. | � � � � � � � C � - � - � May be inoperative or missing | � � � � � provided affected cargo section | � � � � � remains empty. | � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � �

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� U.S. DEPARTMENT OF TRANSPORTATION � � MASTER MINIMUM EQUIPMENT LIST � � FEDERAL AVIATION ADMINISTRATION � � --------------------------------------------------------------------------- � � AIRCRAFT: � REVISION NO: 7 � PAGE: � � � � � � BEECHCRAFT MODEL 99 SERIES � DATE: 01/25/2007 � 26-1 � � --------------------------------------------------------------------------- � � 1. � 2. NUMBER INSTALLED � � SYSTEM & � -------------------------------------------- � � SEQUENCE ITEM � � 3. NUMBER REQUIRED FOR DISPATCH � � NUMBERS � � --------------------------------------- � � ------------------------- � � � 4. REMARKS OR EXCEPTIONS � � 26 FIRE PROTECTION � � � � � � � � � � � � � � � 1. Portable Fire D � - � - � Any in excess of those required by | � � Extinguisher � � � FAR may be inoperative or missing | � � � � � provided: | � � � � � a) Inoperative fire | � � � � � extinguisher is tagged | � � � � � inoperative, removed from | � � � � � the installed location and | � � � � � placed out of sight so it | � � � � � can not be mistaken for a | � � � � � functional unit, and | � � � � � b) Required distribution is | � � � � � maintained. | � � � � � � � 2. Engine Fire C � 2 � 0 � (M) | � � *** Extinguisher Systems � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � �

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� U.S. DEPARTMENT OF TRANSPORTATION � � MASTER MINIMUM EQUIPMENT LIST � � FEDERAL AVIATION ADMINISTRATION � � --------------------------------------------------------------------------- � � AIRCRAFT: � REVISION NO: 7 � PAGE: � � � � � � BEECHCRAFT MODEL 99 SERIES � DATE: 01/25/2007 � 27-1 � � --------------------------------------------------------------------------- � � 1. � 2. NUMBER INSTALLED � � SYSTEM & � -------------------------------------------- � � SEQUENCE ITEM � � 3. NUMBER REQUIRED FOR DISPATCH � � NUMBERS � � --------------------------------------- � � ------------------------- � � � 4. REMARKS OR EXCEPTIONS � � 27 FLIGHT CONTROLS � � � � � � � � � � � � � � � 1. Trim Position C � 2 � 0 � May be inoperative provided: � � Indicators � � � a) Tab is visually checked for � � (Rudder and Aileron) � � � full range of operations, � � � � � b) Tab operation is unaffected, � � � � � and � � � � � c) Tab is positioned at neutral � � � � � prior to each departure and � � � � � neutral position is verified � � � � � by visual inspection. � � � � � � � 2. Flap Position C � 1 � 0 � May be inoperative provided: � � Indicator � � � a) Flaps are visually checked � � � � � for full travel and flap � � � � � operation is not affected, � � � � � b) Flaps are visually checked � � � � � full up or for proper setting � � � � � prior to each departure, � � � � � and � � � � � c) Flaps stop in Approach � � � � � Position when position switch � � � � � placed in Approach detent. � � � � � � � 3. Flap System C � 1 � 0 � May be inoperative provided: | � � � � � a)Flaps remain in the full up | � � � � � position, | � � � � � b)Flaps 0% performance data is | � � � � � available in the AFM for | � � � � � Takeoff and Landing, and | � � � � � c)Landing Gear Warning Silence | � � � � � button is not used to silence | � � � � � the landing gear warning in | � � � � � flight. | � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � �

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