Date: 11/22/2002

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

************************************ *   FOR PART 91 OPERATIONS ONLY!   * ************************************

CESSNA MODELS 310 AND 320

AIRCRAFT EVALUATION GROUP, MKC-AEG DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION 901 LOCUST

ROOM 332

KANSAS CITY, MISSOURI  64106

TELEPHONE:(816)329-3233

FAX:      (816)329-3241

DEPARTMENT OF TRANSPORTATION     Revision: 8

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Table of Contents

SYSTEM NO.  SYSTEM                                  PAGE

--     Table of Contents                       I

--     Log of Revisions                        II

--     Control Page                            III, IV

--     Highlights of Change                    V, VI

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

--     Guidelines for (O) & (M) Procedures     XVIII, XIX

21     Air Conditioning                        21-1

22     Auto Flight                             22-1

23     Communications                          23-1, 2, 3

24     Electrical Power                        24-1

25     Equipment/Furnishings                   25-1, 2

26     Fire Protection                         26-1

27     Flight Controls                         27-1

28     Fuel                                    28-1

30     Ice and Rain Protection                 30-1, 2

31     Indicating/Recording Systems            31-1

32     Landing Gear                            32-1

33     Lights                                  33-1

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

35     Oxygen                                  35-1 37     Vacuum/Pressure                         37-1 61     Propellers                              61-1 77     Engine Indicating                       77-1

FEDERAL AVIATION ADMINISTRATION     Page: I

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Log of Revisions

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

¦ ORIGINAL ¦ 05/23/1979 ¦ --                             ¦           ¦ ¦ 1        ¦ 01/13/1982 ¦ 24, 25, 27, 28, 29, 30, 33, 37 ¦           ¦ ¦ 2        ¦ 09/08/1982 ¦ 29                             ¦           ¦ ¦ 3        ¦ 11/18/1982 ¦ 22, 27, 28, 30, 34             ¦           ¦ ¦ 4        ¦ 01/14/1985 ¦ All pages                      ¦           ¦ ¦ 5        ¦ 04/26/1989 ¦ All pages                      ¦           ¦ ¦ 6        ¦ 06/22/1989 ¦ HIGHLIGHTS OF REV.,DEFINITIONS ¦           ¦ ¦ 6        ¦ 06/22/1989 ¦ PREAMBLE                       ¦           ¦ ¦ 7        ¦ 06/06/1990 ¦ HIGHLIGHTS OF REV.,DEFINITIONS ¦           ¦ ¦ 7        ¦ 06/06/1990 ¦ GUIDELINES                     ¦           ¦ ¦ 7        ¦ 06/06/1990 ¦ 23-1,25-1,27-1,30-1,33-1       ¦           ¦ ¦ 7        ¦ 06/06/1990 ¦ 34-2,37-1                      ¦           ¦ ¦ 7a       ¦ 02/08/1991 ¦ HIGHLIGHTS OF REV.             ¦           ¦ ¦ 7a       ¦ 02/08/1991 ¦ 34-3                           ¦           ¦ ¦ 7b       ¦ 07/23/1992 ¦ HIGHLIGHTS OF REV.             ¦           ¦ ¦ 7b       ¦ 07/23/1992 ¦ 21-1,22-1,23-1,25-1,25-2       ¦           ¦ ¦ 7b       ¦ 07/23/1992 ¦ 26-1,27-1,28-1,31-1,32-1       ¦           ¦ ¦ 7b       ¦ 07/23/1992 ¦ 33-1,33-2,34-1,34-2,34-3       ¦           ¦ ¦ 7b       ¦ 07/23/1992 ¦ 61-1,77-1                      ¦           ¦ ¦ 7c       ¦ 02/15/1996 ¦ HIGHLIGHTS OF REV.,DEFINITIONS ¦           ¦ ¦ 7c       ¦ 02/15/1996 ¦ GUIDELINES                     ¦           ¦ ¦ 7c       ¦ 02/15/1996 ¦ 21-1,22-1,23-1,24-1,25-1       ¦           ¦ ¦ 7c       ¦ 02/15/1996 ¦ 25-2,26-1,27-1,28-1,30-1       ¦           ¦ ¦ 7c       ¦ 02/15/1996 ¦ 30-2,31-1,32-1,33-1,33-2       ¦           ¦ ¦ 7c       ¦ 02/15/1996 ¦ 34-1,34-2,34-3,34-4,34-5       ¦           ¦ ¦ 7c       ¦ 02/15/1996 ¦ 34-6,35-1,37-1,61-1,77-1       ¦           ¦ ¦ 8        ¦ 11/22/2002 ¦ HIGHLIGHTS OF REV.,DEFINITIONS ¦           ¦ ¦ 8        ¦ 11/22/2002 ¦ GUIDELINES                     ¦           ¦ ¦ 8        ¦ 11/22/2002 ¦ 21-1,22-1,23-1,23-2,23-3       ¦           ¦ ¦ 8        ¦ 11/22/2002 ¦ 24-1,25-1,25-2,26-1,27-1       ¦           ¦ ¦ 8        ¦ 11/22/2002 ¦ 28-1,30-1,30-2,31-1,32-1       ¦           ¦ ¦ 8        ¦ 11/22/2002 ¦ 33-1,34-1,34-2,34-3,34-4       ¦           ¦ ¦ 8        ¦ 11/22/2002 ¦ 34-5,34-6,34-7,34-8,34-9       ¦           ¦ ¦ 8        ¦ 11/22/2002 ¦ 35-1,37-1,61-1,77-1            ¦           ¦

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Control Page

SYSTEM                                   PAGE  REV NO.  CURRENT DATE

Cover Page                               -       8        11/22/2002 Table of Contents                        I       8        11/22/2002 Log of Revisions                         II      8        11/22/2002 Control Page                             III     8        11/22/2002 IV      8        11/22/2002 Highlights of Change                     V       8        11/22/2002 VI      8        11/22/2002 Definitions                              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 XIV     6        01/31/1995 Preamble                                 XV      1        07/05/1990 XVI     1        07/05/1990 XVII    1        07/05/1990 Guidelines for (O) & (M)        Procedures      XVIII   8        11/22/2002 XIX     8        11/22/2002 21                                       21-1    8        11/22/2002 22                                       22-1    8        11/22/2002 23                                       23-1    8         11/22/2002 23-2    8        11/22/2002 23-3    8        11/22/2002 24                                       24-1    8        11/22/2002 25                                       25-1    8        11/22/2002 25-2    8        11/22/2002 26                                       26-1    8        11/22/2002 27                                       27-1    8        11/22/2002 28                                       28-1    8        11/22/2002 30                                       30-1    8        11/22/2002 30-2    8        11/22/2002 31                                       31-1    8        11/22/2002 32                                       32-1    8        11/22/2002 33                                       33-1    8        11/22/2002 34                                       34-1    8        11/22/2002 34-2    8                11/22/2002 34-3    8        11/22/2002 34-4    8                                                                  11/22/2002

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Control Page

SYSTEM                                   PAGE  REV NO.  CURRENT DATE

34-5    8        11/22/2002 34-6    8        11/22/2002 34-7    8                11/22/2002 34-8    8        11/22/2002 34-9    8        11/22/2002 35                                       35-1    8        11/22/2002 37                                       37-1    8        11/22/2002 61                                       61-1    8        11/22/2002 77                                       77-1    8                                                                  11/22/2002

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Highlights of Change

ATA #  Remarks

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

22-2 Added in accordance with Policy Letter 93.

22-3 Re-numbered Yaw Damper.

23-1 Revised in accordance with Policy Letter 95 Rev 1 designated as                                 Global Change 111. HF moved to 23-7.

23-4 Revised in accordance with Policy Letter 9 Rev 5 designated as                                                  Global Change 109.

23-5 Revised in accordance with Policy Letter 29 Rev 3.

23-6 Revised in accordance with Policy Letter 58 Rev 3 designated as                                                   Global Change 100.

23-7 Revised in accordance with Policy Letter 106.Designated as                                               Global Change 89.

25-1 Revised repair category, number installed and proviso.

25-2 Revised in accordance with Policy Letter 79 Rev 2 designated as                                                    Global Change 96.

25-3 Revised in accordance with Policy Letter 31 Rev 1 designated as                                                    Global Change 83.

25-4 Removed "or" in accordance with Policy Letter 31 Rev 1 designated a                                                        Global Ghange 83.

25-5 Revised in accordance with Policy Letter 73 Rev 2 designated as                                                   Global Change 104.

34-8 Revised in accordance with Policy Letter 39 Rev 3 designated as                                                    Global Change 95.

34-10 Revised in accordance with Policy Letter 76 Rev 2 designated as                                                    Global Change 110.

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Highlights of Change

34-14 Revised in accordance with Policy Letter 3 Rev 1.

34-17 Removed "or" in accordance with Policy Letter 31 Rev 1 designated as Global Change 83 and revised in accordance with Policy Letter 10 Rev                                                                      1.

34-19 Revised in accordance with Policy Letter 32 Rev 5 designated as                                                     Global Change 81.

34-20 Revised in accordance with Policy Letter 32 Rev 5 designated as                                                     Global Change 81.

34-21 Revised in accordance with Policy Letter 54 Rev 7 designated as                                                    Global Change 107.

34-23 Added in accordance with Policy Letter 98 designated as                                             Global Change 71.

34-24 Added in accordance with Policy Letter 98 designated as                                             Global Change 71.

34-25 Added in accordance with Policy Letter 111 designated as                                             Global Change 113.

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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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Definitions

Certificate Data Sheet.

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

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

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

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

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

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

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

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

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

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

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

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Definitions

operation with the  listed item inoperative.

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

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

14.  Inoperative components of an inoperative system:

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

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

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

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

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Definitions

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

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

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

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

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

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

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

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

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

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

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Definitions

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

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

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

The letter designators are inserted adjacent to Column 2.

23. Electronic fault alerting system - General                  ¦

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

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

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

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

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Definitions

do not affect dispatch and do not require action other than as  ¦ addressed within an operators standard maintenance program.     ¦

b.   DOUGLAS  (MD-11)                                           ¦

Some Douglas aircraft are equipped with an alerting function    ¦ which is a subsystem within the Electronic Instrument System    ¦ (EIS).  The alerting function provides various levels of system ¦ condition alerts (WARNING, CAUTION, ADVISORY, MAINTENANCE and   ¦ STATUS).                                                        ¦

Alerts that affect aircraft dispatch will include WARNING,      ¦ CAUTION, STATUS or MAINTENANCE level.  MAINTENANCE alerts are   ¦ displayed on the status page of the EIS display panel under the ¦ maintenance heading.                                            ¦

A MAINTENANCE alert on the EIS indicates the presence of a      ¦ system fault which can be identified by the Central Fault       ¦ Display System (CFDS) interrogation.  The systems are designed  ¦ to be fault tolerant, however, for any MAINTENANCE alert, the   ¦ MEL must be verified for dispatch purposes.                     ¦

c.   AIRBUS  (A-300-600, A-310, A-320/319/321, A-330, A-340     ¦

Airbus aircraft equipped with Electronic Centralized Aircraft   ¦ Monitoring (ECAM) provide different levels of system condition  ¦ messages (WARNING, CAUTION, STATUS, and ADVISORY). A-320/319/   ¦ 321, A-330, and A-340 also provide MAINTENANCE status messages. ¦

Any message that effects airplane dispatchability will normally ¦ be at the WARNING, CAUTION or STATUS level. MAINTENANCE         ¦ messages (A-320/319/321, A-330, and A-340 only) are also        ¦ indicated on ECAM Status Page below the white Maintenance label.¦

A MAINTENANCE status (Class II) message on ECAM indicates the   ¦ presence of a system fault which can be identified by CFDS      ¦ (A-320/319/321) or CMS (A-330/A-340) interrogation. The systems ¦ are designed to be fault tolerant, however for any MAINTENANCE  ¦ status (Class II) message, the A-320/319/321 MEL must be        ¦ verified for dispatch capability. For the A-330 and A-340,      ¦ MAINTENANCE status messages do not affect dispatch.             ¦

d.   FOKKER  (FK-100)                                           ¦

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Definitions

Fokker aircraft are equipped with Multi Function Display System ¦ (MFDS) which provides electronic message referring to the       ¦ different priority levels of system information (WARNING (red), ¦ CAUTION (amber), AWARENESS (cyan) AND STATUS (white).  Any      ¦ messages that affects aircraft dispatch will be at the WARNING, ¦ CAUTION or AWARENESS level.  In these cases the MEL must be     ¦ verified for dispatch capability and maintenance may be         ¦ required.                                                       ¦

System conditions that only require maintenance are not         ¦ presented on the flight deck.  These maintenance                ¦ indications/messages may be presented on the Maintenance & Test ¦ Panel (MAP) or the Centralized Fault Display Unit (CFDU) and by ¦ dedicated Built In Test Evaluation (BITE) of systems.           ¦

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

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

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

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

  D."

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Definitions

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

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Preamble

(Effective 7/5/90)

This preamble is applicable to, and will be included in, master minimum equipment lists (MMEL) issued under the provisions of Section 91.30(a) ¢NEW Section 91.213(a)(2)|.  It is not applicable to MMEL's issued under the provisions of Parts 121, 125, 129, and 135 of the FAR.

Except as provided in Section 91.30(d) ¢NEW Section 91.213(d)|, or under the provisions of an approved MMEL, all equipment installed on an aircraft in compliance with the airworthiness standards or operating rules must be operative.  Experience has shown that with the various levels of redundancy designed into modern aircraft, operation of every system or component installed may not be necessary when the remaining equipment can provide an acceptable level of safety.

An 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 only those items of equipment which the Administrator finds may be inoperative and yet maintain an acceptable level of safety by appropriate conditions and limitations.  The MMEL and FAA-issued letter of authorization are used as an MEL by an operator and permit operation of the aircraft with inoperative equipment.

The MMEL includes all items of installed equipment that are permitted to be inoperative.  Equipment required by the FAR, and optional equipment in excess of FAR requirements, is included with appropriate conditions and limitations.  For each listed item, the installed equipment configuration considered to be normal for the aircraft is specified.  Items of equipment installed on aircraft (except for passenger convenience items such as galley equipment and passenger entertainment devices), such as "TCAS," windshear detection devices, and ground proximity warning systems (GPWS) that are in excess of what is required, and are not listed on the MMEL, must be operational for dispatch unless MMEL relief is sought through the FSDO having jurisdiction for the operator.  If MMEL relief is sought, the operator must notify the FSDO who will make a request of the FOEB to convene and consider adding the equipment to the MMEL.  The operator may then dispatch with the equipment disabled, or rendered

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Preamble

(Effective 7/5/90)

inoperative, in accordance with all FAR.  It is incumbent on the operator to endeavor to determine if O and/or M procedures for that equipment must be developed.  If so, any procedures developed must comply with all FAR.  Procedures developed to use the MMEL must not conflict with either the aircraft flight manual limitations, emergency procedures, or with airworthiness directives (AD), all of which take precedence over the MMEL and those procedures.  Suitable conditions and limitations in the form of placards, maintenance procedures, crew operating procedures, and other restrictions, as necessary, are required to be accomplished by the operator to ensure that an acceptable level of safety is maintained.  Those procedures should be developed from guidance provided in the manufacturer's aircraft flight and/or maintenance manuals, manufacturer's recommendations, engineering specifications, and other appropriate sources.  Procedures must not be contrary to any FAR. Wherever the statement "as required by FAR" appears in the MMEL, the operator must either list the specific FAR by part and section and carry the FAR on board the aircraft or specify the requirements and/or limitations to conduct the flight in accordance with the appropriate FAR.

The MMEL is intended to permit operations with inoperative items of equipment for the minimum period of time necessary until repairs can be accomplished.  It is important that repairs be accomplished at the earliest opportunity in order to return the aircraft to its design level of safety and reliability. Inoperative equipment in all cases must be repaired, or inspected and deferred, by qualified maintenance personnel at the next required inspection ¢Section 91.165(c), NEW Section 91.405(c)|. The repair intervals indicated by the Letters A, B, and C inserted adjacent to column 2 are NOT applicable to this MMEL.

The MMEL 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 records.  The item is then either repaired or deferred per the MMEL or other approved means acceptable to the Administrator prior to further operation.  In addition to the specific MMEL conditions and limitations, determination by the operator that the aircraft is in condition for safe operations under anticipated flight conditions must be made for all items of inoperative equipment.  When these requirements are met, the

  FEDERAL AVIATION ADMINISTRATION   Page: XVII

Revision: 1

MASTER MINIMUM EQUIPMENT LIST    Date: 07/05/1990

CESSNA MODELS 310/320

Preamble

(Effective  7/5/90)

inoperative equipment.  When these requirements are met, the aircraft may be considered airworthy and returned to service. 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 interrelationship between those items, and the effect on aircraft operation and crew workload, must be considered. Operators are expected to establish a controlled and sound repair program, including the parts, personnel, facilities, procedures, and schedules to ensure timely repair.

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

  FEDERAL AVIATION ADMINISTRATION   Page XVIII

Revision: 8

MASTER MINIMUM EQUIPMENT LIST    Date: 11/22/2002

CESSNA MODELS 310/320

Guidelines for (O) & (M) Procedures

21-1  (M) Maintenance procedure to ensure no fuel leaks, mechanical or

electrical faults exist which could have an adverse affect on aircraft operations.

21-3  (M) Maintenance procedure to ensure no mechanical or electrical faults exist which could have an adverse affect on aircraft operations.

21-4  (O) Operations procedure to record heater time.

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

fault exists which could have any adverse affect on any flight control function.

22-3  (M) Maintenance procedure to ensure no electrical or mechanical

fault exists which could have any adverse affect on any flight control function.

23-4  (O) Operations procedure to ensure passengers are provided the appropriate briefings

23-7  (O) Operations procedure to assure that long range communication system is available.

27-3  (M) Maintenance procedure to ensure failure of electric trim will not interfere with operation of manual trim.

28-1  (O) Operations procedure to determine fuel quantity on board           meets regulatory requirements for the flight.

31-2  (O) Operations procedure to record flight time.

32-1  (O) Operations procedure to ensure aircraft will not move when                             unattended.

34-8  (O) Operations procedure to ensure crew awareness of airplane                      altitude and performance.

  Revision: 8

MASTER MINIMUM EQUIPMENT LIST    Date: 11/22/2002

CESSNA MODELS 310/320

Guidelines for (O) & (M) Procedures

34-19   (M) Maintenance procedure to ensure system is deactivated                            and secure.

(O) Operations procedure to assure that enroute or approach             procedures do not require its use.

-1 (O)Operations procedure to ensure TA and RA display is visible to the non-flying pilot and TA/RA elements and audio functions                are operative on flying pilot side.

-2 (O)Operations procedure to ensure non-flying pilot monitors                        pilot's display.

(O)Operations procedure to ensure TA only mode is selected and            all TA functions/elements are operative.

-3 (O)Operations procedure to ensure all RA display and audio                   functions are operative.

34-20   (M)Maintenance procedure to ensure system is deactivated and                               secured.

(O)Operations procedure to assure enroute or approach          procedures do not require its use.

34-21   (O)Operations procedure to ensure crew awareness of minimum                  -1    altitudes and performance.

-4 (O)Operations procedure to ensure crew awareness of no advisory                             callouts.

-5 (O)Operations procedure to ensure crew awareness of minimum                   altitudes and performance.

34-23   (O)Operations procedure to verify status and suitability

of Navigation Facilities used to define route of flight.

34-24   (O)Operations procedure to verify status and suitability

of Navigation Facilities used to define route of flight.

37-1    (M)Maintenance procedure to ensure no mechanical problem exists because of pump failure which could have an adverse affect on engine                               operation.

FEDERAL AVIATION ADMINISTRATION   Page XIX

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 8        ¦ PAGE:    ¦ ¦          CESSNA MODELS 310/320           ¦                       ¦          ¦ ¦                                          ¦ DATE: 11/22/2002      ¦ 21-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 21  AIR CONDITIONING      ¦    ¦    ¦                                       ¦

¦ 1.  Heater              C ¦ 1  ¦ 0  ¦ (M)                                   ¦

¦ 2.  Heater Fan          C ¦ 1  ¦ 0  ¦ May be inoperative provided:          ¦ ¦                           ¦    ¦    ¦     a) The heater or windshield       ¦ ¦                           ¦    ¦    ¦        defogging is not operated on   ¦ ¦                           ¦    ¦    ¦        the ground, and                ¦ ¦                           ¦    ¦    ¦     b) Heater is turned off prior     ¦ ¦                           ¦    ¦    ¦        to landing.                    ¦

¦ 3.  Air Conditioning    C ¦ 1  ¦ 0  ¦ (M)                                   ¦ ¦     System                ¦    ¦    ¦                                       ¦

¦ 4.  Heater Hour Meter   C ¦ 1  ¦ 0  ¦ (O)                                   ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 8        ¦ PAGE:    ¦ ¦          CESSNA MODELS 310/320           ¦                       ¦          ¦ ¦                                          ¦ DATE: 11/22/2002      ¦ 22-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 22  AUTO FLIGHT           ¦    ¦    ¦                                       ¦

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

¦ 2.  Autopilot           C ¦ -  ¦ -  ¦ One may be inoperative provided     ¦ ¦ ¦     Disconnect            ¦    ¦    ¦ the autopilot is not utilized at    ¦ ¦ ¦                           ¦    ¦    ¦ less than initial approach          ¦ ¦ ¦                           ¦    ¦    ¦ altitude.                           ¦ ¦

¦ 3.  Yaw Damper          C ¦ 1  ¦ 0  ¦ (M)May be inoperative provided yaw  ¦ ¦ ¦                           ¦    ¦    ¦ damper is independent of and          ¦ ¦                           ¦    ¦    ¦ unrelated to the autopilot            ¦ ¦                           ¦    ¦    ¦ operation or the autopilot is not     ¦ ¦                           ¦    ¦    ¦ used.                                 ¦

¦                           ¦    ¦    ¦ NOTE: See AFM supplement for          ¦ ¦                           ¦    ¦    ¦       possible yaw damper vs.         ¦ ¦                           ¦    ¦    ¦       autopilot operating             ¦ ¦                           ¦    ¦    ¦       instructions.                   ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 8        ¦ PAGE:    ¦ ¦          CESSNA MODELS 310/320           ¦                       ¦          ¦ ¦                                          ¦ DATE: 11/22/2002      ¦ 23-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 23  COMMUNICATIONS        ¦    ¦    ¦                                       ¦

¦ 1.  Communications      D ¦ -  ¦ -  ¦ Any in excess of those required by  ¦ ¦ ¦     Systems               ¦    ¦    ¦ FAR may be inoperative provided     ¦ ¦ ¦     (VHF and UHF)         ¦    ¦    ¦ it is not powered by an emergency   ¦ ¦ ¦                           ¦    ¦    ¦ power source and not required       ¦ ¦ ¦                           ¦    ¦    ¦ by emergency procedures.            ¦ ¦

¦ 2.  Audio Amplifier     C ¦ 1  ¦ 0  ¦ As required by FAR.                   ¦

¦ 3.  Cockpit Speaker     C ¦ 1  ¦ 0  ¦ As required by FAR.                   ¦

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

¦     1) Passenger        B ¦ 1  ¦ 0  ¦ (O)May be inoperative provided      ¦ ¦ ¦        Configuration      ¦    ¦    ¦ alternate, normal, and emergency    ¦ ¦ ¦                           ¦    ¦    ¦ procedures are established and      ¦ ¦ ¦                           ¦    ¦    ¦ used.                               ¦ ¦

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

¦     2) Cargo            D ¦ 1  ¦ 0  ¦ May be inoperative unless           ¦ ¦ ¦                           ¦    ¦    ¦ procedures require its use.         ¦ ¦

¦ 5.  Cockpit Voice         ¦    ¦    ¦                                     ¦ ¦ ¦ *** Recorder (CVR)        ¦    ¦    ¦                                     ¦ ¦ ¦     System                ¦    ¦    ¦                                     ¦ ¦

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

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

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 8        ¦ PAGE:    ¦ ¦          CESSNA MODELS 310/320           ¦                       ¦          ¦ ¦                                          ¦ DATE: 11/22/2002      ¦ 23-2     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 23  COMMUNICATIONS        ¦    ¦    ¦                                       ¦

¦ 6.  Boom Microphones      ¦    ¦    ¦                                     ¦ ¦ ¦ *** (CVR and 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 121.359 (e) or ¦    ¦    ¦       three flight days.            ¦ ¦ ¦        FAR 135.151 (d)    ¦    ¦    ¦                                     ¦ ¦

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

¦     Boom Microphones      ¦    ¦    ¦                                     ¦ ¦ ¦ *** (CVR Installed)       ¦    ¦    ¦                                     ¦ ¦

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

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

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 8        ¦ PAGE:    ¦ ¦          CESSNA MODELS 310/320           ¦                       ¦          ¦ ¦                                          ¦ DATE: 11/22/2002      ¦ 23-3     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 23  COMMUNICATIONS        ¦    ¦    ¦                                       ¦

¦ 7.  High Frequency      D ¦ -  ¦ -  ¦ Any in excess of those required by  ¦ ¦ ¦ *** (HF)Communication     ¦    ¦    ¦ FAR may be inoperative.             ¦ ¦ ¦     System                ¦    ¦    ¦                                     ¦ ¦

¦                         C ¦ -  ¦ 1  ¦ (O) May be inoperative while        ¦ ¦ ¦                           ¦    ¦    ¦ conducting operations that require  ¦ ¦ ¦                           ¦    ¦    ¦ two LCRS provided:                  ¦ ¦ ¦                           ¦    ¦    ¦     a)SATCOM (high or low gain)     ¦ ¦ ¦                           ¦    ¦    ¦       Data Link System operates     ¦ ¦ ¦                           ¦    ¦    ¦       normally, and                 ¦ ¦ ¦                           ¦    ¦    ¦     b)SATCOM Data Link              ¦ ¦ ¦                           ¦    ¦    ¦       communication operates        ¦ ¦ ¦                           ¦    ¦    ¦       normally over the intended    ¦ ¦ ¦                           ¦    ¦    ¦       route of flight.              ¦ ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 8        ¦ PAGE:    ¦ ¦          CESSNA MODELS 310/320           ¦                       ¦          ¦ ¦                                          ¦ DATE: 11/22/2002      ¦ 24-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 24  ELECTRICAL POWER      ¦    ¦    ¦                                       ¦

¦ 1.  Volt/Ammeter        B ¦ 1  ¦ 0  ¦ May be inoperative provided           ¦ ¦     (selectable)          ¦    ¦    ¦ Alternator Out Caution Lights are     ¦ ¦                           ¦    ¦    ¦ installed and operative.              ¦

¦ 2.  Alternator Out      B ¦ 2  ¦ 0  ¦ May be inoperative provided           ¦ ¦ *** Caution Lights        ¦    ¦    ¦ Volt/Ammeter is operative.            ¦

¦ 3.  Voltage Regulators  B ¦ 2  ¦ 1  ¦ One may be inoperative for day VFR    ¦ ¦     (selectable)          ¦    ¦    ¦ provided the Volt/Ammeter is          ¦ ¦                           ¦    ¦    ¦ operative and monitored.              ¦

¦ 4.  Low Voltage         B ¦ 1  ¦ 0  ¦ One may be inoperative for day VFR    ¦ ¦     Warning Light         ¦    ¦    ¦ provided Volt/Ammeter is operative.   ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 8        ¦ PAGE:    ¦ ¦          CESSNA MODELS 310/320           ¦                       ¦          ¦ ¦                                          ¦ DATE: 11/22/2002      ¦ 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               ¦    ¦    ¦ for operations not requiring a      ¦ ¦ ¦                           ¦    ¦    ¦ Second in Command provided seat     ¦ ¦ ¦                           ¦    ¦    ¦ remains unoccupied.                 ¦ ¦

¦ 2.  Passenger Seats     C ¦ -  ¦ -  ¦ May be inoperative provided:        ¦ ¦ ¦                           ¦    ¦    ¦     a)Seat does not block an        ¦ ¦ ¦                           ¦    ¦    ¦       emergency exit.               ¦ ¦ ¦                           ¦    ¦    ¦     b)Seat does not restrict        ¦ ¦ ¦                           ¦    ¦    ¦       access to the main aircraft   ¦ ¦ ¦                           ¦    ¦    ¦       aisle and                     ¦ ¦ ¦                           ¦    ¦    ¦     c)The affected seat(s) are      ¦ ¦ ¦                           ¦    ¦    ¦       blocked and placarded " Do    ¦ ¦ ¦                           ¦    ¦    ¦       Not Occupy)".                 ¦ ¦

¦                           ¦    ¦    ¦  NOTE 1:A seat with an inoperative  ¦ ¦ ¦                           ¦    ¦    ¦  seat belt or shoulder harness is   ¦ ¦ ¦                           ¦    ¦    ¦  considered to be inoperative.      ¦ ¦

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

¦ 3.  Approved Flotation  C ¦ -  ¦ -  ¦ As required by FAR.                 ¦ ¦ ¦     Equipment             ¦    ¦    ¦                                     ¦ ¦

¦ 4.  ELT                 C ¦ 1  ¦ 0  ¦ As required by FAR                    ¦

¦                         C ¦ 1  ¦ 0  ¦ May be inoperative for published      ¦ ¦                           ¦    ¦    ¦ scheduled flights in scheduled air    ¦ ¦                           ¦    ¦    ¦ carrier service.                      ¦

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

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 8        ¦ PAGE:    ¦ ¦          CESSNA MODELS 310/320           ¦                       ¦          ¦ ¦                                          ¦ DATE: 11/22/2002      ¦ 25-2     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 25  EQUIPMENT/FURNISHINGS ¦    ¦    ¦                                       ¦

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

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 8        ¦ PAGE:    ¦ ¦          CESSNA MODELS 310/320           ¦                       ¦          ¦ ¦                                          ¦ DATE: 11/22/2002      ¦ 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) The inoperative fire           ¦ ¦                           ¦    ¦    ¦        extinguisher is tagged         ¦ ¦                           ¦    ¦    ¦        inoperative, removed from      ¦ ¦                           ¦    ¦    ¦        the installed location, and    ¦ ¦                           ¦    ¦    ¦        placed out of sight so it      ¦ ¦                           ¦    ¦    ¦        can not be mistaken for a      ¦ ¦                           ¦    ¦    ¦        functional unit, and           ¦ ¦                           ¦    ¦    ¦     b) Required distribution is       ¦ ¦                           ¦    ¦    ¦        maintained.                    ¦

¦ 2.  Fire Detection and  C ¦ 2  ¦ 0  ¦                                       ¦ ¦     Extinguishing Systems ¦    ¦    ¦                                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 8        ¦ PAGE:    ¦ ¦          CESSNA MODELS 310/320           ¦                       ¦          ¦ ¦                                          ¦ DATE: 11/22/2002      ¦ 27-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 27  FLIGHT CONTROLS       ¦    ¦    ¦                                       ¦

¦ 1.  Wing Flap System      ¦    ¦    ¦  Deleted, Rev. 7                      ¦

¦ 2.  Wing Flap Position  C ¦ 1  ¦ 0  ¦ May be inoperative provided:          ¦ ¦     Indicator             ¦    ¦    ¦     a) A notch or detent position     ¦ ¦                           ¦    ¦    ¦        preselect feature is part of   ¦ ¦                           ¦    ¦    ¦        the flap switch,               ¦ ¦                           ¦    ¦    ¦     b) Flaps are visually checked     ¦ ¦                           ¦    ¦    ¦        for full travel and flap       ¦ ¦                           ¦    ¦    ¦        operations are not affected    ¦ ¦                           ¦    ¦    ¦        and                            ¦ ¦                           ¦    ¦    ¦     c) Flaps are visually checked     ¦ ¦                           ¦    ¦    ¦        full up prior to each          ¦ ¦                           ¦    ¦    ¦        departure.                     ¦

¦ 3.  Electric Elevator   C ¦ 1  ¦ 0  ¦ (M)May be inoperative provided        ¦ ¦     Trim System           ¦    ¦    ¦ manual trim is operative and          ¦ ¦                           ¦    ¦    ¦ unaffected.                           ¦

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

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 8        ¦ PAGE:    ¦ ¦          CESSNA MODELS 310/320           ¦                       ¦          ¦ ¦                                          ¦ DATE: 11/22/2002      ¦ 28-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 28  FUEL                  ¦    ¦    ¦                                       ¦

¦ 1.  Fuel Quantity       C ¦ 2  ¦ 1  ¦ (O)One may be inoperative provided    ¦ ¦     Indicators            ¦    ¦    ¦ a reliable means is established to    ¦ ¦                           ¦    ¦    ¦ determine that fuel quantity on       ¦ ¦                           ¦    ¦    ¦ board meets the regulatory            ¦ ¦                           ¦    ¦    ¦ requirements for the intended         ¦ ¦                           ¦    ¦    ¦ flight.                               ¦

¦ 2.  Fuel Low Level      C ¦ 2  ¦ 0  ¦ May be inoperative provided all       ¦ ¦ *** Warning Lights        ¦    ¦    ¦ fuel tank quantity indicators are     ¦ ¦                           ¦    ¦    ¦ operative.                            ¦

¦ 3.  Fuel Totalizer      C ¦ 1  ¦ 0  ¦                                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 8        ¦ PAGE:    ¦ ¦          CESSNA MODELS 310/320           ¦                       ¦          ¦ ¦                                          ¦ DATE: 11/22/2002      ¦ 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.  Pitot Heater        B ¦ 1  ¦ 0  ¦ Right Pitot Heater may be             ¦ ¦                           ¦    ¦    ¦ inoperative.                          ¦

¦                         B ¦ 1  ¦ 0  ¦ Left Pitot Heater may be              ¦ ¦                           ¦    ¦    ¦ inoperative except for:               ¦ ¦                           ¦    ¦    ¦     a) IFR passenger carrying and     ¦ ¦                           ¦    ¦    ¦     b) Flight in known or forecast    ¦ ¦                           ¦    ¦    ¦        icing conditions.              ¦

¦                           ¦    ¦    ¦ NOTE:  Two heated pitot tubes are     ¦ ¦                           ¦    ¦    ¦ required for these conditions if a    ¦ ¦                           ¦    ¦    ¦ second airspeed indicator is          ¦ ¦                           ¦    ¦    ¦ installed and operative.              ¦

¦ 2.  Surface Deicing     C ¦ 1  ¦ 0  ¦ May be inoperative provided           ¦ ¦     System (Wing,         ¦    ¦    ¦ aircraft is not operated in known     ¦ ¦     Vertical and          ¦    ¦    ¦ or forecast icing conditions.         ¦ ¦     Horizontal            ¦    ¦    ¦                                       ¦ ¦     Stabilizer)           ¦    ¦    ¦                                       ¦

¦ 3.  Electric            C ¦ 1  ¦ 0  ¦ May be inoperative provided           ¦ ¦     Windshield Anti-ice   ¦    ¦    ¦ aircraft is not operated in known     ¦ ¦                           ¦    ¦    ¦ or forecast icing conditions.         ¦

¦ 4.  Alcohol Windshield  C ¦ 1  ¦ 0  ¦ May be inoperative provided           ¦ ¦     Deice System          ¦    ¦    ¦ aircraft is not operated in known     ¦ ¦                           ¦    ¦    ¦ or forecast icing conditions.         ¦

¦ 5.  Propeller Deicing/  C ¦ 2  ¦ 0  ¦ May be inoperative provided           ¦ ¦     Anti-icing Systems    ¦    ¦    ¦ aircraft is not operated in known     ¦ ¦                           ¦    ¦    ¦ or forecast icing conditions.         ¦

¦ 6.  Stall Warning/      C ¦ 1  ¦ 0  ¦ May be inoperative provided           ¦ ¦     Angle of Attack       ¦    ¦    ¦ aircraft is not operated in known     ¦ ¦     Heater                ¦    ¦    ¦ or forecast icing conditions.         ¦

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

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 8        ¦ PAGE:    ¦ ¦          CESSNA MODELS 310/320           ¦                       ¦          ¦ ¦                                          ¦ DATE: 11/22/2002      ¦ 30-2     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 30  ICE AND RAIN          ¦    ¦    ¦                                       ¦ ¦     PROTECTION            ¦    ¦    ¦                                       ¦

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

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 8        ¦ PAGE:    ¦ ¦          CESSNA MODELS 310/320           ¦                       ¦          ¦ ¦                                          ¦ DATE: 11/22/2002      ¦ 31-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 31  INDICATING/RECORDING  ¦    ¦    ¦                                       ¦ ¦     SYSTEMS               ¦    ¦    ¦                                       ¦

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

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

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 8        ¦ PAGE:    ¦ ¦          CESSNA MODELS 310/320           ¦                       ¦          ¦ ¦                                          ¦ DATE: 11/22/2002      ¦ 32-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 32  LANDING GEAR          ¦    ¦    ¦                                       ¦

¦ 1.  Parking Brake       C ¦ 1  ¦ 0  ¦ (O)May be inoperative provided      ¦ ¦ ¦                           ¦    ¦    ¦ normal braking system is            ¦ ¦ ¦                           ¦    ¦    ¦ not affected.                       ¦ ¦

¦                         C ¦ 1  ¦ 0  ¦ (O)Wheel chocks will be used if     ¦ ¦ ¦                           ¦    ¦    ¦ parking brake is inoperative.       ¦ ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 8        ¦ PAGE:    ¦ ¦          CESSNA MODELS 310/320           ¦                       ¦          ¦ ¦                                          ¦ DATE: 11/22/2002      ¦ 33-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 33  LIGHTS                ¦    ¦    ¦                                       ¦

¦ 1.  Anti-collision      B ¦ 1  ¦ 0  ¦ May be inoperative for day            ¦ ¦     Light System          ¦    ¦    ¦ operations.                           ¦

¦ 2.  Collision Avoidance C ¦ -  ¦ 0  ¦                                       ¦ ¦ *** Lights (STC SA4222SW) ¦    ¦    ¦                                       ¦

¦ 3.  Strobe Light        C ¦ 1  ¦ 0  ¦                                       ¦ ¦     System                ¦    ¦    ¦                                       ¦

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

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

¦ 6.  Ice Detection       C ¦ 2  ¦ 0  ¦ May be inoperative provided           ¦ ¦     Lights                ¦    ¦    ¦ a portable lamp/light of adequate     ¦ ¦                           ¦    ¦    ¦ capacity for wing and/or control      ¦ ¦                           ¦    ¦    ¦ surface inspection is available       ¦ ¦                           ¦    ¦    ¦ for night operations in icing         ¦ ¦                           ¦    ¦    ¦ conditions.                           ¦

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

¦ 8.  Taxi Light          C ¦ 1  ¦ 0  ¦                                       ¦

¦ 9.  Logo Lights         C ¦ 2  ¦ 0  ¦                                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 8        ¦ PAGE:    ¦ ¦          CESSNA MODELS 310/320           ¦                       ¦          ¦ ¦                                          ¦ DATE: 11/22/2002      ¦ 34-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 34  NAVIGATION            ¦    ¦    ¦                                       ¦

¦ 1.  Altimeter           B ¦ -  ¦ 1  ¦ Right side may be inoperative.        ¦ ¦     Barometric Pressure   ¦    ¦    ¦                                       ¦ ¦     (Adjustable)          ¦    ¦    ¦ NOTE:  Where a servoed electric       ¦ ¦                           ¦    ¦    ¦        altimeter is installed a       ¦ ¦                           ¦    ¦    ¦        functioning pneumatic          ¦ ¦                           ¦    ¦    ¦        altimeter is required.         ¦

¦ 2.  Airspeed Indicator  C ¦ -  ¦ 1  ¦ Right side may be inoperative.        ¦

¦                           ¦    ¦    ¦ NOTE:  Where a servoed electric       ¦ ¦                           ¦    ¦    ¦        airspeed is installed, a       ¦ ¦                           ¦    ¦    ¦        functioning pneumatic          ¦ ¦                           ¦    ¦    ¦        indicator is required.         ¦

¦ 3.  Gyroscopic Pitch    B ¦ -  ¦ 1  ¦ Right side may be inoperative.        ¦ ¦     and Bank Indicators   ¦    ¦    ¦                                       ¦

¦ 4.  Gyroscopic          B ¦ -  ¦ 1  ¦ Right side may be inoperative.        ¦ ¦     Directional           ¦    ¦    ¦                                       ¦ ¦     Indicators            ¦    ¦    ¦                                       ¦

¦ 5.  Gyroscopic Rate of  B ¦ 1  ¦ 0  ¦ May be inoperative except for:        ¦ ¦     Turn/Slip Skid        ¦    ¦    ¦      a)IFR operations,                ¦ ¦     Indicator             ¦    ¦    ¦      b)passenger carrying VFR         ¦ ¦                           ¦    ¦    ¦        over-the-top, and              ¦ ¦                           ¦    ¦    ¦      c)passenger carrying VFR night   ¦ ¦                           ¦    ¦    ¦        flights.                       ¦

¦ 6.  Vertical Speed      B ¦ 1  ¦ 0  ¦ May be inoperative except for IFR     ¦ ¦     Indicator             ¦    ¦    ¦ passenger carrying.                   ¦

¦ 7.  Flight Director     C ¦ 1  ¦ 0  ¦                                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 8        ¦ PAGE:    ¦ ¦          CESSNA MODELS 310/320           ¦                       ¦          ¦ ¦                                          ¦ DATE: 11/22/2002      ¦ 34-2     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 34  NAVIGATION            ¦    ¦    ¦                                       ¦

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

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

¦ 9.  Radio Altimeter     C ¦ 1  ¦ 0  ¦                                       ¦ ¦ ***                       ¦    ¦    ¦                                       ¦

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

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

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

¦ 12. Navigation          C ¦ -  ¦ -  ¦ As required by FAR.                   ¦ ¦     Equipment (VOR/ILS,   ¦    ¦    ¦                                       ¦ ¦     LORAN, OMEGA/VLF,     ¦    ¦    ¦                                       ¦ ¦     INS, DOPPLER, GPS,    ¦    ¦    ¦                                       ¦ ¦     RNAV)                 ¦    ¦    ¦                                       ¦

¦ 13. Marker Beacon       C ¦ 1  ¦ 0  ¦ May be inoperative provided           ¦ ¦                           ¦    ¦    ¦ approach procedure does not           ¦ ¦                           ¦    ¦    ¦ require its use.                      ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 8        ¦ PAGE:    ¦ ¦          CESSNA MODELS 310/320           ¦                       ¦          ¦ ¦                                          ¦ DATE: 11/22/2002      ¦ 34-3     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 34  NAVIGATION            ¦    ¦    ¦                                       ¦

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

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

¦ 16. RMI                 C ¦ 1  ¦ 0  ¦                                       ¦

¦ 17. Nonstabilized       B ¦ 1  ¦ 0  ¦ May be inoperative provided         ¦ ¦ ¦     Magnetic (Standby)    ¦    ¦    ¦ any combination of three gyro       ¦ ¦ ¦     Compass               ¦    ¦    ¦ or INS (IRU) stabilized compass     ¦ ¦ ¦                           ¦    ¦    ¦ systems are operative.              ¦ ¦

¦                         B ¦ 1  ¦ 0  ¦ May be inoperative provided:        ¦ ¦ ¦                           ¦    ¦    ¦   a)Any combination of two gyro or  ¦ ¦ ¦                           ¦    ¦    ¦     INS stabilized compass systems  ¦ ¦ ¦                           ¦    ¦    ¦     are operative, and              ¦ ¦ ¦                           ¦    ¦    ¦   b)Aircraft is operated with dual  ¦ ¦ ¦                           ¦    ¦    ¦     independent navigation          ¦ ¦ ¦                           ¦    ¦    ¦     capability and under positive   ¦ ¦ ¦                           ¦    ¦    ¦     radar control by ATC on the     ¦ ¦ ¦                           ¦    ¦    ¦     enroute portion of the flight.  ¦ ¦

¦                         B ¦ 1  ¦ 0  ¦ May be inoperative for flights      ¦ ¦ ¦                           ¦    ¦    ¦ that are entirely within areas of   ¦ ¦ ¦                           ¦    ¦    ¦ magnetic unreliability provided at  ¦ ¦ ¦                           ¦    ¦    ¦ least two stabilized directional    ¦ ¦ ¦                           ¦    ¦    ¦ gyro systems are installed,         ¦ ¦ ¦                           ¦    ¦    ¦ operative, and used in conjunction  ¦ ¦ ¦                           ¦    ¦    ¦ with approved free gyro navigation  ¦ ¦ ¦                           ¦    ¦    ¦ techniques.                         ¦ ¦

¦ 18. Altitude Encoder      ¦    ¦    ¦ Included with ATA 34-10.              ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 8        ¦ PAGE:    ¦ ¦          CESSNA MODELS 310/320           ¦                       ¦          ¦ ¦                                          ¦ DATE: 11/22/2002      ¦ 34-4     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 34  NAVIGATION            ¦    ¦    ¦                                       ¦

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

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

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

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

¦      (CON'T)              ¦    ¦    ¦                                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 8        ¦ PAGE:    ¦ ¦          CESSNA MODELS 310/320           ¦                       ¦          ¦ ¦                                          ¦ DATE: 11/22/2002      ¦ 34-5     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 34  NAVIGATION            ¦    ¦    ¦                                       ¦

¦      (CON'T)              ¦    ¦    ¦                                       ¦

¦ 19.Traffic Alert and      ¦    ¦    ¦                                       ¦ ¦    Collision Avoidance    ¦    ¦    ¦                                       ¦ ¦    System (TCAS II)       ¦    ¦    ¦                                       ¦

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

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

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

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

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

¦      (CON'T)              ¦    ¦    ¦                                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 8        ¦ PAGE:    ¦ ¦          CESSNA MODELS 310/320           ¦                       ¦          ¦ ¦                                          ¦ DATE: 11/22/2002      ¦ 34-6     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 34  NAVIGATION            ¦    ¦    ¦                                       ¦

¦      (CON'T)              ¦    ¦    ¦                                       ¦

¦ 21.GPWS                   ¦    ¦    ¦                                       ¦

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

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

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

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

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

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

¦      (CON'T)              ¦    ¦    ¦                                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 8        ¦ PAGE:    ¦ ¦          CESSNA MODELS 310/320           ¦                       ¦          ¦ ¦                                          ¦ DATE: 11/22/2002      ¦ 34-7     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 34  NAVIGATION            ¦    ¦    ¦                                       ¦

¦      (CON'T)              ¦    ¦    ¦                                       ¦

¦ 21.GPWS                   ¦    ¦    ¦                                       ¦

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

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

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

¦   22.Flight Profile     C ¦ 1  ¦ 0  ¦                                       ¦ ¦ ***  Advisory System      ¦    ¦    ¦                                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 8        ¦ PAGE:    ¦ ¦          CESSNA MODELS 310/320           ¦                       ¦          ¦ ¦                                          ¦ DATE: 11/22/2002      ¦ 34-8     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 34  NAVIGATION            ¦    ¦    ¦                                       ¦

¦ 23. Flight Management   C ¦ -  ¦ -  ¦ (O)May be out of currency           ¦ ¦ ¦ *** Systems Navigation    ¦    ¦    ¦    provided:                        ¦ ¦ ¦     Databases             ¦    ¦    ¦     a)Current Aeronautical          ¦ ¦ ¦                           ¦    ¦    ¦       Charts are used to verify     ¦ ¦ ¦                           ¦    ¦    ¦       Navigation fixes prior to     ¦ ¦ ¦                           ¦    ¦    ¦       dispatch.                     ¦ ¦ ¦                           ¦    ¦    ¦     b)Procedures are established    ¦ ¦ ¦                           ¦    ¦    ¦       and used to verify status     ¦ ¦ ¦                           ¦    ¦    ¦       and suitability of            ¦ ¦ ¦                           ¦    ¦    ¦       Navigation Facilities used    ¦ ¦ ¦                           ¦    ¦    ¦       to define route of flight,    ¦ ¦ ¦                           ¦    ¦    ¦       and                           ¦ ¦ ¦                           ¦    ¦    ¦     c)Approach Navigation Radios    ¦ ¦ ¦                           ¦    ¦    ¦       are manually tuned and        ¦ ¦ ¦                           ¦    ¦    ¦       identified.                   ¦ ¦

¦ 24. Navigation          C ¦ -  ¦ -  ¦ (O) May be out of currency          ¦ ¦ ¦ *** Management System     ¦    ¦    ¦     provided:                       ¦ ¦ ¦     Navigation            ¦    ¦    ¦     a)Current Aeronautical Charts   ¦ ¦ ¦     Databases             ¦    ¦    ¦       are used to verify            ¦ ¦ ¦                           ¦    ¦    ¦       Navigational Fixes prior to   ¦ ¦ ¦                           ¦    ¦    ¦       dispatch.                     ¦ ¦ ¦                           ¦    ¦    ¦     b)Procedures are established    ¦ ¦ ¦                           ¦    ¦    ¦       and used to verify status     ¦ ¦ ¦                           ¦    ¦    ¦       and suitability of            ¦ ¦ ¦                           ¦    ¦    ¦       Navigation Facilities used    ¦ ¦ ¦                           ¦    ¦    ¦       to define route of flight,    ¦ ¦ ¦                           ¦    ¦    ¦       and                           ¦ ¦ ¦                           ¦    ¦    ¦     c)Approach Navigation Radios    ¦ ¦ ¦                           ¦    ¦    ¦       are manually tuned and        ¦ ¦ ¦                           ¦    ¦    ¦       identified.                     ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 8        ¦ PAGE:    ¦ ¦          CESSNA MODELS 310/320           ¦                       ¦          ¦ ¦                                          ¦ DATE: 11/22/2002      ¦ 34-9     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 34  NAVIGATION            ¦    ¦    ¦                                       ¦

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

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

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 8        ¦ PAGE:    ¦ ¦          CESSNA MODELS 310/320           ¦                       ¦          ¦ ¦                                          ¦ DATE: 11/22/2002      ¦ 35-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 35  OXYGEN                ¦    ¦    ¦                                       ¦

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

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 8        ¦ PAGE:    ¦ ¦          CESSNA MODELS 310/320           ¦                       ¦          ¦ ¦                                          ¦ DATE: 11/22/2002      ¦ 37-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 37  VACUUM/PRESSURE       ¦    ¦    ¦                                       ¦

¦ 1.  Vacuum Pumps        B ¦ 2  ¦ 1  ¦ (M)One may be inoperative for VMC     ¦ ¦                           ¦    ¦    ¦ operations.                           ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 8        ¦ PAGE:    ¦ ¦          CESSNA MODELS 310/320           ¦                       ¦          ¦ ¦                                          ¦ DATE: 11/22/2002      ¦ 61-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 61  PROPELLERS            ¦    ¦    ¦                                       ¦

¦ 1.  Synchronizer/       C ¦ 1  ¦ 0  ¦                                       ¦ ¦     Synchrophasing System ¦    ¦    ¦                                       ¦

¦ 2.  Unfeathering        C ¦ 2  ¦ 0  ¦                                       ¦ ¦     Accumulator System    ¦    ¦    ¦                                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 8        ¦ PAGE:    ¦ ¦          CESSNA MODELS 310/320           ¦                       ¦          ¦ ¦                                          ¦ DATE: 11/22/2002      ¦ 77-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 77  ENGINE INDICATING     ¦    ¦    ¦                                       ¦

¦ 1.  Economy Mixture     C ¦ 2  ¦ 0  ¦                                       ¦ ¦     Indicators (EGT)      ¦    ¦    ¦                                       ¦