Revision: 2

Date:  03/27/2006

DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

WASHINGTON, D.C.

MASTER MINIMUM EQUIPMENT LIST

********************************

* For Part 91 Ops Only       * ********************************

CE-525A

Kansas City Aircraft Evaluation Group MKC-AEG                               DOT Building

901 Locust Street, Room 332

Kansas City, MO 64106

Telephone:

FAX:

(816)-329-3233

(816)-329-3241

  --

--

--

--

--

--

--

21

21-6

22-1

23

24-1

25

26

27-1

28-1

30

31

32-1

33

34

34

35-1

38-1

52-1

73

73-1

77-1

78-1

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

CE-525A

REVISION NO. 2

DATE: 03/27/2006

PAGE NO.

I

TABLE OF CONTENTS

SYSTEM

SYSTEM NO.

PAGE NO.

Table of Contents

Log of Revisions

I

II

Control Page

Highlights of Change

III, IV

V, VI

Definitions

-- Definitions

VII, VIII, IX, X

XI, XII

-- Preamble

XIII, XIV

XV, XVI

Guidelines for (O) & (M) Procedures Guidelines for (O) & (M) Procedures

XVII, XVIII

21-1, 2, 3, 4, 5

                  Air Conditioning 21 Air Conditioning 22 Auto Flight

Communications

24 Electrical Power

23-1, 2, 3, 4

Equipment/Furnishings

Fire Protection

25-1, 2, 3

26-1, 2

27 Flight Controls

28 Fuel

Ice and Rain Protection

Indicating/Recording Systems

30-1, 2

31-1, 2

32 Landing Gear

Lights

33-1, 2, 3

34-1, 2, 3, 4, 5

Navigation

Navigation

34-6, 7, 8, 9

35 Oxygen

38 Water/Waste

52 Doors

Engine Fuel & Control

77 Engine Indicating

78 Engine Exhaust

DEPARTMENT OF TRANSPORTATION

  1

2

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

CE-525A

REVISION: 2

DATE: 03/27/2006

PAGE NO:

II

Log of Revisions

Rev No.

Date

Page Numbers

Initials

Original 01/25/2002 ORIGINAL

05/15/2003

HIGHLIGHTS OF REV.,DEFINITIONS

1 05/15/2003 GUIDELINES

1 05/15/2003 25-1,25-2,25-3,28-1,32-1 1 05/15/2003 34-1,34-2,34-3,34-4,34-6 1 05/15/2003 34-7,73-1,78-1

1a

1a

12/06/2004

12/06/2004

HIGHLIGHTS OF REV.,DEFINITIONS

24-1,25-3

03/27/2006

2 03/27/2006 GUIDELINES

HIGHLIGHTS OF REV.,DEFINITIONS

2 03/27/2006 21-6,23-2,23-4,25-1,25-2,26-1,26-2,27-1

2 03/27/2006 31-1,32-1,33-1,34-1,34-5,

2 03/27/2006 34-6,34-7,52-1,78-1

DEPARTMENT OF TRANSPORTATION

  -

2

2

2

2

2

2

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

CE-525A

REVISION: 2

DATE: 03/27/2006

PAGE NO:

III

Control Page

System

Page No.

Rev. No.

Current Date

Cover Page

Table of Contents

03/27/2006

03/27/2006

I

II

Log of Revisions

Control Page

03/27/2006

03/27/2006

III

IV 2 03/27/2006

Highlights of Change

V

VI 2 03/27/2006

03/27/2006

Definitions VII 6 01/31/1995 VIII 6 01/31/1995 IX

X

6 01/31/1995

                           6 01/31/1995 XI 6 01/31/1995 XII 6 01/31/1995 Preamble XIII 2 06/14/1989 XIV 2 06/14/1989

Guidelines for (O) & (M) Procedures

XV

XVI 2 03/27/2006

03/27/2006

XVII 2 03/27/2006

XVIII 2 03/27/2006

21 21-1 Original 01/25/2002 21-2 Original 01/25/2002 21-3 Original 01/25/2002 21-4 Original 01/25/2002 21-5 Original 01/25/2002   21-6 2 03/27/2006 22 22-1 Original 01/25/2002 23 23-1 Original 01/25/2002 23-2 2 03/27/2006 23-3 Original 01/25/2002 23-4 2 03/27/2006 24 24-1 1 a 12/06/2004   25 25-1 2 03/27/2006 25-2 2 03/27/2006 25-3 1 a 12/06/2004 26 26-1     2 03/27/2006 26-2 2   03/27/2006 27 27-1 2   03/27/2006 28 28-1 1                                                                                                              05/15/2003

DEPARTMENT OF TRANSPORTATION

  MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

CE-525A

REVISION: 2

DATE: 03/27/2006

PAGE NO:

IV

Control Page

System

30 30-1 Original 01/25/2002

Page No.

Rev. No.

Current Date

                                                                         30-2 Original 01/25/2002 31 31-1 2 03/27/2006 31-2 Original 01/25/2002 32 32-1 2 03/27/2006 33 33-1 2 03/27/2006 33-2 Original 01/25/2002 33-3 Original 01/25/2002 34 34-1 2 03/27/2006 34-2 1 05/15/2003 34-3 1 05/15/2003 34-4 1 05/15/2003 34-5 2 03/27/2006 34-6 2 03/27/2006 34-7 2 03/27/2006 34-8 Original 01/25/2002 34-9 Original 01/25/2002 35 35-1 Original 01/25/2002 38 38-1 Original 01/25/2002 52 52-1 2 03/27/2006 73 73-1 1 05/15/2003 77 77-1 Original 01/25/2002 78 78-1 2 03/27/2006

DEPARTMENT OF TRANSPORTATION

  128.

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

CE-525A

REVISION NO. 2

DATE: 03/27/2006

PAGE NO.

V

HIGHLIGHTS OF CHANGE

ATA 21

Item 17, Nose Avionics Fan. Removed Note: “See AFM Limitations and Procedures” as there are no procedures or limitations required. Certification tests completed satisfactorily without this fan operating.

ATA 21

Item 18, Panel Avionics Fan. Made number variable and removed Note: “See AFM Limitations and Procedures” as there are no procedures or limitations required. For 525A units 300 and on only, a single Panel Avionics Fan is installed only if a Garmin 500 GPS is installed as FMS #2 option. Certification tests completed satisfactorily without this fan operating.

ATA 21

Item 19, Glareshield Avionics Fan. Reduced number to one to reflect actual airplane configuration and removed improper reference to units 360 and on.

ATA 23

Items 4A and 4B, Cockpit Voice Recorder (CVR). Revised Column 3, Number Required for Dispatch, in accordance with PL-29, Revision 4, GC-

ATA 23

Item 8, HF Communications System. Revised relief in accordance with PL- 106, Revision 3, GC-106.

ATA 25

Item 1, Passenger Seat. Relief revised in accordance with PL-79, Revision 4, GC-134.

ATA 25

Item 4, added relief for Non Essential Furnishings in accordance with Policy Letter 116, Global Change 138.

ATA 26

Items 2 and 3, Lavatory Fire Extinguisher and Smoke Detector Systems. Relief revised to delete requirement to secure Lavatory Door closed due to fact that there is an Emergency Exit located in the lavatory.

ATA 27

Item 1, Electric Trim. Relief deleted due to AFM Limitation that system must satisfactorily pass a preflight functional test.

ATA 27

Item 2, added relief for Angle of Attack Display provided Stall Warning is operable.

ATA 31

Item 3, Flight Data Recorder. Relief revised in accordance with PL-87.

ATA 32

Item 1, Anti-skid System relief added. Both CJ2 and CJ2+ Airplane Flight Manuals now have Abnormal Procedures allowing dispatch with the Anti-Skid System inoperative.

ATA 33

Item 3, Wing Illumination Light. Removed reference to ground deicing procedures and added remarks to allow portable light source.

DEPARTMENT OF TRANSPORTATION

  MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

CE-525A

REVISION NO. 2

DATE: 03/27/2006

PAGE NO.

VI

HIGHLIGHTS OF CHANGE

ATA 34

Item 2, Standby Attitude Indicator. Deleted. AFM limitation requires the Standby Attitude Indicator to pass a proper preflight test and is required for some Emergency Abnormal AFM procedures.

ATA 34

Item 7, ATC Transponders and Automatic Altitude Reporting Systems. Repair Category changed to B in accordance with PL-76, GC-133.

ATA 34

Item 14, added relief for Class B TAWS in accordance with PL-54, Global Change 139.

ATA 38

Item 2, Lavatory Waste System. Deleted proviso requiring door to be secured CLOSED due to requirement for access to Emergency Exit.

ATA 52

Added item 1, CABIN DOOR Annunciator. Same relief as for CE-525 units 600 and on. (CJ1+)

ATA 52

Added item 2, Baggage Door – FWD Annunciator. Same relief as for CE-525 units 600 and on. (CJ1+)

ATA 52

Added item 3, Baggage Door – FWD Annunciator. Same relief as for CE-525 units 600 and on. (CJ1+)

ATA 52

Added item 4, Door Key Locks. Same relief as for CE-525 units 600 and on. (CJ1+)

ATA 78

Item 1, Thrust Attenuators. Added qualifier that they are installed only on (525A units 1- 299) and added remarks: See AFM Limitation and Abnormal Procedure as there is a limitation against dispatching with both Thrust Attenuators and Antiskid inoperative.

DEPARTMENT OF TRANSPORTATION

  MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

CE-525A

REVISION: 6

DATE:01/31/1995

PAGE NO:

VII

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 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 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.

DEPARTMENT OF TRANSPORTATION

  MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

CE-525A

REVISION: 6

DATE:01/31/1995

PAGE NO:

VIII

DEFINITIONS

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 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).

DEPARTMENT OF TRANSPORTATION

  MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

CE-525A

REVISION: 6

DATE:01/31/1995

PAGE NO:

IX

DEFINITIONS

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 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.

DEPARTMENT OF TRANSPORTATION

  a.

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

CE-525A

REVISION: 6

DATE:01/31/1995

PAGE NO:

X

DEFINITIONS

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 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.

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.

DEPARTMENT OF TRANSPORTATION

  MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

CE-525A

REVISION: 6

DATE:01/31/1995

PAGE:

XI

DEFINITIONS

System conditions that result only in a maintenance level message, i.e. no correlation with a higher level EICAS message, do not affect dispatch and do not require action other than as addressed within an operator’s 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 affects 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)

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.

DEPARTMENT OF TRANSPORTATION

  D."

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

CE-525A

REVISION: 6

DATE:01/31/1995

PAGE:

XII

DEFINITIONS

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 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

DEPARTMENT OF TRANSPORTATION

  MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

CE-525A

REVISION: 1

DATE: 07/05/1990

PAGE NO:

XIII

PREAMBLE

(07/05/1990)

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 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.

DEPARTMENT OF TRANSPORTATION

  MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

CE-525A

REVISION: 1

DATE: 07/05/1990

PAGE NO:

XIV

PREAMBLE

(07/05/1990)

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 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.

DEPARTMENT OF TRANSPORTATION

  21-1

21-2

21-3

21-4

21-5

21-10

21-12

21-13

21-14

21-15

22-1

22-2

23-3

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

CE-525A

REVISION: 2

DATE: 03/27/2006

PAGE NO:

XV

Guidelines for (O) & (M) Procedures

(O) Operations procedure to ensure the Flow Control Valve is CLOSED. One method would be to perform a Pressurization Preflight Test.

(O) Operations procedure to ensure the Flow Control Valve is CLOSED. One method would be to perform a Pressurization Preflight Test.

(O) Operations procedure to ensure the Emergency Pressurization Solenoid Valve is CLOSED.

(O) Operations procedure to ensure the Windshield Anti-Ice Flow Control and Shutoff Valve is CLOSED.

(O) Operations procedure to ensure the Cabin Pressurization Auto Schedule is operating normally. One method would be to perform a Pressurization Preflight Test.

(M) Maintenance procedure to ensure the flow of service air to the Cabin Door Primary Seal is prevented.

(O) Operations procedure to ensure the Isobaric and Manual Modes are operating normally.

(M) Maintenance procedure to pull and collar the Freon Air Conditioning System circuit breaker.

(M) Maintenance Procedure to secure the Air Conditioner and ensure it has not adversely affected any other structure or system.

(M) Maintenance procedure to secure Cabin Outflow Valve(s) in the OPEN position.

(M) Maintenance procedure to ensure no electrical or mechanical fault exists that will have an adverse effect on any flight control system.

(M) Maintenance procedure to ensure no electrical or mechanical fault exists that will have an adverse effect on any flight control system.

(O) Operations procedure to ensure Normal and Emergency procedures and/or operating restrictions are established, used and given to the passengers.

DEPARTMENT OF TRANSPORTATION

  23-8

25-1

25-1-1

25-9

26-1

30-3

30-4

31-2

32-1

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

CE-525A

REVISION:2

DATE: 03/27/2006

PAGE NO:

XVI

Guidelines for (O) & (M) Procedures

(O) Operations procedure to ensure the SATCOM System operates normally.

(M) Maintenance procedure to ensure affected seat is secured and placarded.

(M) Maintenance procedure to ensure affected seat recline mechanism is secure in the up-right position.

(M) Maintenance procedure to ensure Cargo Compartment components are removed or secured and the aircraft Weight and Balance document is current.

(O) Operations procedure to remove and tag the affected fire extinguisher from its holder and place out of site.

(M) Maintenance procedure to ensure the Engine Anti-Ice Valve has failed in the Open position.

(M) Maintenance procedure to ensure the Engine Anti-Ice Valve has failed in the Closed position.

(O) Operations procedure to ensure the Wing Anti-Ice Valve has failed in the Closed position.

(O) Operations procedure to ensure that all flight times are recorded and added to the aircraft total time.

(O) Operations procedure to ensure that the flight crew has knowledge of differing procedures and aircraft performance data.

DEPARTMENT OF TRANSPORTATION

  33-3

33-7

34-9

34-12

34-13

34-13-1

34-13-2

34-13-3

34-14-1

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

CE-525A

REVISION: 2

DATE: 03/27/2006

PAGE NO:

XVII

Guidelines for (O) & (M) Procedures

(O) Operations procedure to ensure adequate light is available.

(O) Operations procedure to ensure that passengers are notified of Seat Belt and no smoking requirements.

(O) Operations procedure to ensure altitude awareness.

(O) Operations procedure to ensure three Compass Systems are available and appropriate for the intended flight.

(O) Operations procedure to operate with any combination of two stabilized Gyro or INS stabilized compass systems.

(O) Procedures to use Free Gyro techniques.

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

(O) Operations procedure to determine that enroute or approach procedures do not require it's use.

(O) Operations procedure to ensure the TA and RA displays are visible to the non-flying pilot and the audio functions are operative on the flying pilot side.

(O) Operations procedure to determine that enroute and approach procedures do not require it's use.

(O) Operations procedure to ensure all RA display/functions are operative.

(O) Operations procedure to ensure alternate procedures are established and used.

34-14-1 a)

(O) Operations procedure to ensure alternate procedures are established and used.

34-14-1 d)

(O) Operations procedure to ensure alternate procedures are established and used.

34-14-1 e)

(O) Operations procedure to ensure alternate procedures are established and used.

DEPARTMENT OF TRANSPORTATION

  34-16

34-17

38-1

38-2

52-1

52-2

52-3

78-1

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

CE-525A

REVISION: 2

DATE: 03/27/2006

PAGE NO:

XVIII

Guidelines for (O) & (M) Procedures

(O) Operations procedure to ensure that alternate procedures are established and used and that the Windshear Detection and Avoidance System operates normally.

(O) Operations procedure to ensure that alternate procedures are established and that takeoff and landings are not conducted in known or forecast windshear conditions.

(O) Operations procedure to ensure that alternate procedures are established and used and that the Windshear Warning and Guidance System operates normally.

(O) Operations procedure to ensure that alternate procedures are established and that takeoff and landings are not conducted in known or forecast windshear conditions.

(M) Maintenance procedures to ensure the affected components are deactivated and secured and that the system has no leaks.

(M) Maintenance procedure to drain the system and ensure the system is not serviced until after repair.

(M) Maintenance procedures to ensure the affected components are deactivated and secured and that the system has no leaks.

(O) Operations procedure to ensure alternate procedures are established and used to ensure the Cabin Door is properly closed and locked.

(O) Operations procedure to ensure alternate procedures are established and used to ensure the Forward Baggage Door is properly closed and locked.

(O) Operations procedure to ensure alternate procedures are established and used to ensure the Aft Baggage Door is properly closed and locked.

(O) Operations procedure to ensure the AFM Performance Limitations are complied with.

DEPARTMENT OF TRANSPORTATION

  21-1

1.

2

1

a)

b)

c)

d)

2

1

a)

b)

1

0

a)

b)

1

0

a)

b)

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

CE-525A

REVISION NO: ORIGINAL

DATE: 01/25/2002

PAGE NO:

1. REPAIR CATEGORY

2. NUMBER INSTALLED

3. NUMBER REQUIRED FOR DISPATCH

4. REMARKS AND EXCEPTIONS

SYSTEM

SEQUENCE &

NUMBERS

21 AIR CONDITIONING

Flow Control Valve

C

(O) One may be inoperative provided:

Flight is conducted unpressurized, Air Source Selector remains FRESH AIR or OFF,

All other components and functions of the Pressurization System operate normally, and Crew and passengers comply with any applicable oxygen requirements.

2. Pressure Regulating

Shutoff Valves

C

(O) One may be inoperative provided:

This affected Pressure regulating Shutoff Valve is verified in the Closed position, and

All other components and functions of the Pressurization System operate normally.

3. Emergency

Pressurization Solenoid

Valve

C

(O) May be inoperative provided:

The Emergency Pressurization Solenoid Valve is verified closed, and

Flight is conducted unpressurized.

4. Windshield Anti-Ice Flow

Control and Shutoff

C

(O) May be inoperative provided:

The Windshield Anti-Ice Flow Control and Shutoff Valve is verified closed, and

The flight is not conducted into known or forecast icing conditions.

DEPARTMENT OF TRANSPORTATION

  21-2

1

0

a)

b)

1

0

a)

b)

6.

1

0

1

0

7.

1

0

a)

b)

1

0

a)

b)

c)

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

CE-525A

REVISION NO: ORIGINAL

DATE: 01/25/2002

PAGE NO:

1. REPAIR CATEGORY

2. NUMBER INSTALLED

3. NUMBER REQUIRED FOR DISPATCH

4. REMARKS AND EXCEPTIONS

SYSTEM

SEQUENCE &

NUMBERS

21 AIR CONDITIONING

5. Cabin Differential

Pressure Gauge

C

May be inoperative provided:

Flight is conducted unpressurized,

and

Crew and passengers comply with any applicable oxygen requirements.

C

(O) May be inoperative provided:

Cabin Altimeter is operating

normally, and

Cabin Pressurization Auto

Schedule is operating normally.

Cabin Altitude Warning

System

C

May be inoperative for unpressurized

flight.

C

May be inoperative for pressurized flight at or below 10,000 feet MSL.

Cabin Altimeter

C

May be inoperative provided:

Flight is conducted unpressurized,

and

Crew and passengers comply with any applicable oxygen requirements.

C

May be inoperative provided:

Cabin Differential Pressure Gauge

is operating normally,

Cabin Altitude Warning System is

operating normally, and

Cabin Pressurization Auto

Schedule is operating normally.

DEPARTMENT OF TRANSPORTATION

  21-3

8.

1

0

1

0

a)

b)

c)

9.

1

0

1

0

a)

b)

c)

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

CE-525A

REVISION NO: ORIGINAL

DATE: 01/25/2002

PAGE NO:

1. REPAIR CATEGORY

2. NUMBER INSTALLED

3. NUMBER REQUIRED FOR DISPATCH

4. REMARKS AND EXCEPTIONS

SYSTEM

SEQUENCE &

NUMBERS

21 AIR CONDITIONING

Automatic Cabin Air

Temperature

C

May be inoperative provided Manual Cabin Air Temperature Control System is operative normally.

C

May be inoperative provided:

Flight is conducted unpressurized, Cabin Pressurization Air Source Selector remains in OFF or FREST AIR, and

Crew and passengers comply with any applicable oxygen requirements.

Manual Cabin Air Temperature Control System

C

May be inoperative provided the Automatic Cabin Air Temperature Control System is operating normally.

C

May be inoperative provided:

Flight is conducted unpressurized, Cabin Pressurization Air Source Selector remains in OFF or FRESH AIR, and

Crew and passengers comply with any applicable oxygen requirements.

DEPARTMENT OF TRANSPORTATION

  21-4

1

0

a)

b)

c)

d)

e)

1

0

a)

b)

c)

1

0

a)

b)

c)

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

CE-525A

REVISION NO: ORIGINAL

DATE: 01/25/2002

PAGE NO:

1. REPAIR CATEGORY

2. NUMBER INSTALLED

3. NUMBER REQUIRED FOR DISPATCH

4. REMARKS AND EXCEPTIONS

SYSTEM

SEQUENCE &

NUMBERS

21 AIR CONDITIONING

10.  Cabin Door Primary Seal

C

(M) May be inoperative provided:

Service Air System is operating

normally,

Any leak of the service air is stopped,

Cabin Pressurization Source Selector Switch remains in OFF or FRESH AIR,

Flight is conducted unpressurized,

and

Crew and passengers comply with any applicable oxygen requirements.

11.  Cabin Door Secondary

Seal

C

May be inoperative provided:

The Secondary Seal does not

interfere with door operation,

The Primary Seal is operative, and The flight is conducted at or below 25,000 feet MSL with passengers or, at or below 31,000 feet without passengers.

C

May be inoperative provided:

The flight is conducted

unpressurized,

Cabin Pressurization Air Source Selector remains in OFF or FRESH AIR, and

Crew and passengers comply with any applicable oxygen requirements.

DEPARTMENT OF TRANSPORTATION

  21-5

1

0

a)

b)

1

0

a)

b)

c)

2

0

1

0

a)

b)

2

0

a)

b)

c)

d)

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

CE-525A

REVISION NO: ORIGINAL

DATE: 01/25/2002

PAGE NO:

1. REPAIR CATEGORY

2. NUMBER INSTALLED

3. NUMBER REQUIRED FOR DISPATCH

4. REMARKS AND EXCEPTIONS

SYSTEM

SEQUENCE &

NUMBERS

21 AIR CONDITIONING

12. Pressurization Controller

(Auto Schedule Mode)

C

(O) May be inoperative provided:

The Isobaric Mode is used, and Manual Mode is operating normally.

C

May be inoperative provided:

The flight is conducted

unpressurized,

Cabin Pressurization Air Source Selector remains in OFF or FRESH AIR, and

Crew and passengers comply with any applicable oxygen requirements.

13.  Cabin Fans

C

(M) May be inoperative provided the Freon Air Conditioning circuit breaker is pulled and collared.

14.  Freon Air Conditioning

System

C

(M) May be inoperative provided:

Freon Air Conditioning System is

deactivated, and

Cabin Temperature Control

System is operating normally.

15.  Cabin Outflow Valves

C

(M) May be inoperative provided:

At least one valve is secured OPEN,

Cabin Pressurization Air Source selector remains in OFF or FRESH AIR,

The flight is conducted

unpressurized, and

Crew and passengers comply with any applicable oxygen requirements.

DEPARTMENT OF TRANSPORTATION

  21-6

1

0

1

0

1

0

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

CE-525A

REVISION NO: 2

DATE: 03/27/2006

PAGE NO:

1. REPAIR CATEGORY

2. NUMBER INSTALLED

3. NUMBER REQUIRED FOR DISPATCH

4. REMARKS AND EXCEPTIONS

SYSTEM

SEQUENCE &

NUMBERS

21 AIR CONDITIONING

16.  Fresh Air Fan

C

May be inoperative provided the normal Pressurization System is operating normally.

17.  Nose Avionics Fan

C

|

|

|

|

18.  Panel Avionics Fans

(annunciated)

C - 0

|

19.  Glareshield Avionics Fan

C

May be inoperative except for ground operations at temperatures greater than

|

|

ISA plus 5 degrees C.

|

DEPARTMENT OF TRANSPORTATION

  22-1

1.

-

0

2.

1

0

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

CE-525A

REVISION NO: ORIGINAL

DATE: 01/25/2002

PAGE NO:

1. REPAIR CATEGORY

2. NUMBER INSTALLED

3. NUMBER REQUIRED FOR DISPATCH

4. REMARKS AND EXCEPTIONS

SYSTEM

SEQUENCE &

NUMBERS

22 AUTO FLIGHT

Autopilot

C

(M) May be inoperative provided

operations do not require its use.

Yaw Damper

C

(M) May be inoperative provided aircraft is operated using a crew of two.

DEPARTMENT OF TRANSPORTATION

  23-1

-

-

2.

1

0

1)

1

0

1

-

a)

b)

2)

1

0

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

CE-525A

REVISION NO: ORIGINAL

DATE: 01/25/2002

PAGE NO:

1. REPAIR CATEGORY

2. NUMBER INSTALLED

3. NUMBER REQUIRED FOR DISPATCH

4. REMARKS AND EXCEPTIONS

SYSTEM

SEQUENCE &

NUMBERS

23 COMMUNICATIONS

1. Communications

Systems (VHF, UHF)

C

Any in excess of those required by FAR may be inoperative provided it is not powered by the Emergency AC Bus, Emergency DC Bus, Battery Bus, Battery Direct Bus, or the DC Transfer Bus, and not required for emergency procedures.

Copilot’s Audio Control

Panel

C

May be inoperative for operations not requiring a Second in Command.

3. Passenger Address (PA)

System

Passenger Configuration

B

(O) May be inoperative provided Alternate, Normal and Emergency procedures, and/or operating restrictions are established and used.

NOTE: Any station that operates normally may be used.

C

(O) May be inoperative provided:

PA is not required by FAR, and Alternate, Normal and Emergency Procedures, and/or operating restrictions are established and used.

NOTE: Any station that operates normally may be used.

Cargo Configuration

D

May be inoperative unless procedures

require its use.

DEPARTMENT OF TRANSPORTATION

  23-2

4.

A)

1

0

a)

b)

B)

1

0

1)

-

0

a)

b)

2)

-

0

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

CE-525A

REVISION NO: 2

DATE: 03/27/2006

PAGE NO:

1. REPAIR CATEGORY

2. NUMBER INSTALLED

3. NUMBER REQUIRED FOR DISPATCH

4. REMARKS AND EXCEPTIONS

SYSTEM

SEQUENCE &

NUMBERS

23 COMMUNICATIONS

Cockpit Voice Recorder

(CVR)

With Fight Data Recorder

(FDR) Installed

A

May be inoperative:

Flight Data Recorder (FDR) operates normally, and Repairs are made within three flight days.

|

I

Without Flight Data

Recorder (FDR) Installed

A

May be inoperative provide repairs are made within three flight days.

|

5. Boom Microphones (With Flight Data Recorder Installed)

Cockpit Voice Recorder quipped to record Boom Microphone per FAR 121.359(g), 135.151(d) or 125.227(e).

A

May be inoperative provided:

Flight Data Recorder (FDR)

operates normally, and

Repairs made within three flight

days.

***  equipped to record Boom Microphone.

Cockpit Voice not

D

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

DEPARTMENT OF TRANSPORTATION

  23-3

1)

-

0

2)

-

0

1

0

7.

15

11

a)

b)

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

CE-525A

REVISION NO: ORIGINAL

DATE: 01/25/2002

PAGE NO:

1. REPAIR CATEGORY

2. NUMBER INSTALLED

3. NUMBER REQUIRED FOR DISPATCH

4. REMARKS AND EXCEPTIONS

SYSTEM

SEQUENCE &

NUMBERS

23 COMMUNICATIONS

5. Boom Microphones

(CON’T.) (Without Flight

Data Recorder Installed)

Cockpit Voice Recorder equipped to record Boom Microphone per FAR 121.359(g), 135.151(d) or 125.227(e).

A

May be inoperative provided repairs are made within three flight days.

***  not equipped to record

Cockpit Voic

e Recorder

Boom Microphone.

D

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

6. Recorded (Talking)

Checklist Function

C

May be inoperative provided written or displayed checklist is available to and used by the flight crew.

Static Wicks

C

One static wick may be missing or broken from each of the following areas:

Right hand wingtip or aileron,

Left hand wingtip or aileron,

c) Rudder,

d) Elevator.

DEPARTMENT OF TRANSPORTATION

  23-4

8.

-

-

-

0

a)

b)

c)

d)

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

CE-525A

REVISION NO: 2

DATE: 03/27/2006

PAGE NO:

1. REPAIR CATEGORY

2. NUMBER INSTALLED

3. NUMBER REQUIRED FOR DISPATCH

4. REMARKS AND EXCEPTIONS

SYSTEM

SEQUENCE &

NUMBERS

23 COMMUNICATIONS

High Frequency (HF)

Communication System

D

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

|

C

(O) May be inoperative while conducting operations that require two LRCS

|

|

provided:

SATCOM Voice or Data Link

operates normally,

Alternate procedures are established and used, SATCOM coverage is available over the intended route of the

|

|

|

flight, and

If Inmarsat codes are not available while using SATCOM voice, prior coordination with the appropriate

|

|

|

ATS facility is required.

|

|

|

|

|

|

NOTE: SATCOM is to be used only as a backup to normal HF communications

|

|

unless otherwise authorized by the

appropriate ATS facilities.

|

|

|

DEPARTMENT OF TRANSPORTATION

  24-1

1.

2

1

2.

3.

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

CE-525A

REVISION NO: 1 a

DATE: 12/06/2004

PAGE NO:

1. REPAIR CATEGORY

2. NUMBER INSTALLED

3. NUMBER REQUIRED FOR DISPATCH

4. REMARKS AND EXCEPTIONS

SYSTEM

SEQUENCE &

NUMBERS

24 ELECTRICAL POWER

DC Ammeters

B

One may be inoperative provided DC voltmeter and generator caution lights are operative.

***  Indicator

Battery Temperature

C 1 0

***  Switch

Ground Power Dispatch

C 1 0

DEPARTMENT OF TRANSPORTATION

  25-1

1.

-

-

a)

b)

c)

1)

-

-

2)

-

-

a)

b)

c)

2

1

3.

1

0

1

0

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

CE-525A

REVISION NO: 2

DATE: 03/27/2006

PAGE NO:

1. REPAIR CATEGORY

2. NUMBER INSTALLED

3. NUMBER REQUIRED FOR DISPATCH

4. REMARKS AND EXCEPTIONS

SYSTEM

SEQUENCE &

NUMBERS

25 EQUIPMENT/

FURNISHINGS

Passenger Seat

C

(M) May be inoperative provided:

Seat does not block an

Emergency Exit,

Seat does not restrict any passenger from access to the main aircraft aisle, and

The affected seat(s) are blocked and placarded “DO NOT OCCUPY”.

NOTE 1: A seat with an inoperative seatbelt is considered to be inoperative.

Recline Mechanism

C

(M) May be inoperative and seat occupied provided the seat is secured in the up- right position.

Armrest

C

May be inoperative or missing and the seat occupied provided:

|

|

Armrest does not block an

Emergency Exit,

Armrest does not restrict any passenger from access to the main aircraft aisle, and

For an armrest with a recline mechanism, seat is secured in the upright position.

|

|

|

|

|

|

|

|

2. Crewmember Shoulder

Harnesses

B

Right side may be inoperative for single pilot operations, however, the seat must remain unoccupied.

***  Locator Transmitter (ELT)

Aircraft Emergency

C

As required by FAR.

C

May be inoperative for published scheduled flights in scheduled air carrier service.

DEPARTMENT OF TRANSPORTATION

  25-2

-

-

-

-

5.

***

-

0

-

-

7.

-

-

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

CE-525A

REVISION NO: 2

DATE: 03/27/2006

PAGE NO:

1. REPAIR CATEGORY

2. NUMBER INSTALLED

3. NUMBER REQUIRED FOR DISPATCH

4. REMARKS AND EXCEPTIONS

SYSTEM

SEQUENCE &

NUMBERS

25 EQUIPMENT/

FURNISHINGS

4. Passenger Convenience

Items

(Expires on

November 1, 2007)

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

|

|

|

|

NOTE: Lavatory door ashtrays are not considered passenger convenience item.

Non-Essential Equipment and Furnishings (NEF) (Before or after November 1, 2007)

May be inoperative, damaged, or missing provided that the item(s) is deferred in

|

|

accordance with the operator’s NEF deferral program. The NEF program, procedures, and processes are outlined in the operator’s (insert name) Manual. (M)

|

|

|

and (O) procedures, if required, must be available to the flight crew and included in

|

|

the operator’s appropriate document.

|

|

NOTE: Exterior lavatory door ash trays are not considered NEF items.

|

|

Passenger Safety Chime

C

6. Emergency Medical

Equipment/First Aid Kits

C

Any in excess of those required by FAR may be incomplete or missing provided the required distribution is maintained.

“Fasten Seat Belt While

Seated” Sign or Placard

C

One or more signs or placards may be illegible or missing provided a legible sign or placard is visible from each occupied passenger seat.

DEPARTMENT OF TRANSPORTATION

  25-3

8.

1)

-

-

2)

1

0

9.

-

-

-

-

2

0

2

0

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

CE-525A

REVISION NO: 1 a

DATE: 12/06/2004

PAGE NO:

1. REPAIR CATEGORY

2. NUMBER INSTALLED

3. NUMBER REQUIRED FOR DISPATCH

4. REMARKS AND EXCEPTIONS

SYSTEM

SEQUENCE &

NUMBERS

25 EQUIPMENT/

FURNISHINGS

Exterior Lavatory Door

Ashtrays

Airplanes with more than one exterior lavatory door ashtray installed.

A

One may be missing provided it is replaced within 10 calendar days.

Airplanes with only one lavatory door ashtray installed.

A

May be missing provided it is replaced within 3 calendar days.

Cargo Restraint Systems

C

(M) May be inoperative, or missing such that the effect is that the item must be considered inoperative, provided acceptable cargo loading limits from an approved source, i.e., and Approved Cargo Loading Manual, Cargo Handling Manual, or Weight and Balance Document are observed.

C

May be inoperative, or missing such that the effect is that the item must be considered inoperative, provided cargo compartment remains empty.

10. Chart Holders

C

11.  Cockpit Sun Visors

C

May be inoperative provided the visors may be stowed so as not to obstruct the pilot’s field of view for takeoff and landing or the quick donning capability of the oxygen masks.

DEPARTMENT OF TRANSPORTATION

  26-1

-

-

a)

b)

-

-

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

CE-525A

REVISION NO: 2

DATE: 03/27/2006

PAGE NO:

1. REPAIR CATEGORY

2. NUMBER INSTALLED

3. NUMBER REQUIRED FOR DISPATCH

4. REMARKS AND EXCEPTIONS

SYSTEM

SEQUENCE &

NUMBERS

26 FIRE PROTECTION

1. Portable Fire

Extinguishers

D

(O) Any in excess of those required by FAR may be inoperative or missing provided:

The inoperative fire extinguisher is tagged inoperative, removed from the installed location, and placed out of sight so it can not be mistaken for functional unit, and Required distribution is maintained.

2. Lavatory Fire

Extinguisher System

C

For each lavatory the Lavatory Fire Extinguisher System may be inoperative provided Lavatory Smoke Detector System operates normally and the Lavatory Waste Receptacle remains empty.

|

|

|

NOTE: A Lavatory Fire Extinguisher System is not required for all-cargo operations.

DEPARTMENT OF TRANSPORTATION

  26-2