Revision: 7

Date: 09/11/2006

DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

WASHINGTON, D.C.

MASTER MINIMUM EQUIPMENT LIST

Piper PA 60-600, 601, 601P, 602P,

700P

***************************************     For Part 91 Operations Only ***************************************

Federal Aviation Administration Aircraft Evaluation Group DOT Building, Room 332 901 Locust       Street Kansas City, MO                    64106-2641

Telephone:

FAX:

(816)-329-3233

(816)-329-3241

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21-1

22-1

23

24-1

25

26-1

28-1

30

30-1

31-1

35-1

37-1

61-1

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

Piper PA 60-600, 601, 601P, 602P,

700P

REVISION: 7

DATE: 09/11/2006

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, XIII, XIV

-- Preamble

XV, XVI

XVII, XVIII, XIX

                  Guidelines for (O) & (M) Procedures 21 Air Conditioning

22 Auto Flight

Communications

24 Electrical Power

23-1, 2, 3

Equipment/Furnishings

25-1, 2, 3

26 Fire Protection

28 Fuel

Ice and Rain Protection

31 Indicating/Recording Systems

33 Lights

34 Navigation

33-1, 2

34-1 THRU 10

35 Oxygen

37 Vacuum/Pressure

61 Propellers

DEPARTMENT OF TRANSPORTATION

  1

5

6

6

6

6

6

7

7

7

7

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

Piper PA 60-600, 601, 601P, 602P,

700P

REVISION: 7

DATE: 09/11/2006

PAGE NO:

II

Log of Revisions

Rev No.

Date

Page Numbers

Initials

Original 07/02/1979 N/A

03/02/1981

Pages 21, 30, 33

2 04/16/1985 ALL PAGES

3 01/06/1986 30-1

4 04/19/1989 ALL PAGES

06/26/1989

HIGHLIGHTS OF REV., DEFINITIONS

5 06/26/1989 PREAMBLE

5a

04/29/1993

HIGHLIGHTS OF REV., DEFINITIONS

5a 04/29/1993 34-1

5b

12/04/1996

HIGHLIGHTS OF REV., DEFINITIONS

5b 12/04/1996 GUIDELINES

5b

12/04/1996

21-1, 22-1, 23-1, 23-2, 24-1

25-1, 25-2, 26-1, 28-1, 30-1

5b

5b

12/04/1996

12/04/1996

31-1, 33-1, 33-2, 34-1, 34-2

34-3, 34-4, 35-1, 37-1, 61-1

5b

12/04/1996

06/18/2002

HIGHLIGHTS OF REV., DEFINITIONS

6 06/18/2002 GUIDELINES

06/18/2002

21-1, 22-1, 23-1, 23-2, 24-1

25-1, 25-2, 26-1, 28-1, 30-1

06/18/2002

06/18/2002

31-1, 33-1, 33-2, 34-1, 34-2

34-3, 34-4, 34-5, 35-1, 37-1

06/18/2002

6 06/18/2002 61-1

09/11/2006

7 09/11/2006 GUIDELINES

HIGHLIGHTS OF REV., DEFINITIONS

09/11/2006

09/11/2006

22-1, 23-1, 23-2, 23-3, 25-1, 25-2, 25-3

31-1, 33-1, 34-1, 34-3, 34-4, 34-5, 34-6

09/11/2006

34-7, 34-8, 34-9, 34-10, 35-1

DEPARTMENT OF TRANSPORTATION

  -

7

7

7

7

7

7

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

Piper PA 60-600, 601, 601P, 602P,

700P

REVISION: 7

DATE: 09/11/2006

PAGE NO:

III

Control Page

System

Page No.

Rev. No.

Current Date

Cover Page

Table of Contents

09/11/2006

09/11/2006

I

II

Log of Revisions

Control Page

09/11/2006

09/11/2006

III

IV 7 09/11/2006

Highlights of Change

V

VI 7 09/11/2006

09/11/2006

Definitions VII 9 07/05/2005 VIII 9 07/05/2005 IX

X

9 07/05/2005

                          9 07/05/2005 XI 9 07/05/2005 XII 9 07/05/2005 XIII 9 07/05/2005 XIV 9 07/05/2005 Preamble XV 2 06/14/1989 XVI 2 06/14/1989

Guidelines for (O) & (M) Procedures

XVII

XVIII 7 09/11/2006

09/11/2006

XIX

21 21-1 6 06/18/2002

7 09/11/2006

22 22-1 7 09/11/2006

23 23-1 7 09/11/2006

23-2 7 09/11/2006

23-3 7 09/11/2006

24 24-1 6 06/18/2002

25 25-1 7 09/11/2006

25-2 7 09/11/2006

25-3 7 09/11/2006

26 26-1 6 06/18/2002

28 28-1 6 06/18/2002

30 30-1 6 06/18/2002

31 31-1 7 09/11/2006

33 33-1 7 09/11/2006

33-2 6 06/18/2002

34 34-1 7 09/11/2006

34-2 6 06/18/2002

34-3 7 09/11/2006

34-4 7 09/11/2006

34-5 7 09/11/2006

34-6 7 09/11/2006

34-7 7 09/11/2006

34-8 7 09/11/2006

34-9 7 09/11/2006

34-10 7 09/11/2006

DEPARTMENT OF TRANSPORTATION

  MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

Piper PA 60-600, 601, 601P, 602P,

700P

REVISION: 7

DATE: 09/11/2006

PAGE NO:

IV

Control Page

System

Page No.

Rev. No.

Current Date

35 35-1 7 09/11/2006

37 37-1 6 06/18/2002

61 61-1 6 06/18/2002

DEPARTMENT OF TRANSPORTATION

  MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

Piper PA 60-600, 601, 601P, 602P,

700P

REVISION: 7

DATE: 09/11/2006

PAGE NO:

V

HIGHLIGHTS OF CHANGE

Definitions

Updated IAW PL-25, Global Change 131.

Guidelines

[(O) & (M)]

Updated IAW applicable Policy Letter Provisos.

ATA 22-1

Added (M) procedure to Auto Pilot proviso per PL-101 (GC-103) to ensure no fault exists that could interfere with any flight control function.

ATA 23-4

Proviso updated IAW PL-09 (GC-119) to comply with wording in the Policy Letter.

ATA 23-5

Updated IAW PL-58 (GC-100) for Boom Microphone relief.

ATA 23-7

Updated IAW PL-106 (GC-135) to grant relief for HF equipment.

ATA 25-1

Updated IAW PL-79 (GC-134) to add proviso for Passenger Seat Armrest relief.

ATA 25-5

Updated to add relief for Non-Essential Equipment IAW PL-116 (GC- 138).

ATA 25-6

Changed to comply with applicable Emergency Medical Equipment proviso phraseology in PL-73 (GC-130).

ATA 25-7

Updated proviso wording IAW PL-100 (GC-114) for Cargo Restraint Systems.

ATA 31-3

Added relief for Flight Data Recorder IAW PL-87 (GC-136).

ATA 33-3

Updated IAW PL-77 (GC-63) for change in lighting title and proviso.

ATA 33-5

Updated IAW PL-72 (GC-54) for change in title to “Wing Illumination Lights” and other proviso rewording.

DEPARTMENT OF TRANSPORTATION

  MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

Piper PA 60-600, 601, 601P, 602P,

700P

REVISION: 7

DATE: 09/11/2006

PAGE NO:

VI

HIGHLIGHTS OF CHANGE

ATA 34-4

Added proviso for Windshear Detection and Avoidance System IAW PL- 67 (GC-88).

ATA 34-13

Removed “***” symbol in the title to comply with PL-32 (GC-115).

ATA 34-15

Updated IAW PL-10 to standardize relief for the Non-Stabilized Magnetic Compass.

ATA 34-18

Updated item IAW PL-67 (GC-88) and PL-54 (GC-132) to add Windshear Warning and Flight Guidance System and provisos to TAWS/GPWS.

ATA 34-19

Updated IAW PL-98 (GC-71) to add Flight Management System Navigation Database relief.

ATA 34-20

Updated to add relief for Navigation Management System Navigation Database IAW PL-98 (GC-71).

ATA 34-21

Updated to add relief for ADS-B equipped aircraft per PL-105 (GC-86).

ATA 34-22

Updated to add relief for the Chelton Flight Logic Instrument System IAW PL-115 (GC-123).

ATA 34-23

Updated to add relief for Standby Attitude Indicator per PL-111.

ATA 35-2

Updated IAW PL-43 to add relief for Protective Breathing Equipment.

DEPARTMENT OF TRANSPORTATION

  MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

Piper PA 60-600, 601, 601P, 602P,

700P

REVISION: 9

DATE: 07/05/2005

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 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 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 the 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:

Piper PA 60-600, 601, 601P, 602P,

700P

REVISION: 9

DATE: 07/05/2005

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 (ETOPS) which has a type design approval for ER operations (ETOPS) 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:

Piper PA 60-600, 601, 601P, 602P,

700P

REVISION: 9

DATE: 07/05/2005

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:

Piper PA 60-600, 601, 601P, 602P,

700P

REVISION: 9

DATE: 07/05/2005

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

  12

DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

Piper PA 60-600, 601, 601P, 602P,

700P

REVISION: 9

DATE: 07/05/2005

PAGE NO:

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. Boeing (B-717, MD-10, MD-11)

These 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-318/320/319/321, 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-318/320/319/ 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-318/319/320/321, 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-318/319/320/321) or CMS (A-330/A- 340) interrogation. The systems are designed to be fault tolerant. For A- 318/319/320/321, MAINTENANCE STATUS (Class II) do not affect dispatch but are listed in the MMEL.  Dispatch is allowed without specific conditions except for:

-  BLUE RSVR MAINTENANCE status:  If applicable, and

-  AIR BLEED MAINTENANCE status: As applicable.

For the A-330 and A-340, MAINTENANCE status messages do not affect dispatch.

  MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

PIPER PA-30 AND 39

REVISION: 6

DATE:01/31/1995

PAGE:

XII

DEFINITIONS

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.

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.

e.  CANADAIR  (CL-65, CL-604)

Canadair aircraft equipped with Engine Indication and Crew Alerting Systems (EICAAS) provide four classes of messages (WARNING, CAUTION, ADVISORY, and STATUS). Any message that affects aircraft dispatch will be at the WARNING, CAUTION, or STATUS level.

System conditions that only require maintenance are not visible to the flight crew.  These maintenance indications/messages are only activated by maintenance personnel using the Maintenance Diagnostics Computer.

f.  EMBRAER (EMB-135/145, ERJ-170 Series)

The EMB-135/145 and ERJ-170/190 are equipped with an Engine Indicating and Crew Alerting System (EICAS) that provides three different message levels:  WARNING, CAUTION, and ADVISORY.  The ERJ-170/190 Series add STATUS messages.

Failures that effect dispatchability are presented to the flight crew at one of these levels. Other failures may be presented only to the maintenance personnel on the Multi Function Display (MFD) maintenance pages or through the download of the Central Maintenance Computer (CMC).  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.

DEPARTMENT OF TRANSPORTATION

  MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

Piper PA 60-600, 601, 601P, 602P,

700P

REVISION: 9

DATE: 07/05/2005

PAGE NO:

XIII

DEFINITIONS

g.  GULFSTREAM (G-IV, G-V, GV-SP, and GIV-X)

Gulfstream airplanes equipped with EICAS provide different priority levels of system messages:  WARNING (red), CAUTION (amber), ADVISORY, STATUS and MAINTENANCE (cyan or blue).  Any WARNING or CAUTION message affects airplane dispatch status and requires that the Airplane Flight Manual or the MEL be used to determine dispatch capability.  STATUS messages which indicate a system failure (e.g., FMS-1 fail) require that the Airplane Flight Manual or the MEL be used to determine dispatch capability.  Maintenance messages do not affect airplane dispatch status.  They indicate the presence of a system fault which can be identified by Maintenance Data Acquisition Unit (MDAU on the G-V) interrogation, Central Maintenance Computer (CMC on the GV-SP/GIV-X) interrogation or by reference to the Airplane Flight Manual.

h.  De- HAVILLAND (DASH 8 SERIES 400)

Series 400 aircraft are equipped with a Caution/Warning Panel that annunciates all cautions and warnings.  Advisory messages are displayed by the Electronic Indication System (EIS) or individual advisory lights supplied in the cockpit.

“Class 1 failures” are failures that prevent continued operation of a specific Line Replacement Unit or channel and are annunciated via advisory messages:  caution, warning or advisory lights in the flight compartment.  Dispatch with such posted failures are to be in accordance with the MMEL.

“Class 2 failures” are failures which do not prevent continued system function.  These faults will not be annunciated to the flight crew and the absence of the higher level alert (warning, caution, advisory) indicates that the system/component is operating within its approved operating limits or tolerances.  Such faults would be evident during maintenance interrogation performed during maintenance activities.  Class 2 faults do not affect dispatch and will be listed in the Fault Isolation Manual (FIM).  Class 2 faults will be left to the discretion of the operators when these faults are to be rectified.

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.

DEPARTMENT OF TRANSPORTATION

  D."

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

Piper PA 60-600, 601, 601P, 602P,

700P

REVISION: 9

DATE: 07/05/2005

PAGE NO:

XIV

DEFINITIONS

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:

Piper PA 60-600, 601, 601P, 602P,

700P

REVISION: 1

DATE: 07/05/1990

PAGE NO:

XV

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:

Piper PA 60-600, 601, 601P, 602P,

700P

REVISION: 1

DATE: 07/05/1990

PAGE NO:

XVI

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 THE MMEL IS REQUIRED

DEPARTMENT OF TRANSPORTATION

  21-5

21-8

21-10

22-1

23-4-1

23-7

25-7

31-2

33-5

34-4-1

34-8

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

Piper PA 60-600, 601, 601P, 602P,

700P

REVISION: 7

DATE: 09/11/2006

PAGE NO:

XVII

Guidelines for (O) & (M) Procedures

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

(M) Maintenance procedure on how to block Safety Valve open for unpressurized flight.

(M) Maintenance procedure to ensure no fuel leak or mechanical/electrical fault exists that could cause damage in the Combustion Heater.

(M) Maintenance procedure to secure the air conditioner to ensure fault will not affect any other system.

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

(O) Operations procedure to establish and use an alternate means of communication for passenger briefings when the PA System is inoperative.

(O) Operations procedure to establish IAW the provisos when the HF is inoperative.

(M) Maintenance procedure to establish and use when the Cargo Restraint System is inoperative or missing provided acceptable Cargo Loading Limits from an approved source can be observed.

(O) Operational procedure to establish and use to record flight time when the Flight Hour Recorder is inoperative.

(O) Operational procedure to ensure adequate light is available for wing surface inspection when the Wing Illumination Lights are inoperative.

(O) Operations procedure to establish and use when the Windshear Detection and Avoidance System is inoperative if the Windshear Warning and Flight Guidance System operates normally and takeoffs and landings are not conducted in known or forecast windshear conditions.

(O) Operations procedure to ensure pilot awareness of altitude when the Altitude Alerting System is inoperative and the Altitude Hold is operative.

DEPARTMENT OF TRANSPORTATION

  34-12

34-12

34-13

34-13

34-13-2

34-13-3

34-15

34-18-1

34-18-2

34-19-1

34-20-1

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

Piper PA 60-600, 601, 601P, 602P,

700P

REVISION: 7

DATE: 09/11/2006

PAGE NO:

XVIII

Guidelines for (O) & (M) Procedures

(M) Maintenance procedure to ensure the TCAS I System is deactivated and secured.

(O) Operations procedure to ensure enroute and approach procedures do not require the use of TCAS I and it is not required by FAR.

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

(O) Operations procedure to establish and use that ensures enroute and approach procedures do not require the use of TCAS II.

(O) Operations procedure to ensure TA visual display and audio functions are operative, TA only mode is selected by the crew and enroute and approach procedures do not require use of the Resolution Advisory Display System(s).

(O) Operations procedure to ensure RA visual display and audio functions are operative and enroute or approach procedures do not require use of the Traffic Alert Display System(s).

(O) Operations procedure to establish and use when the Non-Stabilized Magnetic Compass System is inoperative to ensure compliance with the requirements of the proviso.

(O) Operations procedure to establish alternate procedures when TAWS/GPWS is inoperative.

(O) Operations procedure to establish alternate procedures, determine the Windshear Detection and Avoidance System operates normally, and ensure takeoffs and landings are not conducted in known or forecast windshear conditions.

(O) Operations procedure established to ensure current charts are used, procedures are established to verify status and suitability of Navigational Facilities used and Navigation Radios are manually tuned and identified.

(O) Operations procedure established to ensure current charts are used, procedures are established to verify status and suitability of Navigational Facilities used and Navigation Radios are manually tuned and identified.

DEPARTMENT OF TRANSPORTATION

  34-22-3

34-22-4

37-1

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

Piper PA 60-600, 601, 601P, 602P,

700P

REVISION: 7

DATE: 09/11/2006

PAGE NO:

XIX

Guidelines for (O) & (M) Procedures

(M) Maintenance procedure established to ensure remaining AHRS is verified to be fully operational.

(M) Maintenance procedure established to ensure remaining ADC is verified to be fully operational.

(M) Maintenance procedure to ensure remaining Vacuum/Pressure Pump is verified to be operating normally prior to flight.

DEPARTMENT OF TRANSPORTATION

  21-1

1.

1

0

1

0

3.

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4.

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5.

1

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6.

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7.

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9.

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(M)

1

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MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

Piper PA 60-600, 601, 601P, 602P,

700P

REVISION NO: 6

DATE: 06/18/2002

PAGE NO:

1. REPAIR CATEGORY

2. NUMBER INSTALLED

3. NUMBER REQUIRED FOR DISPATCH

4. REMARKS AND EXCEPTIONS

SYSTEM

SEQUENCE &

NUMBERS

21 AIR CONDITIONING

Cabin Altimeter

C

May be inoperative for unpressurized

flight.

2. Cabin Differential

Pressure Indicator

C

May be inoperative for unpressurized

flight.

Cabin Rate of Climb

Indicator

C

May be inoperative provided Cabin Altimeter and Cabin Differential Pressure Indicator are operative.

Outflow Valve

C

May be inoperative for unpressurized flight provided Safety Valve is in DUMP position.

Safety Valve

C

(M) May be inoperative for unpressurized flight provided Safety Valve is blocked open.

Pressurization Controller

C

May be inoperative for unpressurized

flight.

Cabin Altitude Warning

Light

C

May be inoperative for unpressurized

flight.

8. Combustion Heater

C

0  (M)

Heater Fail Light

C

May be inoperative provided heater is not operated.

10. Air Conditioner

C

11.  Heater Hour Meter

C

NOTE:  Page 21-1, Items 1 through 7, of this MMEL apply to pressurized aircraft only.

DEPARTMENT OF TRANSPORTATION

  22-1

1.

-

0

2.

-

-

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

Piper PA 60-600, 601, 601P, 602P,

700P

REVISION NO: 7

DATE: 09/11/2006

PAGE NO:

1. REPAIR CATEGORY

2. NUMBER INSTALLED

3. NUMBER REQUIRED FOR DISPATCH

4. REMARKS AND EXCEPTIONS

SYSTEM

SEQUENCE &

NUMBERS

22 AUTO FLIGHT

Autopilot System

C

(M) May be inoperative provided

operations do not require its use.

|

Autopilot Disconnect

C

One may be inoperative provided the autopilot is not utilized at less than initial approach altitude.

DEPARTMENT OF TRANSPORTATION

  23-1

-

-

2.

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3.

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1)

1

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a)

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MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

Piper PA 60-600, 601, 601P, 602P,

700P

REVISION NO: 7

DATE: 09/11/2006

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 and UHF)

D

Any in excess of those required by FAR may be inoperative provided it is not powered by the Emergency Power Source and not required for emergency procedures.

Cockpit Speaker

C

May be inoperative provided two operative headsets are available to the flight crew.

Audio Amplifier

C

May be inoperative provided two operative headsets are available to the flight crew.

4. Passenger Address

System (PA)

Passenger Configuration

C

(O) May be inoperative provided:

PA not required by FAR and Alternate, normal and emergency procedures, and/or operating

|

|

|

restrictions are established and

used.

|

|

NOTE:  Any station function(s) that

operate normally may be used.

|

|

|

2) Cargo Configuration

C

D

May be inoperative provided alternate,

normal and emergency procedures,

|

|

and/or operating restrictions are

established and used.

May be inoperative provided procedures

do not require its use.

|

|

|

|

DEPARTMENT OF TRANSPORTATION

  23-2

5.

1)

-

0

a)

b)

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2)

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-

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6.

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0

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

Piper PA 60-600, 601, 601P, 602P,

700P

REVISION NO: 7

DATE: 09/11/2006

PAGE NO:

1. REPAIR CATEGORY

2. NUMBER INSTALLED

3. NUMBER REQUIRED FOR DISPATCH

4. REMARKS AND EXCEPTIONS

SYSTEM

SEQUENCE &

NUMBERS

23 COMMUNICATIONS

Boom Microphones

|

COCKPIT VOICE RECORDER (CVR) WITH FLIGHT DATA RECORDER INSTALLED

|

|

|

|

|

Cockpit Voice Recorder Equipped to Record Boom Microphone per FAR 135.151(d)

A

May be inoperative provided:

Flight Data Recorder (FDR) operates normally and 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.

|

|

|

COCKPIT VOICE RECORDER (CVR) WITHOUT FLIGHT DATA RECORDER INSTALLED

|

|

|

|

|

Cockpit Voice Recorder Equipped to Record Boom Microphone per FAR 135.151(d)

A

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

|

|

|

|

Cockpit Voice Recorder Not Equipped to Record Boom Microphone

D

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

|

|

|

***  (CVR)

Cockpit Voic

e Recorder

A

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

DEPARTMENT OF TRANSPORTATION

  23-3

23

7.

-

-

-

1

a)

b)

c)

d)

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

Piper PA 60-600, 601, 601P, 602P,

700P

REVISION NO: 7

DATE: 09/11/2006

PAGE NO:

1. REPAIR CATEGORY

2. NUMBER INSTALLED

3. NUMBER REQUIRED FOR DISPATCH

4. REMARKS AND EXCEPTIONS

SYSTEM

SEQUENCE &

NUMBERS

COMMUNICATIONS

High Frequency  (HF)

Communication System

D

C

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

(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 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.

|

|

|

|

|

|

|

|

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|

DEPARTMENT OF TRANSPORTATION

  24-1

1.

2.

2

0

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

Piper PA 60-600, 601, 601P, 602P,

700P

REVISION NO: 6

DATE: 06/18/2002

PAGE NO:

1. REPAIR CATEGORY

2. NUMBER INSTALLED

3. NUMBER REQUIRED FOR DISPATCH

4. REMARKS AND EXCEPTIONS

SYSTEM

SEQUENCE &

NUMBERS

24 ELECTRICAL POWER

Alternator

DELETED REVISION 4

Alternator Warning Light

B

DEPARTMENT OF TRANSPORTATION

  25-1

1.

-

-

a)

b)

c)

-

-

2)

-

-

a)

b)

2

1

3.

-

-

4.

1

0

1

0

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

Piper PA 60-600, 601, 601P, 602P,

700P

REVISION NO: 7

DATE: 09/11/2006

PAGE NO:

1. REPAIR CATEGORY

2. NUMBER INSTALLED

3. NUMBER REQUIRED FOR DISPATCH

4. REMARKS AND EXCEPTIONS

SYSTEM

SEQUENCE &

NUMBERS

25 EQUIPMENT/

FURNISHINGS

Passengers Seat(s)

C

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:  A seat with an inoperative seatbelt is considered inoperative.

1) Recline Mechanism

C

May be inoperative and seat occupied provided seat is secured in the upright position.

Armrest

C

May be inoperative or missing and seat occupied provided:

|

|

Armrest does not block an

Emergency Exit and

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

|

|

|

|

|

2. Cockpit Shoulder

Harness

B

May be inoperative on right side provided seat remains unoccupied.

Flotation Equipment

C

As required by FAR.

Emergency Locator

Transmitter (ELT)

C

As required by FAR.

C

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

DEPARTMENT OF TRANSPORTATION

  25-2

-

-

-

-

-

-

2)

-

-

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

Piper PA 60-600, 601, 601P, 602P,

700P

REVISION NO: 7

DATE: 09/11/2006

PAGE NO:

1. REPAIR CATEGORY

2. NUMBER INSTALLED

3. NUMBER REQUIRED FOR DISPATCH

4. REMARKS AND EXCEPTIONS

SYSTEM

SEQUENCE &

NUMBERS

25 EQUIPMENT/

FURNISHINGS

5. 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.

Non-Essential Equipment & 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 operators (insert Name) Manual. (M)

|

|

|

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

|

|

the operator’s appropriate document.

|

|

6. Emergency Medical

Equipment

1) Emergency Medical Kit and/or Associated Equipment

D

Any in excess of those required by FAR may be incomplete, missing or

|

|

inoperative provided that at least one kit contains the minimum content required by

|

|

the FARs.

|

First Aid Kit and/or

Associated Equipment

D

Any in excess of those required by FAR may be incomplete, missing, or

|

|

inoperative.  The number of kits required by the FARs must contain the minimum

|

|

content as required by FARs.

|

DEPARTMENT OF TRANSPORTATION

  25-3

7.

-

-

-

-

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

Piper PA 60-600, 601, 601P, 602P,

700P

REVISION NO: 7

DATE: 09/11/2006

PAGE NO:

1. REPAIR CATEGORY

2. NUMBER INSTALLED

3. NUMBER REQUIRED FOR DISPATCH

4. REMARKS AND EXCEPTIONS

SYSTEM

SEQUENCE &

NUMBERS

25 EQUIPMENT/

FURNISHINGS

Cargo Restraint Systems

C

C

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

|

|

|

May be inoperative, or missing provided cargo compartment remains empty.

|

|

|

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|

DEPARTMENT OF TRANSPORTATION

  26-1

-

-

a)

b)

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

Piper PA 60-600, 601, 601P, 602P,

700P

REVISION NO: 6

DATE: 06/18/02

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

Extinguisher(s)

D

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

The inoperative fire extinguisher is tagged inoperative, removed from its installed location and placed out of sight so that it can not be mistaken for a functional unit and

Required distribution is

maintained.

2. Engine Fire Detection

System

DELETED REVISION 6.

DEPARTMENT OF TRANSPORTATION

  28-1

1.

1

0

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

Piper PA 60-600, 601, 601P, 602P,

700P

REVISION NO: 6

DATE: 06/18/2002

PAGE NO:

1. REPAIR CATEGORY

2. NUMBER INSTALLED

3. NUMBER REQUIRED FOR DISPATCH

4. REMARKS AND EXCEPTIONS

SYSTEM

SEQUENCE &

NUMBERS

28 FUEL

Fuel Flow Totalizer

C

DEPARTMENT OF TRANSPORTATION

  30-1

1.

1

0

2.

1

0

3.

1

0

1

0

1

0

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

Piper PA 60-600, 601, 601P, 602P,

700P

REVISION NO: 6

DATE: 06/18/2002

PAGE NO:

1. REPAIR CATEGORY

2. NUMBER INSTALLED

3. NUMBER REQUIRED FOR DISPATCH

4. REMARKS AND EXCEPTIONS

SYSTEM

SEQUENCE &

NUMBERS

30  ICE AND RAIN

PROTECTION

Surface Deice System (Wing, Vertical, and Horizontal Stabilizer)

C

May be inoperative provided aircraft is not operated in known or forecast icing conditions.

Propeller Deice System

C

May be inoperative provided aircraft is not operated in known or forecast icing conditions.

Pitot Heater

B

Must be operative for IFR passenger carrying and for flight in known or forecast icing conditions.  Two heated pitot tubes are required for these conditions if a second airspeed indicator is installed and operative.

4. Windshield Deicing

System (Alcohol)

C

May be inoperative provided aircraft is not operated in known or forecast icing conditions.

5. Windshield Anti-Icing

System (Electric)

C

May be inoperative provided aircraft is not operated in known or forecast icing conditions.

DEPARTMENT OF TRANSPORTATION

  31-1

1.

1

0

2.

1

0

(O)

-

-

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

Piper PA 60-600, 601, 601P, 602P,

700P

REVISION NO: 7

DATE: 09/11/2006

PAGE NO:

1. REPAIR CATEGORY

2. NUMBER INSTALLED

3. NUMBER REQUIRED FOR DISPATCH

4. REMARKS AND EXCEPTIONS

SYSTEM

SEQUENCE &

NUMBERS

31 INDICATING/

RECORDING SYSTEMS

Clock with Sweep Second Hand or Electric Digital Clock

C

May be inoperative for VFR operations.

Flight Hour Recorder

C

3. Flight Data Recorder

(FDR) System

C

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

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|

DEPARTMENT OF TRANSPORTATION

  33-1

1.

1

0

2.

3

0

-

-

a)

b)

c)

2

2

0

1

5.

-

0

6.

1

0

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

Piper PA 60-600, 601, 601P, 602P,

700P

REVISION NO: 7

DATE: 09/11/2006

PAGE NO:

1. REPAIR CATEGORY

2. NUMBER INSTALLED

3. NUMBER REQUIRED FOR DISPATCH

4. REMARKS AND EXCEPTIONS

SYSTEM

SEQUENCE &

NUMBERS

33 LIGHTS

Anti-Collision Beacon

Light System

B

May be inoperative for day operations.

Position Lights

C

May be inoperative for day operations.

3. Cockpit/Flight Deck/Flight

Compartment and

C

Instrument Lighting

System

Individual lights may be inoperative

provided remaining lights are:

Sufficient to clearly illuminate all required instruments, controls and other devices for which it is provided,

Positioned so that direct rays are shielded from flight crewmembers eyes and

Lighting configuration and intensity is acceptable to the flight crew.

|

|

|

4. Landing Lights

C

C

Both may be inoperative for day operations.

One may be inoperative for night operations.

Wing Illumination Lights

C

(O) May be inoperative provided ground deicing procedures do not require their

|

|

use.

|

Strobe Light System

C

DEPARTMENT OF TRANSPORTATION

  33-2

7.

-

-

a)

b)

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

Piper PA 60-600, 601, 601P, 602P,

700P

REVISION NO: 6

DATE: 06/18/2002

PAGE NO:

1. REPAIR CATEGORY

2. NUMBER INSTALLED

3. NUMBER REQUIRED FOR DISPATCH

4. REMARKS AND EXCEPTIONS

SYSTEM

SEQUENCE &

NUMBERS

33 LIGHTS

Cabin Lights

C

May be inoperative provided:

Sufficient lighting is operative for the crew to perform required duties and

Lighting configuration is

acceptable to the flight crew.

DEPARTMENT OF TRANSPORTATION

  34-

1

1.

1

0

2.

-

-

0

1

a)

b)

-

-

1

0

-

-

0

0

a)

b)

a)

b)

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

Piper PA 60-600, 601, 601P, 602P,

700P

REVISION NO: 7

DATE: 09/11/2006

PAGE NO:

1. REPAIR CATEGORY

2. NUMBER INSTALLED

3. NUMBER REQUIRED FOR DISPATCH

4. REMARKS AND EXCEPTIONS

SYSTEM

SEQUENCE &

NUMBERS

34 NAVIGATION

Gyroscopic Rate of

Turn/Slip Skid Indicator

B

Must be operative on left side for IFR, passenger carrying VFR over-the-top, and passenger carrying VFR night flights.

ATC Transponders and Automatic Altitude Reporting Systems

C

D

May be inoperative provided:

Enroute operations do not

require its use and

Prior to flight, approval is obtained from ATC facilities having jurisdiction over the planned route of flight.

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

3. Navigation Equipment (VOR/ILS, Loran, Omega/VLF, INS, Doppler, GPS, MLS, RNAV)

C

As required by FAR.

4. Weather

Radar/Thunderstorm

Detection Equipment

C

As required by FAR.

1) Windshear Detection and  C Avoidance System

C

(O) May be inoperative provided: Alternate procedures are established and used and Windshear Warning and Flight Guidance System operates normally.

(O) May be inoperative provided: Alternate procedures are established and used and Takeoffs and landings not conducted in known or forecast windshear conditions.

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DEPARTMENT OF TRANSPORTATION

  34-

2

5.

1

0

1

0

-

-

8.

-

-

0

0

a)

b)

c)

1

0

-

-

-

0

-

-

0

0

a)

b)

a)

b)

c)

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

Piper PA 60-600, 601, 601P, 602P,

700P

REVISION NO: 6

DATE: 06/18/2002

PAGE NO:

1. REPAIR CATEGORY

2. NUMBER INSTALLED

3. NUMBER REQUIRED FOR DISPATCH

4. REMARKS AND EXCEPTIONS

SYSTEM

SEQUENCE &

NUMBERS

34 NAVIGATION

Marker Beacon Receiver

C

May be inoperative provided approach

procedure does not require its use.

6. Radar Altimeter

C

7. Distance Measuring Equipment (DME) Systems

D

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

Altitude Alerting System

A

C

(O) May be inoperative provided:

Autopilot with altitude hold is

operative,

Enroute operations do not require

its use and

Repairs are made within three

flight days.

May be inoperative provided it is not required by FAR.

9. RMI

C

10.  ADF

D

As required by FAR.

11.  Moving Map Display

***

C

12. Traffic Alert Collision Avoidance System (TCAS I)

B

C

(M)(O) May be inoperative provided: System is deactivated and secured and

Enroute or approach procedures

do not require its use.

(M)(O) May be inoperative provided: