DEPARTMENT OF TRANSPORTATION     Revision: 6

                                                           Date: 01/23/2003

                         FEDERAL AVIATION ADMINISTRATION

 

                                WASHINGTON, D.C.

 

 

 

 

 

 

 

 

 

 

 

            M A S T E R   M I N I M U M   E Q U I P M E N T   L I S T

 

 

 

 

 

                               PIPER MODEL PA-44

 

 

 

 

 

 

 

 

 

 

 

 

 

                         FEDERAL AVIATION ADMINISTRATION

                         KANSAS CITY AIRCRAFT EVALUATION GROUP

                         DOT BUILDING, 901 LOCUST

                         ROOM 332

                         KANSAS CITY, MO  64106-2641

 

                         TELEPHONE:  (816) 329-3233

                               FAX:  (816) 329-3241


 

 

                       FEDERAL AVIATION ADMINISTRATION     Page: I

                                                           Revision: 6

                        MASTER MINIMUM EQUIPMENT LIST      Date: 01/23/2003

 

 

                             PIPER MODEL PA-44

 

 

                              Table of Contents

 

 

    SYSTEM NO.  SYSTEM                                  PAGE

 

 

         --     Table of Contents                       I

         --     Log of Revisions                        II

         --     Control Page                            III

         --     Highlights of Change                    IV, V

         --     Definitions                             VI, VII, VIII, IX

         --     Definitions                             X, XI, XII, XIII

         --     Preamble                                XIV, XV

         --     Guidelines for (O) & (M) Procedures     XVI, XVII

         21     Air Conditioning                        21-1

         22     Auto Flight                             22-1

         23     Communications                          23-1, 2

         25     Equipment/Furnishings                   25-1

         26     Fire Protection                         26-1

         27     Flight Controls                         27-1

         28     Fuel                                    28-1

         30     Ice and Rain Protection                 30-1

         31     Indicating/Recording Systems            31-1

         33     Lights                                  33-1

         34     Navigation                              34-1, 2, 3, 4, 5

         34     Navigation                              34-6

         37     Vacuum/Pressure                         37-1

         61     Propellers                              61-1

         77     Engine Indicating                       77-1


 

 

                       FEDERAL AVIATION ADMINISTRATION   Page: II

                                                         Revision: 6

                        MASTER MINIMUM EQUIPMENT LIST    Date: 01/23/2003

 

 

                             PIPER MODEL PA-44

 

 

                               Log of Revisions

 

      ----------------------------------------------------------------------

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

      ----------------------------------------------------------------------

      ¦ ORIGINAL ¦ 06/18/1980 ¦ ORIGINAL ISSUE                 ¦           ¦

      ¦ 1        ¦ 01/14/1985 ¦ COMPLETE REVISION              ¦           ¦

      ¦ 2        ¦ 04/19/1989 ¦ ALL PAGES                      ¦           ¦

      ¦ 3        ¦ 06/26/1989 ¦ HIGHLIGHTS OF REV.,DEFINITIONS ¦           ¦

      ¦ 3        ¦ 06/26/1989 ¦ PREAMBLE                       ¦           ¦

      ¦ 4        ¦ 06/12/1990 ¦ HIGHLIGHTS OF REV.,DEFINITIONS ¦           ¦

      ¦ 4        ¦ 06/12/1990 ¦ 23-1,25-1,25-2,26-1,30-1       ¦           ¦

      ¦ 4        ¦ 06/12/1990 ¦ 34-1,34-2,37-1                 ¦           ¦

      ¦ 5        ¦ 03/24/1994 ¦ HIGHLIGHTS OF REV.,DEFINITIONS ¦           ¦

      ¦ 5        ¦ 03/24/1994 ¦ 21-1,22-1,23-1,25-1,25-2       ¦           ¦

      ¦ 5        ¦ 03/24/1994 ¦ 26-1,27-1,28-1,30-1,31-1       ¦           ¦

      ¦ 5        ¦ 03/24/1994 ¦ 33-1,34-1,34-2,37-1,61-1       ¦           ¦

      ¦ 5        ¦ 03/24/1994 ¦ 77-1                           ¦           ¦

      ¦ 5a       ¦ 06/13/1996 ¦ HIGHLIGHTS OF REV.,DEFINITIONS ¦           ¦

      ¦ 5a       ¦ 06/13/1996 ¦ GUIDELINES                     ¦           ¦

      ¦ 5a       ¦ 06/13/1996 ¦ 21-1,31-1                      ¦           ¦

      ¦ 6        ¦ 01/23/2003 ¦ HIGHLIGHTS OF REV.,DEFINITIONS ¦           ¦

      ¦ 6        ¦ 01/23/2003 ¦ GUIDELINES                     ¦           ¦

      ¦ 6        ¦ 01/23/2003 ¦ 21-1,22-1,23-1,23-2,25-1       ¦           ¦

      ¦ 6        ¦ 01/23/2003 ¦ 25-2,26-1,27-1,30-1,31-1       ¦           ¦

      ¦ 6        ¦ 01/23/2003 ¦ 33-1,34-1,34-2,34-3,34-4       ¦           ¦

      ¦ 6        ¦ 01/23/2003 ¦ 34-5,34-6,77-1                 ¦           ¦

      ¦          ¦            ¦                                ¦           ¦

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      ¦          ¦            ¦                                ¦           ¦

      ¦          ¦            ¦                                ¦           ¦

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      ¦          ¦            ¦                                ¦           ¦

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      ¦          ¦            ¦                                ¦           ¦

      ¦          ¦            ¦                                ¦           ¦

      ¦          ¦            ¦                                ¦           ¦

      ¦          ¦            ¦                                ¦           ¦

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      ¦          ¦            ¦                                ¦           ¦

      ¦          ¦            ¦                                ¦           ¦

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      ¦          ¦            ¦                                ¦           ¦

      ¦          ¦            ¦                                ¦           ¦

      ----------------------------------------------------------------------


 

 

                       FEDERAL AVIATION ADMINISTRATION     Page: III

                                                           Revision: 6

                        MASTER MINIMUM EQUIPMENT LIST      Date: 01/23/2003

 

 

                             PIPER MODEL PA-44

 

 

                                 Control Page

 

 

         SYSTEM                                   PAGE  REV NO.  CURRENT DATE

 

 

         Cover Page                               -       6        01/23/2003

         Table of Contents                        I       6        01/23/2003

         Log of Revisions                         II      6        01/23/2003

         Control Page                             III     6        01/23/2003

         Highlights of Change                     IV      6        01/23/2003

                                                  V       6        01/23/2003

         Definitions                              VI      6        01/31/1995

                                                  VII     6        01/31/1995

                                                  VIII    6        01/31/1995

                                                  IX      6        01/31/1995

                                                  X       6        01/31/1995

                                                  XI      6        01/31/1995

                                                  XII     6        01/31/1995

                                                  XIII    6        01/31/1995

         Preamble                                 XIV     2        06/14/1989

                                                  XV      2        06/14/1989

         Guidelines for (O) & (M) Procedures      XVI     6        01/23/2003

                                                  XVII    6        01/23/2003

         21                                       21-1    6        01/23/2003

         22                                       22-1    6        01/23/2003

         23                                       23-1    6        01/23/2003

                                                  23-2    6        01/23/2003

         25                                       25-1    6        01/23/2003

         26                                       26-1    6        01/23/2003

         27                                       27-1    6        01/23/2003

         28                                       28-1    5        03/24/1994

         30                                       30-1    6        01/23/2003

         31                                       31-1    6        01/23/2003

         33                                       33-1    6        01/23/2003

         34                                       34-1    6        01/23/2003

                                                  34-2    6        01/23/2003

                                                  34-3    6        01/23/2003

                                                  34-4    6        01/23/2003

                                                  34-5    6        01/23/2003

                                                  34-6    6        01/23/2003

         37                                       37-1    5        03/24/1994

         61                                       61-1    5        03/24/1994

         77                                       77-1    6        01/23/2003


 

 

                       FEDERAL AVIATION ADMINISTRATION   Page: IV

                                                         Revision: 6

                        MASTER MINIMUM EQUIPMENT LIST    Date: 01/23/2003

 

 

                             PIPER MODEL PA-44

 

                            Highlights of Change

 

 

 

       ATA 22-1  Changed relief for Autopilot System in accordance with Policy

                 Letter 101, designated as Global Change 103.

 

       ATA 22-2  Added relief for Autopilot disconnect in accordance with

                 Policy Letter 93.

 

       ATA 23-1  Changed relief for Communications Systems in accordance with

                 Policy Letter 95, designated as Global Change 111 and moved

                 High Frequency (HF) Communications to ATA 23-5.

 

       ATA 23-3  Changed relief for Cockpit Voice Recorder System in accordance

                 with Policy Letter 29, designated as Global Change 48.

 

       ATA 23-4  Added relief for Boom Microphones in accordance with Policy

                 Letter 58, designated as Global Change 100.

 

       ATA 23-5  Added relief for High Frequency (HF) Communication System in

                 accordance with Policy Letter 106, designated as Global

                 Change 89.

 

       ATA 25-2  Changed relief for Passenger Seats in accordance with Policy

                 Letter 79, designated as Global Change 96.

 

       ATA 25-4  Deleted the word "OR" for clarification and compliance with

                 Policy Letter 31, designated as Global Change 83, and deleted

                 relief for other than "As required by FAR".

 

       ATA 25-5  Changed the number required for dispatch from a variable

                 quantity to "0" required in accordance with Policy Letter 33,

                 designated as Global Change 99.

 

       ATA 26-1  Changed relief for Portable Fire Extinguishers in accordance

                 with Policy Letter 75, designated as Global Change 53.

 

       ATA 27-1  Reformatted Remarks or Exceptions column in accordance with

                 Policy Letter 31, designated as Global Change 83.

 

       ATA 33-1  Changed the repair category and revised the proviso in

                 accordance with Policy Letter 77, designated as Global

                 Change 63.

 

       ATA 33-2  Deleted the word "OR" for clarification and compliance with

                 Policy Letter 31,designated as Global Change 83.


 

 

                       FEDERAL AVIATION ADMINISTRATION   Page: V

                                                         Revision: 6

                        MASTER MINIMUM EQUIPMENT LIST    Date: 01/23/2003

 

 

                             PIPER MODEL PA-44

 

                            Highlights of Change

 

 

 

       ATA 34-1  Revised and edited system description and remarks for

                 clarification.

 

       ATA 34-3  Changed relief for ATC Transponder and Automatic Altitude

                 Reporting Systems in accordance with Policy Letter 76,

                 designated as Global Change 110.

 

       ATA 34-8  Deleted relief for Altitude Encoder since it is now combined

                 with ATA Item 34-3.

 

       ATA 34-9  Changed relief for DME in accordance with Policy Letter 03.

 

       ATA 34-12 Deleted the word "OR" for clarification and reformatted the

                 remarks in accordance with Policy Letter 31,designated as

                 Global Change 83.

 

       ATA 34-13 Changed relief and added TCAS I in accordance with Policy

                 Letter 32, designated as Global Change 115.

 

       ATA 34-14 Added relief for TCAS II in accordance with Policy Letter 32,

                 designated as Global Change 115.

 

       ATA 34-15 Renumbered and changed relief for Ground Proximity Warning

                 System in accordance with Policy Letter 54, designated as

                 Global Change 107.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 


 

 

                       FEDERAL AVIATION ADMINISTRATION     Page: VI

                                                           Revision: 6

                        MASTER MINIMUM EQUIPMENT LIST      Date: 01/31/1995

 

 

                             PIPER MODEL PA-44

 

                                 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


 

 

                       FEDERAL AVIATION ADMINISTRATION     Page: VII

                                                           Revision: 6

                        MASTER MINIMUM EQUIPMENT LIST      Date: 01/31/1995

 

 

                             PIPER MODEL PA-44

 

                                 Definitions

 

 

       Certificate Data Sheet.

 

       3.  "As required by FAR" means that the listed item is subject to

       certain provisions (restrictive or permissive) expressed in the

       Federal Aviation Regulations operating rules.  The number of

       items required by the FAR must be operative.  When the listed

       item is not required by FAR it may be inoperative for time

       specified by repair category.

 

       4.  Each inoperative item must be placarded to inform and remind

       the crewmembers and maintenance personnel of the equipment

       condition.

 

       NOTE:  To the extent practical, placards should be located

       adjacent to the control or indicator for the item affected;

       however, unless otherwise specified, placard wording and location

       will be determined by the operator.

 

       5.  "-" symbol in Column 2 and/or Column 3 indicates a variable

       number (quantity) of the item installed.

                                                                           ¦

       6.  "Deleted" in the remarks column after a sequence item

       indicates that the item was previously listed but is now required

       to be operative if installed in the  aircraft.

 

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

       airplane which has a type design approval for ER operations and

       complies with the provisions of Advisory Circular 120-42A.           ¦

 

       8.  "Federal Aviation Regulations" (FAR) means the applicable

       portions of the Federal Aviation Act and Federal Aviation

       Regulations.

 

       9.  "Flight Day" means a 24 hour period (from midnight to

       midnight) either Universal Coordinated Time (UCT) or local time,

       as established by the operator, during which at least one flight

       is initiated for the affected aircraft.

 

       10.  "Icing Conditions" means an atmospheric environment that may

       cause ice to form on the aircraft or in the engine(s).

 

       11.  Alphabetical symbol in Column 4 indicates a proviso

       (condition or limitation) that must be complied with for


 

 

                       FEDERAL AVIATION ADMINISTRATION     Page: VIII

                                                           Revision: 6

                        MASTER MINIMUM EQUIPMENT LIST      Date: 01/31/1995

 

 

                             PIPER MODEL PA-44

 

                                 Definitions

 

 

       operation with the  listed item inoperative.

 

       12.  "Inoperative" means a system and/or component malfunction to

       the extent that it does not accomplish its intended purpose

       and/or is not consistently functioning normally within its

       approved operating limit(s) or tolerance(s).

 

       13.  "Notes:" in Column 4 provides additional information for

       crewmember or maintenance consideration.  Notes are used to

       identify applicable material which is intended to assist with

       compliance, but do not relieve the operator of the responsibility

       for compliance with all applicable requirements.  Notes are not a

       part of the provisos.

 

       14.  Inoperative components of an inoperative system:

       Inoperative items which are components of a system which is

       inoperative are usually considered components directly associated

       with and having no other function than to support that system.

       (Warning/caution systems associated with the inoperative system

       must be operative unless relief is specifically authorized per

       the MMEL).

 

       15.  "(M)" symbol indicates a requirement for a specific

       maintenance procedure which must be accomplished prior to

       operation with the listed item inoperative.  Normally these

       procedures are accomplished by maintenance personnel;  however,

       other personnel may be qualified and authorized to perform

       certain functions.  Procedures requiring specialized knowledge or

       skill, or requiring the use of tools or test equipment should be

       accomplished by maintenance personnel.  The satisfactory

       accomplishment of all maintenance procedures, regardless of

       who performs them, is the responsibility of the operator.

       Appropriate procedures are required to be published as part of

       the operator's manual or MEL.

 

       16.  "(O)" symbol indicates a requirement for a specific

       operations procedure which must be accomplished in planning for

       and/or operating with the listed item inoperative.  Normally

       these procedures are accomplished by the flight crew; however,

       other personnel may be qualified and authorized to perform

       certain functions.  The satisfactory accomplishment of all

       procedures, regardless of who performs them, is the

       responsibility of the operator.  Appropriate procedures are


 

 

                       FEDERAL AVIATION ADMINISTRATION     Page: IX

                                                           Revision: 6

                        MASTER MINIMUM EQUIPMENT LIST      Date: 01/31/1995

 

 

                             PIPER MODEL PA-44

 

                                 Definitions

 

 

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

       MEL.

 

       NOTE:  The (M) and (O) symbols are required in the operator's MEL

       unless otherwise authorized by the Administrator.

 

       17.  "Deactivated" and "Secured" means that the specified

       component must be put into an acceptable condition for safe

       flight.  An acceptable method of securing or deactivating will be

       established by the operator.

 

       18.  "Visual Flight Rules" (VFR) is as defined in FAR Part 91.

       This precludes a pilot from filing an Instrument Flight Rules

       (IFR) flight plan.

 

       19.  "Visual Meteorological Conditions" (VMC) means the

       atmospheric environment is such that would allow a flight to

       proceed under the visual flight rules applicable to the flight.

       This does not preclude operating under Instrument Flight Rules.

 

       20.  "Visible Moisture" means an atmospheric environment

       containing water in any form that can be seen in natural or

       artificial light; for example, clouds, fog, rain, sleet, hail, or

       snow.

 

       21.  "Passenger Convenience Items" means those items related to

       passenger convenience, comfort or entertainment such as, but not

       limited to, galley equipment, movie equipment, ash trays, stereo

       equipment, overhead reading lamps, etc.

 

       22.  Repair Intervals:  All users of an MEL approved under FAR

       121, 125, 129 and 135 must effect repairs of inoperative systems

       or components, deferred in  accordance with the MEL, at or prior

       to the repair times established by the following letter

       designators:

 

            Category A.  Items in this category shall be repaired within

       the time interval specified in the remarks column of the

       operator's approved MEL.

 

            Category B.  Items in this category shall be repaired within

       three (3) consecutive calendar days (72 hours), excluding the day

       the malfunction was recorded in the aircraft maintenance


 

 

                       FEDERAL AVIATION ADMINISTRATION     Page: X

                                                           Revision: 6

                        MASTER MINIMUM EQUIPMENT LIST      Date: 01/31/1995

 

 

                             PIPER MODEL PA-44

 

                                 Definitions

 

 

       record/logbook.  For example, if it were recorded at 10 a.m. on

       January 26th, the three day interval would begin at midnight the

       26th and end at midnight the 29th.

 

            Category C.  Items in this category shall be repaired within

       ten (10) consecutive calendar days (240 hours), excluding the day

       the malfunction was recorded in the aircraft maintenance

       record/logbook.  For example, if it were recorded at 10 a.m. on

       January 26th, the 10 day interval would begin at midnight the

       26th and end at midnight February 5th.

 

            Category D.  Items in this category shall be repaired within

       one hundred and twenty (120) consecutive calendar days (2880

       hours), excluding the day the malfunction was recorded in the

       aircraft maintenance log and/or record.

 

       The letter designators are inserted adjacent to Column 2.

 

       23. Electronic fault alerting system - General                  ¦

                                                                       ¦

       New generation aircraft display system fault indications to the ¦

       flight crew by use of computerized display systems.  Each       ¦

       aircraft manufacturer has incorporated individual design        ¦

       philosophies in determining the data that would be              ¦

       represented.  The following are customized definitions (specific¦

       to each manufacturer) to help determine the level of messages   ¦

       affecting the aircraft's dispatch status.  When preparing the   ¦

       MEL document, operators are to select the proper Definition No. ¦

       23 for their aircraft, if appropriate.                          ¦

                                                                       ¦

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

                                                                       ¦

       Boeing airplanes equipped with Engine Indicating and Crew       ¦

       Alerting  Systems (EICAS), provide different priority levels of ¦

       system messages (WARNING,  CAUTION, ADVISORY, STATUS and        ¦

       MAINTENANCE).  Any messages that affects airplane dispatch      ¦

       status will be displayed at a STATUS message level or  higher.  ¦

       The absence of an EICAS STATUS or higher level (WARNING,        ¦

       CAUTION, ADVISORY) indicates that the system/component is       ¦

       operating within its approved operating limits or tolerances.   ¦

                                                                       ¦

       System conditions that result only in a maintenance level       ¦

       message, i.e. no correlation with a higher level EICAS message, ¦


 

 

                       FEDERAL AVIATION ADMINISTRATION     Page: XI

                                                           Revision: 6

                        MASTER MINIMUM EQUIPMENT LIST      Date: 01/31/1995

 

 

                             PIPER MODEL PA-44

 

                                 Definitions

 

 

       do not affect dispatch and do not require action other than as  ¦

       addressed within an operators standard maintenance program.     ¦

                                                                       ¦

       b.   DOUGLAS  (MD-11)                                           ¦

                                                                       ¦

       Some Douglas aircraft are equipped with an alerting function    ¦

       which is a subsystem within the Electronic Instrument System    ¦

       (EIS).  The alerting function provides various levels of system ¦

       condition alerts (WARNING, CAUTION, ADVISORY, MAINTENANCE and   ¦

       STATUS).                                                        ¦

                                                                       ¦

       Alerts that affect aircraft dispatch will include WARNING,      ¦

       CAUTION, STATUS or MAINTENANCE level.  MAINTENANCE alerts are   ¦

       displayed on the status page of the EIS display panel under the ¦

       maintenance heading.                                            ¦

                                                                       ¦

       A MAINTENANCE alert on the EIS indicates the presence of a      ¦

       system fault which can be identified by the Central Fault       ¦

       Display System (CFDS) interrogation.  The systems are designed  ¦

       to be fault tolerant, however, for any MAINTENANCE alert, the   ¦

       MEL must be verified for dispatch purposes.                     ¦

                                                                       ¦

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

                                                                       ¦

       Airbus aircraft equipped with Electronic Centralized Aircraft   ¦

       Monitoring (ECAM) provide different levels of system condition  ¦

       messages (WARNING, CAUTION, STATUS, and ADVISORY). A-320/319/   ¦

       321, A-330, and A-340 also provide MAINTENANCE status messages. ¦

                                                                       ¦

       Any message that effects airplane dispatchability will normally ¦

       be at the WARNING, CAUTION or STATUS level. MAINTENANCE         ¦

       messages (A-320/319/321, A-330, and A-340 only) are also        ¦

       indicated on ECAM Status Page below the white Maintenance label.¦

                                                                       ¦

       A MAINTENANCE status (Class II) message on ECAM indicates the   ¦

       presence of a system fault which can be identified by CFDS      ¦

       (A-320/319/321) or CMS (A-330/A-340) interrogation. The systems ¦

       are designed to be fault tolerant, however for any MAINTENANCE  ¦

       status (Class II) message, the A-320/319/321 MEL must be        ¦

       verified for dispatch capability. For the A-330 and A-340,      ¦

       MAINTENANCE status messages do not affect dispatch.             ¦

 

       d.   FOKKER  (FK-100)                                           ¦


 

 

                       FEDERAL AVIATION ADMINISTRATION     Page: XII

                                                           Revision: 6

                        MASTER MINIMUM EQUIPMENT LIST      Date: 01/31/1995

 

 

                             PIPER MODEL PA-44

 

                                 Definitions

 

 

                                                                       ¦

       Fokker aircraft are equipped with Multi Function Display System ¦

       (MFDS) which provides electronic message referring to the       ¦

       different priority levels of system information (WARNING (red), ¦

       CAUTION (amber), AWARENESS (cyan) AND STATUS (white).  Any      ¦

       messages that affects aircraft dispatch will be at the WARNING, ¦

       CAUTION or AWARENESS level.  In these cases the MEL must be     ¦

       verified for dispatch capability and maintenance may be         ¦

       required.                                                       ¦

                                                                       ¦

       System conditions that only require maintenance are not         ¦

       presented on the flight deck.  These maintenance                ¦

       indications/messages may be presented on the Maintenance & Test ¦

       Panel (MAP) or the Centralized Fault Display Unit (CFDU) and by ¦

       dedicated Built In Test Evaluation (BITE) of systems.           ¦

 

       24.  "Administrative control item" means an item listed by the

       operator in the MEL for tracking and informational purposes.  It

       may be added to an operator's MEL by approval of the Principal

       Operations Inspector provided no relief is granted, or provided

       conditions and limitations are contained in an approved document

       (i.e. Structural Repair Manual, airworthiness directive, etc.).

       If relief other than that granted by an approved document is

       sought for an administrative control item, a request must be

       submitted to the Administrator.  If the request results in review

       and approval by the FOEB, the item becomes an MMEL item rather

       than an administrative control item.

 

       25.  "***" symbol in Column 1 indicates an item which is not

       required by regulation but which may have been installed on some

       models of aircraft covered by this MMEL.  This item may be

       included on the operator's MEL after the approving office has

       determined that the item has been installed on one or more of the

       operator's aircraft.  The symbol, however, shall not be carried

       forward into the operator's MEL.  It should be noted that neither

       this policy nor the use of this symbol provide authority to

       install or remove an item from an aircraft.

 

       26.  "Excess Items" means those items that have been installed

       that are redundant to the requirements of the FARs.

 

       27.  "Day of Discovery" is the calendar day an

       equipment/instrument malfunction was recorded in the aircraft


 

 

                       FEDERAL AVIATION ADMINISTRATION     Page: XIII

                                                           Revision: 6

                        MASTER MINIMUM EQUIPMENT LIST      Date: 01/31/1995

 

 

                             PIPER MODEL PA-44

 

                                 Definitions

 

 

       maintenance log and or record.  This day is excluded from the

       calendar days or flight days specified in the MMEL for the

       repair of an inoperative item of equipment. This provision is

       applicable to all MMEL items, i.e., categories "A, B, C, and

       D."

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 


 

 

                       FEDERAL AVIATION ADMINISTRATION   Page: XIV

                                                         Revision: 2

                        MASTER MINIMUM EQUIPMENT LIST    Date: 06/14/1989

 

 

                             PIPER MODEL PA-44

 

                                  Preamble

                            (Effective 6/14/89)

 

       The following is applicable for authorized certificate holders operating

       under Federal Aviation Regulations (FAR) Parts 121, 125, 129, 135: The

       FAR require that all equipment installed on an aircraft in compliance

       with the Airworthiness Standards and the Operating Rules must be

       operative.  However, the Rules also permit the publication of a Minimum

       Equipment List (MEL) where compliance with certain equipment

       requirements is not necessary in the interests of safety under all

       operating conditions.  Experience has shown that with the various levels

       of redundancy designed into aircraft, operation of every system or

       installed component may not be necessary when the remaining operative

       equipment can provide an acceptable level of safety.  A Master Minimum

       Equipment List (MMEL) is developed by the FAA, with participation by the

       aviation industry, to improve aircraft utilization and thereby provide

       more convenient and economic air transportation for the public.  The FAA

       approved MMEL includes those items of equipment related to airworthiness

       and operating regulations and other items of equipment which the

       Administrator finds may be inoperative and yet maintain an acceptable

       level of safety by appropriate conditions and limitations;  it does not

       contain obviously required items such as wings, flaps, and rudders.  The

       MMEL is the basis for development of individual operator MELs which take

       into consideration the operator's particular aircraft equipment

       configuration and operational conditions. Operator MELs, for

       administrative control, may include items not contained in the

       MMEL;  however, relief for administrative control items must be

       approved by the Administrator.  An operator's MEL may differ in

       format from the MMEL, but cannot be less restrictive than the MMEL.

       The individual operator's MEL, when approved and authorized, permits

       operation of the aircraft with inoperative equipment.

 

       Equipment not required by the operation being conducted and equipment in

       excess of FAR requirements are included in the MEL with appropriate

       conditions and limitations.  The MEL must not deviate from the Aircraft

       Flight Manual Limitations, Emergency Procedures or with Airworthiness

       Directives.  It is important to remember that all equipment related to

       the airworthiness and the operating regulations of the aircraft not

       listed on the MMEL must be operative.

 

 

 

 

 

 


 

 

                       FEDERAL AVIATION ADMINISTRATION   Page: XV

                                                         Revision: 2

                        MASTER MINIMUM EQUIPMENT LIST    Date: 06/14/1989

 

 

                             PIPER MODEL PA-44

 

                                  Preamble

                            (Effective 6/14/89)

 

       Suitable conditions and limitations in the form of placards, maintenance

       procedures, crew operating procedures and other restrictions as

       necessary are specified in the MEL to ensure that an acceptable level of

       safety is maintained.

 

       The MEL is intended to permit operation with inoperative items of

       equipment for a period of time until repairs can be accomplished.  It is

       important that repairs be accomplished at the earliest opportunity.  In

       order to maintain an acceptable level of safety and reliability the MMEL

       establishes limitations on the duration of and conditions for operation

       with inoperative equipment.  The MEL provides for release of the

       aircraft for flight with inoperative equipment.  When an item of

       equipment is discovered to be inoperative, it is reported by making an

       entry in the Aircraft Maintenance Record/Logbook as prescribed by FAR.

       The item is then either repaired or may be deferred per the MEL or other

       approved means acceptable to the Administrator prior to further

       operation.  MEL conditions and limitations, do not relieve the operator

       from determining that the aircraft is in condition for safe operation

       with items of equipment inoperative.

 

       When these requirements are met, an Airworthiness Release, Aircraft

       Maintenance Record/Logbook entry, or other approved documentation is

       issued as prescribed by FAR.  Such documentation is required prior to

       operation with any item of equipment inoperative.

 

       Operators are responsible for exercising the necessary operational

       control to ensure that an acceptable level of safety is maintained.

       When operating with multiple inoperative items, the interrelationships

       between those items and the effect on aircraft operation and crew

       workload will be considered.

 

       Operators are to establish a controlled and sound repair program

       including the parts, personnel, facilities, procedures, and schedules to

       ensure timely repair.

 

       WHEN USING THE MEL, COMPLIANCE WITH THE STATED INTENT OF THE PREAMBLE,

       DEFINITIONS, AND THE CONDITIONS AND LIMITATIONS SPECIFIED IN THE MEL IS

       REQUIRED.

 

 

 


 

 

                       FEDERAL AVIATION ADMINISTRATION   Page XVI

                                                         Revision: 6

                        MASTER MINIMUM EQUIPMENT LIST    Date: 01/23/2003

 

 

                             PIPER MODEL PA-44

 

 

                   Guidelines for (O) & (M) Procedures

 

 

 

       The FOEB has identified a need for certain procedures to provide an

       adequate level of safety while providing relief for the following items.

       These procedures must be established by the operator.  The following

       guidelines are to help establish these required procedures.

 

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

                  fault exists.

 

       21-2    (M)Maintenance procedure to ensure no mechanical or electrical

                  fault exists that will cause damage.

 

       21-4    (O)Operations procedure for recording hours of operation.

 

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

                  fault exists that will have an adverse effect on any flight

                  control function.

 

       23-5    (O)Operations procedure to verify that the SATCOM System

                  operates normally.

 

       27-2    (M)Maintenance procedure to ensure that the failure of the

                  electrical pitch trim will not affect the operation of the

                  manual trims or other flight controls.

 

       28-1    (O)Operations procedure to ensure the flight crew can determine

                  the quantity of fuel on board.

 

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

 

       34-13   (M)Maintenance procedure to deactivate and secure the system.

 

       34-13   (O)Operations procedure to ensure that TCAS is not required for

                  the intended flight.

 

       34-14   (M)Maintenance procedure to deactivate and secure the system.

 

       34-14   (O)Operations procedure to ensure that TCAS is not required for

                  the intended flight.

 

       34-14-2 (O)Operations procedure to ensure that TA Only mode is selected

                  and enroute or approach procedures do not require its use.


 

 

                       FEDERAL AVIATION ADMINISTRATION   Page XVII

                                                         Revision: 6

                        MASTER MINIMUM EQUIPMENT LIST    Date: 01/23/2003

 

 

                             PIPER MODEL PA-44

 

 

                   Guidelines for (O) & (M) Procedures

 

 

       34-14-3 (O)Operations procedure to ensure all RA display and audio

                  functions are operative and enroute or approach procedures

                  do not require its use.

 

       34-15   (O)Operations procedure to ensure alternate procedures are

                  established and used.

 

       34-15-1 (O)Operations procedure to ensure alternate procedures are

                  established and used.

 

       34-15-4 (O)Operations procedure to ensure alternate procedures are

                  established and used for advisory callouts.

 

       34-15-5 (O)Operations procedure to ensure alternate procedures are

                  established and used for inoperative windshear mode.

 

       37-1    (M)Maintenance procedure to ensure no unsafe condition exists

                  that could affect engine operations or systems function.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 


 

-------------------------------------------------------------------------------

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

¦ --------------------------------------------------------------------------- ¦

¦ AIRCRAFT:                                ¦ REVISION NO: 6        ¦ PAGE:    ¦

¦                                          ¦                       ¦          ¦

¦            PIPER MODEL PA-44             ¦ DATE: 01/23/2003      ¦ 21-1     ¦

¦ --------------------------------------------------------------------------- ¦

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

¦ SYSTEM &                  ¦    -------------------------------------------- ¦

¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦

¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦

¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦

¦ 21  AIR CONDITIONING      ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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

¦                           ¦    ¦    ¦                                       ¦

¦ 2.  Air Conditioner     C ¦ 1  ¦ 0  ¦ (M)                                   ¦

¦     System                ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 3.  Fresh Air Fan       C ¦ 1  ¦ 0  ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

-------------------------------------------------------------------------------


 

-------------------------------------------------------------------------------

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

¦ --------------------------------------------------------------------------- ¦

¦ AIRCRAFT:                                ¦ REVISION NO: 6        ¦ PAGE:    ¦

¦                                          ¦                       ¦          ¦

¦            PIPER MODEL PA-44             ¦ DATE: 01/23/2003      ¦ 22-1     ¦

¦ --------------------------------------------------------------------------- ¦

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

¦ SYSTEM &                  ¦    -------------------------------------------- ¦

¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦

¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦

¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦

¦ 22  AUTO FLIGHT           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 1.  Autopilot System    C ¦ -  ¦ 0  ¦ (M)May be inoperative provided      | ¦

¦                           ¦    ¦    ¦ operations do not require its use.  | ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 2.  Autopilot           C ¦ -  ¦ -  ¦ One may be inoperative provided     | ¦

¦     Disconnect            ¦    ¦    ¦ the autopilot is not utilized at    | ¦

¦                           ¦    ¦    ¦ less than initial approach          | ¦

¦                           ¦    ¦    ¦ altitude.                           | ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

-------------------------------------------------------------------------------


 

-------------------------------------------------------------------------------

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

¦ --------------------------------------------------------------------------- ¦

¦ AIRCRAFT:                                ¦ REVISION NO: 6        ¦ PAGE:    ¦

¦                                          ¦                       ¦          ¦

¦            PIPER MODEL PA-44             ¦ DATE: 01/23/2003      ¦ 23-1     ¦

¦ --------------------------------------------------------------------------- ¦

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

¦ SYSTEM &                  ¦    -------------------------------------------- ¦

¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦

¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦

¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦

¦ 23  COMMUNICATIONS        ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 1.  Communications      D ¦ -  ¦ -  ¦ Any in excess of those required     | ¦

¦     Equipment             ¦    ¦    ¦ by FAR may be inoperative provided  | ¦

¦     (VHF and UHF)         ¦    ¦    ¦ it is not powered by the emergency  | ¦

¦                           ¦    ¦    ¦ power supply and not required by    | ¦

¦                           ¦    ¦    ¦ emergency procedures.               | ¦

¦                           ¦    ¦    ¦                                       ¦

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

¦                           ¦    ¦    ¦                                       ¦

¦ 3.  Cockpit Voice         ¦    ¦    ¦                                     | ¦

¦     Recorder              ¦    ¦    ¦                                     | ¦

¦                           ¦    ¦    ¦                                       ¦

¦     A) With Flight      A ¦ 1  ¦ 0  ¦ May be inoperative provided:        | ¦

¦        Data Recorder      ¦    ¦    ¦     a) Flight Data Recorder (FDR)   | ¦

¦        (FDR) installed    ¦    ¦    ¦        operates normally, and       | ¦

¦                           ¦    ¦    ¦     b) Repairs are made within      | ¦

¦                           ¦    ¦    ¦        three flight days.           | ¦

¦                           ¦    ¦    ¦                                       ¦

¦     B) Without Flight   A ¦ 1  ¦ 0  ¦ May be inoperative provided repairs | ¦

¦        Data Recorder      ¦    ¦    ¦ are made within three flight days.  | ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 4.  Boom Microphones      ¦    ¦    ¦                                     | ¦

¦                           ¦    ¦    ¦                                       ¦

¦     A) With Cockpit       ¦    ¦    ¦                                     | ¦

¦        Voice Recorder and ¦    ¦    ¦                                     | ¦

¦        Flight Data        ¦    ¦    ¦                                     | ¦

¦        Recorder installed ¦    ¦    ¦                                     | ¦

¦                           ¦    ¦    ¦                                       ¦

¦     1) Cockpit Voice    A ¦ -  ¦ 0  ¦ May be inoperative provided:        | ¦

¦        Recorder equipped  ¦    ¦    ¦     a) Flight Data Recorder         | ¦

¦        to record Boom     ¦    ¦    ¦        operates normally, and       | ¦

¦        Microphone per     ¦    ¦    ¦     b) Repairs are made within      | ¦

¦        14 CFR 135.151(d)  ¦    ¦    ¦        three flight days.           | ¦

¦                           ¦    ¦    ¦                                       ¦

¦     2) Cockpit Voice    D ¦ -  ¦ 0  ¦ Any in excess of those required by  | ¦

¦     ***Recorder not       ¦    ¦    ¦ FAR may be inoperative.             | ¦

¦        equipped to record ¦    ¦    ¦                                     | ¦

¦        Boom Microphone    ¦    ¦    ¦                                     | ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                  (CON'T.) ¦    ¦    ¦                                       ¦

-------------------------------------------------------------------------------


 

-------------------------------------------------------------------------------

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

¦ --------------------------------------------------------------------------- ¦

¦ AIRCRAFT:                                ¦ REVISION NO: 6        ¦ PAGE:    ¦

¦                                          ¦                       ¦          ¦

¦            PIPER MODEL PA-44             ¦ DATE: 01/23/2003      ¦ 23-2     ¦

¦ --------------------------------------------------------------------------- ¦

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

¦ SYSTEM &                  ¦    -------------------------------------------- ¦

¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦

¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦

¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦

¦ 23  COMMUNICATIONS        ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 4.  Boom Microphones      ¦    ¦    ¦                                       ¦

¦                  (CON'T.) ¦    ¦    ¦                                     | ¦

¦                           ¦    ¦    ¦                                       ¦

¦     B) Cockpit Voice      ¦    ¦    ¦                                     | ¦

¦        Recorder without   ¦    ¦    ¦                                     | ¦

¦        Flight Data        ¦    ¦    ¦                                     | ¦

¦        Recorder installed ¦    ¦    ¦                                     | ¦

¦                           ¦    ¦    ¦                                       ¦

¦     1) Cockpit Voice    A ¦ -  ¦ 0  ¦ May be inoperative provided repairs | ¦

¦        Recorder equipped  ¦    ¦    ¦ are made within three flight days.  | ¦

¦        to record Boom     ¦    ¦    ¦                                     | ¦

¦        Microphone per     ¦    ¦    ¦                                     | ¦

¦        14 CFR 135.151(d)  ¦    ¦    ¦                                     | ¦

¦                           ¦    ¦    ¦                                       ¦

¦     2) Cockpit Voice    D ¦ -  ¦ 0  ¦ Any in excess of those required by  | ¦

¦     ***Recorder not       ¦    ¦    ¦ FAR may be inoperative.             | ¦

¦        equipped to record ¦    ¦    ¦                                     | ¦

¦        boom microphone    ¦    ¦    ¦                                     | ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 5.  High Frequency (HF) D ¦ -  ¦ -  ¦ Any in excess of those required by  | ¦

¦     Coomunication System  ¦    ¦    ¦ FAR may be inoperative.             | ¦

¦                           ¦    ¦    ¦                                       ¦

¦                         C ¦ -  ¦ 1  ¦ (O) May be inoperative while        | ¦

¦                           ¦    ¦    ¦ conducting operations that require  | ¦

¦                           ¦    ¦    ¦ two Long Range Communication        | ¦

¦                           ¦    ¦    ¦ Systems provided:                   | ¦

¦                           ¦    ¦    ¦    a) SATCOM (High or Low Gain)     | ¦

¦                           ¦    ¦    ¦       Data Link System operates     | ¦

¦                           ¦    ¦    ¦       normally, and                   ¦

¦                           ¦    ¦    ¦    b) SATCOM Data Link              | ¦

¦                           ¦    ¦    ¦       Communication operates        | ¦

¦                           ¦    ¦    ¦       normally over the intended    | ¦

¦                           ¦    ¦    ¦       route of flight.              | ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

-------------------------------------------------------------------------------


 

-------------------------------------------------------------------------------

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

¦ --------------------------------------------------------------------------- ¦

¦ AIRCRAFT:                                ¦ REVISION NO: 6        ¦ PAGE:    ¦

¦                                          ¦                       ¦          ¦

¦            PIPER MODEL PA-44             ¦ DATE: 01/23/2003      ¦ 25-1     ¦

¦ --------------------------------------------------------------------------- ¦

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

¦ SYSTEM &                  ¦    -------------------------------------------- ¦

¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦

¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦

¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦

¦ 25  EQUIPMENT/FURNISHINGS ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 1.  Cockpit Shoulder    B ¦ 2  ¦ 1  ¦ Right side may be inoperative         ¦

¦     Harness               ¦    ¦    ¦ provided seat remains unoccupied.     ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 2.  Passenger Seat      C ¦ -  ¦ 0  ¦ May be inoperative provided:        | ¦

¦                           ¦    ¦    ¦    a) Seat does not block an        | ¦

¦                           ¦    ¦    ¦       emergency exit, and           | ¦

¦                           ¦    ¦    ¦    b) Affected seats are blocked    | ¦

¦                           ¦    ¦    ¦       and placarded "DO NOT         | ¦

¦                           ¦    ¦    ¦       OCCUPY".                      | ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦ NOTE:  A seat with an inoperative   | ¦

¦                           ¦    ¦    ¦        seatbelt is considered       | ¦

¦                           ¦    ¦    ¦        inoperative.                 | ¦

¦                           ¦    ¦    ¦                                       ¦

¦     1) Recline          C ¦ -  ¦ -  ¦ May be inoperative and seat may be  | ¦

¦        Mechanism          ¦    ¦    ¦ occupied provided seat is secured   | ¦

¦                           ¦    ¦    ¦ in the upright position.            | ¦

¦                           ¦    ¦    ¦                                       ¦

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

¦     Equipment             ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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

¦                           ¦    ¦    ¦                                       ¦

¦ 5.  Passenger Convenience ¦ -  ¦ 0  ¦ Passenger convenience items, as     | ¦

¦     Items(s)              ¦    ¦    ¦ expressed in this MMEL are those      ¦

¦                           ¦    ¦    ¦ related to passenger convenience,     ¦

¦                           ¦    ¦    ¦ comfort or entertainment such as,     ¦

¦                           ¦    ¦    ¦ but not limited to, galley            ¦

¦                           ¦    ¦    ¦ equipment, movie equipment, ash       ¦

¦                           ¦    ¦    ¦ trays, stereo equipment, overhead     ¦

¦                           ¦    ¦    ¦ reading lamps, etc.  Items            ¦

¦                           ¦    ¦    ¦ addressed elsewhere in this           ¦

¦                           ¦    ¦    ¦ document shall not be included.       ¦

¦                           ¦    ¦    ¦ (M) and (O) procedures may be         ¦

¦                           ¦    ¦    ¦ required and included in the air      ¦

¦                           ¦    ¦    ¦ carrier's appropriate document.       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

-------------------------------------------------------------------------------


 

-------------------------------------------------------------------------------

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

¦ --------------------------------------------------------------------------- ¦

¦ AIRCRAFT:                                ¦ REVISION NO: 6        ¦ PAGE:    ¦

¦                                          ¦                       ¦          ¦

¦            PIPER MODEL PA-44             ¦ DATE: 01/23/2003      ¦ 26-1     ¦

¦ --------------------------------------------------------------------------- ¦

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

¦ SYSTEM &                  ¦    -------------------------------------------- ¦

¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦

¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦

¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦

¦ 26  FIRE PROTECTION       ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 1.  Portable Fire       D ¦ -  ¦ -  ¦ Any in excess of those required by  | ¦

¦     Extinguisher          ¦    ¦    ¦ FAR may be inoperative or missing   | ¦

¦                           ¦    ¦    ¦ provided:                           | ¦

¦                           ¦    ¦    ¦     a) The inoperative fire         | ¦

¦                           ¦    ¦    ¦        extinguisher is tagged       | ¦

¦                           ¦    ¦    ¦        inoperative, removed from    | ¦

¦                           ¦    ¦    ¦        the installed location, and  | ¦

¦                           ¦    ¦    ¦        placed out of sight so it    | ¦

¦                           ¦    ¦    ¦        cannot be mistaken for a     | ¦

¦                           ¦    ¦    ¦        functional unit, and         | ¦

¦                           ¦    ¦    ¦     b) Required distribution is     | ¦

¦                           ¦    ¦    ¦        maintained.                  | ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

-------------------------------------------------------------------------------


 

-------------------------------------------------------------------------------

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

¦ --------------------------------------------------------------------------- ¦

¦ AIRCRAFT:                                ¦ REVISION NO: 6        ¦ PAGE:    ¦

¦                                          ¦                       ¦          ¦

¦            PIPER MODEL PA-44             ¦ DATE: 01/23/2003      ¦ 27-1     ¦

¦ --------------------------------------------------------------------------- ¦

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

¦ SYSTEM &                  ¦    -------------------------------------------- ¦

¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦

¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦

¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦

¦ 27  FLIGHT CONTROLS       ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 1.  Trim Tab Position   C ¦ 2  ¦ 0  ¦ May be inoperative provided:          ¦

¦     Indicators            ¦    ¦    ¦     a) Tab is visually checked for  | ¦

¦     (Rudder, Elevator)    ¦    ¦    ¦        full range of operation,     | ¦

¦                           ¦    ¦    ¦     b) Tab operation is not         | ¦

¦                           ¦    ¦    ¦        affected, and                | ¦

¦                           ¦    ¦    ¦     c) Tab is positioned to neutral | ¦

¦                           ¦    ¦    ¦        prior to each takeoff and    | ¦

¦                           ¦    ¦    ¦        neutral is verified by       | ¦

¦                           ¦    ¦    ¦        visual inspection.           | ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 2.  Electric Pitch      C ¦ 1  ¦ 0  ¦ (M)May be inoperative provided        ¦

¦     Trim                  ¦    ¦    ¦  manual trim is operative and         ¦

¦                           ¦    ¦    ¦  unaffected.                          ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

-------------------------------------------------------------------------------


 

-------------------------------------------------------------------------------

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

¦ --------------------------------------------------------------------------- ¦

¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦

¦                                          ¦                       ¦          ¦

¦            PIPER MODEL PA-44             ¦ DATE: 03/24/1994      ¦ 28-1     ¦

¦ --------------------------------------------------------------------------- ¦

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

¦ SYSTEM &                  ¦    -------------------------------------------- ¦

¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦

¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦

¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦

¦ 28  FUEL                  ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 1.  Fuel Quantity       C ¦ 2  ¦ 1  ¦ (O)One may be inoperative provided    ¦

¦     Indicator             ¦    ¦    ¦  a reliable means is established to   ¦

¦                           ¦    ¦    ¦  determine that fuel quantity on      ¦

¦                           ¦    ¦    ¦  board meets the regulatory           ¦

¦                           ¦    ¦    ¦  requirements for the intended        ¦

¦                           ¦    ¦    ¦  flight.                              ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

-------------------------------------------------------------------------------


 

-------------------------------------------------------------------------------

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

¦ --------------------------------------------------------------------------- ¦

¦ AIRCRAFT:                                ¦ REVISION NO: 6        ¦ PAGE:    ¦

¦                                          ¦                       ¦          ¦

¦            PIPER MODEL PA-44             ¦ DATE: 01/23/2003      ¦ 30-1     ¦

¦ --------------------------------------------------------------------------- ¦

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

¦ SYSTEM &                  ¦    -------------------------------------------- ¦

¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦

¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦

¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦

¦ 30  ICE AND RAIN          ¦    ¦    ¦                                       ¦

¦     PROTECTION            ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 1.  Pitot Heater        B ¦ 1  ¦ 0  ¦ May be inoperative provided:          ¦

¦                           ¦    ¦    ¦    a) IFR passenger carrying          ¦

¦                           ¦    ¦    ¦       operations are not conducted,   ¦

¦                           ¦    ¦    ¦       and                             ¦

¦                           ¦    ¦    ¦    b) Aircraft is not operated in     ¦

¦                           ¦    ¦    ¦       known or forecast icing         ¦

¦                           ¦    ¦    ¦       conditions.                     ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 2.  Carburetor Ice      C ¦ 1  ¦ 0  ¦                                       ¦

¦     Detection System      ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

-------------------------------------------------------------------------------


 

-------------------------------------------------------------------------------

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

¦ --------------------------------------------------------------------------- ¦

¦ AIRCRAFT:                                ¦ REVISION NO: 6        ¦ PAGE:    ¦

¦                                          ¦                       ¦          ¦

¦            PIPER MODEL PA-44             ¦ DATE: 01/23/2003      ¦ 31-1     ¦

¦ --------------------------------------------------------------------------- ¦

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

¦ SYSTEM &                  ¦    -------------------------------------------- ¦

¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦

¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦

¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦

¦ 31  INDICATING/RECORDING  ¦    ¦    ¦                                       ¦

¦     SYSTEMS               ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 1.  Clock with sweep    C ¦ 1  ¦ 0  ¦ May be inoperative under VFR          ¦

¦     second hand, or       ¦    ¦    ¦ conditions.                           ¦

¦     electric digital      ¦    ¦    ¦                                       ¦

¦     clock                 ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 2.  Flight Hour         C ¦ -  ¦ 0  ¦ (O)                                   ¦

¦     Recorder              ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

-------------------------------------------------------------------------------


 

-------------------------------------------------------------------------------

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

¦ --------------------------------------------------------------------------- ¦

¦ AIRCRAFT:                                ¦ REVISION NO: 6        ¦ PAGE:    ¦

¦                                          ¦                       ¦          ¦

¦            PIPER MODEL PA-44             ¦ DATE: 01/23/2003      ¦ 33-1     ¦

¦ --------------------------------------------------------------------------- ¦

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

¦ SYSTEM &                  ¦    -------------------------------------------- ¦

¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦

¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦

¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦

¦ 33  LIGHTS                ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 1.  Cockpit and         C ¦ -  ¦ -  ¦ Individual lights may be            | ¦

¦     Instrument Lights     ¦    ¦    ¦ inoperative provided remaining      | ¦

¦                           ¦    ¦    ¦ lights are:                         | ¦

¦                           ¦    ¦    ¦     a) Sufficient to clearly        | ¦

¦                           ¦    ¦    ¦        illuminate all required      | ¦

¦                           ¦    ¦    ¦        instruments, controls, and   | ¦

¦                           ¦    ¦    ¦        other devices for which it   | ¦

¦                           ¦    ¦    ¦        is provided,                 | ¦

¦                           ¦    ¦    ¦     b) Are positioned so that       | ¦

¦                           ¦    ¦    ¦        direct rays are shielded     | ¦

¦                           ¦    ¦    ¦        from crewmembers' eyes, and  | ¦

¦                           ¦    ¦    ¦     c) Lighting configuration and   | ¦

¦                           ¦    ¦    ¦        intensity are acceptable to  | ¦

¦                           ¦    ¦    ¦        the flight crew.             | ¦

¦                           ¦    ¦    ¦                                       ¦

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

¦                           ¦    ¦    ¦ operations.                           ¦

¦                           ¦    ¦    ¦                                     | ¦

¦                         C ¦ 2  ¦ 1  ¦ One may be inoperative for night      ¦

¦                           ¦    ¦    ¦ operations.                           ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 3.  Anti-collision      B ¦ 1  ¦ 0  ¦ May be inoperative for day            ¦

¦     Light System          ¦    ¦    ¦ operations.                           ¦

¦                           ¦    ¦    ¦                                       ¦

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

¦     Position Lights       ¦    ¦    ¦ operations.                           ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 5.  Cabin Light         C ¦ -  ¦ -  ¦ May be inoperative provided           ¦

¦     Systems               ¦    ¦    ¦ lighting configuration is             ¦

¦                           ¦    ¦    ¦ acceptable to the flight crew.        ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

-------------------------------------------------------------------------------


 

-------------------------------------------------------------------------------

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

¦ --------------------------------------------------------------------------- ¦

¦ AIRCRAFT:                                ¦ REVISION NO: 6        ¦ PAGE:    ¦

¦                                          ¦                       ¦          ¦

¦            PIPER MODEL PA-44             ¦ DATE: 01/23/2003      ¦ 34-1     ¦

¦ --------------------------------------------------------------------------- ¦

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

¦ SYSTEM &                  ¦    -------------------------------------------- ¦

¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦

¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦

¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦

¦ 34  NAVIGATION            ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 1.  Gyroscopic Rate of  B ¦ 1  ¦ 0  ¦ Must be operative on left side for  | ¦

¦     Turn/Slip Skid        ¦    ¦    ¦ IFR, passenger carrying VFR over    | ¦

¦     Indicator System      ¦    ¦    ¦ the top and passenger carrying      | ¦

¦                           ¦    ¦    ¦ VFR night operations.               | ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 2.  Vertical Speed      B ¦ 1  ¦ 0  ¦ Must be operative on left side for    ¦

¦     Indicator             ¦    ¦    ¦ IFR passenger carrying operations.    ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 3.  ATC Transponders    C ¦ -  ¦ 0  ¦ May be inoperative provided:        | ¦

¦     and Automatic         ¦    ¦    ¦     a) Enroute operations do not    | ¦

¦     Altitude Reporting    ¦    ¦    ¦        require its use, and         | ¦

¦     Systems               ¦    ¦    ¦     b) Prior to flight, approval is | ¦

¦                           ¦    ¦    ¦        obtained from ATC facilties  | ¦

¦                           ¦    ¦    ¦        having jurisdiction over the | ¦

¦                           ¦    ¦    ¦        planned route of flight.     | ¦

¦                           ¦    ¦    ¦                                       ¦

¦                         D ¦ -  ¦ 1  ¦ Any in excess of those required     | ¦

¦                           ¦    ¦    ¦ by FAR may be inoperative.          | ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 4.  Navigation          C ¦ -  ¦ -  ¦ As required by FAR.                   ¦

¦     Equipment (VOR/ILS,   ¦    ¦    ¦                                       ¦

¦     Loran, Omega/VLF, INS ¦    ¦    ¦                                       ¦

¦     Doppler, RNAV, GPS)   ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 5.  Weather Radar/      C ¦ 1  ¦ 0  ¦ As required by FAR.                   ¦

¦     Thunderstorm          ¦    ¦    ¦                                       ¦

¦     Detection Equipment   ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 6.  Marker Beacon       C ¦ 1  ¦ 0  ¦ May be inoperative provided           ¦

¦     Receiver              ¦    ¦    ¦ approach procedure does not           ¦

¦                           ¦    ¦    ¦ require its use.                      ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 7.  Radar Altimeter     C ¦ 1  ¦ 0  ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 8.  Altitude Encoder      ¦    ¦    ¦ DELETED REVISION 6. Combined        | ¦

¦                           ¦    ¦    ¦ with Item 3.                        | ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 9.  Distance Measuring  D ¦ -  ¦ -  ¦ Any in excess of those required by  | ¦

¦     Equipment (DME)       ¦    ¦    ¦ FAR be be inoperative.              | ¦

¦     Systems               ¦    ¦    ¦                                     | ¦

-------------------------------------------------------------------------------


 

-------------------------------------------------------------------------------

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

¦ --------------------------------------------------------------------------- ¦

¦ AIRCRAFT:                                ¦ REVISION NO: 6        ¦ PAGE:    ¦

¦                                          ¦                       ¦          ¦

¦            PIPER MODEL PA-44             ¦ DATE: 01/23/2003      ¦ 34-2     ¦

¦ --------------------------------------------------------------------------- ¦

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

¦ SYSTEM &                  ¦    -------------------------------------------- ¦

¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦

¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦

¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦

¦ 34  NAVIGATION            ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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

¦                           ¦    ¦    ¦                                       ¦

¦ 11. RMI                 C ¦ 1  ¦ 0  ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 12. Nonstabilized       B ¦ 1  ¦ 0  ¦ May be inoperative provided any     | ¦

¦     Magnetic Compass      ¦    ¦    ¦ combination of three Gyro or INS    | ¦

¦                           ¦    ¦    ¦ (IRU) stabilized compass systems    | ¦

¦                           ¦    ¦    ¦ are operative.                      | ¦

¦                           ¦    ¦    ¦                                       ¦

¦                         B ¦ 1  ¦ 0  ¦ May be inoperative provided         | ¦

¦                           ¦    ¦    ¦     a) Any combination of two Gyro  | ¦

¦                           ¦    ¦    ¦        or INS (IRU) stabilized      | ¦

¦                           ¦    ¦    ¦        compass systems operate      | ¦

¦                           ¦    ¦    ¦        normally, and                | ¦

¦                           ¦    ¦    ¦     b) Airplane is operated with    | ¦

¦                           ¦    ¦    ¦        dual independent navigtaion  | ¦

¦                           ¦    ¦    ¦        capability and under         | ¦

¦                           ¦    ¦    ¦        positive radar control by    | ¦

¦                           ¦    ¦    ¦        ATC on the enroute portion   | ¦

¦                           ¦    ¦    ¦        of the flight.               | ¦

¦                           ¦    ¦    ¦                                       ¦

¦                         B ¦ 1  ¦ 0  ¦ May be inoperative for flights that | ¦

¦                           ¦    ¦    ¦ are entirely within areas of        | ¦

¦                           ¦    ¦    ¦ magnetic unreliability provided at  | ¦

¦                           ¦    ¦    ¦ least two stabilized directional    | ¦

¦                           ¦    ¦    ¦ gyro systems are installed, operate | ¦

¦                           ¦    ¦    ¦ normally, and are used in           | ¦

¦                           ¦    ¦    ¦ conjunction with approved free      | ¦

¦                           ¦    ¦    ¦ gyro navigation techniques.         | ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

-------------------------------------------------------------------------------


 

-------------------------------------------------------------------------------

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

¦ --------------------------------------------------------------------------- ¦

¦ AIRCRAFT:                                ¦ REVISION NO: 6        ¦ PAGE:    ¦

¦                                          ¦                       ¦          ¦

¦            PIPER MODEL PA-44             ¦ DATE: 01/23/2003      ¦ 34-3     ¦

¦ --------------------------------------------------------------------------- ¦

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

¦ SYSTEM &                  ¦    -------------------------------------------- ¦

¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦

¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦

¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦

¦ 34  NAVIGATION            ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 13. Traffic Alert and   B ¦ -  ¦ 0  ¦ (M)(O) May be inoperative provided: | ¦

¦     Collision Avoidance   ¦    ¦    ¦     a) System is deactivated and    | ¦

¦     System (TCAS I)       ¦    ¦    ¦        secured, and                 | ¦

¦                           ¦    ¦    ¦     b) Enroute or approach          | ¦

¦                           ¦    ¦    ¦        procedure do not requires    | ¦

¦                           ¦    ¦    ¦        its use.                     | ¦

¦                           ¦    ¦    ¦                                       ¦

¦                         C ¦ -  ¦ 0  ¦ (M)(O) May be inoperative provided: | ¦

¦                           ¦    ¦    ¦     a) Not required by FAR,         | ¦

¦                           ¦    ¦    ¦     b) System is deactivated and    | ¦

¦                           ¦    ¦    ¦        secured, and                 | ¦

¦                           ¦    ¦    ¦     c) Enroute or approach          | ¦

¦                           ¦    ¦    ¦        procedures do not require    | ¦

¦                           ¦    ¦    ¦        its use.                     | ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 14. Traffic Alert and   B ¦ -  ¦ 0  ¦ (M) May be inoperative provided:    | ¦

¦ *** Collision Avoidance   ¦    ¦    ¦     a) System is deactivated and    | ¦

¦     System (TCAS II)      ¦    ¦    ¦        secured, and                 | ¦

¦                           ¦    ¦    ¦     b) Enroute or approach          | ¦

¦                           ¦    ¦    ¦        procedures do not require    | ¦

¦                           ¦    ¦    ¦        its use.                     | ¦

¦                           ¦    ¦    ¦                                       ¦

¦                         C ¦ -  ¦ 0  ¦ (M)(O) May be inoperative provided: | ¦

¦                           ¦    ¦    ¦     a) Not required by FAR,         | ¦

¦                           ¦    ¦    ¦     b) System is deactivated and    | ¦

¦                           ¦    ¦    ¦        secured, and                 | ¦

¦                           ¦    ¦    ¦     c) Enroute or approach          | ¦

¦                           ¦    ¦    ¦        procedures do not require    | ¦

¦                           ¦    ¦    ¦        its use.                     | ¦

¦                           ¦    ¦    ¦                                       ¦

¦     1) Combined Traffic C ¦ 2  ¦ 1  ¦ May be inoperative on the non-      | ¦

¦        Alert (TA) and     ¦    ¦    ¦ flying pilot side provided:         | ¦

¦        Resolution         ¦    ¦    ¦     a) TA and RA visual display is  | ¦

¦        Advisory (RA) Dual ¦    ¦    ¦        operative on the flying      | ¦

¦        Display Systems    ¦    ¦    ¦        pilot side, and              | ¦

¦                           ¦    ¦    ¦     b) TA and RA audio function is  | ¦

¦                           ¦    ¦    ¦        operative on the flying      | ¦

¦                           ¦    ¦    ¦        pilot side.                  | ¦

¦                           ¦    ¦    ¦                                       ¦

-------------------------------------------------------------------------------


 

-------------------------------------------------------------------------------

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

¦ --------------------------------------------------------------------------- ¦

¦ AIRCRAFT:                                ¦ REVISION NO: 6        ¦ PAGE:    ¦

¦                                          ¦                       ¦          ¦

¦            PIPER MODEL PA-44             ¦ DATE: 01/23/2003      ¦ 34-4     ¦

¦ --------------------------------------------------------------------------- ¦

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

¦ SYSTEM &                  ¦    -------------------------------------------- ¦

¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦

¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦

¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦

¦ 34  NAVIGATION            ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                  (CON'T.) ¦    ¦    ¦                                       ¦

¦ 14. Traffic Alert and     ¦    ¦    ¦                                       ¦

¦ *** Collision Avoidance   ¦    ¦    ¦                                       ¦

¦     System (TCAS II)      ¦    ¦    ¦                                       ¦

¦                  (CON'T.) ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦     2) Resolution       C ¦ 2  ¦ 1  ¦ May be inoperative on non-flying    | ¦

¦        Advisory (RA)      ¦    ¦    ¦ pilot side.                         | ¦

¦        Display Systems    ¦    ¦    ¦                                     | ¦

¦                           ¦    ¦    ¦                                       ¦

¦                         C ¦ -  ¦ 0  ¦ (O) May be inoperative provided:    | ¦

¦                           ¦    ¦    ¦     a) Traffic Alert (TA) visual    | ¦

¦                           ¦    ¦    ¦        display and audio functions  | ¦

¦                           ¦    ¦    ¦        are operative,               | ¦

¦                           ¦    ¦    ¦     b) TA only mode is selected by  | ¦

¦                           ¦    ¦    ¦        the crew, and                | ¦

¦                           ¦    ¦    ¦     c) Enroute or approach          | ¦

¦                           ¦    ¦    ¦        procedures do not require    | ¦

¦                           ¦    ¦    ¦        its use.                     | ¦

¦                           ¦    ¦    ¦                                       ¦

¦     3) Traffic Alert    C ¦ -  ¦ 0  ¦ (O) May be inoperative provided:    | ¦

¦        Display Systems    ¦    ¦    ¦     a) RA visual display and audio  | ¦

¦                           ¦    ¦    ¦        functions are operative, and | ¦

¦                           ¦    ¦    ¦     b) Enroute or approach          | ¦

¦                           ¦    ¦    ¦        procedures do not require    | ¦

¦                           ¦    ¦    ¦        its use.                     | ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

-------------------------------------------------------------------------------


 

-------------------------------------------------------------------------------

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

¦ --------------------------------------------------------------------------- ¦

¦ AIRCRAFT:                                ¦ REVISION NO: 6        ¦ PAGE:    ¦

¦                                          ¦                       ¦          ¦

¦            PIPER MODEL PA-44             ¦ DATE: 01/23/2003      ¦ 34-5     ¦

¦ --------------------------------------------------------------------------- ¦

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

¦ SYSTEM &                  ¦    -------------------------------------------- ¦

¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦

¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦

¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦

¦ 34  NAVIGATION            ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 15. Ground Proximity    A ¦ -  ¦ 0  ¦ (O) May be inoperative provided:    | ¦

¦ *** Warning System        ¦    ¦    ¦     a) Alternate procedures are     | ¦

¦     (GPWS)                ¦    ¦    ¦        established and used, and    | ¦

¦                           ¦    ¦    ¦     b) Repairs are made within      | ¦

¦                           ¦    ¦    ¦        two flight days.             | ¦

¦                           ¦    ¦    ¦                                       ¦

¦                         C ¦ -  ¦ 0  ¦ (O) May be inoperative provided:    | ¦

¦                           ¦    ¦    ¦     a) It is not required by FAR,   | ¦

¦                           ¦    ¦    ¦        and                          | ¦

¦                           ¦    ¦    ¦     b) Alternate procedures are     | ¦

¦                           ¦    ¦    ¦        established and used.        | ¦

¦                           ¦    ¦    ¦                                       ¦

¦     1) Modes 1-4        A ¦ -  ¦ 0  ¦ (0) May be inoperative provided:    | ¦

¦                           ¦    ¦    ¦     a) Alternate procedures are     | ¦

¦                           ¦    ¦    ¦        established and used, and    | ¦

¦                           ¦    ¦    ¦     b) Repairs are made within      | ¦

¦                           ¦    ¦    ¦        two flight days.             | ¦

¦                           ¦    ¦    ¦                                       ¦

¦                         C ¦ -  ¦ 0  ¦ (0) May be inoperative provided:    | ¦

¦                           ¦    ¦    ¦     a) It is not required by FAR,   | ¦

¦                           ¦    ¦    ¦        and                          | ¦

¦                           ¦    ¦    ¦     b) Alternate procedures are     | ¦

¦                           ¦    ¦    ¦        established and used.        | ¦

¦                           ¦    ¦    ¦                                       ¦

¦     2) Test Mode        A ¦ 1  ¦ 0  ¦ May be inoperative provided:        | ¦

¦                           ¦    ¦    ¦     a) GPWS is considered           | ¦

¦                           ¦    ¦    ¦        inoperative, and             | ¦

¦                           ¦    ¦    ¦     b) Repairs are made within      | ¦

¦                           ¦    ¦    ¦        two flight days.             | ¦

¦                           ¦    ¦    ¦                                       ¦

¦                         C ¦ -  ¦ 0  ¦ May be inoperative provided:        | ¦

¦                           ¦    ¦    ¦     a) It is not required by FAR,   | ¦

¦                           ¦    ¦    ¦        and                          | ¦

¦                           ¦    ¦    ¦     b) GPWS is considered           | ¦

¦                           ¦    ¦    ¦        inoperative.                 | ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

-------------------------------------------------------------------------------


 

-------------------------------------------------------------------------------

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

¦ --------------------------------------------------------------------------- ¦

¦ AIRCRAFT:                                ¦ REVISION NO: 6        ¦ PAGE:    ¦

¦                                          ¦                       ¦          ¦

¦            PIPER MODEL PA-44             ¦ DATE: 01/23/2003      ¦ 34-6     ¦

¦ --------------------------------------------------------------------------- ¦

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

¦ SYSTEM &                  ¦    -------------------------------------------- ¦

¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦

¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦

¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦

¦ 34  NAVIGATION            ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 15. Ground Proximity      ¦    ¦    ¦                                       ¦

¦     Warning System        ¦    ¦    ¦                                       ¦

¦     (GPWS)       (CON'T.) ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦     3) Glideslope       B ¦ 2  ¦ 0  ¦                                     | ¦

¦        Deviation          ¦    ¦    ¦                                     | ¦

¦        (Mode 5)           ¦    ¦    ¦                                     | ¦

¦                         C ¦ 2  ¦ 0  ¦ May be inoperative provided it is   | ¦

¦                           ¦    ¦    ¦ not required by FAR.                | ¦

¦                           ¦    ¦    ¦                                       ¦

¦     4) Advisory         C ¦ -  ¦ 0  ¦ (O) May be inoperative provided     | ¦

¦        Callouts           ¦    ¦    ¦ alternate procedures are            | ¦

¦        ***                ¦    ¦    ¦ established and used.               | ¦

¦                           ¦    ¦    ¦                                       ¦

¦     5) Windshear        C ¦ -  ¦ 0  ¦ (O) May be inoperative provided:    | ¦

¦        Mode               ¦    ¦    ¦     a) Alternate procedures are     | ¦

¦                           ¦    ¦    ¦        established and used, and    | ¦

¦                           ¦    ¦    ¦     b) Windshear Detection and      | ¦

¦                           ¦    ¦    ¦        Avoidance System operates    | ¦

¦                           ¦    ¦    ¦        normally.                    | ¦

¦                           ¦    ¦    ¦                                       ¦

¦                         C ¦ -  ¦ 0  ¦ (O) May be inoperative provided:    | ¦

¦                           ¦    ¦    ¦     a) Alternate procedures are     | ¦

¦                           ¦    ¦    ¦        established and used, and    | ¦

¦                           ¦    ¦    ¦     b) Takeoffs and landings are    | ¦

¦                           ¦    ¦    ¦        not conducted in known or    | ¦

¦                           ¦    ¦    ¦        forecast windshear           | ¦

¦                           ¦    ¦    ¦        conditions.                  | ¦

¦                           ¦    ¦    ¦                                       ¦

¦     6. Terrain          C ¦ -  ¦ 0  ¦                                     | ¦

¦        Awareness and      ¦    ¦    ¦                                     | ¦

¦        Warning System     ¦    ¦    ¦                                     | ¦

¦        (TAWS)             ¦    ¦    ¦                                     | ¦

¦        ***                ¦    ¦    ¦                                     | ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

¦ --------------------------------------------------------------------------- ¦

¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦

¦                                          ¦                       ¦          ¦

¦            PIPER MODEL PA-44             ¦ DATE: 03/24/1994      ¦ 37-1     ¦

¦ --------------------------------------------------------------------------- ¦

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

¦ SYSTEM &                  ¦    -------------------------------------------- ¦

¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦

¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦

¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦

¦ 37  VACUUM/PRESSURE       ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 1.  Vacuum Pump         B ¦ 2  ¦ 1  ¦ (M)One may be inoperative for day     ¦

¦                           ¦    ¦    ¦ VFR flights.                          ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 2.  Vacuum Gauge        C ¦ 1  ¦ 0  ¦ May be inoperative for day VFR        ¦

¦                           ¦    ¦    ¦ flight provided the source            ¦

¦                           ¦    ¦    ¦ failure indicators are operative.     ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 3.  Source Failure      C ¦ 2  ¦ 0  ¦ May be inoperative for day VFR        ¦

¦     Indicator             ¦    ¦    ¦ flight provided the vacuum gauge      ¦

¦                           ¦    ¦    ¦ is operative.                         ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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¦                           ¦    ¦    ¦                                       ¦

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¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

¦ --------------------------------------------------------------------------- ¦

¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦

¦                                          ¦                       ¦          ¦

¦            PIPER MODEL PA-44             ¦ DATE: 03/24/1994      ¦ 61-1     ¦

¦ --------------------------------------------------------------------------- ¦

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

¦ SYSTEM &                  ¦    -------------------------------------------- ¦

¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦

¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦

¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦

¦ 61  PROPELLERS            ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 1.  Propeller           C ¦ 1  ¦ 0  ¦                                       ¦

¦     Synchrophaser         ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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¦                           ¦    ¦    ¦                                       ¦

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¦                           ¦    ¦    ¦                                       ¦

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¦                           ¦    ¦    ¦                                       ¦

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¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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¦                           ¦    ¦    ¦                                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                                                             ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

¦ --------------------------------------------------------------------------- ¦

¦ AIRCRAFT:                                ¦ REVISION NO: 6        ¦ PAGE:    ¦

¦                                          ¦                       ¦          ¦

¦            PIPER MODEL PA-44             ¦ DATE: 01/23/2003      ¦ 77-1     ¦

¦ --------------------------------------------------------------------------- ¦

¦                        1. ¦ 2. NUMBER INSTALLED                             ¦

¦ SYSTEM &                  ¦    -------------------------------------------- ¦

¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦

¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦

¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦

¦ 77  ENGINE INDICATING     ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦ 1.  Exhaust Gas         C ¦ 1  ¦ 0  ¦                                       ¦

¦     Temperature           ¦    ¦    ¦                                       ¦

¦     Indicator, Dual       ¦    ¦    ¦                                       ¦

¦     Indicating            ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

¦                           ¦    ¦    ¦                                       ¦

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¦                           ¦    ¦    ¦                                       ¦

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