Date: 03/10/2004

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

ISRAEL AIRCRAFT MODELS

1125, 1125 SP, 1125 SPX

FEDERAL AVIATION ADMINISTRATION

FLIGHT STANDARDS DIVISION

AIRCRAFT EVALUATION GROUP, MKC-AEG

901 LOCUST, ROOM 332

KANSAS CITY, MO  64106-2641

TELEPHONE:  (816) 329-3233

FAX:        (816) 329-3241

DEPARTMENT OF TRANSPORTATION     Revision: 5

  Revision: 5

MASTER MINIMUM EQUIPMENT LIST      Date: 03/10/2004

IA-1125, IA-1125 SP, IA-1125 SPX

Table of Contents

SYSTEM NO.  SYSTEM                                  PAGE

--     Table of Contents                       I

--     Log of Revisions                        II, III

--     Control Page                            IV, V

--     Highlights of Change                    VI, VII, VIII

--     Definitions                             IX, X, XI, XII

--     Definitions                             XIII, XIV, XV, XVI --     Preamble                                XVII, XVIII

--     Guidelines for (O) & (M) Procedures     XIX, XX, XXI, XXII 21     Air Conditioning                        21-1, 2, 3, 4

22     Auto Flight                             22-1

23     Communications                          23-1, 2, 3, 4

24     Electrical Power                        24-1

25     Equipment/Furnishings                   25-1, 2

26     Fire Protection                         26-1

27     Flight Controls                         27-1

28     Fuel                                    28-1, 2

29     Hydraulic Power                         29-1

30     Ice and Rain Protection                 30-1, 2

31     Indicating/Recording Systems            31-1, 2

32     Landing Gear                            32-1

33     Lights                                  33-1, 2, 3

34     Navigation                              34-1, 2, 3, 4, 5 34     Navigation                              34-6  THRU 10

34     Navigation                              34-11 35     Oxygen                                  35-1 49     Airborne Auxiliary Power                49-1 52     Doors                                   52-1 77     Engine Indicating                       77-1 78     Engine Exhaust                          78-1 79     Engine Oil                              79-1

FEDERAL AVIATION ADMINISTRATION     Page: I

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MASTER MINIMUM EQUIPMENT LIST    Date: 03/10/2004

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Log of Revisions

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

¦ 1        ¦ 01/27/1992 ¦ ALL PAGES                      ¦           ¦ ¦ 2        ¦ 01/18/1995 ¦ HIGHLIGHTS OF REV.,DEFINITIONS ¦           ¦ ¦ 2        ¦ 01/18/1995 ¦ GUIDELINES                     ¦           ¦ ¦ 2        ¦ 01/18/1995 ¦ 21-1,21-2,21-3,21-4,22-1       ¦           ¦ ¦ 2        ¦ 01/18/1995 ¦ 23-1,23-2,24-1,25-1,26-1       ¦           ¦ ¦ 2        ¦ 01/18/1995 ¦ 26-2,27-1,28-1,28-2,29-1       ¦           ¦ ¦ 2        ¦ 01/18/1995 ¦ 30-1,30-2,31-1,32-1,33-1       ¦           ¦ ¦ 2        ¦ 01/18/1995 ¦ 33-2,33-3,34-1,34-2,34-3       ¦           ¦ ¦ 2        ¦ 01/18/1995 ¦ 34-4,34-5,35-1,49-1,52-1       ¦           ¦ ¦ 2        ¦ 01/18/1995 ¦ 77-1,78-1,79-1                 ¦           ¦ ¦ 2a       ¦ 01/14/1997 ¦ HIGHLIGHTS OF REV.,DEFINITIONS ¦           ¦ ¦ 2a       ¦ 01/14/1997 ¦ GUIDELINES                     ¦           ¦ ¦ 2a       ¦ 01/14/1997 ¦ 25-1,26-1,30-1,30-2,33-1       ¦           ¦ ¦ 2a       ¦ 01/14/1997 ¦ 33-2,33-3,34-1,34-2,34-3       ¦           ¦ ¦ 2a       ¦ 01/14/1997 ¦ 34-4,34-5,34-6,34-7,77-1       ¦           ¦ ¦ 2b       ¦ 09/10/1997 ¦ HIGHLIGHTS OF REV.,DEFINITIONS ¦           ¦ ¦ 2b       ¦ 09/10/1997 ¦ 23-1,25-1,30-1,34-3            ¦           ¦ ¦ 2c       ¦ 09/21/1998 ¦ HIGHLIGHTS OF REV.,DEFINITIONS ¦           ¦ ¦ 2c       ¦ 09/21/1998 ¦ GUIDELINES                     ¦           ¦ ¦ 2c       ¦ 09/21/1998 ¦ 22-1,23-1,25-1,25-2,30-1       ¦           ¦ ¦ 2c       ¦ 09/21/1998 ¦ 33-1,33-2,33-3,34-3,34-4       ¦           ¦ ¦ 2c       ¦ 09/21/1998 ¦ 34-5,34-6,77-1                 ¦           ¦ ¦ 2d       ¦ 04/11/2000 ¦ HIGHLIGHTS OF REV.,DEFINITIONS ¦           ¦ ¦ 2d       ¦ 04/11/2000 ¦ PREAMBLE,GUIDELINES            ¦           ¦ ¦ 2d       ¦ 04/11/2000 ¦ 22-1,23-1,25-1,25-2,31-1       ¦           ¦ ¦ 2d       ¦ 04/11/2000 ¦ 34-2,34-3,34-4,34-5,34-6       ¦           ¦ ¦ 2d       ¦ 04/11/2000 ¦ 34-7                           ¦           ¦ ¦ 3        ¦ 10/30/2001 ¦ HIGHLIGHTS OF REV.,DEFINITIONS ¦           ¦ ¦ 3        ¦ 10/30/2001 ¦ GUIDELINES                     ¦           ¦ ¦ 3        ¦ 10/30/2001 ¦ 21-1,21-2,21-3,21-4,22-1       ¦           ¦ ¦ 3        ¦ 10/30/2001 ¦ 23-1,23-2,23-3,24-1,25-1       ¦           ¦ ¦ 3        ¦ 10/30/2001 ¦ 25-2,26-1,27-1,28-1,28-2       ¦           ¦ ¦ 3        ¦ 10/30/2001 ¦ 29-1,30-1,30-2,31-1,31-2       ¦           ¦ ¦ 3        ¦ 10/30/2001 ¦ 32-1,33-1,33-2,33-3,34-1       ¦           ¦ ¦ 3        ¦ 10/30/2001 ¦ 34-2,34-3,34-4,34-5,34-6       ¦           ¦ ¦ 3        ¦ 10/30/2001 ¦ 34-7,34-8,34-9,34-10,35-1      ¦           ¦ ¦ 3        ¦ 10/30/2001 ¦ 49-1,52-1,77-1,78-1,79-1       ¦           ¦ ¦ 3a       ¦ 03/11/2002 ¦ HIGHLIGHTS OF REV.,DEFINITIONS ¦           ¦ ¦ 3a       ¦ 03/11/2002 ¦ 23-2                           ¦           ¦ ¦ 4        ¦ 11/21/2002 ¦ HIGHLIGHTS OF REV.,DEFINITIONS ¦           ¦ ¦ 4        ¦ 11/21/2002 ¦ GUIDELINES                     ¦           ¦ ¦ 4        ¦ 11/21/2002 ¦ 23-1,23-2,23-3,24-1,25-1       ¦           ¦ ¦ 4        ¦ 11/21/2002 ¦ 25-2,34-3,34-4,34-5,34-6       ¦           ¦

FEDERAL AVIATION ADMINISTRATION   Page: II

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FEDERAL AVIATION ADMINISTRATION   Page: III

Revision: 5

MASTER MINIMUM EQUIPMENT LIST    Date: 03/10/2004

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Log of Revisions

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

¦ 4        ¦ 11/21/2002 ¦ 34-7,34-8,34-9,34-10,34-11     ¦           ¦ ¦ 5        ¦            ¦ HIGHLIGHTS OF REV.,DEFINITIONS ¦           ¦ ¦ 5        ¦            ¦ GUIDELINES                     ¦           ¦ ¦ 5        ¦            ¦ 21-1,21-2,21-3,21-4,22-1       ¦           ¦ ¦ 5        ¦            ¦ 23-1,23-2,23-3,23-4,24-1       ¦           ¦ ¦ 5        ¦            ¦ 25-1,25-2,26-1,27-1,28-1       ¦           ¦ ¦ 5        ¦            ¦ 28-2,29-1,30-1,30-2,31-1       ¦           ¦ ¦ 5        ¦            ¦ 31-2,33-1,33-2,33-3,34-1       ¦           ¦ ¦ 5        ¦            ¦ 34-2,34-3,34-4,34-5,34-6       ¦           ¦ ¦ 5        ¦            ¦ 34-7,34-8,34-9,34-10,34-11     ¦           ¦ ¦ 5        ¦            ¦ 35-1,49-1,78-1                 ¦           ¦

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MASTER MINIMUM EQUIPMENT LIST      Date: 03/10/2004

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Control Page

SYSTEM                                   PAGE  REV NO.  CURRENT DATE

Cover Page                               -       5        03/10/2004 Table of Contents                        I       5        03/10/2004 Log of Revisions                         II      5        03/10/2004 III     5        03/10/2004 Control Page                             IV      5        03/10/2004 V       5        03/10/2004 Highlights of Change                     VI      5        03/10/2004 VII     5        03/10/2004 VIII    5        03/10/2004 Definitions                                    IX      6        01/31/1995 X       6         01/31/1995 XI      6        01/31/1995 XII     6        01/31/1995 XIII    6        01/31/1995 XIV     6        01/31/1995 XV      6        01/31/1995 XVI     6        01/31/1995 Preamble                                         XVII    2        06/14/1989 XVIII   2        06/14/1989 Guidelines for (O) & (M) Procedures      XIX     5         03/10/2004 XX      5        03/10/2004 XXI     5        03/10/2004 XXII    5        03/10/2004 21                                       21-1    5        03/10/2004 21-2    5        03/10/2004 21-3    5        03/10/2004 21-4    5        03/10/2004 22                                       22-1    5        03/10/2004 23                                               23-1    5        03/10/2004 23-2    5         03/10/2004 23-3    5        03/10/2004 23-4    5        03/10/2004 24                                       24-1    5        03/10/2004 25                                       25-1    5        03/10/2004 25-2    5        03/10/2004 26                                       26-1    5        03/10/2004 27                                       27-1    5        03/10/2004 28                                       28-1    5        03/10/2004 28-2    5        03/10/2004 29                                                    29-1    5        03/10/2004

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MASTER MINIMUM EQUIPMENT LIST      Date: 03/10/2004

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Control Page

SYSTEM                                   PAGE  REV NO.  CURRENT DATE

30                                       30-1    5        03/10/2004 30-2    5        03/10/2004 31                                       31-1    5        03/10/2004 31-2    5        03/10/2004 32                                       32-1    3        10/30/2001 33                                       33-1    5        03/10/2004 33-2    5        03/10/2004 33-3    5        03/10/2004 34                                               34-1    5        03/10/2004 34-2    5         03/10/2004 34-3    5        03/10/2004 34-4    5        03/10/2004 34-5    5        03/10/2004 34-6    5        03/10/2004 34-7    5                03/10/2004 34-8    5        03/10/2004 34-9    5         03/10/2004 34-10   5        03/10/2004 34-11   5        03/10/2004 35                                       35-1    5        03/10/2004 49                                       49-1    5        03/10/2004 52                                       52-1    3        10/30/2001 77                                       77-1    3        10/30/2001 78                                       78-1    5        03/10/2004 79                                       79-1    3        10/30/2001

FEDERAL AVIATION ADMINISTRATION     Page: V

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MASTER MINIMUM EQUIPMENT LIST    Date: 03/10/2004

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Highlights of Change

ATA 21-3    Revised Remarks for Cabin Air Out-Flow Valves.  No change in                                                                  relief.

ATA 21-4    Revised Remarks for Air Conditioning System.  No change in                                                                relief.

ATA 21-9    Added a second proviso to Remarks for Cabin Differential                                                  Pressure Indicator.

ATA 21-11   Added second proviso to Remarks for Cabin Altimeter.

ATA 21-12   Revised Remarks for Cabin Altitude Warning System.  No                                                  change in relief.

ATA 21-15   Revised Remarks for Automatic Cabin Pressure Control System.                                                     No change in relief.

ATA 21-16   Revised Remarks for Manual Pressurization System.  No change                                                               in relief.

ATA 21-23   Added relief for Cabin Overhead Airflow Vents                                          (WEMACS/Gasper).

ATA 22-1-1) Revised Remarks for Autopilot System.  No change in relief.

ATA 22-2    Revised Remarks for Yaw Damper System.  No change in relief.

ATA 23-2    Revised System Item description and Remarks for Cockpit

Voice Recorder (CVR) in accordance with Policy Letter 29, designated as Global Change 48.

ATA 23-3    Revised relief for Passenger Address (PA) System in

accordance with Policy Letter 9, designated as Global Change 119.

ATA 23-7    Added relief for Cockpit Speakers.  Moved High Frequency (HF) Communication System to ATA 23-9.

ATA 23-8    Added relief for Headsets.

ATA 23-9    Moved High Frequency (HF) Communication System from ATA 23-7.  No change in relief.

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  FEDERAL AVIATION ADMINISTRATION   Page: VII

Revision: 5

MASTER MINIMUM EQUIPMENT LIST    Date: 03/10/2004

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Highlights of Change

ATA 23-10   Added relief for Hand Held Microphones.

ATA 23-11   Added relief for Flight Phone Systems.

ATA 23-12   Added relief for Automatic Cabin Briefing System.

ATA 24-8    Added relief for Baggage Compartment Heat.

ATA 24-9    Added relief for 60 Hertz AC System.

ATA 25-5    Removed asterisks from System Item description.

ATA 25-8    Added relief for Life rafts.

ATA 28-3    Deleted the word "OR" in accordance with Policy Letter 31, designated as Global Change 83.

ATA 28-5    Renumbered Pressure Refueling System as ATA 28-5 and

revised the System Item description.  No change in relief.

ATA 30-2    Revised the Remarks for the Pitot-Static Heater System.  No change in relief.

ATA 30-7    Removed the word "OR" in accordance with Policy letter 31, designated as Global Change 83.

ATA 31-1    Changed the System Item description to plural and rewrote the Remarks.  No change in relief.

ATA 33-8    Added relief for one Landing Light inoperative during night operations and revised Remarks.

ATA 33-9    Corrected System Item description to Wing Inspection Lights. No change in relief.

ATA 33-14   Changed Repair Category designation from "C" to "D" and added Remarks for Pulselite Landing Light System.

ATA 34-14   Change to System Item description, Remarks and associated NOTE for Radar Altimeter.

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Highlights of Change

ATA 34-16   Repair Category designation change from "C" to "B" for ATC

Transponders in accordance with Policy Letter 76, designated as Global Change 118.

ATA 34-17   Revised Remarks for Altitude Alerting System.

ATA 34-22   Revised Remarks for Air Data Computers (ADC).

ATA 34-24   Moved Traffic Collision and Avoidance System I (TCAS I) from ATA 34-25 to ATA 34-24.  No change in relief.

ATA 34-25   Moved Traffic Collision and Avoidance System II (TCAS II) from ATA 34-24 to ATA 34-25.  No change in relief.

ATA 34-29   Separated Navigation Management System from ATA 34-28 and assigned this System the next number, ATA 34-29.

ATA 34-30   Renumbered Stormscope as ATA 34-30.  No change in relief.

ATA 34-31   Renumbered Windshear Warning and Flight Guidance System as ATA 34-31.  No change in relief.

ATA 34-32   Renumbered Windshear Detection and Avoidance System as ATA 34-32.  No change in relief.

ATA 34-33   Renumbered Automatic Dependent Surveillance-Broadcast (ADS-B) System as ATA 34-33.  No change in relief.

ATA 34-34   Renumbered Standby Attitude Indicator as ATA 34-34.  No change in relief.

ATA 35-3    Added relief for Protective Breathing Equipment in accordance with Policy Letter 43.

ATA 49-1    Added a proviso to the Remarks for Auxiliary Power Unit.

ATA 49-1-1) Changed Repair Category designation from "B" to "C".

ATA 49-1-2) Changed Repair Category designation from "B" to "C".

ATA 49-1-3) Changed Repair Category designation from "B" to "C".

ATA 49-2    Added relief for APU Generator as a separate item.

  Revision: 6

MASTER MINIMUM EQUIPMENT LIST      Date: 01/31/1995

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Definitions

1.   System Definitions.

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

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

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

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

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

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

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

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

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

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

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Definitions

Certificate Data Sheet.

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

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

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

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

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

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

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

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

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

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

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

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Definitions

operation with the  listed item inoperative.

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

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

14.  Inoperative components of an inoperative system:

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

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

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

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

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Definitions

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

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

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

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

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

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

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

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

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

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

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Definitions

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

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

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

The letter designators are inserted adjacent to Column 2.

23. Electronic fault alerting system - General                  ¦

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

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

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

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

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MASTER MINIMUM EQUIPMENT LIST      Date: 01/31/1995

IA-1125, IA-1125 SP, IA-1125 SPX

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)                                           ¦

  Revision: 6

MASTER MINIMUM EQUIPMENT LIST      Date: 01/31/1995

IA-1125, IA-1125 SP, IA-1125 SPX

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: XV

  D."

FEDERAL AVIATION ADMINISTRATION     Page: XVI

Revision: 6

MASTER MINIMUM EQUIPMENT LIST      Date: 01/31/1995

IA-1125, IA-1125 SP, IA-1125 SPX

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

  FEDERAL AVIATION ADMINISTRATION   Page: XVII

Revision: 2

MASTER MINIMUM EQUIPMENT LIST    Date: 06/14/1989

IA-1125, IA-1125 SP, IA-1125 SPX

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: XVIII Revision: 2 MASTER MINIMUM EQUIPMENT LIST    Date: 06/14/1989

IA-1125, IA-1125 SP, IA-1125 SPX

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.

  Revision: 5

MASTER MINIMUM EQUIPMENT LIST    Date: 03/10/2004

IA-1125, IA-1125 SP, IA-1125 SPX

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 the affected bleed switching valve is closed.

(M) Maintenance procedure to ensure both bleed switching valves are closed.

21-3  (M) Maintenance procedure to secure the affected valve(s) in the open position.

21-15 (M) Maintenance procedure to secure the Cabin Air Out-Flow Valves in the open position.

21-21 (O) Operations procedure to ensure the Ground Bypass Valve is in the closed position.

21-22 (M) Maintenance procedure to ensure there is no air escaping from the HP Bleed Air Duct.

22-1-1(M) Maintenance procedure to ensure no electrical or mechanical fault exists that will have an adverse affect on any flight control function.

22-1-1(O) Operations procedure to ensure crew awareness of equipment

requirements for RVSM, RNP-5, RNP-10 and enroute procedures.

22-1-2(M) Maintenance procedure to ensure no electrical or mechanical fault exists that will have an adverse affect on any flight control function.

22-1-2(O) Operations procedure to ensure remaining Autopilot System operates normally.

22-2  (M) Maintenance procedure to disable the Yaw Damper and to ensure that the rudder servo does not cause binding of the control cables.

22-2  (O) Operations procedure to deactivate the Yaw Damper and to ensure AFM limitations are complied with.

FEDERAL AVIATION ADMINISTRATION   Page XIX

  Revision: 5

MASTER MINIMUM EQUIPMENT LIST    Date: 03/10/2004

IA-1125, IA-1125 SP, IA-1125 SPX

Guidelines for (O) & (M) Procedures

23-3-1 (O) Operations procedure to ensure passengers are adequately briefed.

23-5   (O) Operations procedure to ensure passengers are adequately briefed.

23-9   (O) Operations procedure to ensure remaining Long Range Communications System(s) operate normally.

23-12  (O) Operations procedure to ensure passengers are adequately briefed.

24-8   (M) Maintenance procedure to ensure appropriate circuit breakers are pulled and collared and system is secured.

24-9   (M) Maintenance procedure to ensure AC System is properly secured.

25-7   (O) Operations procedure to ensure that cargo is not mistakenly           secured by an inoperative Cargo Restraint System.

26-4   (M) Maintenance procedure to check the pressure gauge on the                               bottle.

30-2   (O) Operations procedure to ensure operations are not conducted                into known or forecast icing conditions.

30-4   (M) Maintenance procedure to secure Pneumatic De-icing Boot                              System.

31-4   (O) Operations procedure to record aircraft flight time.

33-3   (O) Operations procedure to ensure passengers are adequately                              briefed.

34-17  (O) Operations procedure to ensure altitude restrictions are                           complied with.

34-21  (O) Operations procedure to ensure alternate procedures are                       established and used.

34-21-1(O) Operations procedure to ensure alternate procedures are          established and used for the inoperative modes.

FEDERAL AVIATION ADMINISTRATION   Page XX

  Revision: 5

MASTER MINIMUM EQUIPMENT LIST    Date: 03/10/2004

IA-1125, IA-1125 SP, IA-1125 SPX

Guidelines for (O) & (M) Procedures

34-21-4(O) Operations procedure to ensure alternate procedures are   established and used for the appropriate inoperative callouts.

34-21-5(O) Operations procedure to ensure alternate procedures are            established and used for the windshear mode.

34-22  (O) Operations procedure to ensure both Air Data Computers are                             not required.

(O) Operations procedure to ensure both Air Data Computers are    not required and all air data instrumentations operates                           normally.

34-24  (M) Maintenance procedure to ensure system is deactivated or                              secured.

34-24  (O) Operations procedure to ensure enroute or approach              procedures do not require its use.

34-25  (M) Maintenance procedure to deactivate and secure the system.

34-25  (O) Operations procedure to ensure enroute or approach              procedures do not require its use.

34-25-1(O) Operations procedure to ensure TA and RA display is

visible to the non-flying pilot and audio functions are operative on the flying pilot side.

34-25-2(O) Operations procedure to ensure non-flying pilot monitors pilot's display.

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

34-25-3(O) Operations procedure to ensure all RA display and audio functions are operative.

34-28  (O) Operations procedure to verify status and suitability of navigation facilities used for the route of flight.

34-29  (O) Operations procedure to verify status and suitability of navigation facilities used for the route of flight.

FEDERAL AVIATION ADMINISTRATION   Page XXI

  FEDERAL AVIATION ADMINISTRATION   Page XXII

Revision: 5

MASTER MINIMUM EQUIPMENT LIST    Date: 03/10/2004

IA-1125, IA-1125 SP, IA-1125 SPX

Guidelines for (O) & (M) Procedures

34-31  (O) Operations procedure to ensure alternate procedures are established and used.

34-32  (O) Operations procedure to ensure alternate procedures are established and used.

35-2   (O) Operations procedure to ensure adequate oxygen is            available for all passengers on board.

49-2   (O) Operations procedure to ensure APU Generator switch is OFF                and remains OFF for the entire flight.

77-4   (O) Operations procedure to ensure flight crew uses APR - OFF                          performance data.

78-1   (M) Maintenance procedure to ensure Thrust Reverser System(s)                 is secured in the forward position.

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦

¦     IA-1125, IA-1125 SP, IA-1125 SPX     ¦ DATE: 03/10/2004      ¦ 21-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 21  AIR CONDITIONING      ¦    ¦    ¦                                       ¦

¦ 1.  Bleed Switching     C ¦ 2  ¦ 1  ¦ (M) One may be inoperative provided   ¦ ¦     Valves                ¦    ¦    ¦ the aircraft is not operated above    ¦ ¦                           ¦    ¦    ¦ FL 250.                               ¦

¦                         C ¦ 2  ¦ 0  ¦ (M) May be inoperative provided       ¦ ¦                           ¦    ¦    ¦     a) Affected valves are closed,    ¦ ¦                           ¦    ¦    ¦     b) The aircraft is operated       ¦ ¦                           ¦    ¦    ¦        unpressurized, and             ¦ ¦                           ¦    ¦    ¦     c) Ram air is selected.           ¦

¦ 2.  Ram Air Check       C ¦ 1  ¦ 0  ¦ May be inoperative in the OPEN        ¦ ¦     Valve                 ¦    ¦    ¦ position provided aircraft is         ¦ ¦                           ¦    ¦    ¦ operated unpressurized.               ¦

¦ 3.  Cabin Air Out-Flow  C ¦ 2  ¦ 0  ¦ (M) May be inoperative provided:      ¦ ¦     Valves                ¦    ¦    ¦     a) Affected valves are secured    ¦ ¦                           ¦    ¦    ¦        in the OPEN position, and      ¦ ¦                           ¦    ¦    ¦     b) The aircraft is operated       ¦ ¦                           ¦    ¦    ¦        unpressurized below 10,000   | ¦ ¦                           ¦    ¦    ¦        feet MSL.                    | ¦

¦ 4.  Air Conditioning    C ¦ 1  ¦ 0  ¦ May be inoperative provided:          ¦ ¦     System                ¦    ¦    ¦     a) Aircraft is operated         | ¦ ¦                           ¦    ¦    ¦        unpressurized, and           | ¦ ¦                           ¦    ¦    ¦     b) Aircraft is operated at or   | ¦ ¦                           ¦    ¦    ¦        below 10,000 feet MSL.       | ¦

¦ 5.  Automatic           C ¦ 1  ¦ 0  ¦ May be inoperative provided the       ¦ ¦     Temperature Control   ¦    ¦    ¦ Manual Temperature Control System     ¦ ¦     System                ¦    ¦    ¦ operates normally.                    ¦

¦ 6.  Manual              C ¦ 1  ¦ 0  ¦ May be inoperative provided the       ¦ ¦     Temperature Control   ¦    ¦    ¦ Automatic Temperature Control         ¦ ¦     System                ¦    ¦    ¦ System operates normally.             ¦

¦ 7.  Ground Cooling      C ¦ 1  ¦ 0  ¦                                       ¦ ¦     System                ¦    ¦    ¦                                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦

¦     IA-1125, IA-1125 SP, IA-1125 SPX     ¦ DATE: 03/10/2004      ¦ 21-2     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 21  AIR CONDITIONING      ¦    ¦    ¦                                       ¦

¦ 8.  Pilot's             C ¦ 1  ¦ 0  ¦                                       ¦ ¦     Conditioned Air       ¦    ¦    ¦                                       ¦

¦ 9.  Cabin Differential  C ¦ 1  ¦ 0  ¦ May be inoperative provided:          ¦ ¦     Pressure Indicator    ¦    ¦    ¦     a) Cabin Altitude Indicator       ¦ ¦                           ¦    ¦    ¦        is operative,                  ¦ ¦                           ¦    ¦    ¦     b) Cabin Altitude Warning         ¦ ¦                           ¦    ¦    ¦        System is operative,           ¦ ¦                           ¦    ¦    ¦     c) Cabin Rate of Climb            ¦ ¦                           ¦    ¦    ¦        Indicator is operative,        ¦ ¦                           ¦    ¦    ¦     d) A chart is provided to the     ¦ ¦                           ¦    ¦    ¦        crew for converting cabin      ¦ ¦                           ¦    ¦    ¦        altitude to differential       ¦ ¦                           ¦    ¦    ¦        pressure, and                  ¦

¦                         C ¦ 1  ¦ 0  ¦ May be inoperative provided         | ¦ ¦                           ¦    ¦    ¦ aircraft is operated unpressurized  | ¦ ¦                           ¦    ¦    ¦ at or below 10,000 feet MSL.        | ¦

¦ 10. Cabin Rate of       C ¦ 1  ¦ 0  ¦ May be inoperative provided all       ¦ ¦     Climb Indicator       ¦    ¦    ¦ other components of the pressure      ¦ ¦                           ¦    ¦    ¦ control system are operative.         ¦

¦ 11. Cabin Altimeter     C ¦ 1  ¦ 0  ¦ May be inoperative provided:          ¦ ¦                           ¦    ¦    ¦     a) Cabin differential pressure    ¦ ¦                           ¦    ¦    ¦        indicator is operative,        ¦ ¦                           ¦    ¦    ¦     b) Cabin altitude warning         ¦ ¦                           ¦    ¦    ¦        system is operative, and       ¦ ¦                           ¦    ¦    ¦     c) A chart is provided to the     ¦ ¦                           ¦    ¦    ¦        crew to convert cabin          ¦ ¦                           ¦    ¦    ¦        differential pressure to       ¦ ¦                           ¦    ¦    ¦        cabin altitude.                ¦

¦                         C ¦ 1  ¦ 0  ¦ May be inoperative provided:        | ¦ ¦                           ¦    ¦    ¦     a) Aircraft is operated           ¦ ¦                           ¦    ¦    ¦        unpressurized, and           | ¦ ¦                           ¦    ¦    ¦     b) Aircraft is operated at or   | ¦ ¦                           ¦    ¦    ¦        below 10,000 feet MSL.       | ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦

¦     IA-1125, IA-1125 SP, IA-1125 SPX     ¦ DATE: 03/10/2004      ¦ 21-3     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 21  AIR CONDITIONING      ¦    ¦    ¦                                       ¦

¦ 12. Cabin Altitude      C ¦ 1  ¦ 0  ¦ May be inoperative provided the       ¦ ¦     Warning System        ¦    ¦    ¦ aircraft is operated unpressurized    ¦ ¦                           ¦    ¦    ¦ at or below 10,000 feet MSL.        | ¦

¦ 13. Ditching Valve      C ¦ 1  ¦ 0  ¦ May be inoperative provided           ¦ ¦                           ¦    ¦    ¦ extended overwater flights are not    ¦ ¦                           ¦    ¦    ¦ conducted.                            ¦

¦ 14. Water Separator     C ¦ 1  ¦ 0  ¦ May be inoperative provided the       ¦ ¦     Temperature Control   ¦    ¦    ¦ airplane is operated unpressurized.   ¦ ¦     System                ¦    ¦    ¦                                       ¦

¦ 15. Autonatic Cabin     C ¦ 1  ¦ 0  ¦ (M) May be inoperative provided:      ¦ ¦     Pressure Control      ¦    ¦    ¦     a) Cabin Air Out-Flow Valves      ¦ ¦     System                ¦    ¦    ¦        are secured in the open        ¦ ¦                           ¦    ¦    ¦        position, and                  ¦ ¦                           ¦    ¦    ¦     b) The airplane is operated       ¦ ¦                           ¦    ¦    ¦        unpressurized at or below    | ¦ ¦                           ¦    ¦    ¦        10,000 feet MSL.             | ¦

¦                         C ¦ 1  ¦ 0  ¦ May be inoperative providing the      ¦ ¦                           ¦    ¦    ¦ Manual Pressurization System is       ¦ ¦                           ¦    ¦    ¦ operative.                            ¦

¦ 16. Manual              C ¦ 1  ¦ 0  ¦ May be inoperative provided           ¦ ¦     Pressurization        ¦    ¦    ¦ Automatic Cabin Pressure Control      ¦ ¦     System                ¦    ¦    ¦ system is operative.                  ¦

¦                         C ¦ 1  ¦ 0  ¦ May be inoperative provided the       ¦ ¦                           ¦    ¦    ¦ aircraft is operated unpressurized    ¦ ¦                           ¦    ¦    ¦ at or below 10,000 feet MSL.        | ¦

¦ 17. Landing Field       C ¦ 1  ¦ 0  ¦ May be inoperative provided:          ¦ ¦     Elevation Selector    ¦    ¦    ¦     a) All other components of        ¦ ¦     (A Knob)              ¦    ¦    ¦        Pressurization Control         ¦ ¦                           ¦    ¦    ¦        System are operative, and      ¦ ¦                           ¦    ¦    ¦     b) Cabin is unpressurized prior   ¦ ¦                           ¦    ¦    ¦        to landing.                    ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦

¦     IA-1125, IA-1125 SP, IA-1125 SPX     ¦ DATE: 03/10/2004      ¦ 21-4     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 21  AIR CONDITIONING      ¦    ¦    ¦                                       ¦

¦ 18. Barometric          C ¦ 1  ¦ 0  ¦ May be inoperative provided:          ¦ ¦     Adjustment Selector   ¦    ¦    ¦     a) All other components of        ¦ ¦     (B Knob)              ¦    ¦    ¦        Pressurization Control         ¦ ¦                           ¦    ¦    ¦        System are operative and       ¦ ¦                           ¦    ¦    ¦     b) Cabin is unpressurized prior   ¦ ¦                           ¦    ¦    ¦        to landing.                    ¦

¦ 19. Cabin Rate          C ¦    ¦ 0  ¦ May be inoperative provided:          ¦ ¦     Selector              ¦    ¦    ¦     a) All other components of        ¦ ¦     (R Knob)              ¦    ¦    ¦        Pressurization Control         ¦ ¦                           ¦    ¦    ¦        System are operative and       ¦ ¦                           ¦    ¦    ¦     b) Cabin is unpressurized prior   ¦ ¦                           ¦    ¦    ¦        to landing.                    ¦

¦ 20. CABIN/FUEL/RAT        ¦    ¦    ¦                                       ¦ ¦     TEMP Indicator        ¦    ¦    ¦                                       ¦

¦     Cabin Temp Mode     C ¦ 1  ¦ 0  ¦                                       ¦

¦ 21. Ground Bypass       C ¦ 1  ¦ 0  ¦ (O) May be inoperative in the         ¦ ¦     Valve                 ¦    ¦    ¦ closed position.                      ¦

¦ 22. HP Bleed Air Duct   C ¦ 2  ¦ 0  ¦ (M)                                   ¦ ¦     Blow Out Discs        ¦    ¦    ¦                                       ¦

¦ 23. Cabin Overhead      D ¦ -  ¦ -  ¦                                     | ¦ ¦     Airflow Vents         ¦    ¦    ¦                                     | ¦ ¦     (Wemacs/Gasper)       ¦    ¦    ¦                                     | ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦

¦     IA-1125, IA-1125 SP, IA-1125 SPX     ¦ DATE: 03/10/2004      ¦ 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      ¦    ¦    ¦                                       ¦

¦     1) One Autopilot    B ¦ 1  ¦ 0  ¦ (M)(O) May be inoperative provided:   ¦ ¦        System Installed   ¦    ¦    ¦     a) Enroute operations,          | ¦ ¦                           ¦    ¦    ¦        including RVSM, RNP-5 and    | ¦ ¦                           ¦    ¦    ¦        RNP-10, and approach         | ¦ ¦                           ¦    ¦    ¦        procedures do not require    | ¦ ¦                           ¦    ¦    ¦        its use, and                 | ¦ ¦                           ¦    ¦    ¦     b) AFM limitations are          | ¦ ¦                           ¦    ¦    ¦        observed.                    | ¦

¦     2) Two or more      C ¦ -  ¦ 1  ¦ (M)(O) May be inoperative             ¦ ¦        Autopilot Systems  ¦    ¦    ¦ provided remaining system(s)          ¦ ¦        Installed          ¦    ¦    ¦ operate normally.                     ¦

¦ 2.  Yaw Damper System   C ¦ 1  ¦ 0  ¦ (M)(O) May be inoperative provided:   ¦ ¦                           ¦    ¦    ¦     a) Enroute operations,          | ¦ ¦                           ¦    ¦    ¦        including RVSM, RNP-5 and    | ¦ ¦                           ¦    ¦    ¦        RNP-10, do not require       | ¦ ¦                           ¦    ¦    ¦        its use, and                 | ¦ ¦                           ¦    ¦    ¦     b) AFM limitations are          | ¦ ¦                           ¦    ¦    ¦        observed.                      ¦

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

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦

¦     IA-1125, IA-1125 SP, IA-1125 SPX     ¦ DATE: 03/10/2004      ¦ 23-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 23  COMMUNICATIONS        ¦    ¦    ¦                                       ¦

¦ 1.  Communications      D ¦ -  ¦ -  ¦ Any in excess of those required by    ¦ ¦     Systems               ¦    ¦    ¦ FAR may be inoperative provided it    ¦ ¦     (VHF, UHF)            ¦    ¦    ¦ is not powered by the Emergency AC    ¦ ¦                           ¦    ¦    ¦ Bus, Emergency DC Bus, Battery Bus    ¦ ¦                           ¦    ¦    ¦ Battery Direct Bus, or the DC         ¦ ¦                           ¦    ¦    ¦ Transfer Bus and not required for     ¦ ¦                           ¦    ¦    ¦ Emergency Procedures.                 ¦ ¦     1) VHF Comm           ¦    ¦    ¦                                       ¦

¦        a) Frequency     C ¦ -  ¦ 0  ¦                                       ¦ ¦           Transfer        ¦    ¦    ¦                                       ¦ ¦           Light           ¦    ¦    ¦                                       ¦

¦        b) Frequency     C ¦ -  ¦ 0  ¦                                       ¦ ¦           Transfer        ¦    ¦    ¦                                       ¦ ¦           Switch          ¦    ¦    ¦                                       ¦

¦        c) Frequency     C ¦ -  ¦ 2  ¦                                       ¦ ¦           Selector        ¦    ¦    ¦                                       ¦ ¦           Knob            ¦    ¦    ¦                                       ¦

¦        d) Frequency     C ¦ -  ¦ 2  ¦                                       ¦ ¦           Indication      ¦    ¦    ¦                                       ¦

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

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

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦

¦     IA-1125, IA-1125 SP, IA-1125 SPX     ¦ DATE: 03/10/2004      ¦ 23-2     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 23  COMMUNICATIONS        ¦    ¦    ¦                                       ¦

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

¦     1) Passenger        B ¦ 1  ¦ 0  ¦ (O) May be inoperative provided:      ¦ ¦        Configuration      ¦    ¦    ¦     a) Alternate, normal and        | ¦ ¦                           ¦    ¦    ¦        emergency procedures and/or  | ¦ ¦                           ¦    ¦    ¦        operating restrictions are   | ¦ ¦                           ¦    ¦    ¦        established and used, and    | ¦ ¦                           ¦    ¦    ¦     b) Flight Attendant Alerting    | ¦ ¦                           ¦    ¦    ¦        System (audio and visual)    | ¦ ¦                           ¦    ¦    ¦        operates normally.           | ¦

¦                         C ¦ 1  ¦ 0  ¦ (O) May be inoperative provided:    | ¦ ¦                           ¦    ¦    ¦     a) PA not required by FAR, and  | ¦ ¦                           ¦    ¦    ¦     b) Alternate, normal and        | ¦ ¦                           ¦    ¦    ¦        emergency procedures and/or  | ¦ ¦                           ¦    ¦    ¦        operating restrictions are   | ¦ ¦                           ¦    ¦    ¦        established and used.        | ¦

¦                           ¦    ¦    ¦ NOTE: Any station function(s) that  | ¦ ¦                           ¦    ¦    ¦       operate normally may be used. | ¦

¦     2) Cargo            D ¦ 1  ¦ 0  ¦ May be inoperative provided         | ¦ ¦        Configuration      ¦    ¦    ¦ procedures do not require its use.  | ¦

¦ 4.  Boom Microphones      ¦    ¦    ¦                                       ¦ ¦     (COCKPIT VOICE        ¦    ¦    ¦                                       ¦ ¦     RECORDER WITH FLIGHT  ¦    ¦    ¦                                       ¦ ¦     DATA RECORDER         ¦    ¦    ¦                                       ¦ ¦     INSTALLED)            ¦    ¦    ¦                                       ¦

¦     1) Cockpit Voice    A ¦ -  ¦ 0  ¦ May be inoperative provided:          ¦ ¦        Recorder Equipped  ¦    ¦    ¦     a) Flight Data Recorder (FDR)     ¦ ¦        to record Boom     ¦    ¦    ¦        operates normally, and         ¦ ¦        Microphones per    ¦    ¦    ¦     b) Repairs are made within        ¦ ¦        FAR 135.151(d) or  ¦    ¦    ¦        three flight days.             ¦ ¦        121.139(g).        ¦    ¦    ¦                                       ¦

¦                  (CON'T.) ¦    ¦    ¦                                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦

¦     IA-1125, IA-1125 SP, IA-1125 SPX     ¦ DATE: 03/10/2004      ¦ 23-3     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 23  COMMUNICATIONS        ¦    ¦    ¦                                       ¦

¦ 4.  Boom Microphones      ¦    ¦    ¦                                       ¦ ¦                  (CON'T.) ¦    ¦    ¦                                       ¦

¦ *** 2) Cockpit Voice    D ¦ -  ¦ 0  ¦ Any in excess of those required by    ¦ ¦        Recorder not       ¦    ¦    ¦ FAR may be inoperative.               ¦ ¦        equipped to record ¦    ¦    ¦                                       ¦ ¦        Boom Microphones.  ¦    ¦    ¦                                       ¦

¦     (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     ¦    ¦    ¦                                       ¦ ¦        Microphones per    ¦    ¦    ¦                                       ¦ ¦        FAR 135.151(d) or  ¦    ¦    ¦                                       ¦ ¦        121.139(g).        ¦    ¦    ¦                                       ¦

¦ *** 2) Cockpit Voice    D ¦ -  ¦ 0  ¦ Any in excess of those required by    ¦ ¦        Recorder not       ¦    ¦    ¦ FAR may be inoperative.               ¦ ¦        equipped to record ¦    ¦    ¦                                       ¦ ¦        Boom Microphones.  ¦    ¦    ¦                                       ¦

¦ 5.  Recorded Passenger  C ¦ 1  ¦ 0  ¦ (O)                                   ¦ ¦ *** Briefing System       ¦    ¦    ¦                                       ¦

¦ 6.  Selective Call      C ¦ 1  ¦ 0  ¦                                       ¦ ¦ *** System (SELCAL)       ¦    ¦    ¦                                       ¦

¦ 7.  Cockpit Speakers    C ¦ 2  ¦ 0  ¦ May be inoperative provided         | ¦ ¦                           ¦    ¦    ¦ Headsets are installed and operate  | ¦ ¦                           ¦    ¦    ¦ normally.                           | ¦

¦ 8.  Headsets            C ¦ 2  ¦ 1  ¦ One pilot's Headset may be          | ¦ ¦                           ¦    ¦    ¦ inoperative provided operations do  | ¦ ¦                           ¦    ¦    ¦ not require its use and both pilot  | ¦ ¦                           ¦    ¦    ¦ Cockpit Speakers operate normally.  | ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦

¦     IA-1125, IA-1125 SP, IA-1125 SPX     ¦ DATE: 03/10/2004      ¦ 23-4     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 23  COMMUNICATIONS        ¦    ¦    ¦                                       ¦

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

¦                         C ¦ -  ¦ 1  ¦ (O) May be inoperative while          ¦ ¦                           ¦    ¦    ¦ conducting operations that require    ¦ ¦                           ¦    ¦    ¦ two LRCS 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.               ¦

¦ 10. Hand Held           C ¦ -  ¦ 0  ¦ May be inoperative provided:        | ¦ ¦     Microphones           ¦    ¦    ¦     a) Both cockpit crewmembers use | ¦ ¦                           ¦    ¦    ¦        a Boom Microphone, and       | ¦ ¦                           ¦    ¦    ¦     b) Both control wheel           | ¦ ¦                           ¦    ¦    ¦        Push-To-Talk Switches        | ¦ ¦                           ¦    ¦    ¦        operate normally.            | ¦

¦ 11. Flight Phone        D ¦ -  ¦ 0  ¦                                     | ¦ ¦ *** Systems               ¦    ¦    ¦                                     | ¦

¦ 12. Automatic Cabin     D ¦ -  ¦ 0  ¦ (O) May be inoperative provided     | ¦ ¦ *** Briefing System       ¦    ¦    ¦ alternate procedures are            | ¦ ¦                           ¦    ¦    ¦ established and used.               | ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦

¦     IA-1125, IA-1125 SP, IA-1125 SPX     ¦ DATE: 03/10/2004      ¦ 24-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 24  ELECTRICAL POWER      ¦    ¦    ¦                                       ¦

¦ 1.  DC Voltmeters         ¦    ¦    ¦ DELETED REVISION 2                    ¦

¦ 2.  DC Ammeters           ¦    ¦    ¦ DELETED REVISION 2                    ¦

¦ 3.  Inverters           B ¦ 2  ¦ 1  ¦ One may be inoperative provided       ¦ ¦                           ¦    ¦    ¦ aircraft is operated in Day VMC.      ¦

¦     Inverters           B ¦ 2  ¦ 1  ¦ One may be inoperative provided:      ¦ ¦     (AHRS Equipped)       ¦    ¦    ¦     a) Aircraft is equipped with      ¦ ¦                           ¦    ¦    ¦        the Collins AHRS system and    ¦ ¦                           ¦    ¦    ¦     b) All other AC electrical        ¦ ¦                           ¦    ¦    ¦        system components are          ¦ ¦                           ¦    ¦    ¦        operative.                     ¦

¦ 4.  AC Voltmeters       B ¦ 2  ¦ 1  ¦ One may be inoperative.               ¦

¦ 5.  Battery             C ¦ 1  ¦ 0  ¦ May be inoperative provided           ¦ ¦     Temperature           ¦    ¦    ¦ NI-CAD batteries are not installed.   ¦ ¦     Indicator             ¦    ¦    ¦                                       ¦

¦ 6.  Nose Compartment    C ¦ -  ¦ 0  ¦ May be inoperative provided AFM       ¦ ¦     Blower                ¦    ¦    ¦ procedures are observed.              ¦

¦ 7.  External Power      C ¦ 1  ¦ 0  ¦                                       ¦ ¦     System                ¦    ¦    ¦                                       ¦

¦ 8.  Baggage             C ¦ 1  ¦ 0  ¦ (M) May be inoperative provided:    | ¦ ¦     Compartment Heat      ¦    ¦    ¦ Baggage Compartment Heat Switch     | ¦ ¦                           ¦    ¦    ¦ is in the OFF position for the      | ¦ ¦                           ¦    ¦    ¦ duration of the flight.             | ¦

¦ 9.  60 Hertz AC         C ¦ 1  ¦ 0  ¦ (M)                                 | ¦ ¦     Electrical System     ¦    ¦    ¦                                     | ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦

¦     IA-1125, IA-1125 SP, IA-1125 SPX     ¦ DATE: 03/10/2004      ¦ 25-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 25  EQUIPMENT/FURNISHINGS ¦    ¦    ¦                                       ¦

¦ 1.  Passenger Seat(s)   C ¦ -  ¦ -  ¦ May be inoperative provided:          ¦ ¦                           ¦    ¦    ¦     a) Seat does not block an         ¦ ¦                           ¦    ¦    ¦        Emergency Exit,                ¦ ¦                           ¦    ¦    ¦     b) Seat does not restrict any     ¦ ¦                           ¦    ¦    ¦        passenger from access to the   ¦ ¦                           ¦    ¦    ¦        main aircraft aisle and        ¦ ¦                           ¦    ¦    ¦     c) Affected seat(s) is            ¦ ¦                           ¦    ¦    ¦        blocked and placarded "DO      ¦ ¦                           ¦    ¦    ¦        NOT OCCUPY".                   ¦

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

¦                           ¦    ¦    ¦ NOTE 2: Affected seat(s) may          ¦ ¦                           ¦    ¦    ¦         include the seat(s) behind    ¦ ¦                           ¦    ¦    ¦         and/or adjacent outboard      ¦ ¦                           ¦    ¦    ¦         seats.                        ¦

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

¦ 2.  Passenger Convenience ¦ -  ¦ 0  ¦ Passenger convenience items, as       ¦ ¦     Item(s)               ¦    ¦    ¦ expressed in this MMEL, are those     ¦ ¦                           ¦    ¦    ¦ related to passenger convenience,     ¦ ¦                           ¦    ¦    ¦ comfort, or entertainment such as,    ¦ ¦                           ¦    ¦    ¦ but not limited to, galley equip-     ¦ ¦                           ¦    ¦    ¦ ment, ash trays, stereo equipment,    ¦ ¦                           ¦    ¦    ¦ overhead reading lamps.  Items        ¦ ¦                           ¦    ¦    ¦ addressed elsewhere in this docu-     ¦ ¦                           ¦    ¦    ¦ ment shall not be included.  (M)      ¦ ¦                           ¦    ¦    ¦ or (O) procedures may be required     ¦ ¦                           ¦    ¦    ¦ and included in the air carrier's     ¦ ¦                           ¦    ¦    ¦ appropriate document.                 ¦

¦                           ¦    ¦    ¦ NOTE:  EXTERIOR LAVATORY DOOR         ¦ ¦                           ¦    ¦    ¦        ASHTRAYS ARE NOT CONSIDERED    ¦ ¦                           ¦    ¦    ¦        CONVENIENCE ITEMS.             ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦

¦     IA-1125, IA-1125 SP, IA-1125 SPX     ¦ DATE: 03/10/2004      ¦ 25-2     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 25  EQUIPMENT/FURNISHINGS ¦    ¦    ¦                                       ¦

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

¦ 4.  Flotation Devices   D ¦ -  ¦ -  ¦ Any in excess of those required by    ¦ ¦                           ¦    ¦    ¦ FAR may be inoperative or missing.    ¦

¦ 5.  Emergency Locator   C ¦ 1  ¦ 0  ¦ As required by FAR.                   ¦ ¦     Transmitter (ELT)     ¦    ¦    ¦                                     | ¦

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

¦ 6.  "Fasten Seat Belt   C ¦ -  ¦ -  ¦ One or more signs or placards may     ¦ ¦     While Seated" Sign    ¦    ¦    ¦ be illegible or missing provided      ¦ ¦     or Placard            ¦    ¦    ¦ a legible sign or placard is          ¦ ¦                           ¦    ¦    ¦ visible from each occupied            ¦ ¦                           ¦    ¦    ¦ passenger seat.                       ¦

¦ 7.  Cargo               C ¦ -  ¦ -  ¦ (O) May be inoperative or missing     ¦ ¦     Restraint             ¦    ¦    ¦ provided acceptable cargo loading     ¦ ¦     System(s)             ¦    ¦    ¦ limits from an approved source,       ¦ ¦                           ¦    ¦    ¦ i.e., an Approved Cargo Loading       ¦ ¦                           ¦    ¦    ¦ Manual, Cargo Handling Manual, or     ¦ ¦                           ¦    ¦    ¦ Weight and Balance Documents are      ¦ ¦                           ¦    ¦    ¦ observed.                             ¦

¦                         C ¦ -  ¦ -  ¦ May be inoperative or missing         ¦ ¦                           ¦    ¦    ¦ provided procedures are               ¦ ¦                           ¦    ¦    ¦ established and used to ensure the    ¦ ¦                           ¦    ¦    ¦ associated compartment remains        ¦ ¦                           ¦    ¦    ¦ empty, or is verified to contain      ¦ ¦                           ¦    ¦    ¦ only empty Cargo Handling             ¦ ¦                           ¦    ¦    ¦ Equipment, Ballast and/or Fly Away    ¦ ¦                           ¦    ¦    ¦ Kits.                                 ¦

¦ 8.  Life Rafts          D ¦ -  ¦ -  ¦ Any in excess of those required by  | ¦ ¦                           ¦    ¦    ¦ FAR may be inoperative or missing.  | ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦

¦     IA-1125, IA-1125 SP, IA-1125 SPX     ¦ DATE: 03/10/2004      ¦ 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    ¦ ¦     Extinguishers         ¦    ¦    ¦ FAR may be inoperative or missing     ¦ ¦                           ¦    ¦    ¦ provided:                             ¦ ¦                           ¦    ¦    ¦     a) The inoperative fire           ¦ ¦                           ¦    ¦    ¦        extinguisher is tagged         ¦ ¦                           ¦    ¦    ¦        inoperative, removed from      ¦ ¦                           ¦    ¦    ¦        the installed location, and    ¦ ¦                           ¦    ¦    ¦        placed out of sight so it      ¦ ¦                           ¦    ¦    ¦        can not be mistaken for a      ¦ ¦                           ¦    ¦    ¦        functional unit, and           ¦ ¦                           ¦    ¦    ¦     b) Required distribution is       ¦ ¦                           ¦    ¦    ¦        maintained.                    ¦

¦ 2.  Lavatory Smoke        ¦    ¦    ¦ DELETED REVISION 2.                   ¦ ¦     Detection System      ¦    ¦    ¦                                       ¦

¦ 3.  Lavatory Fire         ¦    ¦    ¦ DELETED REVISION 2.                   ¦ ¦     Extinguisher System   ¦    ¦    ¦                                       ¦

¦ 4.  Fire Bottle Thermal C ¦ 2  ¦ 0  ¦ (M) May be inoperative provided the   ¦ ¦     Discharge Indicator   ¦    ¦    ¦ pressure gauge on the bottle(s) is    ¦ ¦     (Disc)                ¦    ¦    ¦ checked for correct pressure prior    ¦ ¦                           ¦    ¦    ¦ to each departure.                    ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦

¦     IA-1125, IA-1125 SP, IA-1125 SPX     ¦ DATE: 03/10/2004      ¦ 27-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 27  FLIGHT CONTROLS       ¦    ¦    ¦                                       ¦

¦ 1.  Slat and Flap         ¦    ¦    ¦ DELETED REVISION 2                    ¦ ¦     Position Indicator    ¦    ¦    ¦                                       ¦

¦ 2.  Horizontal          C ¦ 1  ¦ 0  ¦ May be inoperative provided:          ¦ ¦     Stabilizer Trim       ¦    ¦    ¦     a) Flight crew verifies by        ¦ ¦     Indicator             ¦    ¦    ¦        visual inspection that         ¦ ¦                           ¦    ¦    ¦        stabilizer setting agrees      ¦ ¦                           ¦    ¦    ¦        with trim markings on          ¦ ¦                           ¦    ¦    ¦        vertical fin before each       ¦ ¦                           ¦    ¦    ¦        flight, and                    ¦ ¦                           ¦    ¦    ¦     b) Rudder and aileron trim        ¦ ¦                           ¦    ¦    ¦        indicators are operative.      ¦

¦ 3.  Aileron Trim        C ¦ 1  ¦ 0  ¦ May be inoperative provided:          ¦ ¦     Indicator             ¦    ¦    ¦     a) Flight crew verifies by        ¦ ¦                           ¦    ¦    ¦        visual inspection that         ¦ ¦                           ¦    ¦    ¦        ailerons are in neutral        ¦ ¦                           ¦    ¦    ¦        position before each flight,   ¦ ¦                           ¦    ¦    ¦        and                            ¦ ¦                           ¦    ¦    ¦     b) Horizontal stabilizer and      ¦ ¦                           ¦    ¦    ¦        rudder trim indicators are     ¦ ¦                           ¦    ¦    ¦        operative.                     ¦

¦ 4.  Rudder Trim         C ¦ 1  ¦ 0  ¦ May be inoperative provided:          ¦ ¦     Indicator             ¦    ¦    ¦     a) Flight crew verifies by        ¦ ¦                           ¦    ¦    ¦        visual inspection that         ¦ ¦                           ¦    ¦    ¦        rudder trim is neutral         ¦ ¦                           ¦    ¦    ¦        before each flight, and        ¦ ¦                           ¦    ¦    ¦     b) Horizontal stabilizer and      ¦ ¦                           ¦    ¦    ¦        aileron trim indicators are    ¦ ¦                           ¦    ¦    ¦        operative.                     ¦

¦ 5.  Automatic Slat      C ¦ 1  ¦ 0  ¦ May be inoperative provided:          ¦ ¦     Extension System      ¦    ¦    ¦     a) The airplane is not operated   ¦ ¦                           ¦    ¦    ¦        into known or forecast icing   ¦ ¦                           ¦    ¦    ¦        coditions,                     ¦ ¦                           ¦    ¦    ¦     b) The airplane is operated in    ¦ ¦                           ¦    ¦    ¦        day VMC, and                   ¦ ¦                           ¦    ¦    ¦     c) AFM limitations are complied   ¦ ¦                           ¦    ¦    ¦        with.                          ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦

¦     IA-1125, IA-1125 SP, IA-1125 SPX     ¦ DATE: 03/10/2004      ¦ 28-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 28  FUEL                  ¦    ¦    ¦                                       ¦

¦ 1.  Interconnect        C ¦ 2  ¦ 1  ¦ One may be inoperative provided       ¦ ¦     Valves                ¦    ¦    ¦ fuel jettison system is operative.    ¦

¦ 2.  Transfer Valves     C ¦ 2  ¦ 1  ¦ One may be inoperative provided:      ¦ ¦                           ¦    ¦    ¦     a) Fuel is limited to 4000 lbs.   ¦ ¦                           ¦    ¦    ¦        maximum, and                   ¦ ¦                           ¦    ¦    ¦     b) Interconnect valves operate    ¦ ¦                           ¦    ¦    ¦        normally.                      ¦

¦ 3.  Jettison Valves     C ¦ 2  ¦ 1  ¦ One may be inoperative provided       ¦ ¦                           ¦    ¦    ¦ interconnect valves operate           ¦ ¦                           ¦    ¦    ¦ normally.                             ¦ ¦                           ¦    ¦    ¦                                     | ¦ ¦                         C ¦ 2  ¦ 0  ¦ May be inoperative provided:          ¦ ¦                           ¦    ¦    ¦     a) Airplane is not operated       ¦ ¦                           ¦    ¦    ¦        above 18,000 lbs. takeoff      ¦ ¦                           ¦    ¦    ¦        weight, and                    ¦ ¦                           ¦    ¦    ¦     b) Interconnect valves operate    ¦ ¦                           ¦    ¦    ¦        normally.                      ¦

¦ 4.  Fuel Low Level      C ¦ 1  ¦ 0  ¦ May be inoperative provided Fuel      ¦ ¦     Light                 ¦    ¦    ¦ Quantity Displays operate normally.   ¦

¦ 5.  Pressure Fueling    C ¦ 1  ¦ 0  ¦                                     | ¦ ¦     System                ¦    ¦    ¦                                     | ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦

¦     IA-1125, IA-1125 SP, IA-1125 SPX     ¦ DATE: 03/10/2004      ¦ 28-2     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 28  FUEL                  ¦    ¦    ¦                                       ¦

¦ 6.  Fuel Management       ¦    ¦    ¦                                       ¦ ¦     Indicator             ¦    ¦    ¦                                       ¦

¦     1) Wing Tank Fuel   C ¦ 2  ¦ 1  ¦ One may be inoperative provided:      ¦ ¦        Quantity Display   ¦    ¦    ¦     a) All other functions of Fuel    ¦ ¦                           ¦    ¦    ¦        Management Indicator are       ¦ ¦                           ¦    ¦    ¦        operative,                     ¦ ¦                           ¦    ¦    ¦     b) Fuel transfer valves are       ¦ ¦                           ¦    ¦    ¦        operative, and                 ¦ ¦                           ¦    ¦    ¦     c) A minimum fuel quantity of     ¦ ¦                           ¦    ¦    ¦        4000 lbs. is required for      ¦ ¦                           ¦    ¦    ¦        takeoff.                       ¦

¦     2) Fuselage Tank    C ¦ 1  ¦ 0  ¦ May be inoperative provided:          ¦ ¦        Fuel Display       ¦    ¦    ¦     a) All other functions of Fuel    ¦ ¦                           ¦    ¦    ¦        Management Indicator are       ¦ ¦                           ¦    ¦    ¦        operative, and                 ¦ ¦                           ¦    ¦    ¦     b) Fuel transfer valves are       ¦ ¦                           ¦    ¦    ¦        operative.                     ¦

¦     3) Fuel Consumed    C ¦ 1  ¦ 0  ¦ May be inoperative provided all       ¦ ¦        Display            ¦    ¦    ¦ other functions of Fuel Management    ¦ ¦                           ¦    ¦    ¦ Indicator are operative.              ¦

¦     4) Fuel Remaining   C ¦ 1  ¦ 0  ¦ May be inoperative provided all       ¦ ¦        Display            ¦    ¦    ¦ other functions of Fuel Management    ¦ ¦                           ¦    ¦    ¦ Indicator are operative.              ¦

¦     5) Fuel Flow        C ¦ 2  ¦ 1  ¦ One may be inoperative provided:      ¦ ¦        Display            ¦    ¦    ¦     a) Fuel quantity indicators are   ¦ ¦                           ¦    ¦    ¦        operative,                     ¦ ¦                           ¦    ¦    ¦     b) Remaining engine indicators    ¦ ¦                           ¦    ¦    ¦        for the associated engine      ¦ ¦                           ¦    ¦    ¦        are operative, and             ¦ ¦                           ¦    ¦    ¦     c) Fuel Flow on Flight            ¦ ¦                           ¦    ¦    ¦        Management System is           ¦ ¦                           ¦    ¦    ¦        operative.                     ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦

¦     IA-1125, IA-1125 SP, IA-1125 SPX     ¦ DATE: 03/10/2004      ¦ 29-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 29  HYDRAULIC POWER       ¦    ¦    ¦                                       ¦

¦ 1.  Hydraulic Tank      C ¦ 1  ¦ 0  ¦ May be inoperative provided:          ¦ ¦     Pressurization        ¦    ¦    ¦     a) All other hydraulic            ¦ ¦                           ¦    ¦    ¦        components are operative,      ¦ ¦                           ¦    ¦    ¦     b) Aircraft is not operated       ¦ ¦                           ¦    ¦    ¦        above FL 350, and              ¦ ¦                           ¦    ¦    ¦     c) Landing gear is not extended   ¦ ¦                           ¦    ¦    ¦        or operated above 8,000 ft     ¦ ¦                           ¦    ¦    ¦        altitude.                      ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦

¦     IA-1125, IA-1125 SP, IA-1125 SPX     ¦ DATE: 03/10/2004      ¦ 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.  Windshield Wipers   C ¦ 2  ¦ -  ¦ May be inoperative provided the       ¦ ¦                           ¦    ¦    ¦ airplane is not operated in           ¦ ¦                           ¦    ¦    ¦ precipitation within 5 NM of the      ¦ ¦                           ¦    ¦    ¦ airport of takeoff or intended        ¦ ¦                           ¦    ¦    ¦ landing.                              ¦

¦ 2.  Pitot-Static        B ¦ 2  ¦ 1  ¦ (O) One may be inoperative, except  | ¦ ¦     Heater System         ¦    ¦    ¦ where enroute operations, including | ¦ ¦                           ¦    ¦    ¦ RVSM, RNP-5 and RNP-10, provided:   | ¦ ¦                           ¦    ¦    ¦     a) The airplane is not operated   ¦ ¦                           ¦    ¦    ¦        into known or forecast icing   ¦ ¦                           ¦    ¦    ¦        conditions,                    ¦ ¦                           ¦    ¦    ¦     b) The airplane is operated in    ¦ ¦                           ¦    ¦    ¦        day VMC, and                   ¦ ¦                           ¦    ¦    ¦     c) AFM limitations for the        ¦ ¦                           ¦    ¦    ¦        Automatic Slat Extension       ¦ ¦                           ¦    ¦    ¦        System Inoperative are         ¦ ¦                           ¦    ¦    ¦        complied with.                 ¦

¦ 3.  Windshield Heat     C ¦ 2  ¦ 0  ¦ May be inoperative provided:          ¦ ¦                           ¦    ¦    ¦     a) De-fog system is operative,    ¦ ¦                           ¦    ¦    ¦        and                            ¦ ¦                           ¦    ¦    ¦     b) The airplane is not operated   ¦ ¦                           ¦    ¦    ¦        into known or forecast icing   ¦ ¦                           ¦    ¦    ¦        conditions.                    ¦

¦ 4.  Pneumatic De-icing  C ¦ 2  ¦ 0  ¦ (M) May be inoperative provided:      ¦ ¦     Boot System           ¦    ¦    ¦     a) The airplane is not operated   ¦ ¦                           ¦    ¦    ¦        into known or forecast icing   ¦ ¦                           ¦    ¦    ¦        conditions, and                ¦ ¦                           ¦    ¦    ¦     b) System is secured to ensure    ¦ ¦                           ¦    ¦    ¦        that boots remain deflated     ¦ ¦                           ¦    ¦    ¦        by suction.                    ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦

¦     IA-1125, IA-1125 SP, IA-1125 SPX     ¦ DATE: 03/10/2004      ¦ 30-2     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 30  ICE AND RAIN          ¦    ¦    ¦                                       ¦ ¦     PROTECTION            ¦    ¦    ¦                                       ¦

¦ 5.  Surface De-icing      ¦    ¦    ¦                                       ¦ ¦     System Control        ¦    ¦    ¦                                       ¦

¦     a) Normal System    C ¦ 1  ¦ 0  ¦ May be inoperative provided the       ¦ ¦                           ¦    ¦    ¦ Alternate System is operative.        ¦

¦     b) Alternate        C ¦ 1  ¦ 0  ¦ May be inoperative provided the       ¦ ¦        System             ¦    ¦    ¦ Normal System is operative.           ¦

¦ 6.  Defog system        C ¦ 1  ¦ 0  ¦ May be inoperative provided both      ¦ ¦                           ¦    ¦    ¦ windshield heat systems are           ¦ ¦                           ¦    ¦    ¦ operative.                            ¦

¦ 7.  Engine Inlet        C ¦ 2  ¦ 0  ¦ May be inoperative in the open        ¦ ¦     Anti-Icing Valve      ¦    ¦    ¦ position.                             ¦ ¦     (TAI Valve)           ¦    ¦    ¦                                       ¦ ¦     SPX only              ¦    ¦    ¦                                     | ¦

¦                         C ¦ 2  ¦ 0  ¦ May be inoperative in the closed      ¦ ¦                           ¦    ¦    ¦ position provided aircraft is not     ¦ ¦                           ¦    ¦    ¦ operated in known or forecast         ¦ ¦                           ¦    ¦    ¦ conditions.                           ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦

¦     IA-1125, IA-1125 SP, IA-1125 SPX     ¦ DATE: 03/10/2004      ¦ 31-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 31  INDICATING/RECORDING  ¦    ¦    ¦                                       ¦ ¦     SYSTEMS               ¦    ¦    ¦                                       ¦

¦ 1.  Clocks              C ¦ -  ¦ 0  ¦ Any in excess of those required by  | ¦ ¦                           ¦    ¦    ¦ FAR may be inoperative.             | ¦

¦ 2.  Flight Data         C ¦ -  ¦ 1  ¦ Any in excess of those required       ¦ ¦ *** Recorder (FDR)        ¦    ¦    ¦ by FAR may be inoperative.            ¦ ¦     System                ¦    ¦    ¦                                       ¦ ¦                         A ¦ -  ¦ 0  ¦ May be inoperative provided:          ¦ ¦                           ¦    ¦    ¦     a) Cockpit Voice Recorder (CVR)   ¦ ¦                           ¦    ¦    ¦        operates normally,             ¦ ¦                           ¦    ¦    ¦     b) Airplane is not dispatched     ¦ ¦                           ¦    ¦    ¦        from a designated airport as   ¦ ¦                           ¦    ¦    ¦        listed in the operator's MEL   ¦ ¦                           ¦    ¦    ¦        unless:                        ¦ ¦                           ¦    ¦    ¦        1. The FDR failure occurs      ¦ ¦                           ¦    ¦    ¦           after pushback but prior    ¦ ¦                           ¦    ¦    ¦           to takeoff, or              ¦ ¦                           ¦    ¦    ¦        2. The FDR repair was          ¦ ¦                           ¦    ¦    ¦           attempted but was not       ¦ ¦                           ¦    ¦    ¦           successful.                 ¦ ¦                           ¦    ¦    ¦     c) In those cases where repair    ¦ ¦                           ¦    ¦    ¦        is attempted but not           ¦ ¦                           ¦    ¦    ¦        successful, the aircraft may   ¦ ¦                           ¦    ¦    ¦        be dispatched on a flight or   ¦ ¦                           ¦    ¦    ¦        series of flights until the    ¦ ¦                           ¦    ¦    ¦        next designated airport        ¦ ¦                           ¦    ¦    ¦        where repair must be           ¦ ¦                           ¦    ¦    ¦        accomplished prior to          ¦ ¦                           ¦    ¦    ¦        dispatch, and                  ¦ ¦                           ¦    ¦    ¦     d) Repairs must be made within    ¦ ¦                           ¦    ¦    ¦        three flight days.             ¦

¦     FDR Recording       A ¦ -  ¦ -  ¦ May be inoperative provided:          ¦ ¦     Parameters required   ¦    ¦    ¦     a) Cockpit Voice Recorder (CVR)   ¦ ¦     by FAR                ¦    ¦    ¦        operates normally, and         ¦ ¦                           ¦    ¦    ¦     b) Repairs are made within 20     ¦ ¦                           ¦    ¦    ¦        calendar days.                 ¦

¦     FDR Recording       A ¦ -  ¦ -  ¦ May be inoperative provided repairs   ¦ ¦     Parameters not        ¦    ¦    ¦ are made prior to the completion of   ¦ ¦     required by FAR       ¦    ¦    ¦ the next heavy maintenance visit.     ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦

¦     IA-1125, IA-1125 SP, IA-1125 SPX     ¦ DATE: 03/10/2004      ¦ 31-2     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 31  INDICATING/RECORDING  ¦    ¦    ¦                                       ¦ ¦     SYSTEMS               ¦    ¦    ¦                                       ¦

¦ 3.  Cockpit Voice         ¦    ¦    ¦ Moved to ATA Chapter 23               ¦ ¦     Recorder              ¦    ¦    ¦                                       ¦

¦ 4.  Flight Hour         C ¦ 1  ¦ 0  ¦ (O)                                   ¦ ¦ *** Recorder              ¦    ¦    ¦                                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 3        ¦ PAGE:    ¦

¦     IA-1125, IA-1125 SP, IA-1125 SPX     ¦ DATE: 10/30/2001      ¦ 32-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 32  LANDING GEAR          ¦    ¦    ¦                                       ¦

¦ 1.  Antiskid System     C ¦ 1  ¦ 0  ¦ May be inoperative provided           ¦ ¦                           ¦    ¦    ¦ AFM is complied with.                 ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦

¦     IA-1125, IA-1125 SP, IA-1125 SPX     ¦ DATE: 03/10/2004      ¦ 33-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 33  LIGHTS                ¦    ¦    ¦                                       ¦

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

¦ 2.  Cabin Interior      C ¦ -  ¦ -  ¦ May be inoperative provided:          ¦ ¦     Illumination          ¦    ¦    ¦     a) Cabin emergency lighting is    ¦ ¦     System                ¦    ¦    ¦        operative, and                 ¦ ¦                           ¦    ¦    ¦     b) Lighting configuration at      ¦ ¦                           ¦    ¦    ¦        dispatch is acceptable to      ¦ ¦                           ¦    ¦    ¦        the flight crew.               ¦

¦ 3.  Passenger Notice    C ¦ 1  ¦ 0  ¦ (O) May be inoperative provided       ¦ ¦     System (Fasten Seat   ¦    ¦    ¦ appropriate verbal briefings are      ¦ ¦     Belts, No Smoking)    ¦    ¦    ¦ given to passengers.                  ¦

¦ 4.  Baggage             C ¦ 1  ¦ 0  ¦                                       ¦ ¦     Compartment           ¦    ¦    ¦                                       ¦ ¦     Light System          ¦    ¦    ¦                                       ¦

¦ 5.  Anti-Collision      B ¦ 1  ¦ 0  ¦ May be inoperative provided the       ¦ ¦     Light System          ¦    ¦    ¦ airplane is operated day only.        ¦ ¦     (Top and/or Bottom    ¦    ¦    ¦                                       ¦ ¦     Strobes)              ¦    ¦    ¦                                       ¦

¦ 6.  Wing Tip Strobes    C ¦ 2  ¦ 0  ¦                                       ¦

¦ 7.  Taxi Light System   C ¦ 1  ¦ 0  ¦                                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦

¦     IA-1125, IA-1125 SP, IA-1125 SPX     ¦ DATE: 03/10/2004      ¦ 33-2     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 33  LIGHTS                ¦    ¦    ¦                                       ¦

¦ 8.  Landing Light       C ¦ 2  ¦ 1  ¦ One may be inoperative for night    | ¦ ¦     System                ¦    ¦    ¦ operations provided taxi lights     | ¦ ¦                           ¦    ¦    ¦ operate normally.                   | ¦

¦                         C ¦ 2  ¦ 0  ¦ May be inoperative for day          | ¦ ¦                           ¦    ¦    ¦ operations.                         | ¦

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

¦ 10. Position Lights     C ¦ 1  ¦ 0  ¦ May be inoperative provided           ¦ ¦     System                ¦    ¦    ¦ the airplane is operated day only.    ¦

¦ 11. Emergency Exit      C ¦ 1  ¦ 0  ¦ May be inoperative for all cargo      ¦ ¦     Lighting System       ¦    ¦    ¦ operations only.                      ¦

¦ 12. Floor Proximity     C ¦ -  ¦ -  ¦ Individual lights may be              ¦ ¦ *** Emergency Escape      ¦    ¦    ¦ inoperative provided it is verified   ¦ ¦     Path Marking          ¦    ¦    ¦ that FAA approved minimum             ¦ ¦     System Lights         ¦    ¦    ¦ acceptable lighting levels            ¦ ¦                           ¦    ¦    ¦ specified in one of the following     ¦ ¦                           ¦    ¦    ¦ documents are complied with:          ¦ ¦                           ¦    ¦    ¦     a) FAA Engineering approval       ¦ ¦                           ¦    ¦    ¦        letter,                        ¦ ¦                           ¦    ¦    ¦     b) FAA approved report of the     ¦ ¦                           ¦    ¦    ¦        Type Design holder,            ¦ ¦                           ¦    ¦    ¦     c) Limitations and Conditions     ¦ ¦                           ¦    ¦    ¦        section of the applicable      ¦ ¦                           ¦    ¦    ¦        Supplemental Type              ¦ ¦                           ¦    ¦    ¦        Certificate (STC), or          ¦ ¦                           ¦    ¦    ¦     d) An FAA approved report         ¦ ¦                           ¦    ¦    ¦        incorporated in the Master     ¦ ¦                           ¦    ¦    ¦        Drawing List for the           ¦ ¦                           ¦    ¦    ¦        applicable STC.                ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦

¦     IA-1125, IA-1125 SP, IA-1125 SPX     ¦ DATE: 03/10/2004      ¦ 33-3     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 33  LIGHTS                ¦    ¦    ¦                                       ¦

¦ 13.  Strobes              ¦    ¦    ¦ Moved to No 6.                        ¦

¦ 14.  Pulselite Landing  D ¦ -  ¦ 0  ¦ May be inoperative provided both    | ¦ ¦ ***  Light System         ¦    ¦    ¦ Landing Lights operate normally.    | ¦

¦ 15.  Logo Lights        D ¦ -  ¦ 0  ¦                                       ¦ ¦ ***                       ¦    ¦    ¦                                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦

¦     IA-1125, IA-1125 SP, IA-1125 SPX     ¦ DATE: 03/10/2004      ¦ 34-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 34  NAVIGATION            ¦    ¦    ¦                                       ¦

¦ 1.  Mach/Airspeed         ¦    ¦    ¦                                       ¦ ¦     Indicator             ¦    ¦    ¦                                       ¦

¦     Mach Indicator      C ¦ 2  ¦ 0  ¦ May be inoperative provided:          ¦ ¦                           ¦    ¦    ¦     a) The airplane is not operated   ¦ ¦                           ¦    ¦    ¦        above FL 250,                  ¦ ¦                           ¦    ¦    ¦     b) Overspeed warning is           ¦ ¦                           ¦    ¦    ¦        operative, and                 ¦ ¦                           ¦    ¦    ¦     c) AFM limitations are            ¦ ¦                           ¦    ¦    ¦        observed.                      ¦

¦ 2.  Mach/Airspeed       C ¦ 1  ¦ 0  ¦ May be inoperative provided:          ¦ ¦     Overspeed Warning     ¦    ¦    ¦     a) Both Mach Meters are           ¦ ¦     System                ¦    ¦    ¦        operative, and                 ¦ ¦                           ¦    ¦    ¦     b) The following airspeed         ¦ ¦                           ¦    ¦    ¦        limitations are observed and   ¦ ¦                           ¦    ¦    ¦        placarded in plain view of     ¦ ¦                           ¦    ¦    ¦        each pilot station:            ¦

¦                           ¦    ¦    ¦        1) Vmo - 350 KIAS below FL     ¦ ¦                           ¦    ¦    ¦           250, or                     ¦ ¦                           ¦    ¦    ¦        2) Mmo - .81 MACH FL 250 and   ¦ ¦                           ¦    ¦    ¦           above.                      ¦

¦ 3.  RAT/CABIN/FUEL        ¦    ¦    ¦                                       ¦ ¦     TEMP Indicator        ¦    ¦    ¦                                       ¦

¦     RAT Mode            C ¦ 1  ¦ 0  ¦ May be inoperative provided SAT       ¦ ¦                           ¦    ¦    ¦ and TAS information is available.     ¦

¦ 4.  Turn and Bank         ¦    ¦    ¦ DELETED REVISION 2                    ¦ ¦     Indicator             ¦    ¦    ¦                                       ¦

¦     a) Slip Indicator   B ¦ 2  ¦ 1  ¦ One may be inoperative.               ¦

¦     b) Turn Indicator     ¦    ¦    ¦ DELETED REVISION 2.                   ¦

¦ 5.  Vertical            C ¦ 1  ¦ 0  ¦                                       ¦ ¦     Navigation System     ¦    ¦    ¦                                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦

¦     IA-1125, IA-1125 SP, IA-1125 SPX     ¦ DATE: 03/10/2004      ¦ 34-2     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 34  NAVIGATION            ¦    ¦    ¦                                       ¦

¦ 6.  Flight Director     C ¦ 2  ¦ 0  ¦ May be inoperative provided           ¦ ¦     System                ¦    ¦    ¦ landing weather minimums do not       ¦ ¦                           ¦    ¦    ¦ require its use.                      ¦

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

¦ 8.  Marker Beacon       C ¦ 1  ¦ 0  ¦ May be inoperative provided           ¦ ¦     Receiver              ¦    ¦    ¦ approach procedures do not require    ¦ ¦                           ¦    ¦    ¦ its use.                              ¦

¦ 9.  Weather Radar       C ¦ 1  ¦ -  ¦ As required by FAR.                   ¦

¦ 10. Automatic           C ¦ -  ¦ -  ¦ Any in excess of those required by    ¦ ¦     Direction Finding     ¦    ¦    ¦ FAR may be inoperative.               ¦ ¦     (ADF) System          ¦    ¦    ¦                                       ¦

¦ 11. Radio Magnetic      C ¦ -  ¦ 0  ¦                                       ¦ ¦     Indicator (RMI)       ¦    ¦    ¦                                       ¦

¦ 12. AOA Indicator       C ¦ 1  ¦ 0  ¦                                       ¦

¦ 13. Navigation          C ¦ -  ¦ -  ¦ Any in excess of those required by    ¦ ¦     Equipment             ¦    ¦    ¦ FAR may be inoperative.               ¦ ¦     (VOR/ILS, Loran,      ¦    ¦    ¦                                       ¦ ¦     RNAV, Omega/VLF, INS, ¦    ¦    ¦                                       ¦ ¦     GPS, Doppler, FMS)    ¦    ¦    ¦                                       ¦

¦ 14. Radio Altimeter     C ¦ 1  ¦ 0  ¦ May be inoperative provided enroute | ¦ ¦                           ¦    ¦    ¦ or approach procedures do not       | ¦ ¦                           ¦    ¦    ¦ require its use.                    | ¦

¦                           ¦    ¦    ¦ NOTE:  Inoperative Radio Altimeter  | ¦ ¦                           ¦    ¦    ¦ may affect the Ground Proximity     | ¦ ¦                           ¦    ¦    ¦ Warning System (GPWS) and Traffic   | ¦ ¦                           ¦    ¦    ¦ Collision and Avoidance System      | ¦ ¦                           ¦    ¦    ¦ (TCAS).                             | ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦

¦     IA-1125, IA-1125 SP, IA-1125 SPX     ¦ DATE: 03/10/2004      ¦ 34-3     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 34  NAVIGATION            ¦    ¦    ¦                                       ¦

¦ 15. Multi-Function        ¦    ¦    ¦                                       ¦ ¦     Display (MFD)         ¦    ¦    ¦                                       ¦ ¦     Symbol Generator      ¦    ¦    ¦                                       ¦

¦     a) 1125             C ¦ 1  ¦ 0  ¦                                       ¦

¦     b) 1125 SPX         C ¦ 2  ¦ 1  ¦ One may be inoperative provided       ¦ ¦                           ¦    ¦    ¦ both Primary Flight Displays (PFD)    ¦ ¦                           ¦    ¦    ¦ are operative.                        ¦

¦ 16. ATC Transponders    B ¦ -  ¦ 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 fcailities   ¦ ¦                           ¦    ¦    ¦        having jurisdiction over the   ¦ ¦                           ¦    ¦    ¦        planned route of flight.       ¦

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

¦ 17. Altitude Alerting   A ¦ -  ¦ 0  ¦ (O) May be inoperative provided:      ¦ ¦     System                ¦    ¦    ¦     a) Autopilot with altitude hold   ¦ ¦                           ¦    ¦    ¦        is operative.                  ¦ ¦                           ¦    ¦    ¦     b) Enroute operations,          | ¦ ¦                           ¦    ¦    ¦        including RVSM, RNP-5 and    | ¦ ¦                           ¦    ¦    ¦        RNP-10 operations do not     | ¦ ¦                           ¦    ¦    ¦        require its use, and           ¦ ¦                           ¦    ¦    ¦     c) Repairs are made within        ¦ ¦                           ¦    ¦    ¦        three flight days.             ¦

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

¦ 18. Remote Tuning Unit  C ¦ 2  ¦ 1  ¦ One may be inoperative provided at    ¦ ¦     (RTU)                 ¦    ¦    ¦ least one FMS is operative.           ¦

¦ 19. Airborne Flight     C ¦ 1  ¦ 0  ¦                                       ¦ ¦ *** Information System    ¦    ¦    ¦                                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦

¦     IA-1125, IA-1125 SP, IA-1125 SPX     ¦ DATE: 03/10/2004      ¦ 34-4     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 34  NAVIGATION            ¦    ¦    ¦                                       ¦

¦ 20. Maintenance         C ¦ 1  ¦ 0  ¦                                       ¦ ¦ *** Diagnostic System     ¦    ¦    ¦                                       ¦

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

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

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

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

¦                         C ¦ 1  ¦ 0  ¦ May be inoperative provided:          ¦ ¦                           ¦    ¦    ¦     a) It is not required by FAR,     ¦ ¦                           ¦    ¦    ¦        and                            ¦ ¦                           ¦    ¦    ¦     b) GPWS is considered             ¦ ¦                           ¦    ¦    ¦        inoperative.                   ¦

¦                  (CON'T.) ¦    ¦    ¦                                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦

¦     IA-1125, IA-1125 SP, IA-1125 SPX     ¦ DATE: 03/10/2004      ¦ 34-5     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 34  NAVIGATION            ¦    ¦    ¦                                       ¦

¦ 21. 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 Mode   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)TAWS              C ¦ -  ¦ 0  ¦                                       ¦

¦ 22.  Air Data           C ¦ 2  ¦ 1  ¦ (O) One may be inoperative except   | ¦ ¦      Computers (ADC)      ¦    ¦    ¦ where enroute operations, including | ¦ ¦                           ¦    ¦    ¦ RVSM, RNP-5 and RNP-10 operations,  | ¦ ¦                           ¦    ¦    ¦ require its use provided right side   ¦ ¦                           ¦    ¦    ¦ Flight Instruments are pneumatic.     ¦

¦                         C ¦ 2  ¦ 1  ¦ (O) One may be inoperative except   | ¦ ¦                           ¦    ¦    ¦ where enroute operations, including | ¦ ¦                           ¦    ¦    ¦ RVSM, RNP-5 and RNP-10 operations,  | ¦ ¦                           ¦    ¦    ¦ require its use provided all Air      ¦ ¦                           ¦    ¦    ¦ Data instrumentation functions        ¦ ¦                           ¦    ¦    ¦ normally.                             ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦

¦     IA-1125, IA-1125 SP, IA-1125 SPX     ¦ DATE: 03/10/2004      ¦ 34-6     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 34  NAVIGATION            ¦    ¦    ¦                                       ¦

¦ 23.  Non-Stabilized     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         ¦ ¦                           ¦    ¦    ¦        Stabilized Gyro or INS         ¦ ¦                           ¦    ¦    ¦        Stabilized Compass Systems     ¦ ¦                           ¦    ¦    ¦        are operative, and             ¦ ¦                           ¦    ¦    ¦     b) Aircraft is operated with      ¦ ¦                           ¦    ¦    ¦        dual independent navigation    ¦ ¦                           ¦    ¦    ¦        capability and under           ¦ ¦                           ¦    ¦    ¦        positive radar control by      ¦ ¦                           ¦    ¦    ¦        ATC on the enroute portion     ¦ ¦                           ¦    ¦    ¦        of the flight.                 ¦

¦                         B ¦ 1  ¦ 0  ¦ May be inoperative for flights        ¦ ¦                           ¦    ¦    ¦ that are entirely within areas        ¦ ¦                           ¦    ¦    ¦ of magnetic unreliability provided    ¦ ¦                           ¦    ¦    ¦ at least two Stabilized Directional   ¦ ¦                           ¦    ¦    ¦ Gyro Systems are installed,           ¦ ¦                           ¦    ¦    ¦ operative and used in conjunction     ¦ ¦                           ¦    ¦    ¦ with approved Free Gyro navigation    ¦ ¦                           ¦    ¦    ¦ techniques.                           ¦

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

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

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦

¦     IA-1125, IA-1125 SP, IA-1125 SPX     ¦ DATE: 03/10/2004      ¦ 34-7     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 34  NAVIGATION            ¦    ¦    ¦                                       ¦

¦ 25. Traffic Collision   B ¦ -  ¦ O  ¦ (M) May be inoperative provided:    | ¦ ¦     and Avoidance         ¦    ¦    ¦     a) System is deactivated and      ¦ ¦     System II (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                   ¦ ¦                           ¦    ¦    ¦     b) Enroute or Approach            ¦ ¦                           ¦    ¦    ¦        procedures do not require      ¦ ¦                           ¦    ¦    ¦        its use.                       ¦

¦ *** 1) Combined         C ¦ -  ¦ 0  ¦ (O) One may be in operative on the    ¦ ¦        Traffic Alert (TA) ¦    ¦    ¦ non-flying pilot side provided:       ¦ ¦        and Resolulion     ¦    ¦    ¦     a) TA and RA visual display is    ¦ ¦        Advisory (RA)      ¦    ¦    ¦        operative on the flying        ¦ ¦        Dual Display       ¦    ¦    ¦        pilot side, and                ¦ ¦        System(s)          ¦    ¦    ¦     b) TA and RA audio function is    ¦ ¦                           ¦    ¦    ¦        operative on the flying        ¦ ¦                           ¦    ¦    ¦        pilot side.                    ¦

¦     2) Resolution       C ¦ 2  ¦ 1  ¦ (O) One may be inoperative on the     ¦ ¦        Advisory (RA)      ¦    ¦    ¦ non-flying pilot side.                ¦ ¦        System(s)          ¦    ¦    ¦                                       ¦

¦                         C ¦ -  ¦ 0  ¦ (O) May be inoperative provided:      ¦ ¦                           ¦    ¦    ¦     a) All Traffic Alert (TA)         ¦ ¦                           ¦    ¦    ¦        display elements 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.                       ¦

¦                  (CON'T.) ¦    ¦    ¦                                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦

¦     IA-1125, IA-1125 SP, IA-1125 SPX     ¦ DATE: 03/10/2004      ¦ 34-8     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 34  NAVIGATION            ¦    ¦    ¦                                       ¦

¦ 25. Traffic Collision     ¦    ¦    ¦                                       ¦ ¦     and Avoidance         ¦    ¦    ¦                                       ¦ ¦     System II (TCAS II)   ¦    ¦    ¦                                       ¦ ¦                  (CON'T.) ¦    ¦    ¦                                       ¦

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

¦ 26. Moving Map          D ¦ -  ¦ -  ¦                                       ¦ ¦ *** Display               ¦    ¦    ¦                                       ¦

¦ 27. Windshear             ¦    ¦    ¦ DELETED REVISION 3                    ¦ ¦ *** Detection and         ¦    ¦    ¦ (Now items 30 and 31)                 ¦ ¦     Guidance Systems      ¦    ¦    ¦                                       ¦

¦ 28. Flight Management     ¦    ¦    ¦                                       ¦ ¦ *** System (FMS)          ¦    ¦    ¦                                       ¦

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

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦

¦     IA-1125, IA-1125 SP, IA-1125 SPX     ¦ DATE: 03/10/2004      ¦ 34-9     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 34  NAVIGATION            ¦    ¦    ¦                                       ¦

¦ 29. Navigation            ¦    ¦    ¦                                     | ¦ ¦ *** Management System     ¦    ¦    ¦                                     | ¦

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

¦ 30.  Stormscope         D ¦ -  ¦ -  ¦                                     | ¦ ¦ ***                       ¦    ¦    ¦                                       ¦

¦ 31. Windshear Warning   C ¦ -  ¦ 0  ¦ (O) May be inoperative provided:    | ¦ ¦     and Flight Guidance   ¦    ¦    ¦     a) Alternate procedures are       ¦ ¦     System                ¦    ¦    ¦        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.                    ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦

¦     IA-1125, IA-1125 SP, IA-1125 SPX     ¦ DATE: 03/10/2004      ¦ 34-10    ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 34  NAVIGATION            ¦    ¦    ¦                                       ¦

¦ 32. Windshear Detection C ¦ -  ¦ 0  ¦ (O) May be inoperative provided:    | ¦ ¦     and Avoidance System  ¦    ¦    ¦     a) Alternate procedures are       ¦ ¦                           ¦    ¦    ¦        established and used, and      ¦ ¦                           ¦    ¦    ¦     b) Windshear Warning and          ¦ ¦                           ¦    ¦    ¦        Guidance 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.                    ¦

¦ 33. Automatic Dependent D ¦ -  ¦ 0  ¦ May be inoperative provided it is   | ¦ ¦     Surveillance-         ¦    ¦    ¦ not required by FAR.                  ¦ ¦     Broadcast (ADS-B)     ¦    ¦    ¦                                       ¦ ¦     System                ¦    ¦    ¦ NOTE: If ADS-B is installed in lieu   ¦ ¦                           ¦    ¦    ¦ of or as a replacement for FAR-       ¦ ¦                           ¦    ¦    ¦ required equipment, the repair        ¦ ¦                           ¦    ¦    ¦ category in the operator's MEL will   ¦ ¦                           ¦    ¦    ¦ be the same as that of the FAR-       ¦ ¦                           ¦    ¦    ¦ required equipment.                   ¦

¦     1) Link and Display D ¦ -  ¦ 0  ¦                                       ¦ ¦        Processor Unit     ¦    ¦    ¦ NOTE: Cockpit Display Traffic         ¦ ¦        (LDPU)             ¦    ¦    ¦ Information (CDTI) display of data    ¦ ¦                           ¦    ¦    ¦ from other aircraft systems may be    ¦ ¦                           ¦    ¦    ¦ used.                                 ¦

¦     2) Cockpit Display  D ¦ -  ¦ 0  ¦                                       ¦ ¦        and Traffic        ¦    ¦    ¦ NOTE: ADS-B data transmissions        ¦ ¦        Information (CDTI) ¦    ¦    ¦ may continue.                         ¦

¦     3) CDTI Control     D ¦ -  ¦ 0  ¦ May be inoperative provided:          ¦ ¦        Panel              ¦    ¦    ¦   a) Flight ID can be set, and        ¦ ¦                           ¦    ¦    ¦   b) Screen display is acceptable     ¦ ¦                           ¦    ¦    ¦        to the flight crew.            ¦ ¦                  (CON'T.) ¦    ¦    ¦                                       ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦

¦     IA-1125, IA-1125 SP, IA-1125 SPX     ¦ DATE: 03/10/2004      ¦ 34-11    ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 34  NAVIGATION            ¦    ¦    ¦                                       ¦

¦ 33. Automatic Dependent   ¦    ¦    ¦                                     | ¦ ¦     Surveillance-         ¦    ¦    ¦                                       ¦ ¦     Broadcast (ADS-B)     ¦    ¦    ¦                                       ¦ ¦     System       (CON'T.) ¦    ¦    ¦                                       ¦

¦     4) Data Link        D ¦ -  ¦ 0  ¦                                       ¦ ¦        Transmitter(s)     ¦    ¦    ¦                                       ¦

¦     5) Data Link        D ¦ -  ¦ 0  ¦                                       ¦ ¦        Receiver(s)        ¦    ¦    ¦                                       ¦

¦ 34. Standby Attitude    C ¦ -  ¦ 0  ¦ May be inoperative provided:        | ¦ ¦       Indicator           ¦    ¦    ¦     a) Operations are conducted       ¦ ¦                           ¦    ¦    ¦        in Day VMC only, and           ¦ ¦                           ¦    ¦    ¦     b) Operations are not             ¦ ¦                           ¦    ¦    ¦        conducted into known or        ¦ ¦                           ¦    ¦    ¦        forecast VFR-on-Top            ¦ ¦                           ¦    ¦    ¦        conditions.                    ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦

¦     IA-1125, IA-1125 SP, IA-1125 SPX     ¦ DATE: 03/10/2004      ¦ 35-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 35  OXYGEN                ¦    ¦    ¦                                       ¦

¦ 1.  Oxygen System and   C ¦ -  ¦ -  ¦ As required by FAR.                   ¦ ¦     Supply (Passenger)    ¦    ¦    ¦                                       ¦

¦ 2.  Oxygen Blow Out     C ¦ 1  ¦ 0  ¦ (O) May be missing provided           ¦ ¦     Disc                  ¦    ¦    ¦ adequate oxygen is available for      ¦ ¦                           ¦    ¦    ¦ number of people on board including   ¦ ¦                           ¦    ¦    ¦ crew.                                 ¦

¦ 3.  Protective          D ¦ -  ¦ -  ¦ Any in excess of those required by  | ¦ ¦ *** Breathing Equipment   ¦    ¦    ¦ FAR may be inoperative.             | ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦

¦     IA-1125, IA-1125 SP, IA-1125 SPX     ¦ DATE: 03/10/2004      ¦ 49-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 49  AIRBORNE AUXILIARY    ¦    ¦    ¦                                       ¦ ¦     POWER                 ¦    ¦    ¦                                       ¦

¦ 1.  Auxiliary Power     B ¦ 1  ¦ 0  ¦ May be inoperative provided APU is  | ¦ ¦ *** Unit (APU)            ¦    ¦    ¦ secured and other procedures do     | ¦ ¦                           ¦    ¦    ¦ not require its use.                | ¦

¦     1) Speed System     C ¦ 1  ¦ 0  ¦ May be inoperative provided the     | ¦ ¦                           ¦    ¦    ¦ APU is not used.                      ¦

¦     2) Temperature      C ¦ 1  ¦ 0  ¦ May be inoperative provided the     | ¦ ¦        System             ¦    ¦    ¦ APU is not used.                      ¦

¦     3) Fire Protection  C ¦ 1  ¦ 0  ¦ May be inoperative provided the     | ¦ ¦        System             ¦    ¦    ¦ APU is not used.                      ¦

¦ 2.  APU Generator       B ¦ 1  ¦ 0  ¦ (O) May be inoperative provided:    | ¦ ¦ ***                       ¦    ¦    ¦     a) Both engine-driven           | ¦ ¦                           ¦    ¦    ¦        Generators are operative,    | ¦ ¦                           ¦    ¦    ¦        and,                         | ¦ ¦                           ¦    ¦    ¦     b) Other procedures do not      | ¦ ¦                           ¦    ¦    ¦        require its use.             | ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 3        ¦ PAGE:    ¦

¦     IA-1125, IA-1125 SP, IA-1125 SPX     ¦ DATE: 10/30/2001      ¦ 52-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 52  DOORS                 ¦    ¦    ¦                                       ¦

¦ 1.  Door Warning Light  C ¦ 1  ¦ 0  ¦ May be inoperative provided           ¦ ¦     System                ¦    ¦    ¦ a crewmember verifies by visual       ¦ ¦                           ¦    ¦    ¦ inspection before each departure      ¦ ¦                           ¦    ¦    ¦ that the door(s) is closed and        ¦ ¦                           ¦    ¦    ¦ locked.                               ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 3        ¦ PAGE:    ¦

¦     IA-1125, IA-1125 SP, IA-1125 SPX     ¦ DATE: 10/30/2001      ¦ 77-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 77  ENGINE INDICATING     ¦    ¦    ¦                                       ¦

¦ 1.  N1 Indicator        C ¦ 2  ¦ 0  ¦ May be inoperative provided           ¦ ¦     Digital Display       ¦    ¦    ¦ associated analog display is          ¦ ¦                           ¦    ¦    ¦ operative.                            ¦

¦ 2.  N2 Indicator        C ¦ 2  ¦ 0  ¦ May be inoperative provided           ¦ ¦     Digital Display       ¦    ¦    ¦ associated analog display is          ¦ ¦                           ¦    ¦    ¦ operative.                            ¦

¦ 3.  ITT Indicator       C ¦ 2  ¦ 0  ¦ May be inoperative provided           ¦ ¦     Digital Display       ¦    ¦    ¦ associated analog display is          ¦ ¦                           ¦    ¦    ¦ operative.                            ¦

¦ 4.  Automatic Power     C ¦ 1  ¦ 0  ¦ (O) May be inoperative provided       ¦ ¦     Reserve (APR)         ¦    ¦    ¦     AFM is complied with.             ¦ ¦     (SPX only)            ¦    ¦    ¦                                       ¦

¦ 5.  Engine Synchronizer C ¦ 1  ¦ 0  ¦                                       ¦ ¦     (ENG SYNC)            ¦    ¦    ¦                                       ¦

¦ 6.  Liquid Crystal      A ¦ 2  ¦ 1  ¦ One may be inoperative provided:      ¦ ¦ *** Displays              ¦    ¦    ¦     a) Reversionary mode is           ¦ ¦                           ¦    ¦    ¦        operative and                  ¦ ¦                           ¦    ¦    ¦     b) Repairs are made within one    ¦ ¦                           ¦    ¦    ¦        flight day.                    ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 5        ¦ PAGE:    ¦

¦     IA-1125, IA-1125 SP, IA-1125 SPX     ¦ DATE: 03/10/2004      ¦ 78-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 78  ENGINE EXHAUST        ¦    ¦    ¦                                       ¦

¦ 1.  Thrust Reversing    C ¦ 2  ¦ 0  ¦ (M) May be inoperative provided       ¦ ¦     System                ¦    ¦    ¦ inoperative thrust reverser           ¦ ¦                           ¦    ¦    ¦ system(s) is secured in the forward   ¦ ¦                           ¦    ¦    ¦ thrust position.                      ¦

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¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 3        ¦ PAGE:    ¦

¦     IA-1125, IA-1125 SP, IA-1125 SPX     ¦ DATE: 10/30/2001      ¦ 79-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 79  ENGINE OIL            ¦    ¦    ¦                                       ¦

¦ 1.  Low Oil Pressure      ¦    ¦    ¦ DELETED REVISION 2.                   ¦ ¦     Warning Light         ¦    ¦    ¦                                       ¦