DEPARTMENT OF TRANSPORTATION     Revision: 5a

                                                           Date: 11/30/2009

                         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

 

 

 

 

 

GULFSTREAM

G100, 1125, 1125 SP, 1125 SPX,

 

 

 

 

 

 

 

APPROVED BY:

 

STEPHEN L. FORD, CHAIRMAN

FLIGHT OPERATIONS EVALUATION BOARD

 

 

 

FEDERAL AVIATION ADMINISTRATION

FLIGHT STANDARDS DIVISION

AIRCRAFT EVALUATION GROUP, LGB-AEG

3690 PARAMOUNT BLVD.

LAKEWOOD, CA.  90712-4137

 

 

                         TELEPHONE:  (562) 627-5379

                         FAX:        (562) 627-5281


 

                       FEDERAL AVIATION ADMINISTRATION     Page: I

                                                           Revision: 5a

                        MASTER MINIMUM EQUIPMENT LIST      Date: 11/30/2009

 

 

                    G100, 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

         --     Definitions                             VII, VIII, IX, X

         --     Definitions                             XI, XII, XIII, XIV

         --     Preamble                                XV, XVI

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

         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: II

                                                         Revision: 5a

                        MASTER MINIMUM EQUIPMENT LIST    Date: 11/30/2009

 

 

                      G100, IA-1125, IA-1125 SP, IA-1125 SPX

 

 

                               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: III

                                                         Revision: 5a

                        MASTER MINIMUM EQUIPMENT LIST    Date: 11/30/2009

 

 

                      G100, IA-1125, IA-1125 SP, IA-1125 SPX

 

 

                               Log of Revisions

 

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

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

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

      ¦ 4        ¦ 11/21/2002 ¦ 34-7,34-8,34-9,34-10,34-11     ¦           ¦

      ¦ 5        ¦ 03/10/2004 ¦ HIGHLIGHTS OF REV.,DEFINITIONS ¦           ¦

      ¦ 5        ¦ 03/10/2004 ¦ GUIDELINES                     ¦           ¦

      ¦ 5        ¦ 03/10/2004 ¦ 21-1,21-2,21-3,21-4,22-1       ¦           ¦

      ¦ 5        ¦ 03/10/2004 ¦ 23-1,23-2,23-3,23-4,24-1       ¦           ¦

      ¦ 5        ¦ 03/10/2004 ¦ 25-1,25-2,26-1,27-1,28-1       ¦           ¦

      ¦ 5        ¦ 03/10/2004 ¦ 28-2,29-1,30-1,30-2,31-1       ¦           ¦

      ¦ 5        ¦ 03/10/2004 ¦ 31-2,33-1,33-2,33-3,34-1       ¦           ¦

      ¦ 5        ¦ 03/10/2004 ¦ 34-2,34-3,34-4,34-5,34-6       ¦           ¦

      ¦ 5        ¦ 03/10/2004 ¦ 34-7,34-8,34-9,34-10,34-11     ¦           ¦

      ¦ 5        ¦ 03/10/2004 ¦ 35-1,49-1,78-1                 ¦           |

      ¦ 5a       ¦ 11/30/2009 ¦ HIGHLIGHTS OF CHANGE           ¦           ¦

      ¦ 5a       ¦ 11/30/2009 ¦ GUIDELINES                     ¦           ¦

      ¦ 5a       ¦ 11/30/2009 ¦ 21-1,21-2,21-3,21-4,22-1       ¦           ¦

      ¦ 5a       ¦ 11/30/2009 ¦ 23-1,23-2,23-3,23-4,24-1       ¦           ¦

      ¦ 5a       ¦ 11/30/2009 ¦ 25-1,25-2,26-1,27-1,28-1       ¦           ¦

      ¦ 5a       ¦ 11/30/2009 ¦ 28-2,29-1,30-1,30-2,31-1       ¦           ¦

      ¦ 5a       ¦ 11/30/2009 ¦ 31-2,33-1,33-2,33-3,34-1       ¦           ¦

      ¦ 5a       ¦ 11/30/2009 ¦ 34-2,34-3,34-4,34-5,34-6       ¦           ¦

      ¦ 5a       ¦ 11/30/2009 ¦ 34-7,34-8,34-9,34-10,34-11     ¦           ¦

      ¦ 5a       ¦ 11/30/2009 ¦ 35-1,49-1,78-1                 ¦           |

     

 

 

 

 

 

 

 

 

 

 

 

 

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


 

                       FEDERAL AVIATION ADMINISTRATION     Page: IV

                                                           Revision: 5a

                        MASTER MINIMUM EQUIPMENT LIST      Date: 11/30/2009

 

 

                      G100, IA-1125, IA-1125 SP, IA-1125 SPX

 

 

                                 Control Page

 

 

         SYSTEM                                   PAGE  REV NO.  CURRENT DATE

 

 

         Cover Page                               -       5a       11/30/2009

         Table of Contents                        I       5a       11/30/2009 Log of Revisions                         II      5a       11/30/2009                                                    III     5a       11/30/2009

         Control Page                             IV      5a       11/30/2009

                                                  V       5a       11/30/2009

         Highlights of Change                     VI      5a       11/30/2009

         Definitions                              VII     6        01/31/1995

                                                  VIII    6        01/31/1995

                                                  IX      6        01/31/1995

                                                  X       6        01/31/1995

                                                  XI      6        01/31/1995

                                                  XII     6        01/31/1995

                                                  XIII    6        01/31/1995

                                                  XIV     6        01/31/1995

         Preamble                                 XV      2        06/14/1989

                                                  XVI     2        06/14/1989

         Guidelines for (O) & (M) Procedures      XVII    5a       11/30/2009

                                                  XVIII   5a       11/30/2009

                                                  XIX     5a       11/30/2009

                                                  XX      5a       11/30/2009

         21                                       21-1    5a       11/30/2009

                                                  21-2    5a       11/30/2009

                                                  21-3    5a       11/30/2009

                                                  21-4    5a       11/30/2009

         22                                       22-1    5a       11/30/2009

         23                                       23-1    5a       11/30/2009

                                                  23-2    5a       11/30/2009

                                                  23-3    5a       11/30/2009

                                                  23-4    5a       11/30/2009

         24                                       24-1    5a       11/30/2009

         25                                       25-1    5a       11/30/2009

                                                  25-2    5a       11/30/2009

         26                                       26-1    5a       11/30/2009

         27                                       27-1    5a       11/30/2009

         28                                       28-1    5a       11/30/2009

                                                  28-2    5a       11/30/2009

         29                                       29-1    5a       11/30/2009


 

                       FEDERAL AVIATION ADMINISTRATION     Page: V

                                                           Revision: 5a

                        MASTER MINIMUM EQUIPMENT LIST      Date: 11/30/2009

 

 

                      G100, IA-1125, IA-1125 SP, IA-1125 SPX

 

 

                                 Control Page

 

 

         SYSTEM                                   PAGE  REV NO.  CURRENT DATE

 

 

         30                                       30-1    5a      11/30/2009

                                                  30-2    5a      11/30/2009

         31                                       31-1    5a      11/30/2009

                                                  31-2    5a      11/30/2009

         32                                       32-1    5a      11/30/2009

         33                                       33-1    5a      11/30/2009

                                                  33-2    5a      11/30/2009

                                                  33-3    5a      11/30/2009

         34                                       34-1    5a      11/30/2009

                                                  34-2    5a      11/30/2009

                                                  34-3    5a      11/30/2009

                                                  34-4    5a      11/30/2009

                                                  34-5    5a      11/30/2009

                                                  34-6    5a      11/30/2009

                                                  34-7    5a      11/30/2009

                                                  34-8    5a      11/30/2009

                                                  34-9    5a      11/30/2009

                                                  34-10   5a      11/30/2009

                                                  34-11   5a      11/30/2009

         35                                       35-1    5a      11/30/2009

         49                                       49-1    5a      11/30/2009

         52                                       52-1    5a      11/30/2009

         77                                       77-1    5a      11/30/2009

         78                                       78-1    5a      11/30/2009

         79                                       79-1    5a      11/30/2009


 

                       FEDERAL AVIATION ADMINISTRATION   Page: VI

                                                         Revision: 5a

                        MASTER MINIMUM EQUIPMENT LIST    Date: 11/30/2009

 

 

                      G100, IA-1125, IA-1125 SP, IA-1125 SPX

 

                            Highlights of Change

 

 

 

MMEL Revision 5a is identical to MMEL Revision 5 for the IA-1125, IA-1125 SP, IA-1125 SPX, with the exception that Revision 5a identifies the G100 in the MMEL document on the cover sheet and in each page header.  All pages that reflect the inclusion of the G100 in the header indicate the 5a revision with a revision date of 11/30/2009. Also page numbering has been modified to reflect fewer pages in the Highlights of Change. Otherwise, no other changes have been made to this MMEL.

 


 

                       FEDERAL AVIATION ADMINISTRATION     Page: VII

                                                           Revision: 6

                        MASTER MINIMUM EQUIPMENT LIST      Date: 01/31/1995

 

 

                      G100, IA-1125, IA-1125 SP, IA-1125 SPX

 

                                 Definitions

 

 

       1.   System Definitions.

 

       System numbers are based on the Air Transport Association (ATA)

       Specification Number 100 and items are numbered sequentially.

 

            a.        "Item" (Column 1) means the equipment, system,

                      component, or function listed in the "Item"

                      column.

 

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

                      (quantity) of items normally installed in the

                      aircraft.  This number represents the aircraft

                      configuration considered in developing this MMEL.

                      Should the number be a variable (e.g., passenger

                      cabin items) a number is not required.

 

            c.        "Number Required for Dispatch" (Column 3) is the

                      minimum number (quantity) of items required for

                      operation provided the conditions specified in

                      Column 4 are met.

 

       NOTE:  Where the MMEL shows a variable number required for

       dispatch, the MEL must reflect the actual number required for

       dispatch or an alternate means of configuration control approved

       by the Administrator.

 

            d.        "Remarks or Exceptions" (Column 4) in this column

                      includes a statement either prohibiting or

                      permitting operation with a specific number of

                      items inoperative, provisos (conditions and

                      limitations) for such operation, and appropriate

                      notes.

 

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

                      indicates a change, addition or deletion in the

                      adjacent text for the current revision of that

                      page only.  The change bar is dropped at the next

                      revision of that page.

 

       2.  "Airplane/Rotorcraft Flight Manual" (AFM/RFM) is the document

       required for type certification and approved by the responsible

       FAA Aircraft Certification  Office. The FAA approved AFM/RFM for

       the specific aircraft is listed on the applicable Type


 

                       FEDERAL AVIATION ADMINISTRATION     Page: VIII

                                                           Revision: 6

                        MASTER MINIMUM EQUIPMENT LIST      Date: 01/31/1995

 

 

                      G100, IA-1125, IA-1125 SP, IA-1125 SPX

 

                                 Definitions

 

 

       Certificate Data Sheet.

 

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

       certain provisions (restrictive or permissive) expressed in the

       Federal Aviation Regulations operating rules.  The number of

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

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

       specified by repair category.

 

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

       the crewmembers and maintenance personnel of the equipment

       condition.

 

       NOTE:  To the extent practical, placards should be located

       adjacent to the control or indicator for the item affected;

       however, unless otherwise specified, placard wording and location

       will be determined by the operator.

 

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

       number (quantity) of the item installed.

 

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

       indicates that the item was previously listed but is now required

       to be operative if installed in the  aircraft.

 

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

       airplane which has a type design approval for ER operations and

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

 

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

       portions of the Federal Aviation Act and Federal Aviation

       Regulations.

 

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

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

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

       is initiated for the affected aircraft.

 

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

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

 

       11.  Alphabetical symbol in Column 4 indicates a proviso

       (condition or limitation) that must be complied with for


 

                       FEDERAL AVIATION ADMINISTRATION     Page: IX

                                                           Revision: 6

                        MASTER MINIMUM EQUIPMENT LIST      Date: 01/31/1995

 

 

                      G100, IA-1125, IA-1125 SP, IA-1125 SPX

 

                                 Definitions

 

 

       operation with the  listed item inoperative.

 

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

       the extent that it does not accomplish its intended purpose

       and/or is not consistently functioning normally within its

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

 

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

       crewmember or maintenance consideration.  Notes are used to

       identify applicable material which is intended to assist with

       compliance, but do not relieve the operator of the responsibility

       for compliance with all applicable requirements.  Notes are not a

       part of the provisos.

 

       14.  Inoperative components of an inoperative system:

       Inoperative items which are components of a system which is

       inoperative are usually considered components directly associated

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

       (Warning/caution systems associated with the inoperative system

       must be operative unless relief is specifically authorized per

       the MMEL).

 

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

       maintenance procedure which must be accomplished prior to

       operation with the listed item inoperative.  Normally these

       procedures are accomplished by maintenance personnel;  however,

       other personnel may be qualified and authorized to perform

       certain functions.  Procedures requiring specialized knowledge or

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

       accomplished by maintenance personnel.  The satisfactory

       accomplishment of all maintenance procedures, regardless of

       who performs them, is the responsibility of the operator.

       Appropriate procedures are required to be published as part of

       the operator's manual or MEL.

 

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

       operations procedure which must be accomplished in planning for

       and/or operating with the listed item inoperative.  Normally

       these procedures are accomplished by the flight crew; however,

       other personnel may be qualified and authorized to perform

       certain functions.  The satisfactory accomplishment of all

       procedures, regardless of who performs them, is the

       responsibility of the operator.  Appropriate procedures are


 

                       FEDERAL AVIATION ADMINISTRATION     Page: X

                                                           Revision: 6

                        MASTER MINIMUM EQUIPMENT LIST      Date: 01/31/1995

 

 

                      G100, IA-1125, IA-1125 SP, IA-1125 SPX

 

                                 Definitions

 

 

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

       MEL.

 

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

       unless otherwise authorized by the Administrator.

 

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

       component must be put into an acceptable condition for safe

       flight.  An acceptable method of securing or deactivating will be

       established by the operator.

 

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

       This precludes a pilot from filing an Instrument Flight Rules

       (IFR) flight plan.

 

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

       atmospheric environment is such that would allow a flight to

       proceed under the visual flight rules applicable to the flight.

       This does not preclude operating under Instrument Flight Rules.

 

       20.  "Visible Moisture" means an atmospheric environment

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

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

       snow.

 

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

       passenger convenience, comfort or entertainment such as, but not

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

       equipment, overhead reading lamps, etc.

 

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

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

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

       to the repair times established by the following letter

       designators:

 

            Category A.  Items in this category shall be repaired within

       the time interval specified in the remarks column of the

       operator's approved MEL.

 

            Category B.  Items in this category shall be repaired within

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

       the malfunction was recorded in the aircraft maintenance


 

                       FEDERAL AVIATION ADMINISTRATION     Page: XI

                                                           Revision: 6

                        MASTER MINIMUM EQUIPMENT LIST      Date: 01/31/1995

 

 

                      G100, IA-1125, IA-1125 SP, IA-1125 SPX

 

                                 Definitions

 

 

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

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

       26th and end at midnight the 29th.

 

            Category C.  Items in this category shall be repaired within

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

       the malfunction was recorded in the aircraft maintenance

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

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

       26th and end at midnight February 5th.

 

            Category D.  Items in this category shall be repaired within

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

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

       aircraft maintenance log and/or record.

 

       The letter designators are inserted adjacent to Column 2.

 

       23. Electronic fault alerting system - General                  ¦

 

       New generation aircraft display system fault indications to the ¦

       flight crew by use of computerized display systems.  Each       ¦

       aircraft manufacturer has incorporated individual design        ¦

       philosophies in determining the data that would be              ¦

       represented.  The following are customized definitions (specific¦

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

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

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

       23 for their aircraft, if appropriate.                          ¦

 

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

 

       Boeing airplanes equipped with Engine Indicating and Crew       ¦

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

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

       MAINTENANCE).  Any messages that affects airplane dispatch      ¦

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

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

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

       operating within its approved operating limits or tolerances.   ¦

 

       System conditions that result only in a maintenance level       ¦

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


 

                       FEDERAL AVIATION ADMINISTRATION     Page: XII

                                                           Revision: 6

                        MASTER MINIMUM EQUIPMENT LIST      Date: 01/31/1995

 

 

                      G100, 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)                                           ¦


 

                       FEDERAL AVIATION ADMINISTRATION     Page: XIII

                                                           Revision: 6

                        MASTER MINIMUM EQUIPMENT LIST      Date: 01/31/1995

 

 

                      G100, 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: XIV

                                                           Revision: 6

                        MASTER MINIMUM EQUIPMENT LIST      Date: 01/31/1995

 

 

                      G100, 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

       D."


 

 

 

                       FEDERAL AVIATION ADMINISTRATION   Page: XV

                                                         Revision: 2

                        MASTER MINIMUM EQUIPMENT LIST    Date: 06/14/1989

 

 

                      G100, 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: XVI

                                                         Revision: 2

                        MASTER MINIMUM EQUIPMENT LIST    Date: 06/14/1989

 

 

                      G100, 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.


 

 

                       FEDERAL AVIATION ADMINISTRATION   Page XVII

                                                         Revision: 5a

                        MASTER MINIMUM EQUIPMENT LIST    Date: 11/30/2009

 

 

                     G100, 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 XVIII

                                                         Revision: 5a

                        MASTER MINIMUM EQUIPMENT LIST    Date: 11/30/2009

 

 

                     G100, 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 XIX

                                                         Revision: 5a

                        MASTER MINIMUM EQUIPMENT LIST    Date: 11/30/2009

 

 

G100, 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 XX

                                                         Revision: 5a

                        MASTER MINIMUM EQUIPMENT LIST    Date: 11/30/2009

 

 

G100, 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.


 

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

 

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

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

 

¦ G100, IA-1125, IA-1125 SP, IA-1125 SPX   ¦ DATE: 11/30/2009     ¦ 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                ¦    ¦    ¦                                       ¦

 

 

 

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


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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

 

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

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

 

¦ G100, IA-1125, IA-1125 SP, IA-1125 SPX   ¦ DATE: 11/30/2009      ¦ 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.       | ¦

 

 

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


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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

 

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

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

¦ G100, IA-1125, IA-1125 SP, IA-1125 SPX   ¦ DATE: 11/30/2009       ¦ 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.                    ¦

 

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


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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

 

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

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

 

¦ G100, IA-1125, IA-1125 SP, IA-1125 SPX   ¦ DATE: 11/30/2009      ¦ 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)       ¦    ¦    ¦                                     | ¦

 

 

 

 

 

 

 

 

 

 

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


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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

 

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

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

 

¦ G100, IA-1125, IA-1125 SP, IA-1125 SPX   ¦ DATE: 11/30/2009      ¦ 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.       ¦

 

 

 

 

 

 

 

 

 

 

 

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


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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

 

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

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

 

¦ G100, IA-1125, IA-1125 SP, IA-1125 SPX   ¦ DATE: 11/30/2009      ¦ 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.            ¦    ¦    ¦                                     | ¦

 

 

 

 

 

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


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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

 

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

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

 

¦ G100, IA-1125, IA-1125 SP, IA-1125 SPX   ¦ DATE: 11/30/2009      ¦ 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.) ¦    ¦    ¦                                       ¦

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


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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

 

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

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

 

¦ G100, IA-1125, IA-1125 SP, IA-1125 SPX   ¦ DATE: 11/30/2009      ¦ 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.  | ¦

 

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


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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

 

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

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

 

¦ G100, IA-1125, IA-1125 SP, IA-1125 SPX   ¦ DATE: 11/30/2009      ¦ 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.               | ¦

 

 

 

 

 

 

 

 

 

 

 

 

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


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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

 

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

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

 

¦ G100, IA-1125, IA-1125 SP, IA-1125 SPX   ¦ DATE: 11/30/2009      ¦ 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     ¦    ¦    ¦                                     | ¦

 

 

 

 

 

 

 

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


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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

 

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

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

 

¦ G100, IA-1125, IA-1125 SP, IA-1125 SPX   ¦ DATE: 11/30/2009      ¦ 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  ¦ Deleted                               ¦

¦     Item(s)               ¦    ¦    ¦

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


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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

 

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

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

 

¦ G100, IA-1125, IA-1125 SP, IA-1125 SPX   ¦ DATE: 11/30/2009      ¦ 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.  | ¦

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


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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

 

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

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

 

¦ G100, IA-1125, IA-1125 SP, IA-1125 SPX   ¦ DATE: 11/30/2009      ¦ 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.                    ¦

 

 

 

 

 

 

 

 

 

 

 

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


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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

 

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

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

 

¦ G100, IA-1125, IA-1125 SP, IA-1125 SPX   ¦ DATE: 11/30/2009      ¦ 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.                          ¦

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


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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

 

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

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

 

¦ G100, IA-1125, IA-1125 SP, IA-1125 SPX   ¦ DATE: 11/30/2009      ¦ 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                ¦    ¦    ¦                                     | ¦

 

 

 

 

 

 

 

 

 

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


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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

 

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

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

 

¦ G100, IA-1125, IA-1125 SP, IA-1125 SPX   ¦ DATE: 11/30/2009      ¦ 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.                     ¦

 

 

 

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


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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

 

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

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

 

¦ G100, IA-1125, IA-1125 SP, IA-1125 SPX   ¦ DATE: 11/30/2009      ¦ 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.                      ¦

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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


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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

 

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

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

 

¦ G100, IA-1125, IA-1125 SP, IA-1125 SPX   ¦ DATE: 11/30/2009      ¦ 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.                    ¦

 

 

 

 

 

 

 

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


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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

 

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

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

 

¦ G100, IA-1125, IA-1125 SP, IA-1125 SPX   ¦ DATE: 11/30/2009      ¦ 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.                           ¦

 

 

 

 

 

 

 

 

 

 

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


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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

 

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

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

 

¦ G100, IA-1125, IA-1125 SP, IA-1125 SPX   ¦ DATE: 11/30/2009      ¦ 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.     ¦

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


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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

 

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

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

 

¦ G100, IA-1125, IA-1125 SP, IA-1125 SPX   ¦ DATE: 11/30/2009      ¦ 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              ¦    ¦    ¦                                       ¦

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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


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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

 

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

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

 

¦ G100, IA-1125, IA-1125 SP, IA-1125 SPX   ¦ DATE: 11/30/2009      ¦ 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.                 ¦

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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


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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

 

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

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

 

¦ G100, IA-1125, IA-1125 SP, IA-1125 SPX   ¦ DATE: 11/30/2009      ¦ 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  ¦                                       ¦

 

 

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


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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

 

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

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

 

¦ G100, IA-1125, IA-1125 SP, IA-1125 SPX   ¦ DATE: 11/30/2009      ¦ 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.                ¦

 

 

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


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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

 

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

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

 

¦ G100, IA-1125, IA-1125 SP, IA-1125 SPX   ¦ DATE: 11/30/2009      ¦ 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  ¦                                       ¦

¦ ***                       ¦    ¦    ¦                                       ¦

 

 

 

 

 

 

 

 

 

 

 

 

 

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


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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

 

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

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

 

¦ G100, IA-1125, IA-1125 SP, IA-1125 SPX   ¦ DATE: 11/30/2009      ¦ 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     ¦    ¦    ¦                                       ¦

 

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


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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

 

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

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

 

¦ G100, IA-1125, IA-1125 SP, IA-1125 SPX   ¦ DATE: 11/30/2009      ¦ 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).                             | ¦

 

 

 

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


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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

 

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

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

 

¦ G100, IA-1125, IA-1125 SP, IA-1125 SPX   ¦ DATE: 11/30/2009      ¦ 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    ¦    ¦    ¦                                       ¦

 

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


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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

 

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

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

 

¦ G100, IA-1125, IA-1125 SP, IA-1125 SPX   ¦ DATE: 11/30/2009      ¦ 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.) ¦    ¦    ¦                                       ¦

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


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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

 

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

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

 

¦ G100, IA-1125, IA-1125 SP, IA-1125 SPX   ¦ DATE: 11/30/2009      ¦ 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.                             ¦

 

 

 

 

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


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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

 

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

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

 

¦ G100, IA-1125, IA-1125 SP, IA-1125 SPX   ¦ DATE: 11/30/2009      ¦ 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.                       ¦

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


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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

 

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

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

 

¦ G100, IA-1125, IA-1125 SP, IA-1125 SPX   ¦ DATE: 11/30/2009      ¦ 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.) ¦    ¦    ¦                                       ¦

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


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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

 

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

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

 

¦ G100, IA-1125, IA-1125 SP, IA-1125 SPX   ¦ DATE: 11/30/2009      ¦ 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.                    ¦

 

 

 

 

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


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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

 

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

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

 

¦ G100, IA-1125, IA-1125 SP, IA-1125 SPX   ¦ DATE: 11/30/2009      ¦ 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.                    ¦

 

 

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


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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

 

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

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

 

¦ G100, IA-1125, IA-1125 SP, IA-1125 SPX   ¦ DATE: 11/30/2009      ¦ 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.) ¦    ¦    ¦                                       ¦

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


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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

 

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

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

 

¦ G100, IA-1125, IA-1125 SP, IA-1125 SPX   ¦ DATE: 11/30/2009      ¦ 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.                    ¦

 

 

 

 

 

 

 

 

 

 

 

 

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


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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

 

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

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

 

¦ G100, IA-1125, IA-1125 SP, IA-1125 SPX   ¦ DATE: 11/30/2009      ¦ 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.             | ¦

 

 

 

 

 

 

 

 

 

 

 

 

 

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


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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

 

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

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

 

¦ G100, IA-1125, IA-1125 SP, IA-1125 SPX   ¦ DATE: 11/30/2009      ¦ 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.             | ¦

 

 

 

 

 

 

 

 

 

 

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


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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

 

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

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

 

¦ G100, IA-1125, IA-1125 SP, IA-1125 SPX   ¦ DATE: 11/30/2009      ¦ 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.                               ¦

 

 

 

 

 

 

 

 

 

 

 

 

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


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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

 

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

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

 

¦ G100, IA-1125, IA-1125 SP, IA-1125 SPX   ¦ DATE: 11/30/2009      ¦ 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.                    ¦

 

 

 

 

 

 

 

 

 

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


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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

 

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

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

 

¦ G100, IA-1125, IA-1125 SP, IA-1125 SPX   ¦ DATE: 11/30/2009      ¦ 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.                      ¦

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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


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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

 

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦

¦ FEDERAL AVIATION ADMINISTRATION                                             ¦

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

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

 

¦ G100, IA-1125, IA-1125 SP, IA-1125 SPX   ¦ DATE: 11/30/2009      ¦ 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         ¦    ¦    ¦                                       ¦

 

 

 

 

 

 

 

 

 

 

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