DEPARTMENT OF TRANSPORTATION     Revision: 24

                                                           Date: 08/24/2000

                         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

 

 

 

 

 

                      LOCKHEED L-1011-385-1, -3, -14, -15

 

 

 

 

 

 

 

 

 

 

 

 

 

                         FEDERAL AVIATION ADMINISTRATION

                         FLIGHT STANDARDS DIVISION

                         AIRCRAFT EVALUATION GROUP, LGB AEG

                         3960 PARAMOUNT BOULEVARD, SUITE 100

                         LAKEWOOD, CA 90712-4137

 

                         TELEPHONE:  (562) 627-5272

                               FAX:  (562) 627-5281


 

 

                       FEDERAL AVIATION ADMINISTRATION     Page: I

                                                           Revision: 24

                        MASTER MINIMUM EQUIPMENT LIST      Date: 08/24/2000

 

                              Lockheed L-1011

 

 

 

                              Table of Contents

 

 

    SYSTEM NO.  SYSTEM                                  PAGE

 

 

         --     Table of Contents                       I, II

         --     Log of Revisions                        III, IV, V

         --     Control Page                            VI, VII, VIII, IX

         --     Control Page                            X, XI

         --     Highlights of Change                    XII, XIII

         --     Definitions                             XIV, XV, XVI, XVII

         --     Definitions                             XVIII, XIX, XX, XXI

         --     Preamble                                XXII, XXIII

         21     Air Conditioning                        21-1, 2, 3, 4, 5

         21     Air Conditioning                        21-6  THRU 10

         21     Air Conditioning                        21-11  THRU 15

         21     Air Conditioning                        21-16  THRU 20

         21     Air Conditioning                        21-21  THRU 24

         22     Auto Flight                             22-1, 2, 3, 4, 5

         22     Auto Flight                             22-6  THRU 10

         22     Auto Flight                             22-11  THRU 15

         22     Auto Flight                             22-16  THRU 20

         22     Auto Flight                             22-21  THRU 24

         23     Communications                          23-1, 2, 3, 4, 5

         24     Electrical Power                        24-1, 2, 3, 4, 5

         24     Electrical Power                        24-6, 7, 8

         25     Equipment/Furnishings                   25-1, 2, 3, 4, 5

         25     Equipment/Furnishings                   25-6  THRU 10

         25     Equipment/Furnishings                   25-11  THRU 15

         25     Equipment/Furnishings                   25-16  THRU 18

         26     Fire Protection                         26-1, 2, 3, 4, 5

         26     Fire Protection                         26-6  THRU 10

         26     Fire Protection                         26-11

         27     Flight Controls                         27-1, 2, 3, 4, 5

         28     Fuel                                    28-1, 2, 3, 4, 5

         28     Fuel                                    28-6  THRU 10

         28     Fuel                                    28-11  THRU 13

         29     Hydraulic Power                         29-1, 2, 3, 4, 5

         30     Ice and Rain Protection                 30-1, 2, 3, 4, 5

         30     Ice and Rain Protection                 30-6


 

                       FEDERAL AVIATION ADMINISTRATION     Page: II

                                                           Revision: 24

                        MASTER MINIMUM EQUIPMENT LIST      Date: 08/24/2000

 

                              Lockheed L-1011

 

 

 

                              Table of Contents

 

 

    SYSTEM NO.  SYSTEM                                  PAGE

 

 

         31     Indicating/Recording Systems            31-1, 2

         32     Landing Gear                            32-1, 2, 3, 4, 5

         32     Landing Gear                            32-6

         33     Lights                                  33-1, 2, 3, 4, 5

         33     Lights                                  33-6  THRU 10

         33     Lights                                  33-11

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

         34     Navigation                              34-6  THRU 10

         35     Oxygen                                  35-1, 2, 3

         36     Pneumatic                               36-1, 2, 3, 4, 5

         36     Pneumatic                               36-6, 7

         38     Water/Waste                             38-1

         49     Airborne Auxiliary Power                49-1, 2

         52     Doors                                   52-1, 2, 3, 4, 5

         52     Doors                                   52-6, 7

         56     Windows                                 56-1

         73     Engine Fuel & Control                   73-1, 2

         74     Ignition                                74-1

         75     Bleed Air                               75-1

         77     Engine Indicating                       77-1, 2, 3, 4

         78     Engine Exhaust                          78-1

         79     Engine Oil                              79-1, 2

         80     Starting                                80-1


 

 

                       FEDERAL AVIATION ADMINISTRATION   Page: III

                                                         Revision: 24

                        MASTER MINIMUM EQUIPMENT LIST    Date: 08/24/2000

 

                              Lockheed L-1011

 

 

 

                               Log of Revisions

 

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

      | REV.NO.  |  DATE      | PAGE NUMBERS                   | INITIALS  |

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

      | 20       | 08/16/1990 | ALL PAGES                      |           |

      | 20a      | 06/12/1991 | HIGHLIGHTS OF REV.             |           |

      | 20a      | 06/12/1991 | 33-8,33-9,34-6                 |           |

      | 20b      | 09/19/1991 | HIGHLIGHTS OF REV.             |           |

      | 20b      | 09/19/1991 | 28-10,28-11,28-12              |           |

      | 20c      | 10/23/1991 | HIGHLIGHTS OF REV.             |           |

      | 20c      | 10/23/1991 | 23-3                           |           |

      | 20d      | 05/06/1993 | HIGHLIGHTS OF REV.             |           |

      | 20d      | 05/06/1993 | 28-4                           |           |

      | 21       | 03/30/1995 | HIGHLIGHTS OF REV.,DEFINITIONS |           |

      | 21       | 03/30/1995 | 21-1,21-2,21-3,21-4,21-5       |           |

      | 21       | 03/30/1995 | 21-6,21-7,21-8,21-9,21-10      |           |

      | 21       | 03/30/1995 | 21-11,21-12,21-13,21-14,21-15  |           |

      | 21       | 03/30/1995 | 21-16,21-17,21-18,21-19,21-20  |           |

      | 21       | 03/30/1995 | 21-21,22-1,22-2,22-3,22-4      |           |

      | 21       | 03/30/1995 | 22-5,22-6,22-7,22-8,22-9       |           |

      | 21       | 03/30/1995 | 22-10,22-11,22-12,22-13,22-14  |           |

      | 21       | 03/30/1995 | 22-15,22-16,22-17,22-18,22-19  |           |

      | 21       | 03/30/1995 | 22-20,22-21,22-22,23-1,23-2    |           |

      | 21       | 03/30/1995 | 23-3,23-4,24-1,24-2,24-3       |           |

      | 21       | 03/30/1995 | 24-4,24-5,24-6,24-7,25-1       |           |

      | 21       | 03/30/1995 | 25-2,25-3,25-4,25-5,25-6       |           |

      | 21       | 03/30/1995 | 25-7,25-8,25-9,25-10,25-11     |           |

      | 21       | 03/30/1995 | 25-12,25-13,25-14,25-15,25-16  |           |

      | 21       | 03/30/1995 | 26-1,26-2,26-3,26-4,26-5       |           |

      | 21       | 03/30/1995 | 26-6,26-7,26-8,26-9,26-10      |           |

      | 21       | 03/30/1995 | 26-11,27-1,27-2,27-3,27-4      |           |

      | 21       | 03/30/1995 | 27-5,28-1,28-2,28-3,28-4       |           |

      | 21       | 03/30/1995 | 28-5,28-6,28-7,28-8,28-9       |           |

      | 21       | 03/30/1995 | 28-10,28-11,28-12,28-13,29-1   |           |

      | 21       | 03/30/1995 | 29-2,29-3,29-4,29-5,30-1       |           |

      | 21       | 03/30/1995 | 30-2,30-3,30-4,30-5,31-1       |           |

      | 21       | 03/30/1995 | 31-2,32-1,32-2,32-3,32-4       |           |

      | 21       | 03/30/1995 | 32-5,32-6,33-1,33-2,33-3       |           |

      | 21       | 03/30/1995 | 33-4,33-5,33-6,33-7,33-8       |           |

      | 21       | 03/30/1995 | 33-9,33-10,34-1,34-2,34-3      |           |

      | 21       | 03/30/1995 | 34-4,34-5,34-6,34-7,35-1       |           |

      | 21       | 03/30/1995 | 36-1,36-2,36-3,36-4,36-5       |           |

      | 21       | 03/30/1995 | 36-6,36-7,49-1,49-2,52-1       |           |

      | 21       | 03/30/1995 | 52-2,52-3,52-4,52-5,56-1       |           |

      | 21       | 03/30/1995 | 73-1,73-2,74-1,75-1,77-1       |           |

      | 21       | 03/30/1995 | 77-2,77-3,77-4,78-1,79-1       |           |

      | 21       | 03/30/1995 | 79-2,80-1                      |           |

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


 

 

                       FEDERAL AVIATION ADMINISTRATION   Page: IV

                                                         Revision: 24

                        MASTER MINIMUM EQUIPMENT LIST    Date: 08/24/2000

 

                              Lockheed L-1011

 

 

 

                               Log of Revisions

 

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

      | REV.NO.  |  DATE      | PAGE NUMBERS                   | INITIALS  |

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

      | 22       | 06/27/1995 | HIGHLIGHTS OF REV.,DEFINITIONS |           |

      | 22       | 06/27/1995 | 26-2                           |           |

      | 22a      | 10/30/1996 | HIGHLIGHTS OF REV.,DEFINITIONS |           |

      | 22a      | 10/30/1996 | 25-2,25-8,25-9,25-10,25-11     |           |

      | 22a      | 10/30/1996 | 25-12,25-13,25-14,25-15,25-16  |           |

      | 22a      | 10/30/1996 | 25-17,26-2,26-3,26-4,26-8      |           |

      | 22a      | 10/30/1996 | 33-4,33-6,33-7,33-8,33-9       |           |

      | 22a      | 10/30/1996 | 33-10,52-4,52-5,52-6,52-7      |           |

      | 23       | 06/24/1998 | HIGHLIGHTS OF REV.,DEFINITIONS |           |

      | 23       | 06/24/1998 | 21-3,21-11,21-13,21-14,21-15   |           |

      | 23       | 06/24/1998 | 21-16,21-17,21-18,21-19,21-20  |           |

      | 23       | 06/24/1998 | 21-21,21-22,21-23,21-24,22-2   |           |

      | 23       | 06/24/1998 | 22-3,22-4,22-5,22-6,22-7       |           |

      | 23       | 06/24/1998 | 22-8,22-9,22-10,22-11,22-12    |           |

      | 23       | 06/24/1998 | 22-13,22-14,22-15,22-16,22-17  |           |

      | 23       | 06/24/1998 | 22-18,22-19,22-20,22-21,22-22  |           |

      | 23       | 06/24/1998 | 22-23,23-1,23-2,23-3,23-4      |           |

      | 23       | 06/24/1998 | 24-2,24-3,24-6,24-7,25-2       |           |

      | 23       | 06/24/1998 | 25-6,25-8,25-14,25-15,25-16    |           |

      | 23       | 06/24/1998 | 25-17,25-18,26-2,26-3,26-4     |           |

      | 23       | 06/24/1998 | 26-5,26-7,26-8,26-9,28-1       |           |

      | 23       | 06/24/1998 | 28-7,29-2,29-4,30-1,30-2       |           |

      | 23       | 06/24/1998 | 30-3,30-5,31-1,31-2,32-2       |           |

      | 23       | 06/24/1998 | 32-5,33-5,33-6,33-7,33-8       |           |

      | 23       | 06/24/1998 | 33-9,33-10,33-11,34-1,34-2     |           |

      | 23       | 06/24/1998 | 34-3,34-4,34-5,34-6,34-7       |           |

      | 23       | 06/24/1998 | 34-8,34-9,35-1,35-2,36-1       |           |

      | 23       | 06/24/1998 | 36-2,36-3,36-6,38-1,52-1       |           |

      | 23       | 06/24/1998 | 52-3,52-4,52-6,52-7,77-3       |           |

      | 23       | 06/24/1998 | 79-2                           |           |

      | 24       | 08/24/2000 | HIGHLIGHTS OF REV.,DEFINITIONS |           |

      | 24       | 08/24/2000 | 21-1,21-2,21-3,21-4,21-9       |           |

      | 24       | 08/24/2000 | 21-10,21-11,21-14,21-15,21-16  |           |

      | 24       | 08/24/2000 | 21-17,21-18,21-19,21-20,21-22  |           |

      | 24       | 08/24/2000 | 21-23,22-3,22-4,22-5,22-6      |           |

      | 24       | 08/24/2000 | 22-7,22-8,22-9,22-10,22-11     |           |

      | 24       | 08/24/2000 | 22-12,22-13,22-14,22-15,22-16  |           |

      | 24       | 08/24/2000 | 22-17,22-18,22-19,22-20,22-21  |           |

      | 24       | 08/24/2000 | 22-22,22-23,22-24,23-1,23-2    |           |

      | 24       | 08/24/2000 | 23-3,23-4,23-5,24-6,24-7       |           |

      | 24       | 08/24/2000 | 24-8,25-1,25-2,25-3,25-4       |           |

      | 24       | 08/24/2000 | 25-5,25-6,25-7,25-8,25-15      |           |

      | 24       | 08/24/2000 | 25-16,25-17,25-18,26-3,26-4    |           |

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


 

 

                       FEDERAL AVIATION ADMINISTRATION   Page: V

                                                         Revision: 24

                        MASTER MINIMUM EQUIPMENT LIST    Date: 08/24/2000

 

                              Lockheed L-1011

 

 

 

                               Log of Revisions

 

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

      | REV.NO.  |  DATE      | PAGE NUMBERS                   | INITIALS  |

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

      | 24       | 08/24/2000 | 26-5,26-7,26-8,26-9,27-1       |           |

      | 24       | 08/24/2000 | 27-3,27-5,28-1,28-2,28-4       |           |

      | 24       | 08/24/2000 | 28-5,28-7,28-11,28-12,29-2     |           |

      | 24       | 08/24/2000 | 29-5,30-2,30-3,30-5,30-6       |           |

      | 24       | 08/24/2000 | 31-1,31-2,32-2,32-3,32-4       |           |

      | 24       | 08/24/2000 | 32-5,33-3,33-5,33-6,33-8       |           |

      | 24       | 08/24/2000 | 33-9,33-10,34-2,34-3,34-4      |           |

      | 24       | 08/24/2000 | 34-5,34-6,34-7,34-8,34-9       |           |

      | 24       | 08/24/2000 | 34-10,35-1,35-2,35-3,36-1      |           |

      | 24       | 08/24/2000 | 36-2,36-3,36-5,36-6,49-2       |           |

      | 24       | 08/24/2000 | 52-1,52-2,52-3,52-4,52-7       |           |

      | 24       | 08/24/2000 | 77-1,77-3                      |           |

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                       FEDERAL AVIATION ADMINISTRATION     Page: VI

                                                           Revision: 24

                        MASTER MINIMUM EQUIPMENT LIST      Date: 08/24/2000

 

                              Lockheed L-1011

 

 

 

                                 Control Page

 

 

         SYSTEM                                   PAGE  REV NO.  CURRENT DATE

 

 

         Cover Page                               -       24       08/24/2000

         Table of Contents                        I       24       08/24/2000

                                                  II      24       08/24/2000

         Log of Revisions                         III     24       08/24/2000

                                                  IV      24       08/24/2000

                                                  V       24       08/24/2000

         Control Page                             VI      24       08/24/2000

                                                  VII     24       08/24/2000

                                                  VIII    24       08/24/2000

                                                  IX      24       08/24/2000

                                                  X       24       08/24/2000

                                                  XI      24       08/24/2000

         Highlights of Change                     XII     24       08/24/2000

                                                  XIII    24       08/24/2000

         Definitions                              XIV     6        01/31/1995

                                                  XV      6        01/31/1995

                                                  XVI     6        01/31/1995

                                                  XVII    6        01/31/1995

                                                  XVIII   6        01/31/1995

                                                  XIX     6        01/31/1995

                                                  XX      6        01/31/1995

                                                  XXI     6        01/31/1995

         Preamble                                 XXII    2        06/14/1989

                                                  XXIII   2        06/14/1989

         21                                       21-1    24       08/24/2000

                                                  21-2    24       08/24/2000

                                                  21-3    24       08/24/2000

                                                  21-4    24       08/24/2000

                                                  21-5    21       03/30/1995

                                                  21-6    21       03/30/1995

                                                  21-7    21       03/30/1995

                                                  21-8    21       03/30/1995

                                                  21-9    24       08/24/2000

                                                  21-10   24       08/24/2000

                                                  21-11   24       08/24/2000

                                                  21-12   21       03/30/1995

                                                  21-13   23       06/24/1998

                                                  21-14   24       08/24/2000

                                                  21-15   24       08/24/2000

                                                  21-16   24       08/24/2000


 

                       FEDERAL AVIATION ADMINISTRATION     Page: VII

                                                           Revision: 24

                        MASTER MINIMUM EQUIPMENT LIST      Date: 08/24/2000

 

                              Lockheed L-1011

 

 

 

                                 Control Page

 

 

         SYSTEM                                   PAGE  REV NO.  CURRENT DATE

 

 

                                                  21-17   24       08/24/2000

                                                  21-18   24       08/24/2000

                                                  21-19   24       08/24/2000

                                                  21-20   24       08/24/2000

                                                  21-21   23       06/24/1998

                                                  21-22   24       08/24/2000

                                                  21-23   24       08/24/2000

                                                  21-24   23       06/24/1998

         22                                       22-1    21       03/30/1995

                                                  22-2    23       06/24/1998

                                                  22-3    24       08/24/2000

                                                  22-4    24       08/24/2000

                                                  22-5    24       08/24/2000

                                                  22-6    24       08/24/2000

                                                  22-7    24       08/24/2000

                                                  22-8    24       08/24/2000

                                                  22-9    24       08/24/2000

                                                  22-10   24       08/24/2000

                                                  22-11   24       08/24/2000

                                                  22-12   24       08/24/2000

                                                  22-13   24       08/24/2000

                                                  22-14   24       08/24/2000

                                                  22-15   24       08/24/2000

                                                  22-16   24       08/24/2000

                                                  22-17   24       08/24/2000

                                                  22-18   24       08/24/2000

                                                  22-19   24       08/24/2000

                                                  22-20   24       08/24/2000

                                                  22-21   24       08/24/2000

                                                  22-22   24       08/24/2000

                                                  22-23   24       08/24/2000

                                                  22-24   24       08/24/2000

         23                                       23-1    24       08/24/2000

                                                  23-2    24       08/24/2000

                                                  23-3    24       08/24/2000

                                                  23-4    24       08/24/2000

                                                  23-5    24       08/24/2000

         24                                       24-1    21       03/30/1995

                                                  24-2    23       06/24/1998

                                                  24-3    23       06/24/1998


 

                       FEDERAL AVIATION ADMINISTRATION     Page: VIII

                                                           Revision: 24

                        MASTER MINIMUM EQUIPMENT LIST      Date: 08/24/2000

 

                              Lockheed L-1011

 

 

 

                                 Control Page

 

 

         SYSTEM                                   PAGE  REV NO.  CURRENT DATE

 

 

                                                  24-4    21       03/30/1995

                                                  24-5    21       03/30/1995

                                                  24-6    24       08/24/2000

                                                  24-7    24       08/24/2000

                                                  24-8    24       08/24/2000

         25                                       25-1    24       08/24/2000

                                                  25-2    24       08/24/2000

                                                  25-3    24       08/24/2000

                                                  25-4    24       08/24/2000

                                                  25-5    24       08/24/2000

                                                  25-6    24       08/24/2000

                                                  25-7    24       08/24/2000

                                                  25-8    24       08/24/2000

                                                  25-9    22 a     10/30/1996

                                                  25-10   22 a     10/30/1996

                                                  25-11   22 a     10/30/1996

                                                  25-12   22 a     10/30/1996

                                                  25-13   22 a     10/30/1996

                                                  25-14   23       06/24/1998

                                                  25-15   24       08/24/2000

                                                  25-16   24       08/24/2000

                                                  25-17   24       08/24/2000

                                                  25-18   24       08/24/2000

         26                                       26-1    21       03/30/1995

                                                  26-2    23       06/24/1998

                                                  26-3    24       08/24/2000

                                                  26-4    24       08/24/2000

                                                  26-5    24       08/24/2000

                                                  26-6    21       03/30/1995

                                                  26-7    24       08/24/2000

                                                  26-8    24       08/24/2000

                                                  26-9    24       08/24/2000

                                                  26-10   21       03/30/1995

                                                  26-11   21       03/30/1995

         27                                       27-1    24       08/24/2000

                                                  27-2    21       03/30/1995

                                                  27-3    24       08/24/2000

                                                  27-4    21       03/30/1995

                                                  27-5    24       08/24/2000

         28                                       28-1    24       08/24/2000


 

                       FEDERAL AVIATION ADMINISTRATION     Page: IX

                                                           Revision: 24

                        MASTER MINIMUM EQUIPMENT LIST      Date: 08/24/2000

 

                              Lockheed L-1011

 

 

 

                                 Control Page

 

 

         SYSTEM                                   PAGE  REV NO.  CURRENT DATE

 

 

                                                  28-2    24       08/24/2000

                                                  28-3    21       03/30/1995

                                                  28-4    24       08/24/2000

                                                  28-5    24       08/24/2000

                                                  28-6    21       03/30/1995

                                                  28-7    24       08/24/2000

                                                  28-8    21       03/30/1995

                                                  28-9    21       03/30/1995

                                                  28-10   21       03/30/1995

                                                  28-11   24       08/24/2000

                                                  28-12   24       08/24/2000

                                                  28-13   21       03/30/1995

         29                                       29-1    21       03/30/1995

                                                  29-2    24       08/24/2000

                                                  29-3    21       03/30/1995

                                                  29-4    23       06/24/1998

                                                  29-5    24       08/24/2000

         30                                       30-1    23       06/24/1998

                                                  30-2    24       08/24/2000

                                                  30-3    24       08/24/2000

                                                  30-4    21       03/30/1995

                                                  30-5    24       08/24/2000

                                                  30-6    24       08/24/2000

         31                                       31-1    24       08/24/2000

                                                  31-2    24       08/24/2000

         32                                       32-1    21       03/30/1995

                                                  32-2    24       08/24/2000

                                                  32-3    24       08/24/2000

                                                  32-4    24       08/24/2000

                                                  32-5    24       08/24/2000

                                                  32-6    21       03/30/1995

         33                                       33-1    21       03/30/1995

                                                  33-2    21       03/30/1995

                                                  33-3    24       08/24/2000

                                                  33-4    22 a     10/30/1996

                                                  33-5    24       08/24/2000

                                                  33-6    24       08/24/2000

                                                  33-7    23       06/24/1998

                                                  33-8    24       08/24/2000

                                                  33-9    24       08/24/2000


 

                       FEDERAL AVIATION ADMINISTRATION     Page: X

                                                           Revision: 24

                        MASTER MINIMUM EQUIPMENT LIST      Date: 08/24/2000

 

                              Lockheed L-1011

 

 

 

                                 Control Page

 

 

         SYSTEM                                   PAGE  REV NO.  CURRENT DATE

 

 

                                                  33-10   24       08/24/2000

                                                  33-11   23       06/24/1998

         34                                       34-1    23       06/24/1998

                                                  34-2    24       08/24/2000

                                                  34-3    24       08/24/2000

                                                  34-4    24       08/24/2000

                                                  34-5    24       08/24/2000

                                                  34-6    24       08/24/2000

                                                  34-7    24       08/24/2000

                                                  34-8    24       08/24/2000

                                                  34-9    24       08/24/2000

                                                  34-10   24       08/24/2000

         35                                       35-1    24       08/24/2000

                                                  35-2    24       08/24/2000

                                                  35-3    24       08/24/2000

         36                                       36-1    24       08/24/2000

                                                  36-2    24       08/24/2000

                                                  36-3    24       08/24/2000

                                                  36-4    21       03/30/1995

                                                  36-5    24       08/24/2000

                                                  36-6    24       08/24/2000

                                                  36-7    21       03/30/1995

         38                                       38-1    23       06/24/1998

         49                                       49-1    21       03/30/1995

                                                  49-2    24       08/24/2000

         52                                       52-1    24       08/24/2000

                                                  52-2    24       08/24/2000

                                                  52-3    24       08/24/2000

                                                  52-4    24       08/24/2000

                                                  52-5    22 a     10/30/1996

                                                  52-6    23       06/24/1998

                                                  52-7    24       08/24/2000

         56                                       56-1    21       03/30/1995

         73                                       73-1    21       03/30/1995

                                                  73-2    21       03/30/1995

         74                                       74-1    21       03/30/1995

         75                                       75-1    21       03/30/1995

         77                                       77-1    24       08/24/2000

                                                  77-2    21       03/30/1995

                                                  77-3    24       08/24/2000


 

                       FEDERAL AVIATION ADMINISTRATION     Page: XI

                                                           Revision: 24

                        MASTER MINIMUM EQUIPMENT LIST      Date: 08/24/2000

 

                              Lockheed L-1011

 

 

 

                                 Control Page

 

 

         SYSTEM                                   PAGE  REV NO.  CURRENT DATE

 

 

                                                  77-4    21       03/30/1995

         78                                       78-1    21       03/30/1995

         79                                       79-1    21       03/30/1995

                                                  79-2    23       06/24/1998

         80                                       80-1    21       03/30/1995


 

 

                       FEDERAL AVIATION ADMINISTRATION   Page: XII

                                                         Revision: 24

                        MASTER MINIMUM EQUIPMENT LIST    Date: 08/24/2000

 

                              Lockheed L-1011

 

 

                            Highlights of Change

 

 

 

       EFFECTIVE ABOVE DATE, the Lockheed L-1011 Master Minimum Equipment List

       (MMEL) is revised.  This STANDARD revision is the result of a public

       Flight Operations Evaluation Board (FOEB) meeting held in Long Beach, CA

       on 9/23/99 to consider approximately 30 requests for change.

 

       The FAA's latest Flight Operations Policy Board (FOPB) policy, reflected

       in FAA Policy Letters 1-103, have also been incorporated in this

       revision.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 


 

 

                       FEDERAL AVIATION ADMINISTRATION   Page: XIII

                                                         Revision: 24

                        MASTER MINIMUM EQUIPMENT LIST    Date: 08/24/2000

 

                              Lockheed L-1011

 

 

                            Highlights of Change

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 


 

 

                       FEDERAL AVIATION ADMINISTRATION     Page: XIV

                                                           Revision: 6

                        MASTER MINIMUM EQUIPMENT LIST      Date: 01/31/1995

 

                              Lockheed L-1011

 

 

                                 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: XV

                                                           Revision: 6

                        MASTER MINIMUM EQUIPMENT LIST      Date: 01/31/1995

 

                              Lockheed L-1011

 

 

                                 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: XVI

                                                           Revision: 6

                        MASTER MINIMUM EQUIPMENT LIST      Date: 01/31/1995

 

                              Lockheed L-1011

 

 

                                 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: XVII

                                                           Revision: 6

                        MASTER MINIMUM EQUIPMENT LIST      Date: 01/31/1995

 

                              Lockheed L-1011

 

 

                                 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: XVIII

                                                           Revision: 6

                        MASTER MINIMUM EQUIPMENT LIST      Date: 01/31/1995

 

                              Lockheed L-1011

 

 

                                 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: XIX

                                                           Revision: 6

                        MASTER MINIMUM EQUIPMENT LIST      Date: 01/31/1995

 

                              Lockheed L-1011

 

 

                                 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: XX

                                                           Revision: 6

                        MASTER MINIMUM EQUIPMENT LIST      Date: 01/31/1995

 

                              Lockheed L-1011

 

 

                                 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: XXI

                                                           Revision: 6

                        MASTER MINIMUM EQUIPMENT LIST      Date: 01/31/1995

 

                              Lockheed L-1011

 

 

                                 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: XXII

                                                         Revision: 2

                        MASTER MINIMUM EQUIPMENT LIST    Date: 06/14/1989

 

                              Lockheed L-1011

 

 

                                  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: XXIII

                                                         Revision: 2

                        MASTER MINIMUM EQUIPMENT LIST    Date: 06/14/1989

 

                              Lockheed L-1011

 

 

                                  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.

 

 

 


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

| --------------------------------------------------------------------------- |

| AIRCRAFT:                                | REVISION NO: 24       | PAGE:    |

|             Lockheed L-1011              |                       |          |

|                                          | DATE: 08/24/2000      | 21-1     |

| --------------------------------------------------------------------------- |

|                        1. | 2. NUMBER INSTALLED                             |

| SYSTEM &                  |    -------------------------------------------- |

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

| NUMBERS                   |    |    --------------------------------------- |

| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |

| 21  AIR CONDITIONING      |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 21-01  Pack Flow        A | 3  | 2  | (M)(O)One may be inoperative          |

|        Control Valves     |    |    | provided:                             |

|                           |    |    |     a) HP Bleed Valve, Engine         |

|                           |    |    |        Isolation Valve and            |

|                           |    |    |        Crossbleed Valve(s)            |

|                           |    |    |        associated with the            |

|                           |    |    |        inoperative Pack Flow          |

|                           |    |    |        Control Valve are operative,   |

|                           |    |    |     b) Affected valve is verified     |

|                           |    |    |        CLOSED, and                    |

|                           |    |    |     c) Repairs are made within one    |

|                           |    |    |        flight day.                    |

|                           |    |    |                                       |

|                         C | 3  | 2  | (M)(O)One may be inoperative        ] |

|                           |    |    | provided affected valve is secured    |

|                           |    |    | CLOSED.                               |

|                           |    |    |                                       |

| 21-21  Compressor       C | 3  | 2  | (O)One may be inoperative provided    |

|        Overheat Trip      |    |    | associated ECS Temperature            |

|        Systems            |    |    | Indicating Systems for CPRSR DISCH    |

|                           |    |    | and ACM DISCH are operative.          |

|                           |    |    |                                       |

|                           |    |    | NOTE:  For inoperative compressor     |

|                           |    |    |        over-temperature switch,       |

|                           |    |    |        limit associated CPRSR DISCH   |

|                           |    |    |        temperature to +200 degrees    |

|                           |    |    |        C maximum.                     |

|                           |    |    |                                       |

| 21-24  Pack Discharge   C | 3  | 2  | (O)One may be inoperative provided    |

|        Overheat Trip      |    |    | associated ECS Temperature            |

|        Systems            |    |    | Indicating Systems for CPRSR DISCH    |

|                           |    |    | and ACM DISCH are operative.          |

|                           |    |    |                                       |

|                           |    |    | NOTE:  For inoperative pack           |

|                           |    |    |        discharge over-temperature     |

|                           |    |    |        switch, limit associated ACM   |

|                           |    |    |        DISCH temperature to +80       |

|                           |    |    |        degrees C maximum.             |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

| --------------------------------------------------------------------------- |

| AIRCRAFT:                                | REVISION NO: 24       | PAGE:    |

|             Lockheed L-1011              |                       |          |

|                                          | DATE: 08/24/2000      | 21-2     |

| --------------------------------------------------------------------------- |

|                        1. | 2. NUMBER INSTALLED                             |

| SYSTEM &                  |    -------------------------------------------- |

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

| NUMBERS                   |    |    --------------------------------------- |

| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |

| 21  AIR CONDITIONING      |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 21-37  Ozone Converters C | 3  | -  | As required by FAR.                   |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 23-15  Cabin Overhead   C | 1  | 0  | (M)May be inoperative provided:       |

|        Exhaust Flow       |    |    |     a) Affected valve is secured      |

|        Control Valve      |    |    |        CLOSED, and                    |

|        (-3)               |    |    |     b) Cabin Overhead Exhaust Fan     |

|                           |    |    |        System is deactivated.         |

|                           |    |    |                                       |

|                         C | 1  | 0  | (M)May be inoperative provided:     ] |

|                           |    |    |     a) Affected valve is secured    ] |

|                           |    |    |        OPEN, and                      |

|                           |    |    |     b) Cabin Galley Exhaust Flow    ] |

|                           |    |    |        Control Valve is operative     |

|                           |    |    |        or secured CLOSED.             |

|                           |    |    |                                       |

| 23-17  Cabin Overhead   C | 1  | 0  |                                       |

|        Exhaust Fan        |    |    |                                       |

|        System (-3)        |    |    |                                       |

|                           |    |    |                                       |

| 23-18  CABIN OVHD       C | 1  | 0  |                                       |

|        EXHAUST FAN        |    |    |                                       |

|        Annunciator        |    |    |                                       |

|        Light System       |    |    |                                       |

|        (-3)               |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

| --------------------------------------------------------------------------- |

| AIRCRAFT:                                | REVISION NO: 24       | PAGE:    |

|             Lockheed L-1011              |                       |          |

|                                          | DATE: 08/24/2000      | 21-3     |

| --------------------------------------------------------------------------- |

|                        1. | 2. NUMBER INSTALLED                             |

| SYSTEM &                  |    -------------------------------------------- |

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

| NUMBERS                   |    |    --------------------------------------- |

| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |

| 21  AIR CONDITIONING      |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 24-02  Galley Exhaust     |    |    |                                       |

|        Flow Control       |    |    |                                       |

|        Valves             |    |    |                                       |

|                           |    |    |                                       |

|        1) Lower Galley  C | 1  | 0  | (M)May be inoperative provided      ] |

|           (-1,-14,-15)    |    |    | affected valve is verified CLOSED.  ] |

|                           |    |    |                                       |

|                         C | 1  | 0  | (M)May be inoperative provided:     ] |

|                           |    |    |     a) Affected valve is OPEN, and  ] |

|                           |    |    |     b) Extended overwater operation ] |

|                           |    |    |        is prohibited.                 |

|                           |    |    |                                       |

|        2) Cabin Galley  C | 1  | 0  | (M)May be inoperative provided:       |

|           (-3)            |    |    |     a) Affected valve is verified     |

|                           |    |    |        CLOSED, and                    |

|                           |    |    |     b) Cabin Galley Exhaust Fan is    |

|                           |    |    |        deactivated.                   |

|                           |    |    |                                       |

|                         C | 1  | 0  | (M)May be inoperative provided:     ] |

|                           |    |    |     a) Affected valve is OPEN, and  ] |

|                           |    |    |     b) Extended overwater operation ] |

|                           |    |    |        is prohibited.                 |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

| --------------------------------------------------------------------------- |

| AIRCRAFT:                                | REVISION NO: 24       | PAGE:    |

|             Lockheed L-1011              |                       |          |

|                                          | DATE: 08/24/2000      | 21-4     |

| --------------------------------------------------------------------------- |

|                        1. | 2. NUMBER INSTALLED                             |

| SYSTEM &                  |    -------------------------------------------- |

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

| NUMBERS                   |    |    --------------------------------------- |

| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |

| 21  AIR CONDITIONING      |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 24-06  Exhaust Fan        |    |    |                                       |

|                           |    |    |                                       |

|        1) Lower Galley  C | 1  | 0  | (M)May be inoperative provided:       |

|           (-1,-14,-15)    |    |    |     a) Lower Galley Exhaust Flow      |

|                           |    |    |        Control Valve is operative,    |

|                           |    |    |        and                            |

|                           |    |    |     b) Mid Electrical Service         |

|                           |    |    |        Center (MESC) Exhaust Fan is   |

|                           |    |    |        operative during ground        |

|                           |    |    |        operations.                    |

|                           |    |    |                                       |

|        2) Cabin Galley  C | 1  | 0  |                                       |

|           (-3)            |    |    |                                       |

|                           |    |    |                                       |

|        3) Cabin Circuit C | 1  | 0  |                                       |

|           Breaker Panel   |    |    |                                       |

|           (-3)            |    |    |                                       |

|                           |    |    |                                       |

| 25-01  Forward          C | 1  | 0  | (M)May be inoperative provided:       |

|        Electronic         |    |    |     a) FESC Exhaust Fans are          |

|        Service Center     |    |    |        operative,                     |

|        (FESC) AVIONIC     |    |    |     b) FESC Exhaust Fan               |

|        AIR-FWD-LO FLO     |    |    |        Differential Pressure Switch   |

|        Light System       |    |    |        is operative, and              |

|                           |    |    |     c) FESC Exhaust Air Flow          |

|                           |    |    |        Control Valve is operative.    |

|                           |    |    |                                       |

| 25-02  Mid Electrical   C | 1  | 0  | (M)May be inoperative provided:       |

|        Service Center     |    |    |     a) MESC Exhaust Fan is            |

|        (MESC) AVIONIC     |    |    |        operative,                     |

|        AIR-MID-LO FLO     |    |    |     b) MESC Exhaust Fan               |

|        Light System       |    |    |        Differential Pressure Switch   |

|                           |    |    |        is operative, and              |

|                           |    |    |     c) MESC Exhaust Air Flow          |

|                           |    |    |        Control Valve is operative.    |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

| --------------------------------------------------------------------------- |

| AIRCRAFT:                                | REVISION NO: 21       | PAGE:    |

|             Lockheed L-1011              |                       |          |

|                                          | DATE: 03/30/1995      | 21-5     |

| --------------------------------------------------------------------------- |

|                        1. | 2. NUMBER INSTALLED                             |

| SYSTEM &                  |    -------------------------------------------- |

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

| NUMBERS                   |    |    --------------------------------------- |

| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |

| 21  AIR CONDITIONING      |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 25-03  Forward          C | -  | 1  | (O)One may be inoperative provided    |

|        Electronic         |    |    | affected fan is deactivated.          |

|        Service Center     |    |    |                                       |

|        (FESC) Exhaust   B | -  | 0  | (M)(O)Both may be inoperative         |

|        Fans               |    |    | provided:                             |

|                           |    |    |     a) Affected fan is deactivated    |

|                           |    |    |        and is free to windmill,       |

|                           |    |    |     b) FESC AVIONIC AIR-FWD-L0 FLO    |

|                           |    |    |        Light System is operative,     |

|                           |    |    |     c) During maintenance/passenger   |

|                           |    |    |        loading operations the         |

|                           |    |    |        electrical system is in        |

|                           |    |    |        Ground Service mode, and       |

|                           |    |    |     d) Within 15 minutes of           |

|                           |    |    |        switching from Ground          |

|                           |    |    |        Service mode to main busses,   |

|                           |    |    |        airplane is pressurized to     |

|                           |    |    |        obtain a cabin altitude        |

|                           |    |    |        250-300 feet below field       |

|                           |    |    |        elevation.                     |

|                           |    |    |                                       |

|                           |    |    | NOTE 1:  Above procedures are         |

|                           |    |    |          required in order to         |

|                           |    |    |          provide adequate FESC        |

|                           |    |    |          equipment cooling.           |

|                           |    |    |                                       |

|                           |    |    | NOTE 2:  DO NOT EXCEED A CABIN        |

|                           |    |    |          DIFFERENTIAL PRESSURE OF     |

|                           |    |    |          0.15 PSI DURING GROUND       |

|                           |    |    |          PRESSURIZATION.              |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

| --------------------------------------------------------------------------- |

| AIRCRAFT:                                | REVISION NO: 21       | PAGE:    |

|             Lockheed L-1011              |                       |          |

|                                          | DATE: 03/30/1995      | 21-6     |

| --------------------------------------------------------------------------- |

|                        1. | 2. NUMBER INSTALLED                             |

| SYSTEM &                  |    -------------------------------------------- |

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

| NUMBERS                   |    |    --------------------------------------- |

| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |

| 21  AIR CONDITIONING      |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 25-04  Mid Electrical   C | 1  | 0  | (M)(O)May be inoperative provided:    |

|        Service Center     |    |    |     a) Battery Charger is operative   |

|        (MESC) Exhaust     |    |    |        but is deactivated when        |

|        Fan                |    |    |        cabin differential pressure    |

|                           |    |    |        is less than 1.0 psig,         |

|                           |    |    |     b) Unattended on-ground use of    |

|                           |    |    |        lower galley ovens is          |

|                           |    |    |        prohibited, and                |

|                           |    |    |     c) Lower galley modules are not   |

|                           |    |    |        serviced with dry ice.         |

|                           |    |    |                                       |

|                           |    |    | NOTE 1:  Inoperative MESC Exhaust     |

|                           |    |    |          Fan renders Lower Galley     |

|                           |    |    |          or Lounge Smoke Detection    |

|                           |    |    |          System ineffective on        |

|                           |    |    |          ground.                      |

|                           |    |    |                                       |

|                           |    |    | NOTE 2:  See AFM Limitations for      |

|                           |    |    |          galley occupancy on          |

|                           |    |    |          ground.                      |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

| --------------------------------------------------------------------------- |

| AIRCRAFT:                                | REVISION NO: 21       | PAGE:    |

|             Lockheed L-1011              |                       |          |

|                                          | DATE: 03/30/1995      | 21-7     |

| --------------------------------------------------------------------------- |

|                        1. | 2. NUMBER INSTALLED                             |

| SYSTEM &                  |    -------------------------------------------- |

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

| NUMBERS                   |    |    --------------------------------------- |

| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |

| 21  AIR CONDITIONING      |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 25-05  Forward          C | 1  | 0  | (M)(O)May be inoperative provided:    |

|        Electronic         |    |    | provided:                             |

|        Service Center     |    |    |     a) FESC Fan Differential          |

|        (FESC) Exhaust     |    |    |        Pressure Sensing System is     |

|        Fan Differential   |    |    |        placed in the NO PRESSURE      |

|        Pressure Switch    |    |    |        position,                      |

|                           |    |    |     b) FESC Exhaust Air Flow          |

|                           |    |    |        Control Valve is operative,    |

|                           |    |    |        and                            |

|                           |    |    |     c) FESC Exhaust Fan is            |

|                           |    |    |        operative.                     |

|                           |    |    |                                       |

|                           |    |    | NOTE:  The FESC Exhaust Air Flow      |

|                           |    |    |        Control Valve will remain      |

|                           |    |    |        OPEN in flight and on          |

|                           |    |    |        ground, and AVIONIC AIR-FWD-   |

|                           |    |    |        OVBD Light will remain         |

|                           |    |    |        illuminated.  Valve can be     |

|                           |    |    |        CLOSED by unlatching COOL      |

|                           |    |    |        AIR OVBD switchlight.          |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

| --------------------------------------------------------------------------- |

| AIRCRAFT:                                | REVISION NO: 21       | PAGE:    |

|             Lockheed L-1011              |                       |          |

|                                          | DATE: 03/30/1995      | 21-8     |

| --------------------------------------------------------------------------- |

|                        1. | 2. NUMBER INSTALLED                             |

| SYSTEM &                  |    -------------------------------------------- |

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

| NUMBERS                   |    |    --------------------------------------- |

| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |

| 21  AIR CONDITIONING      |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 25-06  Mid Electrical   C | 1  | 0  | (M)(O)May be inoperative provided:    |

|        Service Center     |    |    |     a) MESC fan differential          |

|        (MESC) Exhaust     |    |    |        pressure sensing circuit is    |

|        Fan Differential   |    |    |        placed in the NORMAL           |

|        Pressure Switch    |    |    |        PRESSURE position,             |

|                           |    |    |     b) MESC Exhaust Air Flow          |

|                           |    |    |        Control Valve is electric-     |

|                           |    |    |        ally held OPEN, and can be     |

|                           |    |    |        CLOSED with the COOL AIR       |

|                           |    |    |        OVBD switchlight,              |

|                           |    |    |     c) MESC Exhaust Fan is            |

|                           |    |    |        operative, and                 |

|                           |    |    |     d) MESC AVIONIC AIR-MID-LO FLO    |

|                           |    |    |        Light System is operative.     |

|                           |    |    |                                       |

|                           |    |    | NOTE:  MESC Exhaust Air Flow          |

|                           |    |    |        Control Valve must be          |

|                           |    |    |        operative in order to allow    |

|                           |    |    |        it to be CLOSED for ditching   |

|                           |    |    |        and for pressurization         |

|                           |    |    |        control.                       |

|                           |    |    |                                       |

| 25-09  Forward          C | 1  | 0  | (M)(O)May be inoperative OPEN         |

|        Electronic         |    |    | provided:                             |

|        Service Center     |    |    |     a) All Pack Air Cycle Machines    |

|        (FESC) Exhaust     |    |    |        (ACM) are operative, and       |

|        Air Flow Control   |    |    |     b) MESC Exhaust Air Flow          |

|        Valve              |    |    |        Control Valve is operative.    |

|                           |    |    |                                       |

|                           |    |    | NOTE:  With FESC Exhaust Air Flow     |

|                           |    |    |        Control Valve OPEN the         |

|                           |    |    |        AVIONIC AIR-FWD-OVBD Light     |

|                           |    |    |        will remain illuminated in     |

|                           |    |    |        flight.                        |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

| --------------------------------------------------------------------------- |

| AIRCRAFT:                                | REVISION NO: 24       | PAGE:    |

|             Lockheed L-1011              |                       |          |

|                                          | DATE: 08/24/2000      | 21-9     |

| --------------------------------------------------------------------------- |

|                        1. | 2. NUMBER INSTALLED                             |

| SYSTEM &                  |    -------------------------------------------- |

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

| NUMBERS                   |    |    --------------------------------------- |

| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |

| 21  AIR CONDITIONING      |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 25-10  Mid Electrical   C | 1  | 0  | (M)(O)Except for extended over-       |

|        Service Center     |    |    | water operation, may be inoperative   |

|        (MESC) Exhaust     |    |    | OPEN provided:                        |

|        Air Flow Control   |    |    |     a) All Pack Air Cycle Machines    |

|        Valve              |    |    |        (ACM) are operative, and       |

|                           |    |    |     b) FESC Exhaust Air Flow          |

|                           |    |    |        Control Valve is operative.    |

|                           |    |    |                                       |

|                           |    |    | NOTE:  With MESC Exhaust Air Flow     |

|                           |    |    |        Control Valve OPEN, the        |

|                           |    |    |        AVIONIC AIR-MID-OVBD Light     |

|                           |    |    |        will remain illuminated in     |

|                           |    |    |        flight.                        |

|                           |    |    |                                       |

| 25-17  Inertial         C | 1  | 0  | May be inoperative provided FESC      |

|        Navigation         |    |    | Exhaust Fan is operative.             |

|        System Exhaust     |    |    |                                       |

|        Fan                |    |    |                                       |

|                           |    |    |                                       |

| 25-20  Instrument         |    |    |                                       |

|        Cooling            |    |    |                                       |

|        Annunciator        |    |    |                                       |

|        Light System       |    |    |                                       |

|                           |    |    |                                       |

|      1) PILOT INSTR     C | 1  | 0  | (M)May be inoperative provided      ] |

|         COOL SYS          |    |    | Instrument Cooling System Diverter  ] |

|                           |    |    | Valve is operative.                   |

|                           |    |    |                                       |

|                         C | 1  | 0  | (M)May be inoperative provided      ] |

|                           |    |    | Instrument Cooling System Diverter  ] |

|                           |    |    | Valve is secured in NORMAL (cold      |

|                           |    |    | air plenum) position.                 |

|                           |    |    |                                       |

|                           |    |    |  (continued)                          |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

| --------------------------------------------------------------------------- |

| AIRCRAFT:                                | REVISION NO: 24       | PAGE:    |

|             Lockheed L-1011              |                       |          |

|                                          | DATE: 08/24/2000      | 21-10    |

| --------------------------------------------------------------------------- |

|                        1. | 2. NUMBER INSTALLED                             |

| SYSTEM &                  |    -------------------------------------------- |

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

| NUMBERS                   |    |    --------------------------------------- |

| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |

| 21  AIR CONDITIONING      |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 25-20  Instrument         |    |    |                                       |

|        Cooling            |    |    |                                       |

|        Annunciator        |    |    |                                       |

|        Light System       |    |    |                                       |

|        (cont'd)           |    |    |                                       |

|                           |    |    |                                       |

|      2) PILOT INSTR     C | 1  | 0  | (M)May be inoperative provided        |

|         COOL FAN          |    |    | Instrument Cooling Fan is             |

|                           |    |    | operative.                            |

|                           |    |    |                                       |

|                           |    |    | NOTE:  Fan is audible in flight       |

|                           |    |    |        station.                       |

|                           |    |    |                                       |

| 25-21  Instrument         |    |    |                                       |

|        Cooling Fan        |    |    |                                       |

|                           |    |    |                                       |

|      1) SB 093-21-121   B | 1  | 0  | (O)May be inoperative provided        |

|         Not               |    |    | electrical system is maintained in    |

|         Incorporated      |    |    | GND SERVICE mode while loading and    |

|                           |    |    | unloading passengers.                 |

|                           |    |    |                                       |

|      2) SB 093-21-121   C | 1  | 0  |                                       |

|         or Production     |    |    |                                       |

|         Equivalent        |    |    |                                       |

|         Incorporated      |    |    |                                       |

|                           |    |    |                                       |

| 25-22  Battery Cooling  C | 1  | 0  |                                       |

|        System             |    |    |                                       |

|                           |    |    |                                       |

| 25-34  Instrument       C | 1  | 0  | (M)May be inoperative provided      ] |

|        Cooling System     |    |    | Instrument Cooling Fan is             |

|        Diverter Valve     |    |    | operative.                            |

|                           |    |    |                                       |

|                         C | 1  | 0  | (M)May be inoperative provided      ] |

|                           |    |    | Instrument Cooling System Diverter    |

|                           |    |    | Valve is secured in NORMAL (cold      |

|                           |    |    | air plenum) position.                 |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

| --------------------------------------------------------------------------- |

| AIRCRAFT:                                | REVISION NO: 24       | PAGE:    |

|             Lockheed L-1011              |                       |          |

|                                          | DATE: 08/24/2000      | 21-11    |

| --------------------------------------------------------------------------- |

|                        1. | 2. NUMBER INSTALLED                             |

| SYSTEM &                  |    -------------------------------------------- |

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

| NUMBERS                   |    |    --------------------------------------- |

| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |

| 21  AIR CONDITIONING      |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 25-35  Instrument       C | 1  | 0  | (M)May be inoperative provided        |

|        Cooling System     |    |    | Instrument Cooling Annunciator        |

|        Differential       |    |    | Light System is operative.            |

|        Pressure Switch    |    |    |                                       |

|                           |    |    |                                       |

| 25-40  Instrument       C | 1  | 0  | (M)May be inoperative provided      ] |

|        Cooling System     |    |    | Instrument Cooling System Diverter  ] |

|        Moisture Control   |    |    | Valve is operative.                   |

|        Valve              |    |    |                                       |

|                         C | 1  | 0  | (M)May be inoperative provided:     ] |

|                           |    |    |     a) Instrument Cooling System    ] |

|                           |    |    |        Diverter Valve is secured      |

|                           |    |    |        OPEN (FESC air), and           |

|                           |    |    |     b) Instrument Cooling Fan is    ] |

|                           |    |    |        operative.                     |

|                           |    |    |                                       |

| 27-00  Aft Lower Cargo  C | 1  | 0  | (M)(O)May be inoperative provided:    |

|        Compartment        |    |    |     a) Associated ventilation         |

|        Ventilation        |    |    |        system airflow control         |

|        System             |    |    |        valves for Inlet Shutoff,      |

|                           |    |    |        Overboard Shutoff, and Over-   |

|                           |    |    |        board Bypass are secured       |

|                           |    |    |        CLOSED, and                    |

|                           |    |    |     b) Live animals are not carried   |

|                           |    |    |        in Aft Lower Cargo             |

|                           |    |    |        Compartment.                   |

|                           |    |    |                                       |

| 31-00  Cabin Pressure     |    |    |                                       |

|        Control Systems    |    |    |                                       |

|                           |    |    |                                       |

|      1) Normal and      C | -  | -  | (O)May be inoperative for either      |

|         Standby Outflow   |    |    | Forward or Aft Outflow Valve          |

|         Valve Control     |    |    | provided Manual Control and           |

|         and Actuation     |    |    | Actuation is operative for both       |

|         (AC Powered)      |    |    | Forward and Aft Outflow Valves.       |

|                           |    |    |                                       |

|                           |    |    | (Continued)                           |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

| --------------------------------------------------------------------------- |

| AIRCRAFT:                                | REVISION NO: 21       | PAGE:    |

|             Lockheed L-1011              |                       |          |

|                                          | DATE: 03/30/1995      | 21-12    |

| --------------------------------------------------------------------------- |

|                        1. | 2. NUMBER INSTALLED                             |

| SYSTEM &                  |    -------------------------------------------- |

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

| NUMBERS                   |    |    --------------------------------------- |

| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |

| 21  AIR CONDITIONING      |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 31-00  Cabin Pressure     |    |    |                                       |

|        Control Systems    |    |    |                                       |

|         (cont'd)          |    |    |                                       |

|                           |    |    |                                       |

|      2) Manual Out-     C | -  | -  | (O)May be inoperative for Forward     |

|         flow Valve        |    |    | or Aft Outflow Valve provided both    |

|         Control and       |    |    | Normal and Standby Control and        |

|         Actuation (DC     |    |    | Actuation is operative for both       |

|         Powered)          |    |    | Forward and Aft Outflow Valves.       |

|                           |    |    |                                       |

|      3) Normal, Standby C | -  | -  | (M)(O)May be inoperative for either   |

|         and Manual        |    |    | the Forward or Aft Outflow Valve      |

|         Outflow Valve     |    |    | provided:                             |

|         Control and       |    |    |     a) Associated valve is secured    |

|         Actuation (AC     |    |    |        CLOSED,                        |

|         and DC Powered)   |    |    |     b) Normal, Standby and Manual     |

|                           |    |    |        Control and Actuation is       |

|                           |    |    |        operative for unaffected       |

|                           |    |    |        valve,                         |

|                           |    |    |     c) Both Cabin Safety Valves are   |

|                           |    |    |        operative, and                 |

|                           |    |    |     d) If Forward Outflow Valve is    |

|                           |    |    |        inoperative, FESC Fan          |

|                           |    |    |        Differential Pressure          |

|                           |    |    |        Sensing System is placed in    |

|                           |    |    |        NO PRESSURE position.          |

|                           |    |    |                                       |

|                           |    |    |       (Continued)                     |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

| --------------------------------------------------------------------------- |

| AIRCRAFT:                                | REVISION NO: 23       | PAGE:    |

|             Lockheed L-1011              |                       |          |

|                                          | DATE: 06/24/1998      | 21-13    |

| --------------------------------------------------------------------------- |

|                        1. | 2. NUMBER INSTALLED                             |

| SYSTEM &                  |    -------------------------------------------- |

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

| NUMBERS                   |    |    --------------------------------------- |

| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |

| 21  AIR CONDITIONING      |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 31-00  Cabin Pressure     |    |    |                                       |

|        Control Systems    |    |    |                                       |

|         (cont'd)          |    |    |                                       |

|                           |    |    |                                       |

|      3) Normal, Standby C | -  | -  | (M)(O)Except for extended over-       |

|         and Manual        |    |    | water operation, may be inoperative   |

|         Outflow Valve     |    |    | for both Forward and Aft Outflow      |

|         Control and       |    |    | Valves provided:                      |

|         Actuation (AC     |    |    |     a) Both the Forward and Aft       |

|         and DC Powered)   |    |    |        Outflow Valves are position-   |

|         (cont'd)          |    |    |        ed OPEN to 12 o'clock as       |

|                           |    |    |        indicated on the flight        |

|                           |    |    |        station indicator,             |

|                           |    |    |     b) FESC Fan Differential          |

|                           |    |    |        Pressure Sensing Circuit is    |

|                           |    |    |        placed in the NO PRESSURE      |

|                           |    |    |        position, and                  |

|                           |    |    |     c) The airplane is operated       |

|                           |    |    |        unpressurized.                 |

|                           |    |    |                                       |

|                           |    |    | NOTE:   See AFM Limitations.          |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

| --------------------------------------------------------------------------- |

| AIRCRAFT:                                | REVISION NO: 24       | PAGE:    |

|             Lockheed L-1011              |                       |          |

|                                          | DATE: 08/24/2000      | 21-14    |

| --------------------------------------------------------------------------- |

|                        1. | 2. NUMBER INSTALLED                             |

| SYSTEM &                  |    -------------------------------------------- |

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

| NUMBERS                   |    |    --------------------------------------- |

| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |

| 21  AIR CONDITIONING      |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 31-00  Cabin Pressure     |    |    |                                       |

|        Control Systems    |    |    |                                       |

|         (cont'd)          |    |    |                                       |

|                           |    |    |                                       |

| ***  3) STC ST00847AT   C | -  | -  | (M)(O)May be inoperative for the      |

|         ONLY - Normal,    |    |    | Forward Outflow Valve provided:       |

|         Standby and       |    |    |     a) Valve is secured CLOSED,       |

|         Manual Outflow    |    |    |     b) Normal, Standby and Manual     |

|         Valve Control     |    |    |        Control and Actuation is       |

|         and Actuation     |    |    |        operative for Aft Valve,       |

|         (AC and DC        |    |    |     c) Both Cabin Safety Valves are   |

|         Powered)          |    |    |        operative, and                 |

|                           |    |    |     d) FESC Fan Differential          |

|                           |    |    |        Pressure Sensing System is     |

|                           |    |    |        placed in NO PRESSURE          |

|                           |    |    |        position.                      |

|                           |    |    |                                       |

|                           |    |    |       (Continued)                     |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

| --------------------------------------------------------------------------- |

| AIRCRAFT:                                | REVISION NO: 24       | PAGE:    |

|             Lockheed L-1011              |                       |          |

|                                          | DATE: 08/24/2000      | 21-15    |

| --------------------------------------------------------------------------- |

|                        1. | 2. NUMBER INSTALLED                             |

| SYSTEM &                  |    -------------------------------------------- |

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

| NUMBERS                   |    |    --------------------------------------- |

| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |

| 21  AIR CONDITIONING      |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 31-00  Cabin Pressure     |    |    |                                       |

|        Control Systems    |    |    |                                       |

|         (cont'd)          |    |    |                                       |

|                           |    |    |                                       |

| ***  3) STC ST00847AT   A | -  | -  | (M)(O)Except for extended over-       |

|         ONLY - Normal,    |    |    | water operation, may be inoperative   |

|         Standby and       |    |    | for both Forward and Aft Outflow      |

|         Manual Outflow    |    |    | Valves provided:                      |

|         Valve Control     |    |    |     a) Both the Forward and Aft       |

|         and Actuation     |    |    |        Outflow Valves are position-   |

|         (AC and DC        |    |    |        ed OPEN to 12 o'clock as       |

|         Powered)          |    |    |        indicated on the flight        |

|                           |    |    |        station indicator,             |

|                           |    |    |     b) FESC Fan Differential          |

|                           |    |    |        Pressure Sensing Circuit is    |

|                           |    |    |        placed in the NO PRESSURE      |

|                           |    |    |        position,                      |

|                           |    |    |     c) Airplane is operated           |

|                           |    |    |        unpressurized, and             |

|                           |    |    |     d) Repairs are made within one    |

|                           |    |    |        flight day.                    |

|                           |    |    |                                       |

|                           |    |    | NOTE:   See AFM Limitations.          |

|                           |    |    |                                       |

|        4) Normal Mode   C | 1  | 0  | (O)May be inoperative provided      ] |

|                           |    |    | Standby and Manual modes are        ] |

|                           |    |    | operative for both Forward and Aft  ] |

|                           |    |    | Outflow Valves.                     ] |

|                           |    |    |                                       |

|        5) Standby Mode  C | 1  | 0  | (O)May be inoperative provided      ] |

|                           |    |    | Normal and Manual modes are         ] |

|                           |    |    | operative for both Forward and Aft  ] |

|                           |    |    | Outflow Valves.                     ] |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

| --------------------------------------------------------------------------- |

| AIRCRAFT:                                | REVISION NO: 24       | PAGE:    |

|             Lockheed L-1011              |                       |          |

|                                          | DATE: 08/24/2000      | 21-16    |

| --------------------------------------------------------------------------- |

|                        1. | 2. NUMBER INSTALLED                             |

| SYSTEM &                  |    -------------------------------------------- |

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

| NUMBERS                   |    |    --------------------------------------- |

| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |

| 21  AIR CONDITIONING      |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 32-01  Cabin Safety     C | 2  | 1  | (M)One may be inoperative provided:   |

|        Valves             |    |    |     a) Affected valve is secured      |

|                           |    |    |        CLOSED, and                    |

|                           |    |    |     b) Cabin Pressure Control         |

|                           |    |    |        System Normal, Standby and     |

|                           |    |    |        Manual Control and Actuation   |

|                           |    |    |        is operative for both          |

|                           |    |    |        Forward and Aft Outflow        |

|                           |    |    |        Valves.                        |

|                           |    |    |                                       |

| 32-05  Cabin Safety     C | 2  | 0  |                                       |

|        Valve OPEN         |    |    |                                       |

|        Lights             |    |    |                                       |

|                           |    |    |                                       |

| 33-01  Cabin Altitude   C | 1  | 0  | (M)(O)May be inoperative provided:    |

|        and Differential   |    |    |     a) Flight is conducted            |

|        Pressure           |    |    |        unpressurized, and             |

|        Indicator          |    |    |     b) FWD Cabin Air Outflow Valve    |

|                           |    |    |        is selected OPEN in MNL        |

|                           |    |    |        mode.                          |

|                           |    |    |                                       |

|      1) ALTITUDE        C | 1  | 0  | (O)May be inoperative provided:       |

|         Indication        |    |    |     a) Cabin DIFFERENTIAL PRESSURE    |

|                           |    |    |        portion of indicator is        |

|                           |    |    |        operative, and                 |

|                           |    |    |     b) A chart is provided to the     |

|                           |    |    |        crew to convert cabin          |

|                           |    |    |        differential pressure to       |

|                           |    |    |        cabin altitude.                |

|                           |    |    |                                       |

|      2) DIFFERENTIAL    C | 1  | 0  | (O)May be inoperative provided:       |

|         PRESSURE          |    |    |     a) Cabin ALTITUDE portion of      |

|         Indication        |    |    |        indicator is operative, and    |

|                           |    |    |     b) A chart is provided to the     |

|                           |    |    |        crew to convert cabin          |

|                           |    |    |        altitude to cabin              |

|                           |    |    |        differential pressure.         |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

| --------------------------------------------------------------------------- |

| AIRCRAFT:                                | REVISION NO: 24       | PAGE:    |

|             Lockheed L-1011              |                       |          |

|                                          | DATE: 08/24/2000      | 21-17    |

| --------------------------------------------------------------------------- |

|                        1. | 2. NUMBER INSTALLED                             |

| SYSTEM &                  |    -------------------------------------------- |

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

| NUMBERS                   |    |    --------------------------------------- |

| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |

| 21  AIR CONDITIONING      |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 33-01  STC ST00847AT    A | 1  | 0  | (M)(O)May be inoperative provided:    |

| ***    ONLY - Cabin       |    |    |     a) Aft Outflow Valve is secured   |

|        Altitude and       |    |    |        OPEN,                          |

|        Differential       |    |    |     b) FESC Fan Differential          |

|        Pressure           |    |    |        Pressure Sensing Circuit is    |

|        Indicator          |    |    |        placed in the NO PRESSURE      |

|                           |    |    |        position,                      |

|                           |    |    |     c) Airplane is operated           |

|                           |    |    |        unpressurized,                 |

|                           |    |    |     d) Airplane is operated in        |

|                           |    |    |        accordance with AFM            |

|                           |    |    |        Limitations, and               |

|                           |    |    |     e) Repairs are made within one    |

|                           |    |    |        flight day.                    |

|                           |    |    |                                       |

| 33-01  STC ST00847AT      |    |    |                                       |

| ***    ONLY - Cabin       |    |    |                                       |

|        Altitude and       |    |    |                                       |

|        Differential       |    |    |                                       |

|        Pressure           |    |    |                                       |

|        Indicator          |    |    |                                       |

|        (cont'd)           |    |    |                                       |

|                           |    |    |                                       |

|      1) ALTITUDE        C | 1  | 0  | (O)May be inoperative provided:       |

|         Indication        |    |    |     a) Cabin DIFFERENTIAL PRESSURE    |

|                           |    |    |        portion of indicator is        |

|                           |    |    |        operative, and                 |

|                           |    |    |     b) A chart is provided to the     |

|                           |    |    |        crew to convert cabin          |

|                           |    |    |        differential pressure to       |

|                           |    |    |        cabin altitude.                |

|                           |    |    |                                       |

|      2) DIFFERENTIAL    C | 1  | 0  | (O)May be inoperative provided:       |

|         PRESSURE          |    |    |     a) Cabin ALTITUDE portion of      |

|         Indication        |    |    |        indicator is operative, and    |

|                           |    |    |     b) A chart is provided to the     |

|                           |    |    |        crew to convert cabin          |

|                           |    |    |        altitude to cabin              |

|                           |    |    |        differential pressure.         |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

| --------------------------------------------------------------------------- |

| AIRCRAFT:                                | REVISION NO: 24       | PAGE:    |

|             Lockheed L-1011              |                       |          |

|                                          | DATE: 08/24/2000      | 21-18    |

| --------------------------------------------------------------------------- |

|                        1. | 2. NUMBER INSTALLED                             |

| SYSTEM &                  |    -------------------------------------------- |

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

| NUMBERS                   |    |    --------------------------------------- |

| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |

| 21  AIR CONDITIONING      |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 33-02  Cabin Rate-of-   C | 1  | 0  | May be inoperative provided:          |

|        Climb Indicator    |    |    |     a) Cabin Pressure Control         |

|                           |    |    |        Systems Normal and Standby     |

|                           |    |    |        Control and Actuation is       |

|                           |    |    |        operative for both Forward     |

|                           |    |    |        and Aft Outflow Valves, and    |

|                           |    |    |     b) Cabin Altitude and             |

|                           |    |    |        Differential Pressure          |

|                           |    |    |        Indications are operative.     |

|                           |    |    |                                       |

| 41-02  Hot Air Manifold C | 2  | 0  | (M)(O)Both may be inoperative       ] |

|        Temperature        |    |    | provided affected valve is secured    |

|        Control Valves     |    |    | CLOSED.                               |

|                           |    |    |                                       |

|                         C | 2  | 0  | (M)(O)Both may be inoperative       ] |

|                           |    |    | provided associated Hot Air         ] |

|                           |    |    | Manifold Isolation Valve is secured   |

|                           |    |    | CLOSED.                               |

|                           |    |    |                                       |

| 41-05  Hot Air Manifold C | 2  | 0  | (M)(O)Both may be inoperative       ] |

|        Temperature        |    |    | provided associated Hot Air           |

|        Control Sensors    |    |    | Manifold Temperature Control Valve    |

|                           |    |    | is secured CLOSED.                    |

|                           |    |    |                                       |

|                         C | 2  | 0  | (M)(O)Both may be inoperative       ] |

|                           |    |    | provided associated Hot Air         ] |

|                           |    |    | Manifold Isolation Valve is secured   |

|                           |    |    | CLOSED.                               |

|                           |    |    |                                       |

| 41-17  Hot Air Manifold C | 2  | 1  | (M)(O)One may be inoperative either   |

|        Isolation Valves   |    |    | full OPEN or full CLOSED.             |

|                           |    |    |                                       |

|                           |    |    |       (Continued)                     |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

| --------------------------------------------------------------------------- |

| AIRCRAFT:                                | REVISION NO: 24       | PAGE:    |

|             Lockheed L-1011              |                       |          |

|                                          | DATE: 08/24/2000      | 21-19    |

| --------------------------------------------------------------------------- |

|                        1. | 2. NUMBER INSTALLED                             |

| SYSTEM &                  |    -------------------------------------------- |

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

| NUMBERS                   |    |    --------------------------------------- |

| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |

| 21  AIR CONDITIONING      |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 41-17  Hot Air Manifold C | 2  | 0  | (M)(O)Both may be inoperative         |

|        Isolation Valves   |    |    | provided:                             |

|         (continued)       |    |    |     a) Affected valves are secured    |

|                           |    |    |        CLOSED, and                    |

|                           |    |    |     b) Associated ECS Temperature     |

|                           |    |    |        Indicating System for HOT      |

|                           |    |    |        MANF is operative.             |

|                           |    |    |                                       |

| 41-19  Hot Air Manifold C | 1  | 0  | (M)May be inoperative provided both   |

|        Duct               |    |    | Hot Air Manifold Temperature          |

|        Overtemperature    |    |    | Control Valves are secured CLOSED.    |

|        Switch             |    |    |                                       |

|                           |    |    |                                       |

| 43-00  Floor Heat       C | 1  | 0  | (M)May be inoperative provided        |

|        System             |    |    | associated circuit breakers are       |

|                           |    |    | OPEN and COLLARED.                    |

|                           |    |    |                                       |

| 44-00  Lower Cargo        |    |    |                                       |

|        Heating Systems    |    |    |                                       |

|                           |    |    |                                       |

|      1) Fans            C | 3  | 0  | (M)All may be inoperative provided:   |

|                           |    |    |     a) Affected Fan is deactivated,   |

|                           |    |    |        and                            |

|                           |    |    |     b) Live animals are not carried   |

|                           |    |    |        in associated cargo            |

|                           |    |    |        compartment.                   |

|                           |    |    |                                       |

|      2) Cycling         C | 3  | 0  | (M)All may be inoperative provided    |

|         Switches          |    |    | affected switch is OPEN.              |

|                           |    |    |                                       |

|      3) Overtemperature C | 3  | 0  | (M)All may be inoperative provided    |

|         Switches          |    |    | associated fan circuit breaker is     |

|                           |    |    | OPEN and COLLARED.                    |

|                           |    |    |                                       |

|      4) Cold Indication C | 3  | 0  | All may be inoperative provided       |

|         Switches          |    |    | live animals are not carried in Aft   |

|                           |    |    | Cargo area when the associated        |

|                           |    |    | Heating System is inoperative.        |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

| --------------------------------------------------------------------------- |

| AIRCRAFT:                                | REVISION NO: 24       | PAGE:    |

|             Lockheed L-1011              |                       |          |

|                                          | DATE: 08/24/2000      | 21-20    |

| --------------------------------------------------------------------------- |

|                        1. | 2. NUMBER INSTALLED                             |

| SYSTEM &                  |    -------------------------------------------- |

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

| NUMBERS                   |    |    --------------------------------------- |

| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |

| 21  AIR CONDITIONING      |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 51-01  Pack Heat        C | 3  | 2  | (M)One may be inoperative provided    |

|        Exchangers         |    |    | associated Pack Flow Control Valve    |

|                           |    |    | is secured CLOSED.                    |

|                           |    |    |                                       |

|                           |    |    | NOTE 1:  *** STC ST00847AT ONLY -     |

|                           |    |    |          When #1 is inoperative the   |

|                           |    |    |          #2 pack fail override        |

|                           |    |    |          switch must be deselected.   |

|                           |    |    |          When #2 is inoperative the   |

|                           |    |    |          #2 pack fail override        |

|                           |    |    |          switch must be selected.     |

|                           |    |    |          When #3 is inoperative the   |

|                           |    |    |          #2 pack fail override        |

|                           |    |    |          switch may be either         |

|                           |    |    |          selected or deselected.      |

|                           |    |    |                                       |

| 51-04  Ram Cooling      C | 3  | 0  | (M)All may be inoperative provided    |

|        Header and Check   |    |    | associated Pack ACM is not operated   |

|        Valves             |    |    | on the ground.                        |

|                           |    |    |                                       |

| 51-07  Pack Air Cycle   C | 3  | 2  | (M)(O)One may be inoperative          |

|        Machines (ACM)     |    |    | provided:                             |

|                           |    |    |     a) Associated Pack Flow Control   |

|                           |    |    |        Valve is operative and is      |

|                           |    |    |        OPEN only in flight,           |

|                           |    |    |     b) Associated Pack Ram Air        |

|                           |    |    |        Exhaust System is operative,   |

|                           |    |    |     c) Associated Pack Turbine        |

|                           |    |    |        Bypass Valve is deactivated    |

|                           |    |    |        OPEN or remains OPEN using     |

|                           |    |    |        pack MNL control, and          |

|                           |    |    |     d) Associated ECS Temperature     |

|                           |    |    |        Indicating System for ACM      |

|                           |    |    |        DISCH is operative.            |

|                           |    |    |                                       |

|                           |    |    |         (Continued)                   |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

| --------------------------------------------------------------------------- |

| AIRCRAFT:                                | REVISION NO: 23       | PAGE:    |

|             Lockheed L-1011              |                       |          |

|                                          | DATE: 06/24/1998      | 21-21    |

| --------------------------------------------------------------------------- |

|                        1. | 2. NUMBER INSTALLED                             |

| SYSTEM &                  |    -------------------------------------------- |

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

| NUMBERS                   |    |    --------------------------------------- |

| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |

| 21  AIR CONDITIONING      |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 51-07  Pack Air Cycle   C | 3  | 1  | (M)(O)Two may be inoperative          |

|        Machines (ACM)     |    |    | provided:                             |

|        (cont'd)           |    |    |     a) Operative ACM Pack Turbine     |

|                           |    |    |        Bypass Valve is operative,     |

|                           |    |    |     b) Associated Pack Flow Control   |

|                           |    |    |        Valves are operative and are   |

|                           |    |    |        OPEN only in flight,           |

|                           |    |    |     c) Associated Pack Ram Air        |

|                           |    |    |        Exhaust Systems are            |

|                           |    |    |        operative,                     |

|                           |    |    |     d) Associated Pack Turbine        |

|                           |    |    |        Bypass Valves are              |

|                           |    |    |        deactivated OPEN or remain     |

|                           |    |    |        OPEN using pack MNL control,   |

|                           |    |    |     e) Associated ECS Temperature     |

|                           |    |    |        Indicating System for ACM      |

|                           |    |    |        DISCH is operative, and        |

|                           |    |    |     f) Airplane is not operated       |

|                           |    |    |        more than 400 nautical miles   |

|                           |    |    |        from a suitable airport.       |

|                           |    |    |                                       |

|                           |    |    | NOTE:  A pack is considered to be     |

|                           |    |    |        operative even though the      |

|                           |    |    |        following are inoperative:     |

|                           |    |    |        PACK INLET, CMPR DISCH, TURB   |

|                           |    |    |        INLET indications, and AUTO    |

|                           |    |    |        temperature control.           |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 51-22  Pack Water       C | 3  | 0  | (O)All may be inoperative provided    |

|        Separators         |    |    | associated PACK TEMPERATURE CONTROL   |

|                           |    |    | is operated in manual mode on the     |

|                           |    |    | ground.                               |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

| --------------------------------------------------------------------------- |

| AIRCRAFT:                                | REVISION NO: 24       | PAGE:    |

|             Lockheed L-1011              |                       |          |

|                                          | DATE: 08/24/2000      | 21-22    |

| --------------------------------------------------------------------------- |

|                        1. | 2. NUMBER INSTALLED                             |

| SYSTEM &                  |    -------------------------------------------- |

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

| NUMBERS                   |    |    --------------------------------------- |

| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |

| 21  AIR CONDITIONING      |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 61-00  Zone Trim        C | -  | 0  | (M)(O)May be inoperative provided   ] |

|        Control Systems    |    |    | Associated Zone Trim Control Valve    |

|                           |    |    | is CLOSED.                            |

|                           |    |    |                                       |

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

|                           |    |    | Both Hot Air Manifold Isolation       |

|                           |    |    | Valves are CLOSED.                    |

|                           |    |    |                                       |

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

|                           |    |    | Zone Trim Pressure Regulator and      |

|                           |    |    | Shutoff Valve is CLOSED.              |

|                           |    |    |                                       |

| 61-27  Zone Trim        C | 1  | 0  | (M)(O)May be inoperative provided:    |

|        Pressure           |    |    |     a) Valve is verified OPEN or      |

|        Regulator and      |    |    |        CLOSED, and                    |

|        Shutoff Valve      |    |    |     b) Valve position is noted on     |

|                           |    |    |        placard.                       |

|                           |    |    |                                       |

|                           |    |    | NOTE:  When valve is CLOSED all       |

|                           |    |    |        trim air is shut off.          |

|                           |    |    |                                       |

| 62-01  Pack Temperature C | 3  | 0  | (O)All may be inoperative provided:   |

|        Controllers        |    |    |     a) Associated ECS Temperature     |

|                           |    |    |        Indicating Systems for CPRSR   |

|                           |    |    |        DISCH and ACM DISCH are        |

|                           |    |    |        operative, and                 |

|                           |    |    |     b) Associated Pack Manual         |

|                           |    |    |        Control System is verified     |

|                           |    |    |        operative.                     |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

| --------------------------------------------------------------------------- |

| AIRCRAFT:                                | REVISION NO: 24       | PAGE:    |

|             Lockheed L-1011              |                       |          |

|                                          | DATE: 08/24/2000      | 21-23    |

| --------------------------------------------------------------------------- |

|                        1. | 2. NUMBER INSTALLED                             |

| SYSTEM &                  |    -------------------------------------------- |

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

| NUMBERS                   |    |    --------------------------------------- |

| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |

| 21  AIR CONDITIONING      |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 62-04  Pack Ram Air     C | 3  | 2  | (M)One may be inoperative provided    |

|        Exhaust Systems    |    |    | affected Exhaust System is            |

|        (Actuator and      |    |    | deactivated.                          |

|        Louvers)           |    |    |                                       |

|                         C | 3  | 1  | (M)Two may be inoperative provided:   |

|                           |    |    |     a) One affected system is         |

|                           |    |    |        secured in MID position, and   |

|                           |    |    |     b) Other affected system is       |

|                           |    |    |        CLOSED.                        |

|                           |    |    |                                       |

| 62-16  Pack Turbine     C | 3  | 1  | (M)(O)Two may be inoperative          |

|        Bypass Valves      |    |    | provided:                             |

|                           |    |    |     a) All three Pack ACM's and       |

|                           |    |    |        affected components are        |

|                           |    |    |        operative,                     |

|                           |    |    |     b) Associated valve is secured    |

|                           |    |    |        OPEN,                          |

|                           |    |    |     c) Associated Pack Ram Air        |

|                           |    |    |        Exhaust System is operative,   |

|                           |    |    |     d) Associated Turbine Bypass      |

|                           |    |    |        Position Indicating System     |

|                           |    |    |        is operative,                  |

|                           |    |    |     e) Associated Pack Flow Control   |

|                           |    |    |        Valve is operative and OPEN    |

|                           |    |    |        only in flight, and            |

|                           |    |    |     f) Associated ACM DISCH           |

|                           |    |    |        temperature is monitored.      |

|                           |    |    |                                       |

| 62-19  Pack Ice Sensors C | 3  | 0  | (O)All may be inoperative provided    |

|                           |    |    | associated ECS Temperature            |

|                           |    |    | Indicating System for ACM DISCH is    |

|                           |    |    | operative.                            |

|                           |    |    |                                       |

| 62-22  Auto Control     C | 3  | 0  | (O)All may be inoperative provided    |

|        Pack Discharge     |    |    | associated Pack Temperature           |

|        Temperature        |    |    | Controller is considered              |

|        Sensors            |    |    | inoperative.                          |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

| --------------------------------------------------------------------------- |

| AIRCRAFT:                                | REVISION NO: 23       | PAGE:    |

|             Lockheed L-1011              |                       |          |

|                                          | DATE: 06/24/1998      | 21-24    |

| --------------------------------------------------------------------------- |

|                        1. | 2. NUMBER INSTALLED                             |

| SYSTEM &                  |    -------------------------------------------- |

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

| NUMBERS                   |    |    --------------------------------------- |

| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |

| 21  AIR CONDITIONING      |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 62-28  Valve Position     |    |    |                                       |

|        Indicating         |    |    |                                       |

|        Systems            |    |    |                                       |

|                           |    |    |                                       |

|        1) RAM AIR       C | 3  | 1  | Two may be inoperative provided       |

|                           |    |    | associated RAM AIR indicator is       |

|                           |    |    | operative if only one Pack Ram Air    |

|                           |    |    | Exhaust System is operative.          |

|                           |    |    |                                       |

|        2) TURB BYP      C | 3  | 1  | Two may be inoperative provided       |

|                           |    |    | associated TURB BYP indicator is      |

|                           |    |    | operative if only one Pack Turbine    |

|                           |    |    | Bypass Valve is operative.            |

|                           |    |    |                                       |

| 62-31  Humidity Control C | 1  | 0  |                                       |

|        System             |    |    |                                       |

|        (Dehumidifi-       |    |    |                                       |

|         cation)           |    |    |                                       |

|                           |    |    |                                       |

| 63-03  Pack Flow        C | 3  | 0  |                                       |

|        Indicating         |    |    |                                       |

|        Systems            |    |    |                                       |

|                           |    |    |                                       |

| 63-09  Environmental    C | 15 | 0  |                                       |

|        Control System     |    |    |                                       |

|        (ECS)              |    |    |                                       |

|        Temperature        |    |    |                                       |

|        Indicating         |    |    |                                       |

|        Systems            |    |    |                                       |

|                           |    |    |                                       |

| 63-27  Cabin            C | -  | 0  | May be inoperative provided           |

|        Temperature        |    |    | associated ECS Temperature            |

|        Indicating         |    |    | Indicating System for ACM DISCH is    |

|        Systems            |    |    | operative.                            |

|                           |    |    |                                       |

| 70-00  Humidity         C | 1  | 0  |                                       |

|        Regulation         |    |    |                                       |

|        System             |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

| --------------------------------------------------------------------------- |

| AIRCRAFT:                                | REVISION NO: 21       | PAGE:    |

|             Lockheed L-1011              |                       |          |

|                                          | DATE: 03/30/1995      | 22-1     |

| --------------------------------------------------------------------------- |

|                        1. | 2. NUMBER INSTALLED                             |

| SYSTEM &                  |    -------------------------------------------- |

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

| NUMBERS                   |    |    --------------------------------------- |

| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |

| 22  AUTO FLIGHT           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 00-01  Flight Control   C | 2  | 1  | (O)One may be inoperative provided:   |

|        Electronics        |    |    |     a) A YAW SAS Channel is           |

|        System (FCES)      |    |    |        operative, and                 |

|        Computers          |    |    |     b) Approach minimums do not       |

|        (Digital AFCS)     |    |    |        require dual autopilot use.    |

|                           |    |    |                                       |

| 00-03  Glareshield Mode   |    |    |                                       |

|        Control Panel      |    |    |                                       |

|        Functions          |    |    |                                       |

|        (Digital AFCS)     |    |    |                                       |

|                           |    |    |                                       |

|      1) Autothrottle    C | 2  | 0  | (O)Both may be inoperative            |

|         Alpha and         |    |    | provided:                             |

|         Numeric           |    |    |     a) AT mode is considered          |

|         Displays          |    |    |        inoperative, and               |

|                           |    |    |     b) Approach minimums do not       |

|                           |    |    |        require autothrottle use.      |

|                           |    |    |                                       |

|                           |    |    | NOTE:  If TM Mode is available, it    |

|                           |    |    |        may be selected using PMS or   |

|                           |    |    |        FMS CDU.                       |

|                           |    |    |                                       |

|      2) Pitch Alpha and C | 2  | 0  | (O)Both may be inoperative            |

|         Numeric           |    |    | provided:                             |

|         Displays          |    |    |     a) Glareshield panel switch-      |

|                           |    |    |        light illuminates for each     |

|                           |    |    |        operative pitch mode           |

|                           |    |    |        selected,                      |

|                           |    |    |     b) AFCS Mode Annunciators for     |

|                           |    |    |        each Pitch mode used are       |

|                           |    |    |        operative on both pilot's      |

|                           |    |    |        panels.                        |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    | (Continued)                           |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

| --------------------------------------------------------------------------- |

| AIRCRAFT:                                | REVISION NO: 23       | PAGE:    |

|             Lockheed L-1011              |                       |          |

|                                          | DATE: 06/24/1998      | 22-2     |

| --------------------------------------------------------------------------- |

|                        1. | 2. NUMBER INSTALLED                             |

| SYSTEM &                  |    -------------------------------------------- |

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

| NUMBERS                   |    |    --------------------------------------- |

| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |

| 22  AUTO FLIGHT           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 00-03  Glareshield Mode   |    |    |                                       |

|        Control Panel      |    |    |                                       |

|        Functions          |    |    |                                       |

|        (Digital AFCS)     |    |    |                                       |

|        (Cont'd)           |    |    |                                       |

|                           |    |    |                                       |

|      2) Pitch Alpha and   |    |    |     c) Vertical Speed Control Wheel   |

|         Numeric           |    |    |        properly displaces flight      |

|         Displays          |    |    |        director pitch command or VS   |

|         (Cont'd)          |    |    |        Mode is considered             |

|                           |    |    |        inoperative, and               |

|                           |    |    |     d) If VNAV Mode is used, PMS or   |

|                           |    |    |        FMS CDU is operative.          |

|                           |    |    |                                       |

|      3) Heading Numeric C | 1  | 0  | (O)May be inoperative provided:       |

|         Display           |    |    |     a) Glareshield panel HDG mode     |

|                           |    |    |        switchlight illuminates if     |

|                           |    |    |        selected,                      |

|                           |    |    |     b) AFCS Mode Annunciators for     |

|                           |    |    |        HDG mode are operative on      |

|                           |    |    |        both pilot's panels or the     |

|                           |    |    |        HDG Mode is considered         |

|                           |    |    |        inoperative, and               |

|                           |    |    |     c) Heading select knob operates   |

|                           |    |    |        both HSI headings bugs.        |

|                           |    |    |                                       |

|                           |    |    |        (Continued)                    |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

| --------------------------------------------------------------------------- |

| AIRCRAFT:                                | REVISION NO: 24       | PAGE:    |

|             Lockheed L-1011              |                       |          |

|                                          | DATE: 08/24/2000      | 22-3     |

| --------------------------------------------------------------------------- |

|                        1. | 2. NUMBER INSTALLED                             |

| SYSTEM &                  |    -------------------------------------------- |

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

| NUMBERS                   |    |    --------------------------------------- |

| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |

| 22  AUTO FLIGHT           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 00-03  Glareshield Mode   |    |    |                                       |

|        Control Panel      |    |    |                                       |

|        Functions          |    |    |                                       |

|        (Digital AFCS)     |    |    |                                       |

|         (Cont'd)          |    |    |                                       |

|                           |    |    |                                       |

|      4) Course Numeric  C | 2  | 0  | (O)Both may be inoperative            |

|         Displays          |    |    | provided:                             |

|                           |    |    |     a) Glareshield panel switch-      |

|                           |    |    |        light illuminates for each     |

|                           |    |    |        operative Navigation Mode      |

|                           |    |    |        selected,                      |

|                           |    |    |     b) AFCS Mode Annunciators for     |

|                           |    |    |        each Navigation mode used      |

|                           |    |    |        are operative on both          |

|                           |    |    |        pilot's panels, and            |

|                           |    |    |     c) Each Course-Set Knob           |

|                           |    |    |        operates its respective HSI    |

|                           |    |    |        Course Pointer.                |

|                           |    |    |                                       |

|      5) Select Altitude C | 1  | 0  | (O)May be inoperative provided FMS    |

|         Numeric Display   |    |    | or PMS is operative and selected      |

|                           |    |    | altitude is continuously displayed    |

|                           |    |    | on FMS or PMS CDU.                    |

|                           |    |    |                                       |

|      6) AFCS Mode       C | -  | 0  | May be inoperative provided           |

|         Selectors-AT TM   |    |    | approach minimums do not require      |

|         VNAV VS ALT IAS   |    |    | its use.                              |

|         MACH HDG TURB     |    |    |                                       |

|         ILS LOC VOR INS   |    |    | NOTE 1:  See AFM Procedures for       |

|         BC                |    |    |          approach and landing         |

|                           |    |    |          equipment requirements.      |

|                           |    |    |                                       |

|                           |    |    | NOTE 2:  ALT Mode Selector must be    |

|                           |    |    |          operative where enroute      |

|                           |    |    |          operations require its       |

|                           |    |    |          use.                         |

|                           |    |    |                                       |

|                           |    |    |          (continued)                  |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

| --------------------------------------------------------------------------- |

| AIRCRAFT:                                | REVISION NO: 24       | PAGE:    |

|             Lockheed L-1011              |                       |          |

|                                          | DATE: 08/24/2000      | 22-4     |

| --------------------------------------------------------------------------- |

|                        1. | 2. NUMBER INSTALLED                             |

| SYSTEM &                  |    -------------------------------------------- |

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

| NUMBERS                   |    |    --------------------------------------- |

| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |

| 22  AUTO FLIGHT           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 00-03  Glareshield Mode   |    |    |                                       |

|        Control Panel      |    |    |                                       |

|        Functions          |    |    |                                       |

|        (Digital AFCS)     |    |    |                                       |

|        (continued)        |    |    |                                       |

|                         B | 2  | 1  | (O)One may be inoperative provided:   |

|      7) Course-Set        |    |    |     a) Operative Course-Set Knob    ] |

|         Knobs (COURSE     |    |    |        controls associated HSI      ] |

|         1, COURSE 2)      |    |    |        Course Pointer,                |

|                           |    |    |     b) RDDMI VOR function is          |

|                           |    |    |        operative for bearing to       |

|                           |    |    |        station display on             |

|                           |    |    |        associated pilot's panel,      |

|                           |    |    |        and                            |

|                           |    |    |     c) Airplane is operated in VMC    |

|                           |    |    |        only.                          |

|                           |    |    |                                       |

|      8) Autopilot       C | 2  | 0  | Both may be inoperative provided:     |

|         Engage Switches   |    |    |     a) Associated autopilot system    |

|         (Bat Handles)     |    |    |        is considered inoperative,     |

|                           |    |    |     b) Approach minimums do not       |

|                           |    |    |        require autopilot use, and     |

|                           |    |    |     c) Enroute operations do not      |

|                           |    |    |        require its use.               |

|                           |    |    |                                       |

| 00-05  Power Supply     C | 2  | 1  | (O)One may be inoperative provided:   |

|        Units (Digital     |    |    |     a) A YAW SAS Channel is           |

|        AFCS)              |    |    |        operative,                     |

|                           |    |    |     b) Associated APFDS is            |

|                           |    |    |        considered inoperative, and    |

|                           |    |    |     c) Approach minimums do not       |

|                           |    |    |        require autopilot use.         |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

| --------------------------------------------------------------------------- |

| AIRCRAFT:                                | REVISION NO: 24       | PAGE:    |

|             Lockheed L-1011              |                       |          |

|                                          | DATE: 08/24/2000      | 22-5     |

| --------------------------------------------------------------------------- |

|                        1. | 2. NUMBER INSTALLED                             |

| SYSTEM &                  |    -------------------------------------------- |

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

| NUMBERS                   |    |    --------------------------------------- |

| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |

| 22  AUTO FLIGHT           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 10-00  Autopilot and      |    |    |                                       |

|        Flight Director    |    |    |                                       |

|        Systems (APFDS)    |    |    |                                       |

|                           |    |    |                                       |

|      1) Autopilots      B | 2  | 0  | Both may be inoperative provided:   ] |

|                           |    |    |     a) Approach minimums do not     ] |

|                           |    |    |        require autopilot use, and   ] |

|                           |    |    |     b) Enroute operations do not    ] |

|                           |    |    |        require its use.             ] |

|                           |    |    |                                       |

|                         C | 2  | 1  | One may be inoperative provided:    ] |

|                           |    |    |     a) Approach minimums do not       |

|                           |    |    |        require autopilot use, and     |

|                           |    |    |     b) Enroute operations do not      |

|                           |    |    |        require its use.               |

|                           |    |    |                                       |

|      2) Flight          C | 2  | 0  | Both may be inoperative provided      |

|         Directors         |    |    | approach minimums do not require      |

|                           |    |    | flight director use.                  |

|                           |    |    |                                       |

| 10-01  Autopilot Engage C | 2  | 0  | Both may be inoperative provided:     |

|        Switches (Bat      |    |    |     a) Associated autopilot is        |

|        Handles) (Analog   |    |    |        considered inoperative, and    |

|        AFCS)              |    |    |     b) Approach minimums do not       |

|                           |    |    |        require autopilot use, and     |

|                           |    |    |     c) Enroute operations do not      |

|                           |    |    |        require its use.               |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

| --------------------------------------------------------------------------- |

| AIRCRAFT:                                | REVISION NO: 24       | PAGE:    |

|             Lockheed L-1011              |                       |          |

|                                          | DATE: 08/24/2000      | 22-6     |

| --------------------------------------------------------------------------- |

|                        1. | 2. NUMBER INSTALLED                             |

| SYSTEM &                  |    -------------------------------------------- |

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

| NUMBERS                   |    |    --------------------------------------- |

| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |

| 22  AUTO FLIGHT           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 10-02  Nav Mode Select  B | 2  | 1  | (O)One may be inoperative provided:   |

|        Panels (Analog     |    |    |     a) Affected knob properly         |

|        AFCS) COURSE 1,    |    |    |        controls associated HSI        |

|        2 Set Knob         |    |    |        Course Pointer or glare-       |

|                           |    |    |        shield panel course display,   |

|                           |    |    |     b) VOR SPLIT-1-2 function is      |

|                           |    |    |        operative,                     |

|                           |    |    |     c) RDDMI VOR function is          |

|                           |    |    |        operative for bearing to       |

|                           |    |    |        station display on             |

|                           |    |    |        associated pilot's panel,      |

|                           |    |    |        and                            |

|                           |    |    |     d) Airplane is operated in VMC    |

|                           |    |    |        only.                          |

|                           |    |    |                                       |

| 10-03  AFCS Mode        C | -  | 0  | (O)May be inoperative provided        |

|        Selectors          |    |    | approach minimums do not require      |

|        (Analog AFCS) TM   |    |    | its use.                              |

|        (THR MGT) VS ALT   |    |    |                                       |

|        IAS VNAV or MACH   |    |    | NOTE 1:  See AFM Procedures for       |

|        HDG TURB A/L APR   |    |    |          Approach and Landing         |

|        LOC NAV            |    |    |          equipment requirements.      |

|        GLARESHIELD        |    |    |                                       |

|        VERTICAL SPEED     |    |    | NOTE 2:  ALT Mode Selector must be    |

|        INDICATOR          |    |    |          operative where enroute      |

|                           |    |    |          operations require its       |

|                           |    |    |          use.                         |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

| --------------------------------------------------------------------------- |

| AIRCRAFT:                                | REVISION NO: 24       | PAGE:    |

|             Lockheed L-1011              |                       |          |

|                                          | DATE: 08/24/2000      | 22-7     |

| --------------------------------------------------------------------------- |

|                        1. | 2. NUMBER INSTALLED                             |

| SYSTEM &                  |    -------------------------------------------- |

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

| NUMBERS                   |    |    --------------------------------------- |

| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |

| 22  AUTO FLIGHT           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 10-05  AFCS Mode        C | -  | 0  | (O)May be inoperative provided:       |

|        Annunciators       |    |    |     a) Associated AFCS Mode or        |

|                           |    |    |        engage switchlight is          |

|      1) Analog AFCS       |    |    |        operative, and                 |

|         HDG SEL V NAV     |    |    |     b) Approach minimums do not       |

|         R NAV   VS        |    |    |        require use of associated      |

|         TURB    IAS       |    |    |        annunciator.                   |

|         THR MGT MACH      |    |    |                                       |

|         TEST    RNAV      |    |    | NOTE:  See AFM Procedures for         |

|         ARM     CAPTURE   |    |    |        approach and landing           |

|         WINDSHEAR         |    |    |        equipment requirements.        |

|                           |    |    |                                       |

|      2) Digital AFCS      |    |    |                                       |

|         HDG     V NAV     |    |    |                                       |

|         VS      TURB      |    |    |                                       |

|         M/IAS   THR MGT   |    |    |                                       |

|         INS     BCK CRS   |    |    |                                       |

|         RNAV    ARM       |    |    |                                       |

|         CAPTURE           |    |    |                                       |

|         WINDSHEAR         |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

| --------------------------------------------------------------------------- |

| AIRCRAFT:                                | REVISION NO: 24       | PAGE:    |

|             Lockheed L-1011              |                       |          |

|                                          | DATE: 08/24/2000      | 22-8     |

| --------------------------------------------------------------------------- |

|                        1. | 2. NUMBER INSTALLED                             |

| SYSTEM &                  |    -------------------------------------------- |

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

| NUMBERS                   |    |    --------------------------------------- |

| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |

| 22  AUTO FLIGHT           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 10-06  AFCS Warning       |    |    |                                       |

|        Annunciators       |    |    |                                       |

|                           |    |    |                                       |

|      1) ALERT Lights    C | 2  | 1  | First Officer's may be inoperative    |

|                           |    |    | provided:                             |

|                           |    |    |     a) All remaining AFCS Warning     |

|                           |    |    |        Annunciators on both           |

|                           |    |    |        indicators are operative,      |

|                           |    |    |        and                            |

|                           |    |    |     b) Enroute operations do not      |

|                           |    |    |        require its use.               |

|                           |    |    |                                       |

|                         C | 2  | 0  | Both may be inoperative provided:     |

|                           |    |    |     a) Both Autopilot Systems are     |

|                           |    |    |        considered inoperative and     |

|                           |    |    |        not used,                      |

|                           |    |    |     b) ATS/AT/TM Systems are          |

|                           |    |    |        considered inoperative,        |

|                           |    |    |     c) Approach minimums do not       |

|                           |    |    |        require use of Autopilot,      |

|                           |    |    |        Autothrottle or Speed          |

|                           |    |    |        Control Systems, and           |

|                           |    |    |     d) Enroute operations do not      |

|                           |    |    |        require its use.               |

|                           |    |    |                                       |

|      2) AP DISC         C | 2  | 0  | Except where enroute operations     ] |

|                           |    |    | require its use both may be           |

|                           |    |    | inoperative provided Captain's        |

|                           |    |    | ALERT light and autopilot           ] |

|                           |    |    | disconnect aural warning is           |

|                           |    |    | operative.                            |

|                           |    |    |                                       |

|                         C | 2  | 0  | Except where enroute operations     ] |

|                           |    |    | require its use both may be         ] |

|                           |    |    | inoperative provided both Autopilot ] |

|                           |    |    | Systems are considered inoperative.   |

|                           |    |    |                                       |

|                           |    |    |       (Continued)                     |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

| --------------------------------------------------------------------------- |

| AIRCRAFT:                                | REVISION NO: 24       | PAGE:    |

|             Lockheed L-1011              |                       |          |

|                                          | DATE: 08/24/2000      | 22-9     |

| --------------------------------------------------------------------------- |

|                        1. | 2. NUMBER INSTALLED                             |

| SYSTEM &                  |    -------------------------------------------- |

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

| NUMBERS                   |    |    --------------------------------------- |

| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |

| 22  AUTO FLIGHT           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 10-06  AFCS Warning       |    |    |                                       |

|        Annunciators       |    |    |                                       |

|         (cont'd)          |    |    |                                       |

|                           |    |    |                                       |

|     3) NO DUAL          C | 2  | 0  | Both may be inoperative provided      |

|                           |    |    | approach minimums do not require      |

|                           |    |    | use of dual autoland.                 |

|                           |    |    |                                       |

|                           |    |    |                                       |

|      4) AP LIMIT        C | 2  | 0  | Except where enroute operations     ] |

|                           |    |    | require its use both may be           |

|                           |    |    | inoperative provided Associated       |

|                           |    |    | Auto-Trim Out-of-Trim Warning         |

|                           |    |    | Indicators are operative.             |

|                           |    |    |                                       |

|                         C | 2  | 0  | Except where enroute operations     ] |

|                           |    |    | require its use both may be         ] |

|                           |    |    | inoperative provided both Autopilot   |

|                           |    |    | Systems are considered inoperative.   |

|                           |    |    |                                       |

|      5) NO ALIGN        C | 2  | 0  | Both may be inoperative provided      |

|                           |    |    | approach minimums do not require      |

|                           |    |    | use of Align mode.                    |

|                           |    |    |                                       |

|      6) ATS DISC        C | 2  | 1  | One may be inoperative provided       |

|                           |    |    | both ALERT Lights are operative.      |

|                           |    |    |                                       |

|                         C | 2  | 0  | Both may be inoperative provided      |

|                           |    |    | ATS/AT/TM Systems are considered      |

|                           |    |    | inoperative.                          |

|                           |    |    |                                       |

|      7) NO GA           C | 2  | 1  | First Officer's may be inoperative    |

|                           |    |    | provided both ALERT Lights are        |

|                           |    |    | operative.                            |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

| --------------------------------------------------------------------------- |

| AIRCRAFT:                                | REVISION NO: 24       | PAGE:    |

|             Lockheed L-1011              |                       |          |

|                                          | DATE: 08/24/2000      | 22-10    |

| --------------------------------------------------------------------------- |

|                        1. | 2. NUMBER INSTALLED                             |

| SYSTEM &                  |    -------------------------------------------- |

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

| NUMBERS                   |    |    --------------------------------------- |

| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |

| 22  AUTO FLIGHT           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 10-06  AFCS Warning     C | 2  | 0  | Both may be inoperative provided      |

|        Annunciators       |    |    | automatic go-around placarded         |

|                           |    |    | inoperative and not used.             |

|      7) NO GA             |    |    |                                       |

|         (Cont'd)          |    |    | (Continued)                           |

|                           |    |    |                                       |

|      8) SPLIT (Digital  C | 2  | 1  | First Officer's may be inoperative    |

|         AFCS)             |    |    | provided both ALERT Lights are        |

|                           |    |    | operative.                            |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                         C | 2  | 0  | Both may be inoperative provided      |

|                           |    |    | all AFCS Mode Annunciators are        |

|                           |    |    | operative.                            |

|                           |    |    |                                       |

|                           |    |    |                                       |

|      9) NO FLARE        C | 2  | 0  |                                       |

|         (Analog AFCS)     |    |    |                                       |

|                           |    |    |                                       |

|      10)  CMD DISC      C | 2  | 1  | First Officer's may be inoperative    |

|                           |    |    | provided:                             |

|                           |    |    |     a) Both ALERT Lights are          |

|                           |    |    |        operative, and                 |

|                           |    |    |     b) Enroute operations do not      |

|                           |    |    |        require its use.               |

|                           |    |    |                                       |

|                         C | 2  | 0  | Both may be inoperative provided:     |

|                           |    |    |     a) Both Autopilot Systems are     |

|                           |    |    |        considered inoperative, and    |

|                           |    |    |     b) Enroute operations do not      |

|                           |    |    |        require its use.               |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

| --------------------------------------------------------------------------- |

| AIRCRAFT:                                | REVISION NO: 24       | PAGE:    |

|             Lockheed L-1011              |                       |          |

|                                          | DATE: 08/24/2000      | 22-11    |

| --------------------------------------------------------------------------- |

|                        1. | 2. NUMBER INSTALLED                             |

| SYSTEM &                  |    -------------------------------------------- |

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

| NUMBERS                   |    |    --------------------------------------- |

| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |

| 22  AUTO FLIGHT           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 10-07  Flight Control     |    |    |                                       |

|        Electronic         |    |    |                                       |

|        Systems (FCES)     |    |    |                                       |

|        Panel              |    |    |                                       |

|        Switchlights       |    |    |                                       |

|                           |    |    |                                       |

|      1) Pitch Trim/     C | 6  | 0  |                                       |

|         Mach Trim/ATS     |    |    |                                       |

|         OFF Lights        |    |    |                                       |

|                           |    |    |                                       |

|      2) Pitch Trim/     C | -  | 0  | May be inoperative provided           |

|         Mach Trim/ATS/    |    |    | associated FCES Channel is            |

|         MDLC/DLC/Auto     |    |    | considered inoperative and is not     |

|         SPLR FAIL         |    |    | engaged.                              |

|         Lights            |    |    |                                       |

|                           |    |    |                                       |

|      3) YAW FIRST FAIL  C | 1  | 0  | May be inoperative provided two YAW   |

|         Light (-3)        |    |    | SAS Channels are operative.           |

|                           |    |    |                                       |

| 10-12  Flight Control   C | 15 | 0  | (M)May be inoperative provided:       |

|        Auxiliary Unit     |    |    |     a) Surface Position Indicator     |

|        (FCAU) Switches    |    |    |        (SPI) System is operative,     |

|        and Status Fault   |    |    |        and                            |

|        Lights             |    |    |     b) Affected switch or status/     |

|                           |    |    |        fault light does not render    |

|                           |    |    |        any other system or            |

|                           |    |    |        equipment inoperative.         |

|                           |    |    |                                       |

| 10-21  Autopilot        C | -  | -  | One may be inoperative provided the   |

|        Disconnect         |    |    | autopilot is not utilized at less     |

|        Switches           |    |    | than initial approach altitude.       |

|        (Control Wheel)    |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

| --------------------------------------------------------------------------- |

| AIRCRAFT:                                | REVISION NO: 24       | PAGE:    |

|             Lockheed L-1011              |                       |          |

|                                          | DATE: 08/24/2000      | 22-12    |

| --------------------------------------------------------------------------- |

|                        1. | 2. NUMBER INSTALLED                             |

| SYSTEM &                  |    -------------------------------------------- |

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

| NUMBERS                   |    |    --------------------------------------- |

| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |

| 22  AUTO FLIGHT           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 10-22  TO/GA Switches   C | 2  | 1  | (O)May be inoperative provided:     ] |

|                           |    |    |     a) Inoperative switch is at the ] |

|                           |    |    |        Pilot Not Flying (PNF)       ] |

|                           |    |    |        position, and                ] |

|                           |    |    |     b) Approach minimums do not     ] |

|                           |    |    |        require its use.             ] |

|                           |    |    |                                       |

| 10-24  ILS Deviation    C | 2  | 0  |                                       |

|        Lights             |    |    |                                       |

|                           |    |    |                                       |

| 11-00  Autopilot and      |    |    |                                       |

|        Flight Director    |    |    |                                       |

|        Pitch Systems      |    |    |                                       |

|        (Digital AFCS)     |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|      1) Pitch Axis      C | 2  | 0  | Both may be inoperative provided:     |

|         Channels          |    |    |     a) Associated APFDS is            |

|                           |    |    |        considered inoperative, and    |

|                           |    |    |     b) Enroute operations do not      |

|                           |    |    |        require its use.               |

|                           |    |    |                                       |

| 11-01  Pitch AFCS       C | 2  | 0  | Both may be inoperative provided:     |

|        Computers          |    |    |     a) Associated APFDS is            |

|        (Analog AFCS)      |    |    |        considered inoperative, and    |

|                           |    |    |     b) Enroute operations do not      |

|                           |    |    |        require its use.               |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

| --------------------------------------------------------------------------- |

| AIRCRAFT:                                | REVISION NO: 24       | PAGE:    |

|             Lockheed L-1011              |                       |          |

|                                          | DATE: 08/24/2000      | 22-13    |

| --------------------------------------------------------------------------- |

|                        1. | 2. NUMBER INSTALLED                             |

| SYSTEM &                  |    -------------------------------------------- |

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

| NUMBERS                   |    |    --------------------------------------- |

| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |

| 22  AUTO FLIGHT           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 11-03  Altitude Alert     |    |    |                                       |

|        Systems (Analog    |    |    |                                       |

|        and Digital        |    |    |                                       |

|        AFCS)              |    |    |                                       |

|                           |    |    |                                       |

|      1) NORM and STBY   A | 2  | 0  | (O)Both may be inoperative            |

|         Modes             |    |    | provided:                             |

|                           |    |    |     a) Autopilot with altitude hold   |

|                           |    |    |        is operative,                  |

|                           |    |    |     b) Operators are limited to       |

|                           |    |    |        not more than three            |

|                           |    |    |        flight days before             |

|                           |    |    |        repairs are made, and          |

|                           |    |    |     c) Enroute operations do not      |

|                           |    |    |        require its use.               |

|                           |    |    |                                       |

|                         C | 2  | 1  | (O)One may be inoperative provided:   |

|                           |    |    |     a) Remaining system is verified   |

|                           |    |    |        operative before each          |

|                           |    |    |        takeoff,                       |

|                           |    |    |     b) All altitude alert functions   |

|                           |    |    |        of operative system            |

|                           |    |    |        (altitude select, alert        |

|                           |    |    |        lights, and aural signal)      |

|                           |    |    |        are operative, and             |

|                           |    |    |     c) Enroute operations do not      |

|                           |    |    |        require its use.               |

|                           |    |    |                                       |

|      2) Autopilot and   C | 2  | 0  | May be inoperative except where       |

|         Flight Director   |    |    | enroute operations require its use.   |

|         Altitude          |    |    |                                       |

|         Capture           |    |    |                                       |

|         Functions         |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

| --------------------------------------------------------------------------- |

| AIRCRAFT:                                | REVISION NO: 24       | PAGE:    |

|             Lockheed L-1011              |                       |          |

|                                          | DATE: 08/24/2000      | 22-14    |

| --------------------------------------------------------------------------- |

|                        1. | 2. NUMBER INSTALLED                             |

| SYSTEM &                  |    -------------------------------------------- |

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

| NUMBERS                   |    |    --------------------------------------- |

| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |

| 22  AUTO FLIGHT           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 11-05  Autopilot Pitch  C | 2  | 0  | Both may be inoperative provided:     |

|        Servos (Dual       |    |    |     a) Associated APFDS is            |

|        Servo Assembly)    |    |    |        considered inoperative, and    |

|                           |    |    |     b) Enroute operations do not      |

|                           |    |    |        require its use.               |

|                           |    |    |                                       |

| 13-00  Autopilot and    C | 2  | 0  | Both may be inoperative provided:     |

|        Flight Director    |    |    |     a) Associated APFDS is            |

|        Roll Axis          |    |    |        considered inoperative, and    |

|        Channels           |    |    |     b) Enroute operations do not      |

|        (Digital AFCS)     |    |    |        require its use.               |

|                           |    |    |                                       |

| 13-01  Roll AFCS        C | 2  | 0  | Both may be inoperative provided:     |

|        Computers          |    |    |     a) Associated APFDS is            |

|        (Analog AFCS)      |    |    |        considered inoperative, and    |

|                           |    |    |     b) Enroute operations do not      |

|                           |    |    |        require its use.               |

|                           |    |    |                                       |

| 13-02  Roll Lateral     C | 3  | 0  | (M)(O)All may be inoperative          |

|        Accelerometers     |    |    | provided approach minimums do not     |

|        (Triple)           |    |    | require use of APFDS modes which      |

|                           |    |    | are rendered inoperative.             |

|                           |    |    |                                       |

|                           |    |    | NOTE: Modes rendered inoperative:     |

|                           |    |    | (Analog AFCS)  (Digital AFCS)         |

|                           |    |    |      A/L            ILS               |

|                           |    |    |      APR                              |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

| --------------------------------------------------------------------------- |

| AIRCRAFT:                                | REVISION NO: 24       | PAGE:    |

|             Lockheed L-1011              |                       |          |

|                                          | DATE: 08/24/2000      | 22-15    |

| --------------------------------------------------------------------------- |

|                        1. | 2. NUMBER INSTALLED                             |

| SYSTEM &                  |    -------------------------------------------- |

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

| NUMBERS                   |    |    --------------------------------------- |

| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |

| 22  AUTO FLIGHT           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 13-03  Roll AFCS        C | 2  | 1  | (M)(O)One may be inoperative          |

|        Transducers        |    |    | provided:                             |

|        (Left Inboard      |    |    |     a) Associated autopilot is        |

|        Aileron)           |    |    |        considered inoperative and     |

|                           |    |    |        is not used, and               |

|                           |    |    |     b) YAW SAS Channel is             |

|                           |    |    |        operative.                     |

|                           |    |    |                                       |

|                           |    |    | NOTE 1:  Digital AFCS - Do not pull   |

|                           |    |    |          associated AFCS CMPTR        |

|                           |    |    |          circuit breaker, since       |

|                           |    |    |          that will activate ACS       |

|                           |    |    |          FIRST FAIL annunciator       |

|                           |    |    |          light. Associated Altitude   |

|                           |    |    |          Alert System and             |

|                           |    |    |          Autothrottle System          |

|                           |    |    |          Channel will be rendered     |

|                           |    |    |          inoperative.                 |

|                           |    |    |                                       |

|                           |    |    | NOTE 2:  Analog AFCS - Do not pull    |

|                           |    |    |          associated YAW SAS circuit   |

|                           |    |    |          breaker, since that will     |

|                           |    |    |          activate ACS FIRST FAIL      |

|                           |    |    |          annunciator light.           |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

| --------------------------------------------------------------------------- |

| AIRCRAFT:                                | REVISION NO: 24       | PAGE:    |

|             Lockheed L-1011              |                       |          |

|                                          | DATE: 08/24/2000      | 22-16    |

| --------------------------------------------------------------------------- |

|                        1. | 2. NUMBER INSTALLED                             |

| SYSTEM &                  |    -------------------------------------------- |

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

| NUMBERS                   |    |    --------------------------------------- |

| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |

| 22  AUTO FLIGHT           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 15-00  YAW SAS          C | 2  | 1  | (O)One may be inoperative provided    |

|        Computers          |    |    | approach minimums do not require      |

|        (Analog AFCS) or   |    |    | its use.                              |

|        YAW SAS Channels   |    |    |                                       |

|        (Digital AFCS)     |    |    | NOTE 1:  Digital AFCS - Do not pull   |

|                           |    |    |          associated AFCS CMPTR        |

|                           |    |    |          circuit breaker, since       |

|                           |    |    |          that will activate ACS       |

|                           |    |    |          FIRST FAIL annunciator       |

|                           |    |    |          light. Associated Altitude   |

|                           |    |    |          Alert System and             |

|                           |    |    |          Autothrottle System          |

|                           |    |    |          Channel will be rendered     |

|                           |    |    |          inoperative.                 |

|                           |    |    |                                       |

|                           |    |    | NOTE 2:  Analog AFCS - Do not pull    |

|                           |    |    |          associated YAW SAS circuit   |

|                           |    |    |          breaker, since that will     |

|                           |    |    |          activate ACS FIRST FAIL      |

|                           |    |    |          annunciator light.           |

|                           |    |    |                                       |

|                           |    |    | NOTE 3:  Depending on failure:        |

|                           |    |    |          1. Associated APFDS may be   |

|                           |    |    |          inoperative. Dispatch in     |

|                           |    |    |          accordance with MMEL. 2.     |

|                           |    |    |          Some AFCS Mode               |

|                           |    |    |          Annunciators or AFCS         |

|                           |    |    |          Warning Annunciators on      |

|                           |    |    |          the associated side may be   |

|                           |    |    |          inoperative. Dispatch in     |

|                           |    |    |          accordance with MMEL.        |

|                           |    |    |                                       |

|                           |    |    | NOTE 4:  See AFM Procedures for       |

|                           |    |    |          approach and landing         |

|                           |    |    |          equipment requirements.      |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

| --------------------------------------------------------------------------- |

| AIRCRAFT:                                | REVISION NO: 24       | PAGE:    |

|             Lockheed L-1011              |                       |          |

|                                          | DATE: 08/24/2000      | 22-17    |

| --------------------------------------------------------------------------- |

|                        1. | 2. NUMBER INSTALLED                             |

| SYSTEM &                  |    -------------------------------------------- |

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

| NUMBERS                   |    |    --------------------------------------- |

| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |

| 22  AUTO FLIGHT           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 15-02  Yaw Rate Gyros   C | 3  | 2  | One may be inoperative provided       |

|                           |    |    | approach minimums do not require      |

|                           |    |    | dual autopilot use.                   |

|                           |    |    |                                       |

|                           |    |    | NOTE 1:  For analog autopilots,       |

|                           |    |    |          DUAL A/L NOT AVAIL light     |

|                           |    |    |          on Caution/Warning Panel     |

|                           |    |    |          will be illuminated.         |

|                           |    |    |                                       |

|                           |    |    | NOTE 2:  For digital autopilots,      |

|                           |    |    |          the APFDS FIRST FAIL light   |

|                           |    |    |          on the Caution/Warning       |

|                           |    |    |          Panel will be illuminated.   |

|                           |    |    |                                       |

|                           |    |    | NOTE 3:  See AFM Procedures for       |

|                           |    |    |          approach and landing         |

|                           |    |    |          equipment requirements.      |

|                           |    |    |                                       |

| 15-03  Rudder Position  C | 2  | 0  | Both may be inoperative provided      |

|        Transducers        |    |    | approach minimums do not require      |

|        (Dual)             |    |    | use of ALIGN or ROLLOUT modes.        |

|                           |    |    |                                       |

| 17-00  Spoiler Control    |    |    |                                       |

|        Systems            |    |    |                                       |

|                           |    |    |                                       |

|      1) Direct Lift     C | 2  | 0  | (O)Both may be inoperative            |

|         Control (DLC)     |    |    | provided:                             |

|         Systems (-1,      |    |    |     a) Affected Auto Ground Spoiler   |

|         -14, -15)         |    |    |        System is considered           |

|                           |    |    |        inoperative, and               |

|                           |    |    |     b) Approach minimums do not       |

|                           |    |    |        require use of autoland.       |

|                           |    |    |                                       |

|                           |    |    | NOTE:  See AFM Performance when       |

|                           |    |    |        operating with both DLC        |

|                           |    |    |        Systems inoperative.           |

|                           |    |    |                                       |

|                           |    |    |         (Continued)                   |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

| --------------------------------------------------------------------------- |

| AIRCRAFT:                                | REVISION NO: 24       | PAGE:    |

|             Lockheed L-1011              |                       |          |

|                                          | DATE: 08/24/2000      | 22-18    |

| --------------------------------------------------------------------------- |

|                        1. | 2. NUMBER INSTALLED                             |

| SYSTEM &                  |    -------------------------------------------- |

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

| NUMBERS                   |    |    --------------------------------------- |

| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |

| 22  AUTO FLIGHT           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 17-00  Spoiler Control    |    |    |                                       |

|        Systems (Cont'd)   |    |    |                                       |

|                           |    |    |                                       |

|      2) Direct Lift     C | 2  | 0  | (M)(O)Both Direct Lift Control        |

|         Control (DLC)     |    |    | Channels may be inoperative           |

|         Systems (-3)      |    |    | provided:                             |

|                           |    |    |     a) Affected Auto Ground Spoiler   |

|                           |    |    |        System is considered           |

|                           |    |    |        inoperative.                   |

|                           |    |    |     b) Approach minimums do not       |

|                           |    |    |        require use of Autoland.       |

|                           |    |    |                                       |

|                           |    |    | NOTE 1:  See AFM Performance when     |

|                           |    |    |          operation with both          |

|                           |    |    |          DLC/MDLC Systems             |

|                           |    |    |          inoperative.                 |

|                           |    |    |                                       |

|                           |    |    | NOTE 2:  See AFM Procedures for       |

|                           |    |    |          approach and landing         |

|                           |    |    |          equipment requirements.      |

|                           |    |    |                                       |

|                           |    |    | NOTE 3:  DLC/AUTO SPLR switchlights   |

|                           |    |    |          must be latched in to        |

|                           |    |    |          provide circuits for         |

|                           |    |    |          G-Sensitive Stick Shaker     |

|                           |    |    |          unless dispatch is in        |

|                           |    |    |          accordance with MMEL         |

|                           |    |    |          G-Sensitive Stick Shaker     |

|                           |    |    |          inoperative provisos         |

|                           |    |    |          22-17-01.                    |

|                           |    |    |                                       |

|                           |    |    |          (Continued)                  |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

| --------------------------------------------------------------------------- |

| AIRCRAFT:                                | REVISION NO: 24       | PAGE:    |

|             Lockheed L-1011              |                       |          |

|                                          | DATE: 08/24/2000      | 22-19    |

| --------------------------------------------------------------------------- |

|                        1. | 2. NUMBER INSTALLED                             |

| SYSTEM &                  |    -------------------------------------------- |

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

| NUMBERS                   |    |    --------------------------------------- |

| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |

| 22  AUTO FLIGHT           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 17-00  Spoiler Control    |    |    |                                       |

|        Systems (Cont'd)   |    |    |                                       |

|                           |    |    |                                       |

|        3) Maneuvering   C | 2  | 0  | (M)(O)Both Maneuvering Direct Lift    |

|           Direct Lift     |    |    | Control Channels may be inoperative   |

|           Control         |    |    | provided affected system is           |

|           (MDLC)          |    |    | deactivated.                          |

|           Systems (-3)    |    |    |                                       |

|                           |    |    | NOTE 1:  With MDLC deactivated        |

|                           |    |    |          Auto Ground spoiler System   |

|                           |    |    |          will be inoperative.         |

|                           |    |    |                                       |

|                           |    |    | NOTE 2:  See AFM Limitation and       |

|                           |    |    |          Performance for operation    |

|                           |    |    |          with DLC/MDLC inoperative.   |

|                           |    |    |                                       |

|                           |    |    | NOTE 3:  See AFM Procedures for       |

|                           |    |    |          approach and landing         |

|                           |    |    |          equipment requirements.      |

|                           |    |    |                                       |

|                           |    |    | NOTE 4:  DLC/AUTO SPLR switchlights   |

|                           |    |    |          must be latched in to        |

|                           |    |    |          provide circuits for         |

|                           |    |    |          G-Sensitive Stick Shakers    |

|                           |    |    |          unless dispatch is in        |

|                           |    |    |          accordance with MMEL         |

|                           |    |    |          G-Sensitive Stick Shaker     |

|                           |    |    |          inoperative provisos         |

|                           |    |    |          22-17-01.                    |

|                           |    |    |                                       |

|                           |    |    | NOTE 5:  DLC/AUTO SPLR FAIL light     |

|                           |    |    |          may be illuminated on        |

|                           |    |    |          inoperative system.          |

|                           |    |    |                                       |

|                           |    |    | NOTE 6:  No movement of speed brake   |

|                           |    |    |          handle will occur during     |

|                           |    |    |          MDLC TEST of inoperative     |

|                           |    |    |          system.                      |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

| --------------------------------------------------------------------------- |

| AIRCRAFT:                                | REVISION NO: 24       | PAGE:    |

|             Lockheed L-1011              |                       |          |

|                                          | DATE: 08/24/2000      | 22-20    |

| --------------------------------------------------------------------------- |

|                        1. | 2. NUMBER INSTALLED                             |

| SYSTEM &                  |    -------------------------------------------- |

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

| NUMBERS                   |    |    --------------------------------------- |

| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |

| 22  AUTO FLIGHT           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 17-00  Spoiler Control    |    |    |                                       |

|        Systems (Cont'd)   |    |    |                                       |

|                           |    |    |                                       |

|      4) Auto Ground     C | 2  | 0  | (M)(O)Both may be inoperative         |

|         Spoiler (AGS)     |    |    | provided 'on -3 aircraft' MDLC        |

|         System            |    |    | System is verified operative before   |

|                           |    |    | each flight.                          |

|                           |    |    |                                       |

|                           |    |    | NOTE:  See AFM Performance for        |

|                           |    |    |        operation with AGS System      |

|                           |    |    |        inoperative and landing with   |

|                           |    |    |        33 degrees or greater flap     |

|                           |    |    |        setting.                       |

|                           |    |    |                                       |

| 17-01  G-Sensitive      B | 2  | 0  | (M)(O)Both may be inoperative         |

|        Stick Shaker       |    |    | provided:                             |

|        Channels           |    |    |     a) Associated airspeed            |

|        (Activation        |    |    |        indicator is reset for 270     |

|        Circuit) (-3)      |    |    |        KTS warning, and               |

|                           |    |    |     b) Airplane is operated at        |

|                           |    |    |        FL370 or below.                |

|                           |    |    |                                       |

|                           |    |    | NOTE:  See AFM Limitations for        |

|                           |    |    |        operation with either one or   |

|                           |    |    |        two G-Sensitive Stick          |

|                           |    |    |        Shakers inoperative.           |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

| --------------------------------------------------------------------------- |

| AIRCRAFT:                                | REVISION NO: 24       | PAGE:    |

|             Lockheed L-1011              |                       |          |

|                                          | DATE: 08/24/2000      | 22-21    |

| --------------------------------------------------------------------------- |

|                        1. | 2. NUMBER INSTALLED                             |

| SYSTEM &                  |    -------------------------------------------- |

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

| NUMBERS                   |    |    --------------------------------------- |

| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |

| 22  AUTO FLIGHT           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 17-02  Primary Flight     |    |    |                                       |

|        Control System     |    |    |                                       |

|        (PFCS) Monitors    |    |    |                                       |

|                           |    |    |                                       |

|      1) Roll Channels   C | 2  | 1  | (O)One may be inoperative provided:   |

|                           |    |    |     a) Associated channel switch-     |

|                           |    |    |        light remains OFF,             |

|                           |    |    |     b) Surface Position Indicating    |

|                           |    |    |        System is operative, and       |

|                           |    |    |     c) Operative channel switch-      |

|                           |    |    |        light is latched IN, and       |

|                           |    |    |        FAIL and OFF lights are        |

|                           |    |    |        operative.                     |

|                           |    |    |                                       |

|      2) Pitch Channels  C | 2  | 1  | (M)(O)One may be inoperative          |

|                           |    |    | provided:                             |

|                           |    |    |     a) Associated channel switch-     |

|                           |    |    |        light remains OFF,             |

|                           |    |    |     b) Surface Position Indicating    |

|                           |    |    |        System is operative,           |

|                           |    |    |     c) Operative channel switch-      |

|                           |    |    |        light is latched IN, and       |

|                           |    |    |        FAIL and OFF Lights are        |

|                           |    |    |        operative, and                 |

|                           |    |    |     d) Jam and Open Cable Detectors   |

|                           |    |    |        of the operative channel are   |

|                           |    |    |        verified operative before      |

|                           |    |    |        the first flight of each       |

|                           |    |    |        day.                           |

|                           |    |    |                                       |

| 18-00  Trim               |    |    |                                       |

|        Augmentation       |    |    |                                       |

|        Systems            |    |    |                                       |

|                           |    |    |                                       |

|      1) Proportional/   C | 2  | 1  | (O)One may be inoperative provided    |

|         Auto Pitch Trim   |    |    | Auto-Trim is monitored during Auto    |

|         System Channels   |    |    | Pilot use.                            |

|                           |    |    |                                       |

|                           |    |    |         (continued)                   |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

| --------------------------------------------------------------------------- |

| AIRCRAFT:                                | REVISION NO: 24       | PAGE:    |

|             Lockheed L-1011              |                       |          |

|                                          | DATE: 08/24/2000      | 22-22    |

| --------------------------------------------------------------------------- |

|                        1. | 2. NUMBER INSTALLED                             |

| SYSTEM &                  |    -------------------------------------------- |

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

| NUMBERS                   |    |    --------------------------------------- |

| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |

| 22  AUTO FLIGHT           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 18-00  Trim               |    |    |                                       |

|        Augmentation       |    |    |                                       |

|        Systems            |    |    |                                       |

|        (cont'd)           |    |    |                                       |

|                           |    |    |                                       |

|      2) Surface         C | 2  | 0  | (O)Both may be inoperative provided   |

|         Position          |    |    | Auto-Trim is monitored during Auto    |

|         Indicator         |    |    | Pilot use.                            |

|         Auto-Trim         |    |    |                                       |

|         Out-of-Trim       |    |    |                                       |

|         Warning           |    |    |                                       |

|         Indicators        |    |    |                                       |

|                           |    |    |                                       |

| 21-01  Mach Trim System C | 2  | 1  | (O)One may be inoperative provided    |

|        Channels           |    |    | one autopilot is operative.           |

|                           |    |    |                                       |

|                         C | 2  | 0  | (O)Both may be inoperative provided   |

|                           |    |    | both autopilots are operative.        |

|                           |    |    |                                       |

|                           |    |    | NOTE:  See AFM Limitations for        |

|                           |    |    |        operation with both Mach       |

|                           |    |    |        Trim Systems inoperative.      |

|                           |    |    |                                       |

| 21-02  Mach Feel System C | 2  | 1  | (O)One may be inoperative provided:   |

|        Channels           |    |    |     a) Operative channel switch-      |

|                           |    |    |        light is latched IN, and       |

|                           |    |    |     b) FAIL and OFF Lights are        |

|                           |    |    |        operative.                     |

|                           |    |    |                                       |

|                           |    |    | NOTE:  See AFM Limitations for        |

|                           |    |    |        operational information        |

|                           |    |    |        should operative channel       |

|                           |    |    |        fail enroute.                  |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

| --------------------------------------------------------------------------- |

| AIRCRAFT:                                | REVISION NO: 24       | PAGE:    |

|             Lockheed L-1011              |                       |          |

|                                          | DATE: 08/24/2000      | 22-23    |

| --------------------------------------------------------------------------- |

|                        1. | 2. NUMBER INSTALLED                             |

| SYSTEM &                  |    -------------------------------------------- |

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

| NUMBERS                   |    |    --------------------------------------- |

| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |

| 22  AUTO FLIGHT           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 31-00  Autothrottle     C | 2  | 0  | (M)(O)Both may be inoperative         |

|        System (ATS)       |    |    | provided:                             |

|        Channels (Analog   |    |    |     a) Approach minimums do not re-   |

|        AFCS) or           |    |    |        quire use of associated        |

|        Autothrottle and   |    |    |        autothrottle system, and       |

|        Thrust             |    |    |     b) Throttle handling              |

|        Management         |    |    |        characteristics are not        |

|        System (AT & TM)   |    |    |        adversely affected (binding,   |

|        Channels           |    |    |        creeping, etc.) by ATS or AT   |

|        (Digital AFCS)     |    |    |        and TM deactivation.           |

|                           |    |    |                                       |

|                           |    |    | NOTE:  With AT & TM Channels          |

|                           |    |    |        inoperative associated Speed   |

|                           |    |    |        Control System SLO-FAST        |

|                           |    |    |        indication will be             |

|                           |    |    |        inoperative.                   |

|                           |    |    |                                       |

| 31-05  Longitudinal     C | 2  | 0  | (O)Both may be inoperative            |

|        Accelerometers     |    |    | provided:                             |

|                           |    |    |     a) Associated ATS or AT & TM      |

|                           |    |    |        Channel is considered          |

|                           |    |    |        inoperative,                   |

|                           |    |    |     b) Associated TO & GA modes are   |

|                           |    |    |        considered inoperative, and    |

|                           |    |    |     c) Automatic Braking System is    |

|                           |    |    |        considered inoperative.        |

|                           |    |    |                                       |

| 31-07  Speed Control    C | 1  | 0  | (O)May be inoperative provided:       |

|        System (SCS)       |    |    |     a) Both Autothrottle System       |

|        Computer (Analog   |    |    |        Channels are considered        |

|        AFCS)              |    |    |        inoperative, and               |

|                           |    |    |     b) Automatic Braking System is    |

|                           |    |    |        considered inoperative.        |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

| --------------------------------------------------------------------------- |

| AIRCRAFT:                                | REVISION NO: 24       | PAGE:    |

|             Lockheed L-1011              |                       |          |

|                                          | DATE: 08/24/2000      | 22-24    |

| --------------------------------------------------------------------------- |

|                        1. | 2. NUMBER INSTALLED                             |

| SYSTEM &                  |    -------------------------------------------- |

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

| NUMBERS                   |    |    --------------------------------------- |

| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |

| 22  AUTO FLIGHT           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 31-08  ATS DISC         C | 2  | 0  | (O)Both may be inoperative provided   |

|        Switches (On       |    |    | Autothrottles are controlled using    |

|        Throttles)         |    |    | glareshield or FCES control           |

|                           |    |    | switches.                             |

|                           |    |    |                                       |

|                           |    |    | NOTE:  ATS or AT & TM may be          |

|                           |    |    |        operated with ATS DISC         |

|                           |    |    |        Switches inoperative.          |

|                           |    |    |                                       |

| 31-09  Flight           C | 1  | 0  |                                       |

|        Management         |    |    |                                       |

|        System Thrust      |    |    |                                       |

|        Management Mode    |    |    |                                       |

|                           |    |    |                                       |

| 40-00  Fault Isolation  C | 1  | 0  |                                       |

|        Data Display       |    |    |                                       |

|        System (FIDDS)     |    |    |                                       |

|        (Digital AFCS)     |    |    |                                       |

|        (-3)               |    |    |                                       |

|                           |    |    |                                       |

| 70-00  Active Control   B | 2  | 1  | (O)One may be inoperative, or an      |

|        System (ACS)       |    |    | ACS FIRST FAIL light may be           |

|        Channels (-3)      |    |    | illuminated provided operations are   |

|                           |    |    | conducted in accordance with          |

|                           |    |    | appropriate AFM appendix.             |

|                           |    |    |                                       |

|                         B | 2  | 0  | (M)(O)Both may be inoperative         |

|                           |    |    | provided operations and maintenance   |

|                           |    |    | are conducted in accordance with      |

|                           |    |    | appropriate AFM appendix.             |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

| --------------------------------------------------------------------------- |

| AIRCRAFT:                                | REVISION NO: 24       | PAGE:    |

|             Lockheed L-1011              |                       |          |

|                                          | DATE: 08/24/2000      | 23-1     |

| --------------------------------------------------------------------------- |

|                        1. | 2. NUMBER INSTALLED                             |

| SYSTEM &                  |    -------------------------------------------- |

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

| NUMBERS                   |    |    --------------------------------------- |

| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |

| 23  COMMUNICATIONS        |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 11-00  Communications   C | -  | -  | As required by FAR. No relief is      |

|        Systems (VHF,      |    |    | provided to an inoperative system     |

|        HF, UHF)           |    |    | or component if powered by an         |

|                           |    |    | emergency bus or equivalent and       |

|                           |    |    | required to accomplish an emergency   |

|                           |    |    | procedure.                            |

|                           |    |    |                                       |

| 11-01  Satellite        C | -  | 0  | (O)May be inoperative provided      ] |

| ***    Communications     |    |    | alternate procedures are            ] |

|        Systems (SATCOM)   |    |    | established and used.               ] |

|                           |    |    |                                       |

|                         D | -  | 0  | May be inoperative provided         ] |

|                           |    |    | procedures do not require its use.  ] |

|                           |    |    |                                       |

| 22-00  Selective Call   C | 2  | 0  | Both may be inoperative provided    ] |

|        (SELCAL) Systems   |    |    | procedures do not require its use.    |

|                           |    |    |                                       |

|                         C | 2  | 0  | Both may be inoperative provided    ] |

|                           |    |    | flight crew continuously monitors   ] |

|                           |    |    | appropriate radio frequencies.        |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

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


 

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

| U.S. DEPARTMENT OF TRANSPORTATION                                           |

|                                                                             |

|                                            MASTER MINIMUM EQUIPMENT LIST    |

| FEDERAL AVIATION ADMINISTRATION                                             |

| --------------------------------------------------------------------------- |

| AIRCRAFT:                                | REVISION NO: 24       | PAGE:    |

|             Lockheed L-1011              |                       |          |

|                                          | DATE: 08/24/2000      | 23-2     |

| --------------------------------------------------------------------------- |

|                        1. | 2. NUMBER INSTALLED                             |

| SYSTEM &                  |    -------------------------------------------- |

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

| NUMBERS                   |    |    --------------------------------------- |

| ------------------------- |    |    | 4. REMARKS OR EXCEPTIONS              |

| 23  COMMUNICATIONS        |    |    |                                       |

|                           |    |    |                                       |

|                           |    |    |                                       |

| 31-00  Passenger          |    |    |                                       |

|        Address (PA)       |    |    |                                       |

|        System             |    |    |                                       |

|                           |    |    |                                       |

|        1) Passenger     B | 1  | 0  | (O)May be inoperative provided:       |

|           Configuration   |    |    |     a) Alternate, normal and          |

|                           |    |    |        emergency procedures, and/or   |

|                           |    |    |        operation restrictions are     |

|                           |    |    |        established and used; and      |

|                           |    |    |     b) Flight Deck/Cabin Interphone   |

|                           |    |    |        system is operative.           |

|                           |    |    |                                       |

|        2) Cargo         C | 1  | 0  | May be inoperative.                   |

|           Configuration   |    |    |                                       |

|                           |    |    |                                       |

| ***    3) STC ST00847AT B | 1  | 0  | (O)May be inoperative provided      ] |

|           ONLY - Cargo    |    |    | alternate procedures are            ] |

|           Configuration   |    |    | established and used.                 |

|                           |    |    |                                       |

|                         C | 1  | 0  | (O)May be inoperative provided      ] |

|                           |    |    | courier area is unoccupied.         ] |

|                           |    |    |                                       |

| 41-00  Interphone         |    |    |                                       |

|        System             |