Date: 10/29/2004

FEDERAL AVIATION ADMINISTRATION

WASHINGTON, D.C.

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

LOCKHEED L-382, L-382B, L-382E, L-382F L-382G, (C-130E & SUBSEQUENT) L-282                (C-130B)

C-130A

Federal Aviation Administration

Flight Standards Division

AIRCRAFT EVALUATION GROUP, LGB-AEG

3960 PARAMOUNT BLVD.

LONG BEACH, CA 90712-4137

TELEPHONE:  (562) 627-5270

FAX:  (562) 627-5281

DEPARTMENT OF TRANSPORTATION     Revision: 19

  Revision: 19

MASTER MINIMUM EQUIPMENT LIST      Date: 10/29/2004

L-382 (C-130)

Table of Contents

SYSTEM NO.  SYSTEM                                  PAGE

--     Table of Contents                       I, II

--     Log of Revisions                        III

--     Control Page                            IV, V, VI

--     Highlights of Change                    VII, VIII, IX, X

--     Highlights of Change                    XI, XII, XIII, XIV

--     Highlights of Change                    XV, XVI

--     Definitions                             XVII, XVIII, XIX, XX --     Definitions                             XXI, XXII, XXIII, XXIV --     Preamble                                XXV, XXVI

21     Air Conditioning                        21-1, 2, 3, 4, 5 21     Air Conditioning                        21-6, 7

22     Auto Flight                             22-1, 2

23     Communications                          23-1, 2, 3, 4, 5 23     Communications                          23-6, 7

24     Electrical Power                        24-1, 2, 3

25     Equipment/Furnishings                   25-1, 2, 3, 4, 5 25     Equipment/Furnishings                   25-6  THRU 10

25     Equipment/Furnishings                   25-11  THRU 13 26     Fire Protection                         26-1, 2, 3, 4

27     Flight Controls                         27-1

28     Fuel                                    28-1, 2, 3, 4, 5 28     Fuel                                    28-6

29     Hydraulic Power                         29-1

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

31     Indicating/Recording Systems            31-1, 2

32     Landing Gear                            32-1

33     Lights                                  33-1, 2, 3

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

34     Navigation                              34-11  THRU 15 35     Oxygen                                  35-1

36     Pneumatic                               36-1, 2 38     Water/Waste                             38-1, 2 49     Airborne Auxiliary Power                49-1

52     Doors                                   52-1

FEDERAL AVIATION ADMINISTRATION     Page: I

  Revision: 19

MASTER MINIMUM EQUIPMENT LIST      Date: 10/29/2004

L-382 (C-130)

Table of Contents

SYSTEM NO.  SYSTEM                                  PAGE

56     Windows                                 56-1 61     Propellers                              61-1 72     Engine                                  72-1 73     Engine Fuel & Control                   73-1 77     Engine Indicating                       77-1 79     Engine Oil                              79-1 80     Starting                                80-1

FEDERAL AVIATION ADMINISTRATION     Page: II

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

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

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

Revision: 19

MASTER MINIMUM EQUIPMENT LIST    Date: 10/29/2004

L-382 (C-130)

Log of Revisions

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

¦ 18       ¦ 04/15/1994 ¦ ALL PAGES                      ¦           ¦ ¦ 18a      ¦ 08/22/1994 ¦ HIGHLIGHTS OF REV.,DEFINITIONS ¦           ¦ ¦ 18a      ¦ 08/22/1994 ¦ 23-1,23-2,23-3,28-1,28-2       ¦           ¦ ¦ 18a      ¦ 08/22/1994 ¦ 28-3,28-4,28-5,29-1,29-2       ¦           ¦ ¦ 18a      ¦ 08/22/1994 ¦ 30-1,30-2,30-3,30-4,32-1       ¦           ¦ ¦ 18a      ¦ 08/22/1994 ¦ 33-1,33-2,33-3,49-1,52-1       ¦           ¦ ¦ 18a      ¦ 08/22/1994 ¦ 56-1,72-1,72-2                 ¦           ¦ ¦ 18b      ¦ 02/10/2003 ¦ HIGHLIGHTS OF REV.,DEFINITIONS ¦           ¦ ¦ 18b      ¦ 02/10/2003 ¦ 23-3,34-3,34-7,34-8            ¦           ¦ ¦ 18c      ¦ 06/24/2003 ¦ HIGHLIGHTS OF REV.,DEFINITIONS ¦           ¦ ¦ 18c      ¦ 06/24/2003 ¦ 34-7,34-8,34-9                 ¦           ¦ ¦ 19       ¦ 10/29/2004 ¦ HIGHLIGHTS OF REV.,DEFINITIONS ¦           ¦ ¦ 19       ¦ 10/29/2004 ¦ 21-1,21-2,21-3,21-4,21-5       ¦           ¦ ¦ 19       ¦ 10/29/2004 ¦ 21-6,21-7,22-1,22-2,23-1       ¦           ¦ ¦ 19       ¦ 10/29/2004 ¦ 23-2,23-3,23-4,23-5,23-6       ¦           ¦ ¦ 19       ¦ 10/29/2004 ¦ 23-7,24-1,24-2,24-3,24-4       ¦           ¦ ¦ 19       ¦ 10/29/2004 ¦ 25-2,25-3,25-4,25-5,25-6       ¦           ¦ ¦ 19       ¦ 10/29/2004 ¦ 25-7,25-8,25-9,25-10,25-11     ¦           ¦ ¦ 19       ¦ 10/29/2004 ¦ 25-12,25-13,26-1,26-2,26-3     ¦           ¦ ¦ 19       ¦ 10/29/2004 ¦ 26-4,27-1,27-2,28-1,28-4       ¦           ¦ ¦ 19       ¦ 10/29/2004 ¦ 28-5,28-6,29-1,29-2,30-1       ¦           ¦ ¦ 19       ¦ 10/29/2004 ¦ 30-2,30-3,30-4,31-1,31-2       ¦           ¦ ¦ 19       ¦ 10/29/2004 ¦ 32-1,33-1,33-2,33-3,34-1       ¦           ¦ ¦ 19       ¦ 10/29/2004 ¦ 34-2,34-3,34-4,34-5,34-6       ¦           ¦ ¦ 19       ¦ 10/29/2004 ¦ 34-7,34-8,34-9,34-10,34-11     ¦           ¦ ¦ 19       ¦ 10/29/2004 ¦ 34-12,34-13,34-14,34-15,35-1   ¦           ¦ ¦ 19       ¦ 10/29/2004 ¦ 36-1,36-2,38-1,38-2,49-1       ¦           ¦ ¦ 19       ¦ 10/29/2004 ¦ 52-1,61-1,72-1,72-2,73-1       ¦           ¦ ¦ 19       ¦ 10/29/2004 ¦ 77-1,79-1,80-1                 ¦           ¦

FEDERAL AVIATION ADMINISTRATION   Page: III

  Revision: 19

MASTER MINIMUM EQUIPMENT LIST      Date: 10/29/2004

L-382 (C-130)

Control Page

SYSTEM                                   PAGE  REV NO.  CURRENT DATE

Cover Page                               -       19       10/29/2004 Table of Contents                        I       19       10/29/2004 II      19       10/29/2004 Log of Revisions                         III     19       10/29/2004 Control Page                             IV      19       10/29/2004 V       19       10/29/2004 VI      19       10/29/2004 Highlights of Change                     VII     19               10/29/2004 VIII    19       10/29/2004 IX      19       10/29/2004 X       19       10/29/2004 XI      19       10/29/2004 XII     19       10/29/2004 XIII    19       10/29/2004 XIV     19               10/29/2004 XV      19       10/29/2004 XVI     19       10/29/2004 Definitions                              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 XXII    6                01/31/1995 XXIII   6        01/31/1995 XXIV    6        01/31/1995 Preamble                                 XXV     2        06/14/1989 XXVI    2        06/14/1989 21                                        21-1    19       10/29/2004 21-2    19       10/29/2004 21-3    19       10/29/2004 21-4    19       10/29/2004 21-5    19               10/29/2004 21-6    19       10/29/2004 21-7    19       10/29/2004 22                                       22-1    19       10/29/2004 22-2    19       10/29/2004 23                                        23-1    19       10/29/2004 23-2    19       10/29/2004              23-3    19       10/29/2004 23-4    19       10/29/2004

FEDERAL AVIATION ADMINISTRATION     Page: IV

  Revision: 19

MASTER MINIMUM EQUIPMENT LIST      Date: 10/29/2004

L-382 (C-130)

Control Page

SYSTEM                                   PAGE  REV NO.  CURRENT DATE

23-5    19       10/29/2004 23-6    19       10/29/2004 23-7    19       10/29/2004 24                                       24-1    19               10/29/2004 24-2    19       10/29/2004 24-3    19       10/29/2004 25                                       25-1    18       04/15/1994 25-2    19       10/29/2004 25-3    19       10/29/2004 25-4    19       10/29/2004 25-5    19       10/29/2004 25-6    19               10/29/2004 25-7    19       10/29/2004 25-8    19       10/29/2004 25-9    19       10/29/2004 25-10   19       10/29/2004 25-11   19       10/29/2004 25-12   19       10/29/2004 25-13   19       10/29/2004 26                                       26-1    19               10/29/2004 26-2    19       10/29/2004 26-3    19       10/29/2004 26-4    19       10/29/2004 27                                       27-1    19       10/29/2004 28                                        28-1    19       10/29/2004 28-2    18 a     08/22/1994 28-3    18 a     08/22/1994 28-4    19       10/29/2004 28-5    19       10/29/2004 28-6    19       10/29/2004 29                                       29-1    19       10/29/2004 30                                               30-1    19       10/29/2004 30-2    19       10/29/2004 30-3    19       10/29/2004 30-4    19       10/29/2004 31                                       31-1    19       10/29/2004 31-2    19       10/29/2004 32                                       32-1    19       10/29/2004 33                                                    33-1    19       10/29/2004 33-2    19       10/29/2004

FEDERAL AVIATION ADMINISTRATION     Page: V

  Revision: 19

MASTER MINIMUM EQUIPMENT LIST      Date: 10/29/2004

L-382 (C-130)

Control Page

SYSTEM                                   PAGE  REV NO.  CURRENT DATE

                                         33-3    19       10/29/2004 34                                       34-1    19       10/29/2004 34-2    19       10/29/2004 34-3    19       10/29/2004 34-4    19       10/29/2004 34-5    19       10/29/2004 34-6    19       10/29/2004 34-7    19       10/29/2004 34-8    19       10/29/2004 34-9    19       10/29/2004 34-10   19       10/29/2004 34-11   19       10/29/2004 34-12   19       10/29/2004 34-13   19       10/29/2004 34-14   19       10/29/2004 34-15   19       10/29/2004 35                                       35-1    19       10/29/2004 36                                       36-1    19       10/29/2004 36-2    19       10/29/2004 38                                       38-1    19       10/29/2004 38-2    19       10/29/2004 49                                       49-1    19       10/29/2004 52                                       52-1    19       10/29/2004 56                                       56-1    18 a     08/22/1994 61                                       61-1    19       10/29/2004 72                                       72-1    19       10/29/2004 73                                       73-1    19       10/29/2004 77                                       77-1    19       10/29/2004 79                                       79-1    19       10/29/2004 80                                       80-1    19       10/29/2004

FEDERAL AVIATION ADMINISTRATION     Page: VI

  Revision: 19

MASTER MINIMUM EQUIPMENT LIST    Date: 10/29/2004

L-382 (C-130)

Highlights of Change

EFFECTIVE ABOVE DATE, the Lockheed L-382 Master Minimum Equipment List is revised.  Revision 19 is a complete reissue of this MMEL. This revision affects all of the following items:

ATA 21 AIR CONDITIONING

21-1   Corrected item title and corrected system component name to

align with terms used in L382 Maintenance and Flight Manuals.

21-2   Added airplane serial number effectivity.

21-3   Corrected item title and reformatted by deleting "OR" (PL-31).

21-4   Corrected item title and deleted (M).

21-5   Deleted (M) and reformatted by deleting "OR" (PL-31).

21-6   Deleted (M).

21-8   Corrected item title, deleted (M), added (O) and reformatted by deleting "OR" (PL-31).

21-10  Corrected item title and added airplane serial number effectivity.

21-11  Corrected item title, corrected airplane serial number

effectivity, deleted (M) and provided relief for variable airplane configurations.

21-12  Corrected item title, corrected airplane serial number effectivity, deleted (M) and clarified relief for new airplane configurations, added icing restrictions, combined with MMEL item 21-23.

21-18  Revised to clarify relief for specific airplane configurations, deleted (M) and added (O).

21-19  Added (O).

21-22  Corrected airplane serial number effectivity, and provided relief for variable airplane configurations.

21-23  Combined with and moved to MMEL item 21-12.

FEDERAL AVIATION ADMINISTRATION   Page: VII

  FEDERAL AVIATION ADMINISTRATION   Page: VIII

Revision: 19

MASTER MINIMUM EQUIPMENT LIST    Date: 10/29/2004

L-382 (C-130)

Highlights of Change

21-25  Deleted (O).

21-26  Added airplane serial number effectivity, specify relief applies to AIR COND HOT light and deleted (O) for single system inoperative.

21-27  Moved to MMEL item 21-25.

ATA 22 AUTOFLIGHT

22-1   Add relief for individual autopilot modes and incorporated Policy Letters 84 and 101.

22-2   Revised item title to include relief for AP DISENG light and add relief for multiple light installations.

22-3   Corrected item title, delete (O) and added relief for both switches inoperative.

22-4   Moved to MMEL item 22-1.

22-5   Add (E4) to item title and incorporate PL-101.

22-6   Add relief for Yaw Damper.

ATA 23 COMMUNICATIONS

23-1   Reinstate relief for Crewmember Interphone Systems per PL-9.

23-2   Add *** and align relief with PL-9.

23-3   Incorporate PL-95 and move HF relief to MMEL item 23-4.

23-4   Moved from MMEL 23-3 and incorporated PL-106.

23-5   Revised to specify relief applies to NAV station.

23-7   Moved to MMEL item 25-9.

23-9   Reformatted by deleting "OR" (PL-31).

23-14  Add relief for Push-to-Talk (PTT) switches.

  Revision: 19

MASTER MINIMUM EQUIPMENT LIST    Date: 10/29/2004

L-382 (C-130)

Highlights of Change

23-15  Add relief for excess headphones/hand microphones.

ATA 24 ELECTRICAL POWER

24-1   Item renumbered.

24-2   Item renumbered and reformatted by deleting "OR" (PL-31).

24-3   Item renumbered and adds relief for APU generator.

24-4   Item renumbered, deleted Remarks or Exceptions.

24-5   Item renumbered, revised to clarify relief.

24-6   Item renumbered, changed to Repair Category C.

24-7   Item renumbered, revised to clarify applicability of relief.

24-8   Item renumbered, revised item title to clarify applicability of relief.

24-9   Corrected item title, deleted relief.

24-10  Item renumbered.

24-11  Item renumbered.

24-12  Item renumbered.

24-13  Item renumbered.

ATA 25 EQUIPMENT/FURNISHINGS

25-3   Incorporated PL-97.

25-4   Moved to MMEL item 25-3.

25-5   Incorporated PL-56.

25-6   Incorporated PL-97.

25-7   Incorporated PL-89.

FEDERAL AVIATION ADMINISTRATION   Page: IX

  Revision: 19

MASTER MINIMUM EQUIPMENT LIST    Date: 10/29/2004

L-382 (C-130)

Highlights of Change

25-9   Incorporated PL-47.

25-11  Incorporated PL-73.

25-12  Added relief provided by PL-100.

25-13  Added relief provided by PL-85.

25-14  Added relief provided by PL-96.

25-15  Added relief provided by PL-104.

ATA 26 FIRE PROTECTION

26-1   Item renumbered.

26-2   Item renumbered and reformatted by deleting "OR" (PL-31).

26-3   Item renumbered and corrected item title.

26-4   Item renumbered and corrected item title.

26-5   Item renumbered, incorporated PL-24, added ***.

26-6   Item renumbered, reformatted by deleting "OR" (PL-31), incorporated PL-24 and added ***.

26-7   Item renumbered, incorporated PL-75.

26-12  Added relief provided by PL-102.

ATA 27 FLIGHT CONTROLS

27-1   Item renumbered.

27-2   Item renumbered.

27-3   Item renumbered.

ATA 28 FUEL

28-2   Reformatted by deleting "OR" (PL-31).

FEDERAL AVIATION ADMINISTRATION   Page: X

  Revision: 19

MASTER MINIMUM EQUIPMENT LIST    Date: 10/29/2004

L-382 (C-130)

Highlights of Change

28-11  Item renumbered.

28-12  Item renumbered.

28-13  Item renumbered, added NOTE to allow use of operative

functions, added relief for SPR Drain Transfer Pump and SPR Panel Fuel Quantity Indicators.

28-14  Item renumbered.

28-15  Item renumbered and corrected item title.

28-16  Item renumbered, provide relief for one inoperative light and provide relief and tank useable by monitoring fuel pressure output.

28-17  Item renumbered, provide relief and tank useable by monitoring fuel pressure output.

ATA 29 HYDRAULIC POWER

29-1  Reinstate relief for Engine Pump Pressure warning light.

29-2  Reinstate relief for Utility Hydraulic Pressure Gauge.

29-3  Renumber item, deleted (M) and deleted Remarks.

29-4   Renumbered item and corrected Number Installed.

29-5   Renumbered item , corrected Number Installed and deleted Remarks.

29-6   Item renumbered.

ATA 30 ICE AND RAIN PROTECTION

30-1   Moved relief for Wing and Empennage Anti-Icing Valves to to this item.

30-2   Reformatted by deleting "OR" (PL-31).

30-3   Reformatted by deleting "OR" (PL-31).

FEDERAL AVIATION ADMINISTRATION   Page: XI

  Revision: 19

MASTER MINIMUM EQUIPMENT LIST    Date: 10/29/2004

L-382 (C-130)

Highlights of Change

30-4   Moved to MMEL item 36-6.

30-5   Moved relief for Pitot Heat OFF lights to this item.

30-6   Added relief for system inoperative ON and revised item title to include system sub-components.

30-7   Added ***.

30-9   Reformatted by deleting "OR" (PL-31), revised item title.

30-10  Reformatted by deleting "OR" (PL-31), revised item title.

30-14  Moved to MMEL item 30-5.

ATA 31 INDICATING/RECORDING SYSTEMS

31-2   Incorporated PL-87.

ATA 32 LANDING GEAR

32-2   Item renumbered.

32-3   Item renumbered.

ATA 33 LIGHTS

33-2   Add relief for one tail navigation light inoperative.

33-3   Incorporated PL-72.

33-8   Incorporate PL-77 and specify cockpit emergency lighting that must be operative.

33-9   Item renumbered and moved to MMEL item 52-7.

33-10  Item renumbered.

33-11  Item renumbered and moved to MMEL item 49-4.

33-12  Item renumbered.

FEDERAL AVIATION ADMINISTRATION   Page: XII

  FEDERAL AVIATION ADMINISTRATION   Page: XIII

Revision: 19

MASTER MINIMUM EQUIPMENT LIST    Date: 10/29/2004

L-382 (C-130)

Highlights of Change

ATA 34 NAVIGATION

34-5   Incorporated PL-10.

34-7   Deleted proviso a) (no relief for airspeed indicators).

34-8   Revised title for clarity and corrected number required for dispatch.

34-9   Revised to align with new MMEL item 34-35.

34-10  Incorporated PL-111.

34-11  Clarify Remarks and incorporated PL-67.

34-12  Incorporated PL-3.

34-13  Incorporated PL-76.

34-17  Added relief for individual Flight Director modes and

added relief for Digital-to-Analog Converters (EPIC mod).

34-19  Expanded title to include additional types of navigation systems, added relief for navigation data base, added relief for system Status Annunciator Panel and deleted VLF/Omega.

34-21  Incorporated PL-54.

34-22  Added relief for multiple system installation.

34-25  Incorporated PL-39 and PL-84.

34-28  Incorporated PL-32.

34-31  Revised proviso c) to allow use of operative TCAS functions and delete (M).

34-33  Revised to provide relief for #1, 2 or 3 (AUX) IRS.

34-34  Incorporated PL-111.

  Revision: 19

MASTER MINIMUM EQUIPMENT LIST    Date: 10/29/2004

L-382 (C-130)

Highlights of Change

34-35  Added relief for attitude reference systems in excess of FAR requirements.

ATA 35 OXYGEN

35-1   Add relief for oxygen system components in excess of FAR requirements.

35-2   Incorporated PL-52.

35-3   Incorporated PL-52.

35-4   Incorporated PL-43.

ATA 36 PNEUMATICS

36-1   Item renumbered, clarified relief and corrected restrictions.

36-2   Item renumbered.

36-3   Item renumbered and moved to MMEL item 49-3.

36-4   Item renumbered, added airplane serial number effectivity and changed to Repair Category C.

36-5   Item renumbered and moved to MMEL item 30-1.

36-6   Item for Bleed Air Pressure Gauge deleted and added new item for Nacelle Preheat System.

36-7   Item renumbered, corrected airplane serial number effectivity.

ATA 38 WATER/WASTE

38-1   Added relief for Potable Water Systems per PL-83.

38-2   Added relief for Lavatory Waste Systems per PL-83.

ATA 49 AUXILIARY POWER UNIT

49-2   Moved to MMEL item 24-3.

FEDERAL AVIATION ADMINISTRATION   Page: XIV

  Revision: 19

MASTER MINIMUM EQUIPMENT LIST    Date: 10/29/2004

L-382 (C-130)

Highlights of Change

49-3   Moved from ATA 36, added *** and added airplane serial number effectivity.

49-4   Moved from ATA 33 and corrected item title.

ATA 52 DOORS

52-2   Added *** and corrected item title.

52-7   Moved from ATA 33 and changed (O) to (M).

ATA 61 PROPELLERS

61-2   Item renumbered.

ATA 72 ENGINE

ATA 72 Items moved to the correct ATA chapters or deleted if no relief was ever provided.

ATA 73 ENGINE FUEL AND CONTROL

73-1   Moved from ATA 72.

73-2   Moved from ATA 72.

73-3   Moved from ATA 72.

73-4   Moved from ATA 72.

ATA 77 ENGINE INDICATING

77-1   Moved from ATA 72.

77-2   Moved from ATA 72.

ATA 79 ENGINE OIL

79-1   Moved from ATA 72.

79-2   Moved from ATA 72.

79-3   Moved from ATA 72.

FEDERAL AVIATION ADMINISTRATION   Page: XV

  Revision: 19

MASTER MINIMUM EQUIPMENT LIST    Date: 10/29/2004

L-382 (C-130)

Highlights of Change

79-4   Moved from ATA 72.

79-5   Moved from ATA 72.

ATA 80 ENGINE STARTING

80-1   Moved from ATA 72.

FEDERAL AVIATION ADMINISTRATION   Page: XVI

  FEDERAL AVIATION ADMINISTRATION     Page: XVII

Revision: 6

MASTER MINIMUM EQUIPMENT LIST      Date: 01/31/1995

L-382 (C-130)

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: XVIII Revision: 6 MASTER MINIMUM EQUIPMENT LIST      Date: 01/31/1995

L-382 (C-130)

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: XIX

Revision: 6

MASTER MINIMUM EQUIPMENT LIST      Date: 01/31/1995

L-382 (C-130)

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

  Revision: 6

MASTER MINIMUM EQUIPMENT LIST      Date: 01/31/1995

L-382 (C-130)

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: XX

  FEDERAL AVIATION ADMINISTRATION     Page: XXI

Revision: 6

MASTER MINIMUM EQUIPMENT LIST      Date: 01/31/1995

L-382 (C-130)

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: XXII

Revision: 6

MASTER MINIMUM EQUIPMENT LIST      Date: 01/31/1995

L-382 (C-130)

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: XXIII Revision: 6 MASTER MINIMUM EQUIPMENT LIST      Date: 01/31/1995

L-382 (C-130)

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

  D."

FEDERAL AVIATION ADMINISTRATION     Page: XXIV

Revision: 6

MASTER MINIMUM EQUIPMENT LIST      Date: 01/31/1995

L-382 (C-130)

Definitions

maintenance log and or record.  This day is excluded from the calendar days or flight days specified in the MMEL for the repair of an inoperative item of equipment. This provision is applicable to all MMEL items, i.e., categories "A, B, C, and

  FEDERAL AVIATION ADMINISTRATION   Page: XXV

Revision: 2

MASTER MINIMUM EQUIPMENT LIST    Date: 06/14/1989

L-382 (C-130)

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: XXVI

Revision: 2

MASTER MINIMUM EQUIPMENT LIST    Date: 06/14/1989

L-382 (C-130)

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: 19       ¦ PAGE:    ¦ ¦              L-382 (C-130)               ¦                       ¦          ¦ ¦                                          ¦ DATE: 10/29/2004      ¦ 21-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 21  AIR CONDITIONING      ¦    ¦    ¦                                       ¦

¦ 1.  Air Conditioning    C ¦ 2  ¦ 1  ¦ (M)One may be inoperative provided    ¦ ¦     Systems               ¦    ¦    ¦ associated Flow Control and Shutoff | ¦ ¦                           ¦    ¦    ¦ Valve is secured CLOSED.            | ¦

¦                         C ¦ 2  ¦ 0  ¦ (M)(O)May be inoperative provided:    ¦ ¦                           ¦    ¦    ¦     a) Both Flow Control and        | ¦ ¦                           ¦    ¦    ¦        Shutoff Valves are secured   | ¦ ¦                           ¦    ¦    ¦        CLOSED, and                  | ¦ ¦                           ¦    ¦    ¦     b) Aircraft is operated         | ¦ ¦                           ¦    ¦    ¦        unpressurized.               | ¦

¦ 2.  Under Floor Heater  C ¦ 1  ¦ 0  ¦ (M)May be inoperative provided        ¦ ¦     Diverter Valve        ¦    ¦    ¦ Valve is secured OPEN.                ¦ ¦     (Airplanes prior to   ¦    ¦    ¦                                     | ¦ ¦     Serial Number 4653)   ¦    ¦    ¦                                     | ¦

¦ 3.  Cargo Compartment   C ¦ 1  ¦ 0  ¦ May be inoperative provided Cargo   | ¦ ¦     Automatic             ¦    ¦    ¦ Compartment Manual Temperature      | ¦ ¦     Temperature           ¦    ¦    ¦ Control System is operative.        | ¦ ¦     Control System        ¦    ¦    ¦                                       ¦ ¦                         C ¦ 1  ¦ 0  ¦ May be inoperative provided Cargo   | ¦ ¦                           ¦    ¦    ¦ Compartment Air Conditioning System | ¦ ¦                           ¦    ¦    ¦ is considered inoperative.          | ¦

¦ 4.  Cargo Compartment   C ¦ 1  ¦ 0  ¦ May be inoperative provided         | ¦ ¦     Manual Temperature    ¦    ¦    ¦ Cargo Compartment Air Conditioning  | ¦ ¦     Control System        ¦    ¦    ¦ System is considered inoperative.   | ¦

¦ 5.  Flight Station      C ¦ 1  ¦ 0  ¦ May be inoperative provided Flight  | ¦ ¦     Automatic             ¦    ¦    ¦ Station Manual Temperature Control  | ¦ ¦     Temperature Control   ¦    ¦    ¦ System is operative.                | ¦ ¦     System                ¦    ¦    ¦                                       ¦ ¦                         C ¦ 1  ¦ 0  ¦ May be inoperative provided Flight  | ¦ ¦                           ¦    ¦    ¦ Station Air Conditioning System is  | ¦ ¦                           ¦    ¦    ¦ considered inoperative.             | ¦

¦ 6.  Flight Station      C ¦ 1  ¦ 0  ¦ May be inoperative provided         | ¦ ¦     Manual Temperature    ¦    ¦    ¦ Flight Station Air Conditioning       ¦ ¦     Control System        ¦    ¦    ¦ System is considered inoperative.     ¦

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

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 19       ¦ PAGE:    ¦ ¦              L-382 (C-130)               ¦                       ¦          ¦ ¦                                          ¦ DATE: 10/29/2004      ¦ 21-2     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 21  AIR CONDITIONING      ¦    ¦    ¦                                       ¦

¦ 7.  Outflow Valve       C ¦ 1  ¦ 0  ¦ (M)(O)May be inoperative provided:    ¦ ¦                           ¦    ¦    ¦     a) Valve is secured OPEN, and     ¦ ¦                           ¦    ¦    ¦     b) Aircraft is operated           ¦ ¦                           ¦    ¦    ¦        unpressurized.                 ¦

¦ 8.  Automatic           C ¦ 1  ¦ 0  ¦ May be inoperative provided:        | ¦ ¦     Pressurization        ¦    ¦    ¦     a) Manual Pressure Control      | ¦ ¦     Control System        ¦    ¦    ¦        System is operative, and     | ¦ ¦                           ¦    ¦    ¦     b) Cabin Rate of Climb,           ¦ ¦                           ¦    ¦    ¦        Differential Pressure and      ¦ ¦                           ¦    ¦    ¦        Cabin Altitude Gauges are      ¦ ¦                           ¦    ¦    ¦        operative.                     ¦

¦                         C ¦ 1  ¦ 0  ¦ (O)May be inoperative provided      | ¦ ¦                           ¦    ¦    ¦ aircraft is operated unpressurized. | ¦

¦ 9.  Manual              C ¦ 1  ¦ 0  ¦ (M)May be inoperative provided:       ¦ ¦     Pressurization        ¦    ¦    ¦     a) Manual Pressurization Cam is   ¦ ¦     Control System        ¦    ¦    ¦        NEUTRAL, and                   ¦ ¦                           ¦    ¦    ¦     b) Automatic Pressurization       ¦ ¦                           ¦    ¦    ¦        System is operative.           ¦

¦ 10. GTC Function of     C ¦ 1  ¦ 0  ¦                                     | ¦ ¦     Air Conditioning      ¦    ¦    ¦                                     | ¦ ¦     Master Control        ¦    ¦    ¦                                     | ¦ ¦     Switch                ¦    ¦    ¦                                     | ¦ ¦     (Airplanes prior to   ¦    ¦    ¦                                     | ¦ ¦     Serial Number 4653)   ¦    ¦    ¦                                     | ¦

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

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 19       ¦ PAGE:    ¦ ¦              L-382 (C-130)               ¦                       ¦          ¦ ¦                                          ¦ DATE: 10/29/2004      ¦ 21-3     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 21  AIR CONDITIONING      ¦    ¦    ¦                                       ¦

¦ 11. Cargo Compartment     ¦    ¦    ¦                                     | ¦ ¦     Air Conditioning      ¦    ¦    ¦                                     | ¦ ¦     Shutoff Switch        ¦    ¦    ¦                                     | ¦ ¦     (Except C-130A)       ¦    ¦    ¦                                       ¦

¦     1) Airplanes Prior  C ¦ 1  ¦ 0  ¦ May be inoperative provided:        | ¦ ¦        to Serial Number   ¦    ¦    ¦     a) Both Wing Isolation Valves   | ¦ ¦        4653 Without       ¦    ¦    ¦        are operative, and           | ¦ ¦        Bleed Air          ¦    ¦    ¦     b) Aircraft is not operated in  | ¦ ¦        Divider Valve      ¦    ¦    ¦        known or forecast icing      | ¦ ¦                           ¦    ¦    ¦        conditions.                  | ¦

¦     2) Airplanes Prior  C ¦ 1  ¦ 0  ¦ May be inoperative provided Right   | ¦ ¦        to Serial Number   ¦    ¦    ¦ Wing Isolation Valve and Bleed Air  | ¦ ¦        4653 With Bleed    ¦    ¦    ¦ Divider Valve are operative.        | ¦ ¦        Air Divider Valve  ¦    ¦    ¦                                     | ¦

¦     3) Airplanes Serial C ¦ 1  ¦ 0  ¦ May be inoperative provided:        | ¦ ¦        Number 4653 and    ¦    ¦    ¦     a) No. 3 and 4 Bleed Air        | ¦ ¦        Subsequent         ¦    ¦    ¦        Pressure Regulating and      | ¦ ¦                           ¦    ¦    ¦        Shutoff Valves are           | ¦ ¦                           ¦    ¦    ¦        operative,                   | ¦ ¦                           ¦    ¦    ¦     b) Bleed Air Divider Valve is   | ¦ ¦                           ¦    ¦    ¦        operative, and               | ¦ ¦                           ¦    ¦    ¦     c) Aircraft is not operated in  | ¦ ¦                           ¦    ¦    ¦        known or forecast icing      | ¦ ¦                           ¦    ¦    ¦        conditions.                  | ¦

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

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 19       ¦ PAGE:    ¦ ¦              L-382 (C-130)               ¦                       ¦          ¦ ¦                                          ¦ DATE: 10/29/2004      ¦ 21-4     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 21  AIR CONDITIONING      ¦    ¦    ¦                                       ¦

¦ 12. Flight Station Air    ¦    ¦    ¦                                     | ¦ ¦     Conditioning Flow     ¦    ¦    ¦                                     | ¦ ¦     Control and Shutoff   ¦    ¦    ¦                                     | ¦ ¦     Valve System          ¦    ¦    ¦                                     | ¦

¦     1) Airplanes Prior  C ¦ 1  ¦ 0  ¦ May be inoperative provided Flow    | ¦ ¦        to Serial Number   ¦    ¦    ¦ Control and Shutoff Valve Override  | ¦ ¦        4653               ¦    ¦    ¦ is operative.                       | ¦

¦     2) Airplanes Serial C ¦ 1  ¦ 0  ¦ May be inoperative provided:        | ¦ ¦        Number 4653 and    ¦    ¦    ¦     a) No. 1 and 2 Bleed Air        | ¦ ¦        Subsequent         ¦    ¦    ¦        Pressure Regulating and      | ¦ ¦                           ¦    ¦    ¦        Shutoff Valves are           | ¦ ¦                           ¦    ¦    ¦        operative,                   | ¦ ¦                           ¦    ¦    ¦     b) Bleed Air Divider Valve is   | ¦ ¦                           ¦    ¦    ¦        operative, and               | ¦ ¦                           ¦    ¦    ¦     c) Aircraft is not operated in  | ¦ ¦                           ¦    ¦    ¦        known or forecast icing        ¦ ¦                           ¦    ¦    ¦        conditions.                    ¦

¦ 13. Cabin Rate-of-      C ¦ 1  ¦ 0  ¦ May be inoperative provided:          ¦ ¦     Climb Indicator       ¦    ¦    ¦     a) Cabin Altimeter is             ¦ ¦                           ¦    ¦    ¦        operative, and                 ¦ ¦                           ¦    ¦    ¦     b) Differential Pressure Gauge    ¦ ¦                           ¦    ¦    ¦        is operative.                  ¦

¦ 14. Differential        C ¦ 1  ¦ 0  ¦ (O)May be inoperative provided:       ¦ ¦     Pressure Gauge        ¦    ¦    ¦     a) Cabin Altimeter is             ¦ ¦                           ¦    ¦    ¦        operative, and                 ¦ ¦                           ¦    ¦    ¦     b) A chart is available for the   ¦ ¦                           ¦    ¦    ¦        Flight Engineer to convert     ¦ ¦                           ¦    ¦    ¦        Cabin Altitude to              ¦ ¦                           ¦    ¦    ¦        Differential Pressure.         ¦

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

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 19       ¦ PAGE:    ¦ ¦              L-382 (C-130)               ¦                       ¦          ¦ ¦                                          ¦ DATE: 10/29/2004      ¦ 21-5     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 21  AIR CONDITIONING      ¦    ¦    ¦                                       ¦

¦ 15. Cabin Altimeter     C ¦ 1  ¦ 0  ¦ (O)May be inoperative provided:       ¦ ¦                           ¦    ¦    ¦     a) Differential Pressure Gauge    ¦ ¦                           ¦    ¦    ¦        is operative, and              ¦ ¦                           ¦    ¦    ¦     b) A chart is available for the   ¦ ¦                           ¦    ¦    ¦        Flight Engineer to convert     ¦ ¦                           ¦    ¦    ¦        Differential Pressure to       ¦ ¦                           ¦    ¦    ¦        Cabin Altitude.                ¦

¦ 16. Cargo Compartment   C ¦ 1  ¦ 0  ¦                                       ¦ ¦     Underfloor Heating    ¦    ¦    ¦                                       ¦

¦ 17. Emergency           C ¦ 1  ¦ 0  ¦ May be inoperative provided           ¦ ¦     Depressurization      ¦    ¦    ¦ Emergency Depressurization Handle     ¦ ¦     Switch                ¦    ¦    ¦ is operative.                         ¦

¦ 18. Emergency             ¦    ¦    ¦                                     | ¦ ¦     Depressurization      ¦    ¦    ¦                                     | ¦ ¦     Handle                ¦    ¦    ¦                                     | ¦

¦     1) Airplanes        C ¦ 1  ¦ 0  ¦ (O)May be inoperative provided      | ¦ ¦        Equipped with      ¦    ¦    ¦ aircraft is operated unpressurized. | ¦ ¦        Bleed Air Shutoff  ¦    ¦    ¦                                     | ¦ ¦        Valves             ¦    ¦    ¦                                     | ¦

¦     2) Airplanes        C ¦ 1  ¦ 0  ¦                                     | ¦ ¦        Equipped with      ¦    ¦    ¦                                     | ¦ ¦        Bleed Air          ¦    ¦    ¦                                     | ¦ ¦        Pressure           ¦    ¦    ¦                                     | ¦ ¦        Regulating and     ¦    ¦    ¦                                     | ¦ ¦        Shutoff Valves     ¦    ¦    ¦                                     | ¦

¦ 19. Safety Valve        C ¦ 1  ¦ 0  ¦ (M)(O)May be inoperative provided:  | ¦ ¦                           ¦    ¦    ¦     a) Outflow Valve is secured     | ¦ ¦                           ¦    ¦    ¦        OPEN, and                      ¦ ¦                           ¦    ¦    ¦     b) Aircraft is operated           ¦ ¦                           ¦    ¦    ¦        unpressurized.                 ¦

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

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 19       ¦ PAGE:    ¦ ¦              L-382 (C-130)               ¦                       ¦          ¦ ¦                                          ¦ DATE: 10/29/2004      ¦ 21-6     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 21  AIR CONDITIONING      ¦    ¦    ¦                                       ¦

¦ 20. Cargo Compartment   C ¦ 1  ¦ 0  ¦ (M)May be inoperative provided:       ¦ ¦     Auxiliary Vent        ¦    ¦    ¦     a) Affected Valve is secured      ¦ ¦     Valve                 ¦    ¦    ¦        CLOSED, and                    ¦ ¦                           ¦    ¦    ¦     b) Flight Station Auxiliary       ¦ ¦                           ¦    ¦    ¦        Vent Valve is operative.       ¦

¦ 21. Flight Station      C ¦ 1  ¦ 0  ¦ (M)May be inoperative provided:       ¦ ¦     Auxiliary Vent        ¦    ¦    ¦     a) Affected Valve is secured      ¦ ¦     Valve                 ¦    ¦    ¦        CLOSED, and                    ¦ ¦                           ¦    ¦    ¦     b) Cargo Compartment Auxiliary    ¦ ¦                           ¦    ¦    ¦        Vent Valve is operative.       ¦

¦ 22. Cargo Compartment     ¦    ¦    ¦                                       ¦ ¦     Flow Control and      ¦    ¦    ¦                                     | ¦ ¦     Shutoff Valve         ¦    ¦    ¦                                       ¦

¦     1) Airplanes Prior  C ¦ 1  ¦ 0  ¦ May be inoperative provided:        | ¦ ¦        to Serial Number   ¦    ¦    ¦     a) Both Wing Isolation Valves   | ¦ ¦        4653 Without       ¦    ¦    ¦        are operative, and           | ¦ ¦        Bleed Air Divider  ¦    ¦    ¦     b) Aircraft is not operated in  | ¦ ¦        Valve              ¦    ¦    ¦        known or forecast icing      | ¦ ¦                           ¦    ¦    ¦        conditions.                  | ¦

¦     2) Airplanes Prior  C ¦ 1  ¦ 0  ¦ May be inoperative provided Right   | ¦ ¦        to Serial Number   ¦    ¦    ¦ Wing Isolation Valve and Bleed Air  | ¦ ¦        4653 With Bleed    ¦    ¦    ¦ Divider Valve are operative.        | ¦ ¦        Air Divider Valve  ¦    ¦    ¦                                     | ¦

¦     3) Airplanes Serial C ¦ 1  ¦ 0  ¦ May be inoperative provided:        | ¦ ¦        Number 4653 and    ¦    ¦    ¦     a) No. 3 and 4 Bleed Air        | ¦ ¦        Subsequent         ¦    ¦    ¦        Pressure Regulating and      | ¦ ¦                           ¦    ¦    ¦        Shutoff Valves are           | ¦ ¦                           ¦    ¦    ¦        operative,                   | ¦ ¦                           ¦    ¦    ¦     b) Bleed Air Divider Valve is   | ¦ ¦                           ¦    ¦    ¦        operative, and               | ¦ ¦                           ¦    ¦    ¦     c) Aircraft is not operated in  | ¦ ¦                           ¦    ¦    ¦        known or forecast icing      | ¦ ¦                           ¦    ¦    ¦        conditions.                  | ¦

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

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 19       ¦ PAGE:    ¦ ¦              L-382 (C-130)               ¦                       ¦          ¦ ¦                                          ¦ DATE: 10/29/2004      ¦ 21-7     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 21  AIR CONDITIONING      ¦    ¦    ¦                                       ¦

¦ 23. Flight Station Flow   ¦    ¦    ¦ Moved to 21-12, Revision 19.        | ¦ ¦     Control and Shutoff   ¦    ¦    ¦                                     | ¦ ¦     Valve                 ¦    ¦    ¦                                       ¦

¦ 24. Cargo Compartment   C ¦ 1  ¦ 0  ¦                                       ¦ ¦     Recirculation Fan     ¦    ¦    ¦                                       ¦ ¦     System                ¦    ¦    ¦                                       ¦

¦ 25. Cargo Compartment   C ¦ 1  ¦ 0  ¦ May be inoperative provided         | ¦ ¦     Refrigeration         ¦    ¦    ¦ Cargo Compartment Air Conditioning    ¦ ¦     Overheat Warning      ¦    ¦    ¦ System is considered inoperative      ¦ ¦     Light                 ¦    ¦    ¦ and not used.                         ¦

¦ 26. Air Conditioning    C ¦ 2  ¦ 1  ¦ May be inoperative provided         | ¦ ¦     Anti-Ice Overtemp     ¦    ¦    ¦ associated Air Conditioning System  | ¦ ¦     Warning Light         ¦    ¦    ¦ is considered inoperative and not   | ¦ ¦     System/AIR COND HOT   ¦    ¦    ¦ used.                               | ¦ ¦     Light System          ¦    ¦    ¦                                     | ¦ ¦     (Airplanes Serial     ¦    ¦    ¦                                     | ¦ ¦     Number 4653 through   ¦    ¦    ¦                                     | ¦ ¦     4946 Not Modified     ¦    ¦    ¦                                     | ¦ ¦     by Service Bulletin   ¦    ¦    ¦                                     | ¦ ¦     382-21-12/82-503)     ¦    ¦    ¦                                     | ¦

¦                         C ¦ 2  ¦ 0  ¦ (O)May be inoperative provided      | ¦ ¦                           ¦    ¦    ¦ both Air Conditioning Systems are   | ¦ ¦                           ¦    ¦    ¦ considered inoperative and not      | ¦ ¦                           ¦    ¦    ¦ used.                               | ¦

¦ 27. Cargo Compartment     ¦    ¦    ¦ Moved to 21-25, Revision 19.        | ¦ ¦     Air Conditioning      ¦    ¦    ¦                                       ¦ ¦     Pack Overheat         ¦    ¦    ¦                                       ¦ ¦     Warning System        ¦    ¦    ¦                                       ¦

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

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 19       ¦ PAGE:    ¦ ¦              L-382 (C-130)               ¦                       ¦          ¦ ¦                                          ¦ DATE: 10/29/2004      ¦ 22-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 1.  Autopilot System    B ¦ 1  ¦ 0  ¦ May be inoperative provided         | ¦ ¦                           ¦    ¦    ¦ enroute operations or approach      | ¦ ¦                           ¦    ¦    ¦ minimums do not require its use.    | ¦

¦                           ¦    ¦    ¦ NOTE: Any mode that operates        | ¦ ¦                           ¦    ¦    ¦       normally may be used.         | ¦

¦     1) Lateral          C ¦ -  ¦ 0  ¦ May be inoperative provided         | ¦ ¦        Navigation Modes   ¦    ¦    ¦ enroute operations or approach      | ¦ ¦        (NAV/LOC, HDG)     ¦    ¦    ¦ minimums do not require their use.  | ¦

¦                           ¦    ¦    ¦ NOTE: Any mode that operates        | ¦ ¦                           ¦    ¦    ¦       normally may be used.         | ¦

¦     2) Vertical         C ¦ -  ¦ 0  ¦ May be inoperative provided         | ¦ ¦        Navigation Modes   ¦    ¦    ¦ enroute operations or approach      | ¦ ¦        (ALT, ALT SEL,     ¦    ¦    ¦ minimums do not require their use.  | ¦ ¦        VS, IAS)           ¦    ¦    ¦                                       ¦ ¦                           ¦    ¦    ¦ NOTE: Any mode that operates        | ¦ ¦                           ¦    ¦    ¦       normally may be used.         | ¦

¦ *** 3) APPR Mode        C ¦ -  ¦ 0  ¦ May be inoperative provided         | ¦ ¦                           ¦    ¦    ¦ approach minimums do not require    | ¦ ¦                           ¦    ¦    ¦ its use.                            | ¦

¦ *** 4) AP CPLD Mode     C ¦ -  ¦ 0  ¦ May be inoperative provided         | ¦ ¦                           ¦    ¦    ¦ enroute operations or approach      | ¦ ¦                           ¦    ¦    ¦ minimums do not require its use.    | ¦

¦ *** 5) BACK LOC Mode    C ¦ -  ¦ 0  ¦ May be inoperative provided         | ¦ ¦                           ¦    ¦    ¦ approach minimums do not require    | ¦ ¦                           ¦    ¦    ¦ its use.                            | ¦

¦ *** 6) Radio Beam       C ¦ -  ¦ 0  ¦ May be inoperative provided         | ¦ ¦        Coupler            ¦    ¦    ¦ approach minimums do not require    | ¦ ¦                           ¦    ¦    ¦ its use.                            | ¦

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

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 19       ¦ PAGE:    ¦ ¦              L-382 (C-130)               ¦                       ¦          ¦ ¦                                          ¦ DATE: 10/29/2004      ¦ 22-2     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 2.  AUTOPILOT OFF or    C ¦ 2  ¦ 1  ¦                                     | ¦ ¦     AP DISENG Light       ¦    ¦    ¦                                     | ¦

¦                         B ¦ -  ¦ 0  ¦ May be inoperative provided         | ¦ ¦                           ¦    ¦    ¦ autopilot is considered inoperative | ¦ ¦                           ¦    ¦    ¦ and not used.                       | ¦

¦ 3.  Autopilot Release   C ¦ 2  ¦ 1  ¦ One may be inoperative provided:    | ¦ ¦     Switch, Wheel         ¦    ¦    ¦     a) Pilot using the autopilot    | ¦ ¦     Mounted               ¦    ¦    ¦        has an operative release       ¦ ¦                           ¦    ¦    ¦        switch, and                  | ¦ ¦                           ¦    ¦    ¦     b) Autopilot is not operated      ¦ ¦                           ¦    ¦    ¦        below initial approach         ¦ ¦                           ¦    ¦    ¦        altitude.                      ¦

¦                         B ¦ 2  ¦ 0  ¦ May be inoperative provided         | ¦ ¦                           ¦    ¦    ¦ autopilot is considered inoperative | ¦ ¦                           ¦    ¦    ¦ and not used.                       | ¦

¦ 4.  Radio Beam Coupler    ¦    ¦    ¦ Moved to 22-1, Revision 19.         | ¦

¦ 5.  Autopilot Trim      B ¦ 3  ¦ 0  ¦ May be inoperative provided         | ¦ ¦     Indices (E-4)         ¦    ¦    ¦ autopilot is considered inoperative | ¦ ¦                           ¦    ¦    ¦ and not used.                         ¦

¦ 6.  Yaw Damper (AP105)  B ¦ 1  ¦ 0  ¦ May be inoperative provided         | ¦ ¦                           ¦    ¦    ¦ autopilot is considered inoperative | ¦ ¦                           ¦    ¦    ¦ and not used.                       | ¦

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

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 19       ¦ PAGE:    ¦ ¦              L-382 (C-130)               ¦                       ¦          ¦ ¦                                          ¦ DATE: 10/29/2004      ¦ 23-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 23  COMMUNICATIONS        ¦    ¦    ¦                                       ¦

¦ 1.  Crewmember            ¦    ¦    ¦                                     | ¦ ¦     Interphone System     ¦    ¦    ¦                                     | ¦

¦     1) Flight Station   C ¦ 1  ¦ 0  ¦ (O)May be inoperative provided      | ¦ ¦        to Cargo           ¦    ¦    ¦ alternate Normal and Emergency      | ¦ ¦        Compartment,       ¦    ¦    ¦ Procedures and/or operating         | ¦ ¦        Cargo Compartment  ¦    ¦    ¦ restrictions are established and    | ¦ ¦        To Flight Station  ¦    ¦    ¦ used.                               | ¦ ¦        Function           ¦    ¦    ¦                                     | ¦ ¦                           ¦    ¦    ¦ NOTE: Any station functions that    | ¦ ¦                           ¦    ¦    ¦       operate normally may be used. | ¦

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

¦     2) Flight Station   C ¦ 1  ¦ 0  ¦ (O)May be inoperative provided      | ¦ ¦        to Ground          ¦    ¦    ¦ alternate procedures are            | ¦ ¦        Function           ¦    ¦    ¦ established and used.               | ¦

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

¦     3) Flight Station   C ¦ 1  ¦ 0  ¦ (O)May be inoperative provided:     | ¦ ¦        to Passenger       ¦    ¦    ¦     a) Public Address System is     | ¦ ¦        Cabin, Passenger   ¦    ¦    ¦        operative, and               | ¦ ¦        Cabin to Flight    ¦    ¦    ¦     b) Alternate procedures are     | ¦ ¦        Station Function   ¦    ¦    ¦        established and used.        | ¦ ¦        (Combi Aircraft    ¦    ¦    ¦                                     | ¦ ¦        Only)              ¦    ¦    ¦ NOTE: Any station functions that    | ¦ ¦                           ¦    ¦    ¦       operate normally may be used. | ¦

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

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

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 19       ¦ PAGE:    ¦ ¦              L-382 (C-130)               ¦                       ¦          ¦ ¦                                          ¦ DATE: 10/29/2004      ¦ 23-2     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 23  COMMUNICATIONS        ¦    ¦    ¦                                       ¦

¦ 2.  Public Address (PA)   ¦    ¦    ¦                                       ¦ ¦ *** System                ¦    ¦    ¦                                     | ¦

¦     1) Passenger/Combi  B ¦ 1  ¦ 0  ¦ (O)May be inoperative provided:     | ¦ ¦        Configuration      ¦    ¦    ¦     a) Alternate Normal and           ¦ ¦                           ¦    ¦    ¦        Emergency Procedures and/or  | ¦ ¦                           ¦    ¦    ¦        operating restrictions are     ¦ ¦                           ¦    ¦    ¦        established and used, and      ¦ ¦                           ¦    ¦    ¦     b) Flight Station to Cabin      | ¦ ¦                           ¦    ¦    ¦        Interphone System is           ¦ ¦                           ¦    ¦    ¦        operative.                     ¦

¦                           ¦    ¦    ¦ NOTE: Any station functions that    | ¦ ¦                           ¦    ¦    ¦       operate normally may be used. | ¦

¦        a) Lavatory      C ¦ 1  ¦ 0  ¦ (O)May be inoperative provided      | ¦ ¦           Speaker         ¦    ¦    ¦ alternate procedures are            | ¦ ¦                           ¦    ¦    ¦ established and used.               | ¦

¦     2) Cargo            C ¦ 1  ¦ 0  ¦ (O)May be inoperative provided      | ¦ ¦        Configuration      ¦    ¦    ¦ alternate Normal and Emergency      | ¦ ¦                           ¦    ¦    ¦ Procedures and/or operating         | ¦ ¦                           ¦    ¦    ¦ restrictions are established and    | ¦ ¦                           ¦    ¦    ¦ used.                               | ¦

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

¦        a) Lavatory      C ¦ 1  ¦ 0  ¦ (O)May be inoperative provided      | ¦ ¦           Speaker         ¦    ¦    ¦ alternate procedures are            | ¦ ¦                           ¦    ¦    ¦ established and used.               | ¦

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

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

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 19       ¦ PAGE:    ¦ ¦              L-382 (C-130)               ¦                       ¦          ¦ ¦                                          ¦ DATE: 10/29/2004      ¦ 23-3     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 23  COMMUNICATIONS        ¦    ¦    ¦                                       ¦

¦ 3.  Communication       D ¦ -  ¦ -  ¦ Any in excess of those required by  | ¦ ¦     Systems (VHF, UHF)    ¦    ¦    ¦ FAR may be inoperative provided     | ¦ ¦                           ¦    ¦    ¦ Communications Systems powered by     ¦ ¦                           ¦    ¦    ¦ Isolated DC Bus are operative.        ¦

¦     1) VHF Comm           ¦    ¦    ¦                                     | ¦ ¦        Control Panels     ¦    ¦    ¦                                     | ¦

¦        a) Frequency     C ¦ -  ¦ 0  ¦                                     | ¦ ¦           Transfer        ¦    ¦    ¦                                     | ¦ ¦           Lights          ¦    ¦    ¦                                     | ¦

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

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

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

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

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 19       ¦ PAGE:    ¦ ¦              L-382 (C-130)               ¦                       ¦          ¦ ¦                                          ¦ DATE: 10/29/2004      ¦ 23-4     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 23  COMMUNICATIONS        ¦    ¦    ¦                                       ¦

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

¦                         C ¦ -  ¦ 1  ¦ (O)May be inoperative while         | ¦ ¦                           ¦    ¦    ¦ conducting operations that require  | ¦ ¦                           ¦    ¦    ¦ two LRCS provided:                  | ¦ ¦                           ¦    ¦    ¦     a) SATCOM Voice or Data Link    | ¦ ¦                           ¦    ¦    ¦        operates normally,           | ¦ ¦                           ¦    ¦    ¦     b) Alternate procedures are     | ¦ ¦                           ¦    ¦    ¦        established and used,        | ¦ ¦                           ¦    ¦    ¦     c) SATCOM coverage is available | ¦ ¦                           ¦    ¦    ¦        over the intended route of   | ¦ ¦                           ¦    ¦    ¦        flight, and                  | ¦ ¦                           ¦    ¦    ¦     d) Prior coordination with the  | ¦ ¦                           ¦    ¦    ¦        appropriate ATS facility is  | ¦ ¦                           ¦    ¦    ¦        required when Inmarsat Codes | ¦ ¦                           ¦    ¦    ¦        for SATCOM Voice are not     | ¦ ¦                           ¦    ¦    ¦        available.                   | ¦

¦                           ¦    ¦    ¦ NOTE: SATCOM is to be used only as  | ¦ ¦                           ¦    ¦    ¦       a backup to normal HF         | ¦ ¦                           ¦    ¦    ¦       communications unless         | ¦ ¦                           ¦    ¦    ¦       otherwise authorized by the   | ¦ ¦                           ¦    ¦    ¦       appropriate ATS facilities.   | ¦

¦ 5.  Audio Selector        ¦    ¦    ¦                                       ¦ ¦     Panels                ¦    ¦    ¦                                     | ¦

¦     1) NAV Station      D ¦ 1  ¦ 0  ¦ As required by FAR.                 | ¦

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

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 19       ¦ PAGE:    ¦ ¦              L-382 (C-130)               ¦                       ¦          ¦ ¦                                          ¦ DATE: 10/29/2004      ¦ 23-5     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 23  COMMUNICATIONS        ¦    ¦    ¦                                       ¦

¦ 6.  Boom Microphones      ¦    ¦    ¦                                       ¦

¦     1) Cockpit Voice    A ¦ -  ¦ 0  ¦ May be inoperative provided:          ¦ ¦        Recorder           ¦    ¦    ¦     a) Flight Data Recorder (FDR)     ¦ ¦        Equipped to        ¦    ¦    ¦        is operative, and              ¦ ¦        Record Boom        ¦    ¦    ¦     b) Repair is made within three    ¦ ¦        Microphone per     ¦    ¦    ¦        flight days.                   ¦ ¦        FAR 121.139(e),    ¦    ¦    ¦                                       ¦ ¦        135.151(d), or     ¦    ¦    ¦                                       ¦ ¦        125.227(e)         ¦    ¦    ¦                                       ¦

¦     2) Cockpit Voice    D ¦ -  ¦ 0  ¦                                       ¦ ¦        Recorder Not       ¦    ¦    ¦                                       ¦ ¦        Equipped to        ¦    ¦    ¦                                       ¦ ¦        Record Boom        ¦    ¦    ¦                                       ¦ ¦        Microphone         ¦    ¦    ¦                                       ¦

¦ 7.  Megaphones            ¦    ¦    ¦ Moved to 25-9, Revision 19.         | ¦

¦ 8.  Cockpit Voice       A ¦ 1  ¦ 0  ¦ May be inoperative provided:          ¦ ¦     Recorder (CVR)        ¦    ¦    ¦     a) Flight Data Recorder (FDR)     ¦ ¦                           ¦    ¦    ¦        is operative, and              ¦ ¦                           ¦    ¦    ¦     b) Repair is made within three    ¦ ¦                           ¦    ¦    ¦        flight days.                   ¦

¦ 9.  Selective Call      C ¦ -  ¦ 0  ¦ (O)May be inoperative provided      | ¦ ¦ *** System (SELCAL)       ¦    ¦    ¦ flight crew monitors appropriate    | ¦ ¦                           ¦    ¦    ¦ communications frequency.           | ¦

¦                         D ¦ -  ¦ 0  ¦ May be inoperative provided         | ¦ ¦                           ¦    ¦    ¦ procedures do not require its use.  | ¦

¦ 10. Radio Management    B ¦ 2  ¦ 1  ¦ (O)May be inoperative provided:       ¦ ¦     Unit (RMU)            ¦    ¦    ¦     a) Cross-side tuning function     ¦ ¦     (STC#ST01162LA)       ¦    ¦    ¦        of the operative RMU           ¦ ¦                           ¦    ¦    ¦        operates normally, and         ¦ ¦                           ¦    ¦    ¦     b) Radio tuning function of       ¦ ¦                           ¦    ¦    ¦        both FMS CDUs operate          ¦ ¦                           ¦    ¦    ¦        normally.                      ¦

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

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 19       ¦ PAGE:    ¦ ¦              L-382 (C-130)               ¦                       ¦          ¦ ¦                                          ¦ DATE: 10/29/2004      ¦ 23-6     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 23  COMMUNICATIONS        ¦    ¦    ¦                                       ¦

¦ 11. Intercom Control    C ¦ -  ¦ 0  ¦ (O)May be inoperative provided        ¦ ¦     Panel (ICS)           ¦    ¦    ¦ alternate procedures are              ¦ ¦                           ¦    ¦    ¦ established and used.                 ¦

¦                         D ¦ -  ¦ 0  ¦ May be inoperative provided           ¦ ¦                           ¦    ¦    ¦ procedures do not require its use.    ¦

¦ 12. Satellite           C ¦ -  ¦ 0  ¦ (O)May be inoperative provided        ¦ ¦     Communications        ¦    ¦    ¦ alternate procedures are              ¦ ¦     System (SATCOM)       ¦    ¦    ¦ established and used.                 ¦

¦                         D ¦ -  ¦ 0  ¦ May be inoperative provided           ¦ ¦                           ¦    ¦    ¦ procedures do not require its use.    ¦

¦ 13. Data Link System    C ¦ -  ¦ 0  ¦ (O)May be inoperative provided        ¦ ¦                           ¦    ¦    ¦ alternate procedures are              ¦ ¦                           ¦    ¦    ¦ established and used.                 ¦

¦                         D ¦ -  ¦ 0  ¦ May be inoperative provided           ¦ ¦                           ¦    ¦    ¦ procedures do not require its use.    ¦

¦ 14. Push-To-Talk          ¦    ¦    ¦                                     | ¦ ¦     Switches (PTT)        ¦    ¦    ¦                                     | ¦

¦     1) Control Wheel    C ¦ 2  ¦ 1  ¦ (M)May be inoperative provided:     | ¦ ¦        Switches           ¦    ¦    ¦     a) Associated audio control     | ¦ ¦                           ¦    ¦    ¦        panel PTT or hand microphone | ¦ ¦                           ¦    ¦    ¦        operates normally, and       | ¦ ¦                           ¦    ¦    ¦     b) Failed switch is verified    | ¦ ¦                           ¦    ¦    ¦        failed open.                 | ¦

¦                           ¦    ¦    ¦ (Continued)                         | ¦

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

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 19       ¦ PAGE:    ¦ ¦              L-382 (C-130)               ¦                       ¦          ¦ ¦                                          ¦ DATE: 10/29/2004      ¦ 23-7     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 23  COMMUNICATIONS        ¦    ¦    ¦                                       ¦

¦ 14. Push-To-Talk          ¦    ¦    ¦                                     | ¦ ¦     Switches (PTT)        ¦    ¦    ¦                                     | ¦ ¦     (Cont'd)              ¦    ¦    ¦                                     | ¦

¦ *** 2) Engineer's       C ¦ -  ¦ 1  ¦ (M)May be inoperative provided:     | ¦ ¦        Push-To-Talk       ¦    ¦    ¦     a) Associated audio control     | ¦ ¦        Switch             ¦    ¦    ¦        panel PTT or hand microphone | ¦ ¦        (Includes Foot     ¦    ¦    ¦        operates normally, and       | ¦ ¦        Switch)            ¦    ¦    ¦     b) Failed switch is verified    | ¦ ¦                           ¦    ¦    ¦        failed open.                 | ¦

¦     3) Other Stations   C ¦ -  ¦ -  ¦ (M)May be inoperative provided:     | ¦ ¦        Switches           ¦    ¦    ¦     a) Associated audio control     | ¦ ¦                           ¦    ¦    ¦        panel PTT or hand microphone | ¦ ¦                           ¦    ¦    ¦        operates normally, and       | ¦ ¦                           ¦    ¦    ¦     b) Failed switch is verified    | ¦ ¦                           ¦    ¦    ¦        failed open.                 | ¦

¦ 15. Headphones/Hand     D ¦ -  ¦ -  ¦ Any in excess of those required by  | ¦ ¦ *** Microphones           ¦    ¦    ¦ FAR for flight deck crewmembers may | ¦ ¦                           ¦    ¦    ¦ be inoperative or missing.          | ¦

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

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 19       ¦ PAGE:    ¦ ¦              L-382 (C-130)               ¦                       ¦          ¦ ¦                                          ¦ DATE: 10/29/2004      ¦ 24-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 24  ELECTRICAL POWER      ¦    ¦    ¦                                       ¦

¦ 1.  Frequency Meter     C ¦ 1  ¦ 0  ¦ May be inoperative provided all     | ¦ ¦     System                ¦    ¦    ¦ Engine Tachometers are operative.   | ¦

¦ 2.  AC Generator          ¦    ¦    ¦                                       ¦ ¦     (Engine Driven)       ¦    ¦    ¦                                       ¦

¦     1) C-130A           B ¦ 2  ¦ 1  ¦ (M)May be inoperative provided:     | ¦ ¦                           ¦    ¦    ¦     a) ATM Generator is operative,    ¦ ¦                           ¦    ¦    ¦        and                            ¦ ¦                           ¦    ¦    ¦     b) Affected Generator or          ¦ ¦                           ¦    ¦    ¦        Generator Drive Shaft is       ¦ ¦                           ¦    ¦    ¦        removed using an accepted      ¦ ¦                           ¦    ¦    ¦        procedure.                     ¦

¦                         B ¦ 2  ¦ 1  ¦ (M)May be inoperative provided:     | ¦ ¦                           ¦    ¦    ¦     a) ATM Generator is operative,  | ¦ ¦                           ¦    ¦    ¦     b) Affected Generator is        | ¦ ¦                           ¦    ¦    ¦        verified mechanically sound,   ¦ ¦                           ¦    ¦    ¦        and                            ¦ ¦                           ¦    ¦    ¦     c) Associated Generator Bearing | ¦ ¦                           ¦    ¦    ¦        Failure light is operative.    ¦

¦     2) Except C-130A    C ¦ 4  ¦ 3  ¦ (M)May be inoperative provided      | ¦ ¦                           ¦    ¦    ¦ affected Generator or Generator     | ¦ ¦                           ¦    ¦    ¦ Drive Shaft is removed using an     | ¦ ¦                           ¦    ¦    ¦ accepted procedure.                 | ¦

¦                         B ¦ 4  ¦ 3  ¦ (M)May be inoperative provided:     | ¦ ¦                           ¦    ¦    ¦     a) Affected Generator is        | ¦ ¦                           ¦    ¦    ¦        verified mechanically sound,   ¦ ¦                           ¦    ¦    ¦        and                            ¦ ¦                           ¦    ¦    ¦     b) Associated Generator Bearing | ¦ ¦                           ¦    ¦    ¦        Failure light is operative.    ¦

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

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 19       ¦ PAGE:    ¦ ¦              L-382 (C-130)               ¦                       ¦          ¦ ¦                                          ¦ DATE: 10/29/2004      ¦ 24-2     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 24  ELECTRICAL POWER      ¦    ¦    ¦                                       ¦

¦ 3.  AC Generator          ¦    ¦    ¦                                     | ¦ ¦     (ATM/APU)             ¦    ¦    ¦                                     | ¦

¦     1) C-130A           B ¦ 1  ¦ 0  ¦ May be inoperative provided:          ¦ ¦                           ¦    ¦    ¦     a) Both Engine Driven AC          ¦ ¦                           ¦    ¦    ¦        Generators are operative,      ¦ ¦                           ¦    ¦    ¦        and                            ¦ ¦                           ¦    ¦    ¦     b) All Inverters are operative.   ¦

¦     2) Except C-130A    C ¦ 1  ¦ 0  ¦                                       ¦

¦ 4.  Essential Bus       C ¦ 2  ¦ 1  ¦                                     | ¦ ¦     Transformer           ¦    ¦    ¦                                       ¦ ¦     Rectifier (Except     ¦    ¦    ¦                                       ¦ ¦     C-130A)               ¦    ¦    ¦                                       ¦

¦ 5.  Generator OUT Light C ¦ 5  ¦ -  ¦ May be inoperative provided         | ¦ ¦                           ¦    ¦    ¦ associated Generator is considered    ¦ ¦                           ¦    ¦    ¦ inoperative.                          ¦

¦                         B ¦ 5  ¦ 4  ¦ May be inoperative provided         | ¦ ¦                           ¦    ¦    ¦ Frequency Meter is operative.       | ¦

¦ 6.  Generator Bearing     ¦    ¦    ¦                                     | ¦ ¦     Failure Light         ¦    ¦    ¦                                       ¦

¦     1) C-130A           B ¦ 2  ¦ 1  ¦ (M)May be inoperative provided      | ¦ ¦                           ¦    ¦    ¦ the Generator or Generator Drive      ¦ ¦                           ¦    ¦    ¦ Shaft is removed using an accepted    ¦ ¦                           ¦    ¦    ¦ procedure.                            ¦

¦     2) Except C-130A    C ¦ 4  ¦ 3  ¦ (M)May be inoperative provided      | ¦ ¦                           ¦    ¦    ¦ the Generator or Generator Drive      ¦ ¦                           ¦    ¦    ¦ Shaft is removed using an accepted    ¦ ¦                           ¦    ¦    ¦ procedure.                            ¦

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

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 19       ¦ PAGE:    ¦ ¦              L-382 (C-130)               ¦                       ¦          ¦ ¦                                          ¦ DATE: 10/29/2004      ¦ 24-3     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 24  ELECTRICAL POWER      ¦    ¦    ¦                                       ¦

¦ 7.  AC Loadmeter (40      ¦    ¦    ¦                                     | ¦ ¦     KVA Generator)        ¦    ¦    ¦                                       ¦

¦     1) C-130A           B ¦ 3  ¦ 2  ¦ May be inoperative provided         | ¦ ¦                           ¦    ¦    ¦ associated generator is considered  | ¦ ¦                           ¦    ¦    ¦ inoperative and not used.           | ¦

¦     2) Except C-130A    C ¦ 5  ¦ -  ¦ May be inoperative provided         | ¦ ¦                           ¦    ¦    ¦ associated generator is considered  | ¦ ¦                           ¦    ¦    ¦ inoperative and not used.           | ¦

¦ 8.  AC Instruments and  B ¦ 1  ¦ 0  ¦ May be inoperative provided AC      | ¦ ¦     Engine Fuel Control   ¦    ¦    ¦ electrical power is available for   | ¦ ¦     Inverter (2500 VA)    ¦    ¦    ¦ engine start.                       | ¦ ¦     (Except C-130A)       ¦    ¦    ¦                                     | ¦

¦ 9.  Co-Pilot's AC         ¦    ¦    ¦ Deleted, Revision 19.               | ¦ ¦     Instruments Inverter  ¦    ¦    ¦                                     | ¦ ¦     (250 VA) (Except      ¦    ¦    ¦                                     | ¦ ¦     C-130A)               ¦    ¦    ¦                                     | ¦

¦ 10. Inverter (500 VA)   B ¦ 1  ¦ 0  ¦ May be inoperative provided both AC | ¦ ¦     Pilot's (C-130A)      ¦    ¦    ¦ Generators are operative.             ¦

¦ 11. Inverter (100 VA)   B ¦ 1  ¦ 0  ¦ May be inoperative provided both AC | ¦ ¦     Copilot's (C-130A)    ¦    ¦    ¦ Generators are operative.             ¦

¦ 12. DC Generators       B ¦ 4  ¦ 3  ¦ May be inoperative provided         | ¦ ¦     (C-130A)              ¦    ¦    ¦ associated voltmeter and ammeter      ¦ ¦                           ¦    ¦    ¦ are operative.                        ¦

¦ 13. Transformer         B ¦ 2  ¦ 1  ¦                                     | ¦ ¦     Rectifier (C-130A)    ¦    ¦    ¦                                       ¦

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

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 18       ¦ PAGE:    ¦ ¦              L-382 (C-130)               ¦                       ¦          ¦ ¦                                          ¦ DATE: 04/15/1994      ¦ 25-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 25  EQUIPMENT/FURNISHINGS ¦    ¦    ¦                                       ¦

¦ 1.  Crewmember Shoulder   ¦    ¦    ¦ DELETED in Revision 18.               ¦ ¦     Harness               ¦    ¦    ¦                                       ¦

¦ 2.  Emergency Locator   A ¦ -  ¦ 0  ¦ (M)May be inoperative provided:       ¦ ¦ *** Transmitter (ELT)     ¦    ¦    ¦     a) Affected ELT is deactivated    ¦ ¦                           ¦    ¦    ¦        or removed using accepted      ¦ ¦                           ¦    ¦    ¦        procedures, and                ¦ ¦                           ¦    ¦    ¦     b) Repair is made within FAR      ¦ ¦                           ¦    ¦    ¦        time limits.                   ¦

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

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 19       ¦ PAGE:    ¦ ¦              L-382 (C-130)               ¦                       ¦          ¦ ¦                                          ¦ DATE: 10/29/2004      ¦ 25-2     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 25  EQUIPMENT/FURNISHINGS ¦    ¦    ¦                                       ¦

¦ 3.  Flight Attendant      ¦    ¦    ¦                                       ¦ ¦     Seat (Single or       ¦    ¦    ¦                                       ¦ ¦     Dual Position)        ¦    ¦    ¦                                       ¦

¦     Aircraft With       A ¦ 1  ¦ 0  ¦ (M)(O)May be inoperative provided:  | ¦ ¦     Only One Flight       ¦    ¦    ¦     a) Affected seat is not         | ¦ ¦     Attendant Seat        ¦    ¦    ¦        occupied,                    | ¦ ¦                           ¦    ¦    ¦     b) Flight Attendant displaced   | ¦ ¦                           ¦    ¦    ¦        by inoperative seat occupies | ¦ ¦                           ¦    ¦    ¦        the passenger seat most      | ¦ ¦                           ¦    ¦    ¦        accessible to the            | ¦ ¦                           ¦    ¦    ¦        inoperative seat,            | ¦ ¦                           ¦    ¦    ¦     c) Alternate procedures are     | ¦ ¦                           ¦    ¦    ¦        established and used as      | ¦ ¦                           ¦    ¦    ¦        published in crewmember      | ¦ ¦                           ¦    ¦    ¦        manuals,                     | ¦ ¦                           ¦    ¦    ¦     d) Folding type seat stows      | ¦ ¦                           ¦    ¦    ¦        automatically or is secured  | ¦ ¦                           ¦    ¦    ¦        in the retracted position,   | ¦ ¦                           ¦    ¦    ¦     e) Passenger seat assigned to   | ¦ ¦                           ¦    ¦    ¦        Flight Attendant is          | ¦ ¦                           ¦    ¦    ¦        placarded "FOR FLIGHT        | ¦ ¦                           ¦    ¦    ¦        ATTENDANT USE ONLY", and     | ¦ ¦                           ¦    ¦    ¦     f) Repairs are made within two  | ¦ ¦                           ¦    ¦    ¦        (2) flight days.             | ¦

¦                           ¦    ¦    ¦ NOTE 1:  An automatic folding seat  | ¦ ¦                           ¦    ¦    ¦          that will not stow         | ¦ ¦                           ¦    ¦    ¦          automatically is           | ¦ ¦                           ¦    ¦    ¦          considered inoperative.    | ¦

¦                           ¦    ¦    ¦ NOTE 2:  A seat position with an    | ¦ ¦                           ¦    ¦    ¦          inoperative or missing     | ¦ ¦                           ¦    ¦    ¦          restraint system is        | ¦ ¦                           ¦    ¦    ¦          considered inoperative.    | ¦

¦                           ¦    ¦    ¦ (Continued)                         | ¦

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

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 19       ¦ PAGE:    ¦ ¦              L-382 (C-130)               ¦                       ¦          ¦ ¦                                          ¦ DATE: 10/29/2004      ¦ 25-3     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 25  EQUIPMENT/FURNISHINGS ¦    ¦    ¦                                       ¦

¦ 3.  Flight Attendant      ¦    ¦    ¦                                       ¦ ¦     Seat (Single or       ¦    ¦    ¦                                       ¦ ¦     Dual Position)        ¦    ¦    ¦                                       ¦ ¦     (Continued)           ¦    ¦    ¦                                     | ¦

¦     Aircraft With         ¦    ¦    ¦                                     | ¦ ¦     Only One Flight       ¦    ¦    ¦                                     | ¦ ¦     Attendant Seat        ¦    ¦    ¦                                     | ¦ ¦     (Continued)           ¦    ¦    ¦                                     | ¦

¦                           ¦    ¦    ¦ NOTE 3:  The above provisos apply   | ¦ ¦                           ¦    ¦    ¦          to flight attendant seats. | ¦ ¦                           ¦    ¦    ¦          Individual operators, when | ¦ ¦                           ¦    ¦    ¦          operating with inoperative | ¦ ¦                           ¦    ¦    ¦          seats, will consider the   | ¦ ¦                           ¦    ¦    ¦          locations and combinations | ¦ ¦                           ¦    ¦    ¦          of seats to ensure that    | ¦ ¦                           ¦    ¦    ¦          the proximity to exits and | ¦ ¦                           ¦    ¦    ¦          distribution requirements  | ¦ ¦                           ¦    ¦    ¦          of the applicable FAR are  | ¦ ¦                           ¦    ¦    ¦          met.                       | ¦

¦                           ¦    ¦    ¦ (Continued)                         | ¦

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

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 19       ¦ PAGE:    ¦ ¦              L-382 (C-130)               ¦                       ¦          ¦ ¦                                          ¦ DATE: 10/29/2004      ¦ 25-4     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 25  EQUIPMENT/FURNISHINGS ¦    ¦    ¦                                       ¦

¦ 3.  Flight Attendant      ¦    ¦    ¦                                     | ¦ ¦     Seat (Single or       ¦    ¦    ¦                                     | ¦ ¦     Dual Position)        ¦    ¦    ¦                                     | ¦ ¦     (Continued)           ¦    ¦    ¦                                     | ¦

¦     Aircraft With More    ¦    ¦    ¦                                     | ¦ ¦     Than One Flight       ¦    ¦    ¦                                     | ¦ ¦     Attendant Seat        ¦    ¦    ¦                                     | ¦

¦     1) Required Flight  B ¦ -  ¦ -  ¦ (M)(O)One seat or assembly (dual    | ¦ ¦        Attendant Seats    ¦    ¦    ¦ position) may be inoperative        | ¦ ¦                           ¦    ¦    ¦ provided:                           | ¦ ¦                           ¦    ¦    ¦     a) Affected seat position or    | ¦ ¦                           ¦    ¦    ¦        seat assembly is not         | ¦ ¦                           ¦    ¦    ¦        occupied,                    | ¦ ¦                           ¦    ¦    ¦     b) Flight Attendant(s)          | ¦ ¦                           ¦    ¦    ¦        displaced by inoperative     | ¦ ¦                           ¦    ¦    ¦        seat(s) occupies either an   | ¦ ¦                           ¦    ¦    ¦        an adjacent flight attendant | ¦ ¦                           ¦    ¦    ¦        seat or the passenger seat   | ¦ ¦                           ¦    ¦    ¦        which is most accessible to  | ¦ ¦                           ¦    ¦    ¦        the inoperative seat(s), so  | ¦ ¦                           ¦    ¦    ¦        as to most effectively       | ¦ ¦                           ¦    ¦    ¦        perform assigned duties,     | ¦ ¦                           ¦    ¦    ¦     c) Alternate procedures are     | ¦ ¦                           ¦    ¦    ¦        established and used as      | ¦ ¦                           ¦    ¦    ¦        published in crewmember      | ¦ ¦                           ¦    ¦    ¦        manuals,                     | ¦ ¦                           ¦    ¦    ¦     d) Folding type seat stows      | ¦ ¦                           ¦    ¦    ¦        automatically or is secured  | ¦ ¦                           ¦    ¦    ¦        in the retracted position,   | ¦ ¦                           ¦    ¦    ¦        and                          | ¦ ¦                           ¦    ¦    ¦     e) Passenger seat assigned to   | ¦ ¦                           ¦    ¦    ¦        Flight Attendant is          | ¦ ¦                           ¦    ¦    ¦        placarded "FOR FLIGHT        | ¦ ¦                           ¦    ¦    ¦        ATTENDANT USE ONLY".         | ¦

¦                           ¦    ¦    ¦ (Continued)                         | ¦

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

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 19       ¦ PAGE:    ¦ ¦              L-382 (C-130)               ¦                       ¦          ¦ ¦                                          ¦ DATE: 10/29/2004      ¦ 25-5     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 25  EQUIPMENT/FURNISHINGS ¦    ¦    ¦                                       ¦

¦ 3.  Flight Attendant      ¦    ¦    ¦                                     | ¦ ¦     Seat (Single or       ¦    ¦    ¦                                     | ¦ ¦     Dual Position)        ¦    ¦    ¦                                     | ¦ ¦     (Continued)           ¦    ¦    ¦                                     | ¦

¦     Aircraft With More    ¦    ¦    ¦                                     | ¦ ¦     Than One Flight       ¦    ¦    ¦                                     | ¦ ¦     Attendant Seat        ¦    ¦    ¦                                     | ¦ ¦     (Continued)           ¦    ¦    ¦                                     | ¦

¦     1) Required Flight    ¦    ¦    ¦                                     | ¦ ¦        Attendant Seats    ¦    ¦    ¦                                     | ¦ ¦        (Continued)        ¦    ¦    ¦ NOTE 1:  An automatic folding seat  | ¦ ¦                           ¦    ¦    ¦          that will not stow         | ¦ ¦                           ¦    ¦    ¦          automatically is           | ¦ ¦                           ¦    ¦    ¦          considered inoperative.    | ¦

¦                           ¦    ¦    ¦ NOTE 2:  A seat position with an    | ¦ ¦                           ¦    ¦    ¦          inoperative or missing     | ¦ ¦                           ¦    ¦    ¦          restraint system is        | ¦ ¦                           ¦    ¦    ¦          considered inoperative.    | ¦

¦                           ¦    ¦    ¦ NOTE 3:  Individual operators, when | ¦ ¦                           ¦    ¦    ¦          operating with inoperative | ¦ ¦                           ¦    ¦    ¦          seats, will consider the   | ¦ ¦                           ¦    ¦    ¦          locations and combinations | ¦ ¦                           ¦    ¦    ¦          of seats to ensure that    | ¦ ¦                           ¦    ¦    ¦          the proximity to exits and | ¦ ¦                           ¦    ¦    ¦          distribution requirements  | ¦ ¦                           ¦    ¦    ¦          of the applicable FAR are  | ¦ ¦                           ¦    ¦    ¦          met.                       | ¦

¦                           ¦    ¦    ¦ NOTE 4:  If one side of a dual seat | ¦ ¦                           ¦    ¦    ¦          assembly is inoperative    | ¦ ¦                           ¦    ¦    ¦          and a flight attendant is  | ¦ ¦                           ¦    ¦    ¦          displaced to an adjacent   | ¦ ¦                           ¦    ¦    ¦          seat, the adjacent seat    | ¦ ¦                           ¦    ¦    ¦          must operate normally      | ¦

¦                           ¦    ¦    ¦ (Continued)                         | ¦

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

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 19       ¦ PAGE:    ¦ ¦              L-382 (C-130)               ¦                       ¦          ¦ ¦                                          ¦ DATE: 10/29/2004      ¦ 25-6     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 25  EQUIPMENT/FURNISHINGS ¦    ¦    ¦                                       ¦

¦ 3.  Flight Attendant      ¦    ¦    ¦                                     | ¦ ¦     Seat (Single or       ¦    ¦    ¦                                     | ¦ ¦     Dual Position)        ¦    ¦    ¦                                     | ¦ ¦     (Continued)           ¦    ¦    ¦                                     | ¦

¦     Aircraft With More    ¦    ¦    ¦                                     | ¦ ¦     Than One Flight       ¦    ¦    ¦                                     | ¦ ¦     Attendant Seat        ¦    ¦    ¦                                     | ¦ ¦     (Continued)           ¦    ¦    ¦                                     | ¦

¦     2) Excess Flight    C ¦ -  ¦ -  ¦ (M)May be inoperative provided:     | ¦ ¦        Attendant Seats    ¦    ¦    ¦     a) Affected seat position or    | ¦ ¦                           ¦    ¦    ¦        seat assembly is not         | ¦ ¦                           ¦    ¦    ¦        occupied, and                | ¦ ¦                           ¦    ¦    ¦     b) Folding type seat stows      | ¦ ¦                           ¦    ¦    ¦        automatically or is secured  | ¦ ¦                           ¦    ¦    ¦        in the retracted position.   | ¦

¦                           ¦    ¦    ¦ NOTE 1:  An automatic folding seat  | ¦ ¦                           ¦    ¦    ¦          that will not stow         | ¦ ¦                           ¦    ¦    ¦          automatically is           | ¦ ¦                           ¦    ¦    ¦          considered inoperative.    | ¦

¦                           ¦    ¦    ¦ NOTE 2:  A seat position with an    | ¦ ¦                           ¦    ¦    ¦          inoperative or missing     | ¦ ¦                           ¦    ¦    ¦          restraint system is        | ¦ ¦                           ¦    ¦    ¦          considered inoperative.    | ¦

¦     3) All Cargo        D ¦ -  ¦ -  ¦ May be inoperative provided         | ¦ ¦        Configuration      ¦    ¦    ¦ affected seat or seat assembly is   | ¦ ¦                           ¦    ¦    ¦ not occupied.                       | ¦

¦ 4.  Flight Attendant      ¦    ¦    ¦ Moved to 25-3, Revision 19.         | ¦ ¦     Seat Lap Belt         ¦    ¦    ¦                                       ¦

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

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 19       ¦ PAGE:    ¦ ¦              L-382 (C-130)               ¦                       ¦          ¦ ¦                                          ¦ DATE: 10/29/2004      ¦ 25-7     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 25  EQUIPMENT/FURNISHINGS ¦    ¦    ¦                                       ¦

¦ 5.  Observer Seat(s)      ¦    ¦    ¦                                     | ¦

¦     1) Primary          A ¦ -  ¦ -  ¦ May be inoperative provided:        | ¦ ¦        Observer Seat      ¦    ¦    ¦     a) A passenger seat in the      | ¦ ¦        (Including         ¦    ¦    ¦        passenger cabin is made      | ¦ ¦        Associated         ¦    ¦    ¦        available to an FAA          | ¦ ¦        Equipment)         ¦    ¦    ¦        inspector for performance of | ¦ ¦                           ¦    ¦    ¦        official duties, and         | ¦ ¦                           ¦    ¦    ¦     b) Repairs are made within two  | ¦ ¦                           ¦    ¦    ¦        flight days.                 | ¦

¦                         A ¦ -  ¦ -  ¦ May be inoperative provided:        | ¦ ¦                           ¦    ¦    ¦     a) The secondary observer's     | ¦ ¦                           ¦    ¦    ¦        seat is available to the FAA | ¦ ¦                           ¦    ¦    ¦        inspector for performance of | ¦ ¦                           ¦    ¦    ¦        official duties, and         | ¦ ¦                           ¦    ¦    ¦     b) Repairs are made within two  | ¦ ¦                           ¦    ¦    ¦        flight days.                 | ¦

¦                         A ¦ -  ¦ -  ¦ May be inoperative provided:        | ¦ ¦                           ¦    ¦    ¦     a) Required minimum safety      | ¦ ¦                           ¦    ¦    ¦        equipment (safety belt and   | ¦ ¦                           ¦    ¦    ¦        oxygen) is available,        | ¦ ¦                           ¦    ¦    ¦     b) Seat is acceptable to the    | ¦ ¦                           ¦    ¦    ¦        FAA inspector for            | ¦ ¦                           ¦    ¦    ¦        performance of official      | ¦ ¦                           ¦    ¦    ¦        duties, and                  | ¦ ¦                           ¦    ¦    ¦     c) Repairs are made within two  | ¦ ¦                           ¦    ¦    ¦        flight days.                 | ¦ ¦                           ¦    ¦    ¦                                     | ¦ ¦                           ¦    ¦    ¦ (Continued)                         | ¦

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

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 19       ¦ PAGE:    ¦ ¦              L-382 (C-130)               ¦                       ¦          ¦ ¦                                          ¦ DATE: 10/29/2004      ¦ 25-8     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 25  EQUIPMENT/FURNISHINGS ¦    ¦    ¦                                       ¦

¦ 5.  Observer Seat(s)      ¦    ¦    ¦                                     | ¦

¦     1) Primary            ¦    ¦    ¦                                     | ¦ ¦        Observer Seat      ¦    ¦    ¦                                     | ¦ ¦        (Including         ¦    ¦    ¦                                     | ¦ ¦        Associated         ¦    ¦    ¦                                     | ¦ ¦        Equipment)         ¦    ¦    ¦                                     | ¦ ¦        (Cont'd)           ¦    ¦    ¦                                     | ¦ ¦                           ¦    ¦    ¦ NOTE 1:  These provisos are         | ¦ ¦                           ¦    ¦    ¦          intended to provide for    | ¦ ¦                           ¦    ¦    ¦          occupancy of the above     | ¦ ¦                           ¦    ¦    ¦          seats by an FAA inspector  | ¦ ¦                           ¦    ¦    ¦          when the minimum safety    | ¦ ¦                           ¦    ¦    ¦          equipment (oxygen and      | ¦ ¦                           ¦    ¦    ¦          safety belt) is            | ¦ ¦                           ¦    ¦    ¦          functional and the         | ¦ ¦                           ¦    ¦    ¦          inspector determines the   | ¦ ¦                           ¦    ¦    ¦          conditions to be           | ¦ ¦                           ¦    ¦    ¦          acceptable.                | ¦

¦                           ¦    ¦    ¦ NOTE 2:  The pilot-in-command will  | ¦ ¦                           ¦    ¦    ¦          determine if the minimum   | ¦ ¦                           ¦    ¦    ¦          safety equipment is        | ¦ ¦                           ¦    ¦    ¦          functional for other       | ¦ ¦                           ¦    ¦    ¦          persons authorized to      | ¦ ¦                           ¦    ¦    ¦          occupy any observer's      | ¦ ¦                           ¦    ¦    ¦          seats.                     | ¦

¦     2) Additional       D ¦ -  ¦ 0  ¦ May be inoperative.                 | ¦ ¦        Observer Seat(s)   ¦    ¦    ¦                                     | ¦ ¦        (Including         ¦    ¦    ¦ NOTE:   The pilot-in-command will   | ¦ ¦        Associated         ¦    ¦    ¦         determine if the minimum    | ¦ ¦        Equipment)         ¦    ¦    ¦         safety equipment is         | ¦ ¦                           ¦    ¦    ¦         functional for other        | ¦ ¦                           ¦    ¦    ¦         persons authorized to       | ¦ ¦                           ¦    ¦    ¦         occupy any observer's       | ¦ ¦                           ¦    ¦    ¦         seats.                      | ¦

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

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 19       ¦ PAGE:    ¦ ¦              L-382 (C-130)               ¦                       ¦          ¦ ¦                                          ¦ DATE: 10/29/2004      ¦ 25-9     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 25  EQUIPMENT/FURNISHINGS ¦    ¦    ¦                                       ¦

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

¦                           ¦    ¦    ¦ NOTE 1:  A seat with an inoperative | ¦ ¦                           ¦    ¦    ¦          seat belt is considered    | ¦ ¦                           ¦    ¦    ¦          inoperative.               | ¦

¦                           ¦    ¦    ¦ NOTE 2:  Inoperative seats do not   | ¦ ¦                           ¦    ¦    ¦          affect the required number | ¦ ¦                           ¦    ¦    ¦          of Flight Attendants.      | ¦

¦                           ¦    ¦    ¦ NOTE 3:  Affected seat(s) may       | ¦ ¦                           ¦    ¦    ¦          include the seat(s)        | ¦ ¦                           ¦    ¦    ¦          behind and/or adjacent     | ¦ ¦                           ¦    ¦    ¦          outboard seats.            | ¦

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

¦     2) Underseat        C ¦ -  ¦ -  ¦ (O)May be inoperative provided:     | ¦ ¦        Restraining Bars   ¦    ¦    ¦     a) Baggage is not stowed under  | ¦ ¦                           ¦    ¦    ¦        seat with inoperative        | ¦ ¦                           ¦    ¦    ¦        restraining bar,             | ¦ ¦                           ¦    ¦    ¦     b) Associated seat is placarded | ¦ ¦                           ¦    ¦    ¦        "DO NOT STOW BAGGAGE UNDER   | ¦ ¦                           ¦    ¦    ¦        THIS SEAT", and              | ¦ ¦                           ¦    ¦    ¦     c) Procedures are established   | ¦ ¦                           ¦    ¦    ¦        to alert Cabin Crew of       | ¦ ¦                           ¦    ¦    ¦        inoperative restraining bar. | ¦

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

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 19       ¦ PAGE:    ¦ ¦              L-382 (C-130)               ¦                       ¦          ¦ ¦                                          ¦ DATE: 10/29/2004      ¦ 25-10    ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 25  EQUIPMENT/FURNISHINGS ¦    ¦    ¦                                       ¦

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

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

¦                           ¦    ¦    ¦ NOTE:  Lavatory door ash tray is      ¦ ¦                           ¦    ¦    ¦        not considered a passenger     ¦ ¦                           ¦    ¦    ¦        convenience item.              ¦

¦ 9.  Megaphones          D ¦ -  ¦ -  ¦ Any in excess of those required     | ¦ ¦                           ¦    ¦    ¦ by FAR may be inoperative provided:   ¦ ¦                           ¦    ¦    ¦     a) The inoperative megaphone is   ¦ ¦                           ¦    ¦    ¦        removed from the passenger     ¦ ¦                           ¦    ¦    ¦        cabin, and                     ¦ ¦                           ¦    ¦    ¦     b) Required distribution is       ¦ ¦                           ¦    ¦    ¦        maintained.                    ¦

¦                           ¦    ¦    ¦ NOTE:  Not required for all cargo     ¦ ¦                           ¦    ¦    ¦        operations.                    ¦

¦ 10. Cabin Emergency     C ¦ -  ¦ 0  ¦ May be inoperative or missing         ¦ ¦     Flashlights/Holders   ¦    ¦    ¦ provided cabin crewmember assigned    ¦ ¦                           ¦    ¦    ¦ to affected position has an           ¦ ¦                           ¦    ¦    ¦ operative flashlight readily          ¦ ¦                           ¦    ¦    ¦ available.                            ¦

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

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 19       ¦ PAGE:    ¦ ¦              L-382 (C-130)               ¦                       ¦          ¦ ¦                                          ¦ DATE: 10/29/2004      ¦ 25-11    ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 25  EQUIPMENT/FURNISHINGS ¦    ¦    ¦                                       ¦

¦ 11. Emergency Medical     ¦    ¦    ¦                                     | ¦ ¦     Equipment             ¦    ¦    ¦                                     | ¦

¦     1) First Aid Kits   D ¦ -  ¦ -  ¦ Any in excess of those required by  | ¦ ¦                           ¦    ¦    ¦ FAR may be incomplete or missing    | ¦ ¦                           ¦    ¦    ¦ provided required distribution is   | ¦ ¦                           ¦    ¦    ¦ maintained.                         | ¦

¦     2) Emergency        D ¦ -  ¦ -  ¦ Any in excess of those required by  | ¦ ¦        Medical Kits       ¦    ¦    ¦ FAR may be incomplete or missing    | ¦ ¦                           ¦    ¦    ¦ provided required distribution is   | ¦ ¦                           ¦    ¦    ¦ maintained.                         | ¦

¦     3) Automated        D ¦ -  ¦ -  ¦ Any in excess of those required by  | ¦ ¦        External           ¦    ¦    ¦ FAR may be incomplete or missing    | ¦ ¦        Defibrillators     ¦    ¦    ¦ provided required distribution is   | ¦ ¦        (AED)              ¦    ¦    ¦ maintained.                         | ¦

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

¦                         C ¦ -  ¦ -  ¦ May be inoperative or missing         ¦ ¦                           ¦    ¦    ¦ provided cargo compartment remains  | ¦ ¦                           ¦    ¦    ¦ empty.                              | ¦

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

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 19       ¦ PAGE:    ¦ ¦              L-382 (C-130)               ¦                       ¦          ¦ ¦                                          ¦ DATE: 10/29/2004      ¦ 25-12    ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 25  EQUIPMENT/FURNISHINGS ¦    ¦    ¦                                       ¦

¦ 13. Exterior Lavatory     ¦    ¦    ¦                                     | ¦ ¦     Door Ashtrays         ¦    ¦    ¦                                     | ¦

¦     1) Airplanes With   A ¦ -  ¦ -  ¦ One may be missing provided it is   | ¦ ¦        More Than One      ¦    ¦    ¦ replace within 10 calendar days.    | ¦ ¦        Exterior Lavatory  ¦    ¦    ¦                                     | ¦ ¦        Door Ashtray       ¦    ¦    ¦                                     | ¦ ¦        Installed          ¦    ¦    ¦                                     | ¦

¦     2) Airplanes With   A ¦ 1  ¦ 0  ¦ May be missing provided it is       | ¦ ¦        Only One Exterior  ¦    ¦    ¦ replaced within 3 calendar days.    | ¦ ¦        Lavatory Door      ¦    ¦    ¦                                     | ¦ ¦        Ashtray Installed  ¦    ¦    ¦                                     | ¦

¦ 14. Galley Waste        C ¦ -  ¦ -  ¦ (M)(O)May be inoperative provided:  | ¦ ¦     Receptacle Access     ¦    ¦    ¦     a) The container is empty and   | ¦ ¦     Doors/Covers          ¦    ¦    ¦        the access is secured to     | ¦ ¦                           ¦    ¦    ¦        prevent waste introduction   | ¦ ¦                           ¦    ¦    ¦        into the compartment, and    | ¦ ¦                           ¦    ¦    ¦     b) Procedures are established   | ¦ ¦                           ¦    ¦    ¦        to ensure that sufficient    | ¦ ¦                           ¦    ¦    ¦        galley waste receptacles are | ¦ ¦                           ¦    ¦    ¦        available to accommodate all | ¦ ¦                           ¦    ¦    ¦        waste that may be generated  | ¦ ¦                           ¦    ¦    ¦        on a flight.                 | ¦

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

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 19       ¦ PAGE:    ¦ ¦              L-382 (C-130)               ¦                       ¦          ¦ ¦                                          ¦ DATE: 10/29/2004      ¦ 25-13    ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 25  EQUIPMENT/FURNISHINGS ¦    ¦    ¦                                       ¦

¦ 15. Overhead Storage    C ¦ -  ¦ -  ¦ (M)May be inoperative provided:     | ¦ ¦     Bin(s)/Cabin and      ¦    ¦    ¦     a) Procedures are established   | ¦ ¦     Galley Storage        ¦    ¦    ¦        to secure compartment        | ¦ ¦     Compartments/Closets  ¦    ¦    ¦        CLOSED,                      | ¦ ¦                           ¦    ¦    ¦     b) Compartment is not used for  | ¦ ¦                           ¦    ¦    ¦        storage of emergency         | ¦ ¦                           ¦    ¦    ¦        equipment, and               | ¦ ¦                           ¦    ¦    ¦     c) Affected compartment is not  | ¦ ¦                           ¦    ¦    ¦        used for storage of any      | ¦ ¦                           ¦    ¦    ¦        item(s) except for those     | ¦ ¦                           ¦    ¦    ¦        permanently affixed.         | ¦

¦                           ¦    ¦    ¦ NOTE:  If no partitions are         | ¦ ¦                           ¦    ¦    ¦        installed, the entire        | ¦ ¦                           ¦    ¦    ¦        overhead storage compartment | ¦ ¦                           ¦    ¦    ¦        is considered one bin.       | ¦

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

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 19       ¦ PAGE:    ¦ ¦              L-382 (C-130)               ¦                       ¦          ¦ ¦                                          ¦ DATE: 10/29/2004      ¦ 26-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 26  FIRE PROTECTION       ¦    ¦    ¦                                       ¦

¦ 1.  Audible Fire        C ¦ -  ¦ 0  ¦                                     | ¦ ¦ *** Warning System        ¦    ¦    ¦                                       ¦

¦ 2.  GTC/APU Fire        C ¦ 1  ¦ 0  ¦ (M)May be inoperative provided:       ¦ ¦     Detection and         ¦    ¦    ¦     a) Fire Guard is posted, and    | ¦ ¦     Extinguisher          ¦    ¦    ¦     b) Visual check of GTC          | ¦ ¦     System (Includes      ¦    ¦    ¦        compartment is accomplished    ¦ ¦     Fuel Shutoff Valve)   ¦    ¦    ¦        before starting left           ¦ ¦                           ¦    ¦    ¦        engines.                       ¦

¦                         C ¦ 1  ¦ 0  ¦ May be inoperative provided         | ¦ ¦                           ¦    ¦    ¦ APU/GTC is considered inoperative   | ¦ ¦                           ¦    ¦    ¦ and not used.                       | ¦

¦ 3.  Smoke Detectors     C ¦ 2  ¦ 1  ¦                                     | ¦ ¦     (#2 and #3 located    ¦    ¦    ¦                                     | ¦ ¦     at FS 467)            ¦    ¦    ¦                                     | ¦

¦ 4.  ATM Compartment     C ¦ 1  ¦ 0  ¦ May be inoperative provided:        | ¦ ¦     Overheat Warning      ¦    ¦    ¦     a) ATM is considered            | ¦ ¦     System                ¦    ¦    ¦        inoperative, and             | ¦ ¦                           ¦    ¦    ¦     b) ATM Shutoff Valve is         | ¦ ¦                           ¦    ¦    ¦        secured CLOSED.                ¦

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

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 19       ¦ PAGE:    ¦ ¦              L-382 (C-130)               ¦                       ¦          ¦ ¦                                          ¦ DATE: 10/29/2004      ¦ 26-2     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 26  FIRE PROTECTION       ¦    ¦    ¦                                       ¦

¦ 5.  Lavatory Smoke      C ¦ -  ¦ -  ¦ (M)(O)For each lavatory, the        | ¦ ¦ *** Detection Systems     ¦    ¦    ¦ lavatory smoke detection system may | ¦ ¦                           ¦    ¦    ¦ be inoperative provided:              ¦ ¦                           ¦    ¦    ¦     a) Lavatory waste receptacle is | ¦ ¦                           ¦    ¦    ¦        empty,                       | ¦ ¦                           ¦    ¦    ¦     b) Lavatory Door is locked      | ¦ ¦                           ¦    ¦    ¦        CLOSED and placarded         | ¦ ¦                           ¦    ¦    ¦        "INOPERATIVE - DO NOT        | ¦ ¦                           ¦    ¦    ¦        ENTER", and                  | ¦ ¦                           ¦    ¦    ¦     c) Lavatory is used only by     | ¦ ¦                           ¦    ¦    ¦        crewmembers.                 | ¦

¦                           ¦    ¦    ¦ NOTE 1:  These provisos are not       ¦ ¦                           ¦    ¦    ¦          intended to prohibit         ¦ ¦                           ¦    ¦    ¦          lavatory inspections or    | ¦ ¦                           ¦    ¦    ¦          use by crewmembers.        | ¦

¦                           ¦    ¦    ¦ NOTE 2:  A lavatory smoke detection   ¦ ¦                           ¦    ¦    ¦          system is not required for   ¦ ¦                           ¦    ¦    ¦          all-cargo operations.        ¦

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

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 19       ¦ PAGE:    ¦ ¦              L-382 (C-130)               ¦                       ¦          ¦ ¦                                          ¦ DATE: 10/29/2004      ¦ 26-3     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 26  FIRE PROTECTION       ¦    ¦    ¦                                       ¦

¦ 6.  Lavatory Fire       C ¦ -  ¦ -  ¦ For each lavatory, the lavatory     | ¦ ¦ *** Extinguisher          ¦    ¦    ¦ Fire Extinguisher system may be     | ¦ ¦     Systems               ¦    ¦    ¦ inoperative provided Lavatory       | ¦ ¦                           ¦    ¦    ¦ Smoke Detection System operates     | ¦ ¦                           ¦    ¦    ¦ normally.                           | ¦

¦                         C ¦ -  ¦ -  ¦ (M)(O)For each lavatory, the        | ¦ ¦                           ¦    ¦    ¦ lavatory Fire Extinguisher system   | ¦ ¦                           ¦    ¦    ¦ may be inoperative provided:        | ¦ ¦                           ¦    ¦    ¦     a) Lavatory waste receptacle is | ¦ ¦                           ¦    ¦    ¦        empty,                       | ¦ ¦                           ¦    ¦    ¦     b) Lavatory Door is locked      | ¦ ¦                           ¦    ¦    ¦        CLOSED and placarded         | ¦ ¦                           ¦    ¦    ¦        "INOPERATIVE - DO NOT        | ¦ ¦                           ¦    ¦    ¦        ENTER", and                  | ¦ ¦                           ¦    ¦    ¦     c) Lavatory is used only by     | ¦ ¦                           ¦    ¦    ¦        crewmembers.                 | ¦

¦                           ¦    ¦    ¦ NOTE 1:  These provisos are not       ¦ ¦                           ¦    ¦    ¦          intended to prohibit         ¦ ¦                           ¦    ¦    ¦          lavatory inspections or    | ¦ ¦                           ¦    ¦    ¦          use by crewmembers.        | ¦

¦                           ¦    ¦    ¦ NOTE 2:  A lavatory Fire              ¦ ¦                           ¦    ¦    ¦          Extinguisher system is not   ¦ ¦                           ¦    ¦    ¦          required for all-cargo       ¦ ¦                           ¦    ¦    ¦          operations.                  ¦

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

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 19       ¦ PAGE:    ¦ ¦              L-382 (C-130)               ¦                       ¦          ¦ ¦                                          ¦ DATE: 10/29/2004      ¦ 26-4     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 26  FIRE PROTECTION       ¦    ¦    ¦                                       ¦

¦ 7.  Portable Fire       D ¦ -  ¦ -  ¦ Any in excess of those required by  | ¦ ¦     Extinguishers         ¦    ¦    ¦ FAR may be inoperative or missing   | ¦ ¦                           ¦    ¦    ¦ provided:                           | ¦ ¦                           ¦    ¦    ¦     a) The inoperative fire         | ¦ ¦                           ¦    ¦    ¦        extinguisher is tagged       | ¦ ¦                           ¦    ¦    ¦        inoperative, removed from    | ¦ ¦                           ¦    ¦    ¦        the installed location, and  | ¦ ¦                           ¦    ¦    ¦        placed out of sight so it    | ¦ ¦                           ¦    ¦    ¦        can not be mistaken for a    | ¦ ¦                           ¦    ¦    ¦        functional unit, and         | ¦ ¦                           ¦    ¦    ¦     b) Required distribution is     | ¦ ¦                           ¦    ¦    ¦        maintained.                  | ¦

¦ 8.  Cargo Compartment   C ¦ -  ¦ 0  ¦ May be inoperative provided         | ¦ ¦ *** Fire Detection /      ¦    ¦    ¦ associated cargo compartment(s)     | ¦ ¦     Suppression Systems   ¦    ¦    ¦ remains empty.                      | ¦

¦                           ¦    ¦    ¦ NOTE 1:  Does not preclude the      | ¦ ¦                           ¦    ¦    ¦          carriage of empty cargo    | ¦ ¦                           ¦    ¦    ¦          containers, pallets,       | ¦ ¦                           ¦    ¦    ¦          ballast, etc.              | ¦

¦                           ¦    ¦    ¦ NOTE 2:  Class E cargo compartments | ¦ ¦                           ¦    ¦    ¦          require only the           | ¦ ¦                           ¦    ¦    ¦          installation of fire       | ¦ ¦                           ¦    ¦    ¦          detection systems (not     | ¦ ¦                           ¦    ¦    ¦          suppression).              | ¦

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

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 19       ¦ PAGE:    ¦ ¦              L-382 (C-130)               ¦                       ¦          ¦ ¦                                          ¦ DATE: 10/29/2004      ¦ 27-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 27  FLIGHT CONTROLS       ¦    ¦    ¦                                       ¦

¦ 1.  Aileron Trim        C ¦ 1  ¦ 0  ¦ (M)May be inoperative provided      | ¦ ¦     Position Indicator    ¦    ¦    ¦ neutral trim is determined before     ¦ ¦                           ¦    ¦    ¦ each takeoff.                         ¦

¦ 2.  Rudder Trim         C ¦ 1  ¦ 0  ¦ (M)May be inoperative provided      | ¦ ¦     Position Indicator    ¦    ¦    ¦ neutral trim is determined before     ¦ ¦                           ¦    ¦    ¦ each takeoff.                         ¦

¦ 3.  Control Boost       C ¦ 6  ¦ 0  ¦                                     | ¦ ¦     Warning Lights        ¦    ¦    ¦                                       ¦

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

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 19       ¦ PAGE:    ¦ ¦              L-382 (C-130)               ¦                       ¦          ¦ ¦                                          ¦ DATE: 10/29/2004      ¦ 28-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 28  FUEL                  ¦    ¦    ¦                                       ¦

¦ 1.  Main Tank Boost     C ¦ 4  ¦ 3  ¦ One may be inoperative provided       ¦ ¦     Pump                  ¦    ¦    ¦ aircraft is operated at FL200 or      ¦ ¦                           ¦    ¦    ¦ below.                                ¦

¦ 2.  Auxiliary Tank      C ¦ 2  ¦ 0  ¦ (M)May be inoperative provided      | ¦ ¦     Boost Pump            ¦    ¦    ¦ affected tank is empty.             | ¦

¦                         C ¦ 2  ¦ 0  ¦ (M)May be inoperative provided:     | ¦ ¦                           ¦    ¦    ¦     a) Fuel in the associated tank  | ¦ ¦                           ¦    ¦    ¦        is carried as cargo, and     | ¦ ¦                           ¦    ¦    ¦     b) AFM Limitations are          | ¦ ¦                           ¦    ¦    ¦        observed.                    | ¦

¦ 3.  External Tank Fuel  C ¦ 4  ¦ 0  ¦ May be inoperative provided           ¦ ¦     Pumps                 ¦    ¦    ¦ external tanks are empty.             ¦

¦ 4.  Main Tank Crossfeed C ¦ 4  ¦ 3  ¦ (M)One may be inoperative provided:   ¦ ¦     Valve                 ¦    ¦    ¦     a) Affected valve is secured      ¦ ¦                           ¦    ¦    ¦        OPEN, and                      ¦ ¦                           ¦    ¦    ¦     b) Crossfeed Separation Valve     ¦ ¦                           ¦    ¦    ¦        is operative.                  ¦

¦ 5.  Auxiliary and       C ¦ 4  ¦ 2  ¦ (M)Two may be inoperative provided:   ¦ ¦     External Tank         ¦    ¦    ¦     a) One is operative on each       ¦ ¦     Crossfeed Valves      ¦    ¦    ¦        side,                          ¦ ¦                           ¦    ¦    ¦     b) Affected Valve is secured      ¦ ¦                           ¦    ¦    ¦        CLOSED, and                    ¦ ¦                           ¦    ¦    ¦     c) Associated Bypass Valve is     ¦ ¦                           ¦    ¦    ¦        operative.                     ¦

¦                         C ¦ 4  ¦ 0  ¦ May be inoperative provided all       ¦ ¦                           ¦    ¦    ¦ Auxiliary and External Tanks are      ¦ ¦                           ¦    ¦    ¦ empty.                                ¦

¦ 6.  Auxiliary and         ¦    ¦    ¦ DELETED in Revision 18.               ¦ ¦     External Tank         ¦    ¦    ¦                                       ¦ ¦     Crossfeed Valves      ¦    ¦    ¦                                       ¦ ¦     (Aux Tanks Not        ¦    ¦    ¦                                       ¦ ¦     Installed)            ¦    ¦    ¦                                       ¦

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

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 18 a     ¦ PAGE:    ¦ ¦              L-382 (C-130)               ¦                       ¦          ¦ ¦                                          ¦ DATE: 08/22/1994      ¦ 28-2     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 28  FUEL                  ¦    ¦    ¦                                       ¦

¦ 7.  By-Pass Valve       C ¦ 2  ¦ 0  ¦ (M)May be inoperative provided:       ¦ ¦                           ¦    ¦    ¦     a) Affected Valve is secured      ¦ ¦                           ¦    ¦    ¦        OPEN, and                      ¦ ¦                           ¦    ¦    ¦     b) Associated Crossfeed Valves    ¦ ¦                           ¦    ¦    ¦        are operative.                 ¦

¦ 8.  Main Tank Fuel      C ¦ 4  ¦ 3  ¦ (M)(O)One may be inoperative          ¦ ¦     Quantity Indicators   ¦    ¦    ¦ provided:                             ¦ ¦     (Flight Station)      ¦    ¦    ¦     a) All Fuel Flow Indicators are   ¦ ¦                           ¦    ¦    ¦        operative,                     ¦ ¦                           ¦    ¦    ¦     b) Associated Fuel Boost Pumps    ¦ ¦                           ¦    ¦    ¦        are operative,                 ¦ ¦                           ¦    ¦    ¦     c) All other Fuel Quantity        ¦ ¦                           ¦    ¦    ¦        Indicators for tanks with      ¦ ¦                           ¦    ¦    ¦        fuel on the same side of the   ¦ ¦                           ¦    ¦    ¦        Separation Valve are           ¦ ¦                           ¦    ¦    ¦        operative,                     ¦ ¦                           ¦    ¦    ¦     d) Affected Indicator is          ¦ ¦                           ¦    ¦    ¦        electrically secured,          ¦ ¦                           ¦    ¦    ¦     e) Fuel quantity in the           ¦ ¦                           ¦    ¦    ¦        associated tank is verified    ¦ ¦                           ¦    ¦    ¦        by an accepted procedure       ¦ ¦                           ¦    ¦    ¦        before each takeoff, and       ¦ ¦                           ¦    ¦    ¦     f) A Fuel Use Log is              ¦ ¦                           ¦    ¦    ¦        maintained.                    ¦

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

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 18 a     ¦ PAGE:    ¦ ¦              L-382 (C-130)               ¦                       ¦          ¦ ¦                                          ¦ DATE: 08/22/1994      ¦ 28-3     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 28  FUEL                  ¦    ¦    ¦                                       ¦

¦ 9.  Fuel Quantity         ¦    ¦    ¦                                       ¦ ¦ *** Indicators (Flight    ¦    ¦    ¦                                       ¦ ¦     Station)              ¦    ¦    ¦                                       ¦

¦ *** 1) Auxiliary Tank   C ¦ 2  ¦ 1  ¦ (M)(O)One may be inoperative          ¦ ¦                           ¦    ¦    ¦ provided:                             ¦ ¦                           ¦    ¦    ¦     a) All Fuel Flow Indicators are   ¦ ¦                           ¦    ¦    ¦        operative,                     ¦ ¦                           ¦    ¦    ¦     b) Associated Fuel Boost Pump     ¦ ¦                           ¦    ¦    ¦        is operative,                  ¦ ¦                           ¦    ¦    ¦     c) All other Fuel Quantity        ¦ ¦                           ¦    ¦    ¦        Indicators for tanks with      ¦ ¦                           ¦    ¦    ¦        fuel on the same side of the   ¦ ¦                           ¦    ¦    ¦        Separation Valve are           ¦ ¦                           ¦    ¦    ¦        operative,                     ¦ ¦                           ¦    ¦    ¦     d) Affected Indicator is          ¦ ¦                           ¦    ¦    ¦        electrically secured,          ¦ ¦                           ¦    ¦    ¦     e) Fuel quantity in the           ¦ ¦                           ¦    ¦    ¦        associated tank is verified    ¦ ¦                           ¦    ¦    ¦        by an accepted procedure       ¦ ¦                           ¦    ¦    ¦        before each takeoff, and       ¦ ¦                           ¦    ¦    ¦     f) A Fuel Use Log is              ¦ ¦                           ¦    ¦    ¦        maintained.                    ¦

¦                         C ¦ 2  ¦ 0  ¦ (M)May be inoperative provided:       ¦ ¦                           ¦    ¦    ¦     a) Associated Fuel Tanks are      ¦ ¦                           ¦    ¦    ¦        verified EMPTY, and            ¦ ¦                           ¦    ¦    ¦     b) Affected Indicators are        ¦ ¦                           ¦    ¦    ¦        electrically secured.          ¦

¦                           ¦    ¦    ¦ (Continued)                           ¦

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

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 19       ¦ PAGE:    ¦ ¦              L-382 (C-130)               ¦                       ¦          ¦ ¦                                          ¦ DATE: 10/29/2004      ¦ 28-4     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 28  FUEL                  ¦    ¦    ¦                                       ¦

¦ 9.  Fuel Quantity         ¦    ¦    ¦                                       ¦ ¦ *** Indicators (Flight    ¦    ¦    ¦                                       ¦ ¦     Station) (Cont'd)     ¦    ¦    ¦                                       ¦

¦ *** 2) External Tank    C ¦ 2  ¦ 1  ¦ (M)(O)One may be inoperative          ¦ ¦                           ¦    ¦    ¦ provided:                             ¦ ¦                           ¦    ¦    ¦     a) All Fuel Flow Indicators are   ¦ ¦                           ¦    ¦    ¦        operative,                     ¦ ¦                           ¦    ¦    ¦     b) Associated Fuel Boost Pump     ¦ ¦                           ¦    ¦    ¦        is operative,                  ¦ ¦                           ¦    ¦    ¦     c) All other Fuel Quantity        ¦ ¦                           ¦    ¦    ¦        Indicators for tanks with      ¦ ¦                           ¦    ¦    ¦        fuel on the same side of the   ¦ ¦                           ¦    ¦    ¦        Separation Valve are           ¦ ¦                           ¦    ¦    ¦        operative,                     ¦ ¦                           ¦    ¦    ¦     d) Affected Indicator is          ¦ ¦                           ¦    ¦    ¦        electrically secured,          ¦ ¦                           ¦    ¦    ¦     e) Fuel quantity in the           ¦ ¦                           ¦    ¦    ¦        associated tank is verified    ¦ ¦                           ¦    ¦    ¦        by an accepted procedure       ¦ ¦                           ¦    ¦    ¦        before each takeoff, and       ¦ ¦                           ¦    ¦    ¦     f) A Fuel Use Log is              ¦ ¦                           ¦    ¦    ¦        maintained.                    ¦

¦                         C ¦ 2  ¦ 0  ¦ (M)May be inoperative provided:       ¦ ¦                           ¦    ¦    ¦     a) Associated Fuel Tanks are      ¦ ¦                           ¦    ¦    ¦        verified EMPTY, and            ¦ ¦                           ¦    ¦    ¦     b) Affected Indicators are        ¦ ¦                           ¦    ¦    ¦        electrically secured.          ¦

¦ 10. Crossfeed Manifold  B ¦ 1  ¦ 0  ¦ (M)May be inoperative provided        ¦ ¦     Fuel Pressure Gauge   ¦    ¦    ¦ External and Auxiliary Fuel Tanks     ¦ ¦                           ¦    ¦    ¦ are verified EMPTY.                   ¦

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

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 19       ¦ PAGE:    ¦ ¦              L-382 (C-130)               ¦                       ¦          ¦ ¦                                          ¦ DATE: 10/29/2004      ¦ 28-5     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 28  FUEL                  ¦    ¦    ¦                                       ¦

¦ 11. Crossfeed           C ¦ 1  ¦ 0  ¦ (M)May be inoperative provided:     | ¦ ¦     Separation Valve      ¦    ¦    ¦     a) Valve is secured OPEN,       | ¦ ¦                           ¦    ¦    ¦     b) All Main Tank Crossfeed        ¦ ¦                           ¦    ¦    ¦        Valves are operative, and      ¦ ¦                           ¦    ¦    ¦     c) Fuel Quantity Indicators for   ¦ ¦                           ¦    ¦    ¦        all tanks containing fuel      ¦ ¦                           ¦    ¦    ¦        are operative.                 ¦

¦ 12. Crossfeed Primer    C ¦ 1  ¦ 0  ¦ (M)May be inoperative provided      | ¦ ¦     System                ¦    ¦    ¦ affected valve is secured CLOSED.     ¦

¦ 13. Single Point Refuel C ¦ 1  ¦ 0  ¦ (M)May be inoperative provided:     | ¦ ¦     System (SPR)          ¦    ¦    ¦     a) Alternate refueling            ¦ ¦                           ¦    ¦    ¦        procedures are established   | ¦ ¦                           ¦    ¦    ¦        and used, and                | ¦ ¦                           ¦    ¦    ¦     b) SPR Manifold is drained        ¦ ¦                           ¦    ¦    ¦        through the Manual Valve       ¦ ¦                           ¦    ¦    ¦        after each refueling.          ¦

¦                           ¦    ¦    ¦ NOTE: Any portion of the system     | ¦ ¦                           ¦    ¦    ¦       that operates normally may    | ¦ ¦                           ¦    ¦    ¦       be used.                      | ¦

¦     1) Fuel Drain       C ¦ 1  ¦ 0  ¦ (M)May be inoperative provided SPR  | ¦ ¦        Transfer Pump      ¦    ¦    ¦ manifold is drained after each      | ¦ ¦                           ¦    ¦    ¦ refueling.                          | ¦

¦     2) Fuel Quantity    C ¦ -  ¦ 0  ¦ (M)May be inoperative provided fuel | ¦ ¦        Indicators         ¦    ¦    ¦ quantity in associated tank is      | ¦ ¦        (SPR Panel)        ¦    ¦    ¦ determined using Flight Station     | ¦ ¦                           ¦    ¦    ¦ Fuel Quantity Indicator or other    | ¦ ¦                           ¦    ¦    ¦ approved means.                     | ¦

¦ 14. Main Tank Dump Pump C ¦ 4  ¦ 0  ¦                                     | ¦

¦ 15. Fuel Quantity       C ¦ 1  ¦ 0  ¦                                     | ¦ ¦     Totalizer (Flight     ¦    ¦    ¦                                     | ¦ ¦     Station)              ¦    ¦    ¦                                     | ¦

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

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 19       ¦ PAGE:    ¦ ¦              L-382 (C-130)               ¦                       ¦          ¦ ¦                                          ¦ DATE: 10/29/2004      ¦ 28-6     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 28  FUEL                  ¦    ¦    ¦                                       ¦

¦ 16. Auxiliary Tank      C ¦ 2  ¦ 1  ¦ (O)May be inoperative provided:     | ¦ ¦ *** Empty Warning Light   ¦    ¦    ¦     a) Crossfeed Manifold Fuel      | ¦ ¦                           ¦    ¦    ¦        Pressure Gauge is operative, | ¦ ¦                           ¦    ¦    ¦     b) All Crossfeed Valves are     | ¦ ¦                           ¦    ¦    ¦        operative, and               | ¦ ¦                           ¦    ¦    ¦     c) Associated Flight Station    | ¦ ¦                           ¦    ¦    ¦        Fuel Quantity Indicator is   | ¦ ¦                           ¦    ¦    ¦        operative.                   | ¦

¦                         C ¦ 2  ¦ 1  ¦ (M)May be inoperative provided      | ¦ ¦                           ¦    ¦    ¦ associated Auxiliary Tank is        | ¦ ¦                           ¦    ¦    ¦ verified empty before each flight.  | ¦

¦                         C ¦ 2  ¦ 0  ¦ (M)May be inoperative provided both | ¦ ¦                           ¦    ¦    ¦ Auxiliary Tanks are verified empty  | ¦ ¦                           ¦    ¦    ¦ before each flight.                 | ¦

¦ 17. External Tank       C ¦ 2  ¦ 1  ¦ (O)May be inoperative provided:     | ¦ ¦ *** Empty Warning Light   ¦    ¦    ¦     a) Crossfeed Manifold Fuel      | ¦ ¦                           ¦    ¦    ¦        Pressure Gauge is operative, | ¦ ¦                           ¦    ¦    ¦     b) All Crossfeed Valves are     | ¦ ¦                           ¦    ¦    ¦        operative, and               | ¦ ¦                           ¦    ¦    ¦     c) Associated Flight Station    | ¦ ¦                           ¦    ¦    ¦        Fuel Quantity Indicator is   | ¦ ¦                           ¦    ¦    ¦        operative.                   | ¦

¦                         C ¦ 2  ¦ 0  ¦ (M)May be inoperative provided both | ¦ ¦                           ¦    ¦    ¦ External Tanks are verified empty   | ¦ ¦                           ¦    ¦    ¦ before each flight.                 | ¦

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

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 19       ¦ PAGE:    ¦ ¦              L-382 (C-130)               ¦                       ¦          ¦ ¦                                          ¦ DATE: 10/29/2004      ¦ 29-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 29  HYDRAULIC POWER       ¦    ¦    ¦                                       ¦

¦ 1.  Engine Pump         C ¦ 4  ¦ 3  ¦ (O)May be inoperative provided      | ¦ ¦     Pressure Warning      ¦    ¦    ¦ pump output pressure is checked     | ¦ ¦     Lights                ¦    ¦    ¦ prior to each flight.               | ¦

¦ 2.  Utility Hydraulic   C ¦ 1  ¦ 0  ¦                                     | ¦ ¦     Pressure Gauge        ¦    ¦    ¦                                     | ¦

¦ 3.  Booster Hydraulic   C ¦ 1  ¦ 0  ¦                                     | ¦ ¦     Pressure Gauge        ¦    ¦    ¦                                     | ¦

¦ 4.  Auxiliary Hydraulic C ¦ -  ¦ 0  ¦                                     | ¦ ¦     Hand Pumps            ¦    ¦    ¦                                     | ¦

¦ 5.  Auxiliary Hydraulic C ¦ 2  ¦ 0  ¦                                     | ¦ ¦     Pressure Gauges       ¦    ¦    ¦                                     | ¦

¦ 6.  Ground Test System  C ¦ 1  ¦ 0  ¦ (M)May be inoperative provided      | ¦ ¦                           ¦    ¦    ¦ Valve is secured in FLIGHT            ¦ ¦                           ¦    ¦    ¦ position.                             ¦

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

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 19       ¦ PAGE:    ¦ ¦              L-382 (C-130)               ¦                       ¦          ¦ ¦                                          ¦ DATE: 10/29/2004      ¦ 30-1     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 30  ICE AND RAIN          ¦    ¦    ¦                                       ¦ ¦     PROTECTION            ¦    ¦    ¦                                       ¦

¦ 1.  Wing and Empennage  C ¦ 2  ¦ 0  ¦ May be inoperative provided           ¦ ¦     Anti-Ice Systems      ¦    ¦    ¦ aircraft is not operated in known     ¦ ¦                           ¦    ¦    ¦ or forecast icing conditions.       | ¦

¦     1) Automatic        C ¦ 1  ¦ 0  ¦ (O)May be inoperative provided:       ¦ ¦        Temperature        ¦    ¦    ¦     a) All associated Temperature     ¦ ¦        Control            ¦    ¦    ¦        Indicators are operative,      ¦ ¦                           ¦    ¦    ¦     b) All associated Warning         ¦ ¦                           ¦    ¦    ¦        Lights are operative, and      ¦ ¦                           ¦    ¦    ¦     c) Manual operating procedures    ¦ ¦                           ¦    ¦    ¦        are established and used.    | ¦

¦     2) Wing and         C ¦ 6  ¦ 0  ¦ (M)May be inoperative provided:     | ¦ ¦        Empennage          ¦    ¦    ¦     a) Affected valves are secured  | ¦ ¦        Anti-Icing Valves  ¦    ¦    ¦        CLOSED, and                  | ¦ ¦                           ¦    ¦    ¦     b) Aircraft is not operated in  | ¦ ¦                           ¦    ¦    ¦        known or forecast icing      | ¦ ¦                           ¦    ¦    ¦        conditions.                  | ¦

¦ 2.  Anti-Icing Over     C ¦ 1  ¦ 0  ¦ May be inoperative provided:          ¦ ¦     Temperature Warning   ¦    ¦    ¦     a) Wing and Empennage Anti-Ice    ¦ ¦     System                ¦    ¦    ¦        Automatic Control System is    ¦ ¦                           ¦    ¦    ¦        operative, and                 ¦ ¦                           ¦    ¦    ¦     b) All Wing and Empennage Anti-   ¦ ¦                           ¦    ¦    ¦        Ice Leading Edge Temperature   ¦ ¦                           ¦    ¦    ¦        Indicators are operative.      ¦

¦                         C ¦ 1  ¦ 0  ¦ May be inoperative provided         | ¦ ¦                           ¦    ¦    ¦ aircraft is not operated in known   | ¦ ¦                           ¦    ¦    ¦ or forecast icing conditions.       | ¦

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

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 19       ¦ PAGE:    ¦ ¦              L-382 (C-130)               ¦                       ¦          ¦ ¦                                          ¦ DATE: 10/29/2004      ¦ 30-2     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 30  ICE AND RAIN          ¦    ¦    ¦                                       ¦ ¦     PROTECTION            ¦    ¦    ¦                                       ¦

¦ 3.  Leading Edge        C ¦ 1  ¦ 0  ¦ May be inoperative provided:          ¦ ¦     Temperature           ¦    ¦    ¦     a) Wing and Empennage Anti-Ice    ¦ ¦     Indicating System     ¦    ¦    ¦        Automatic Control System is    ¦ ¦                           ¦    ¦    ¦        operative, and                 ¦ ¦                           ¦    ¦    ¦     b) Anti-Icing Over Temperature    ¦ ¦                           ¦    ¦    ¦        Warning System is operative.   ¦

¦                         C ¦ 1  ¦ 0  ¦ May be inoperative provided         | ¦ ¦                           ¦    ¦    ¦ aircraft is not operated in known   | ¦ ¦                           ¦    ¦    ¦ or forecast icing conditions.       | ¦

¦ 4.  Nacelle Preheat       ¦    ¦    ¦ Moved to 36-6, Revision 19.         | ¦ ¦     System                ¦    ¦    ¦                                       ¦

¦ 5.  Pitot Heat System   C ¦ 2  ¦ 1  ¦ May be inoperative provided:        | ¦ ¦                           ¦    ¦    ¦     a) Aircraft is not operated in    ¦ ¦                           ¦    ¦    ¦        known or forecast Icing        ¦ ¦                           ¦    ¦    ¦        conditions, and                ¦ ¦                           ¦    ¦    ¦     b) Aircraft is operated in VMC.   ¦

¦     1) Pitot Heat       C ¦ 2  ¦ 0  ¦ (M)May be inoperative provided:     | ¦ ¦        OFF Warning        ¦    ¦    ¦     a) All other components of the  | ¦ ¦        Lights             ¦    ¦    ¦        Pitot Heat System are        | ¦ ¦                           ¦    ¦    ¦        verified operative before    | ¦ ¦                           ¦    ¦    ¦        each departure, and          | ¦ ¦                           ¦    ¦    ¦     b) Aircraft is not operated in  | ¦ ¦                           ¦    ¦    ¦        known or forecast icing      | ¦ ¦                           ¦    ¦    ¦        conditions.                  | ¦

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

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 19       ¦ PAGE:    ¦ ¦              L-382 (C-130)               ¦                       ¦          ¦ ¦                                          ¦ DATE: 10/29/2004      ¦ 30-3     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 30  ICE AND RAIN          ¦    ¦    ¦                                       ¦ ¦     PROTECTION            ¦    ¦    ¦                                       ¦

¦ 6.  Engine Inlet Duct   C ¦ 4  ¦ 3  ¦ May be inoperative provided         | ¦ ¦     Anti-Ice System       ¦    ¦    ¦ aircraft is not operated in known     ¦ ¦     (Includes Engine      ¦    ¦    ¦ or forecast icing conditions.       | ¦ ¦     Inlet Guide Vane and  ¦    ¦    ¦                                     | ¦ ¦     Torquemeter Shroud)   ¦    ¦    ¦                                     | ¦ ¦                         C ¦ 4  ¦ 0  ¦ (O)May be inoperative ON provided   | ¦ ¦                           ¦    ¦    ¦ associated:                         | ¦ ¦                           ¦    ¦    ¦     a) Engine Inlet Air Duct Anti-  | ¦ ¦                           ¦    ¦    ¦        Icing ON Light is operative, | ¦ ¦                           ¦    ¦    ¦     b) System is verified ON before | ¦ ¦                           ¦    ¦    ¦        each flight, and             | ¦ ¦                           ¦    ¦    ¦     c) Appropriate AFM performance  | ¦ ¦                           ¦    ¦    ¦        penalty is applied.          | ¦

¦ 7.  Radome Anti-Icing   C ¦ 1  ¦ 0  ¦                                       ¦ ¦ *** System                ¦    ¦    ¦                                     | ¦

¦ 8.  Propeller and       C ¦ 1  ¦ 0  ¦ May be inoperative provided           ¦ ¦     Engine Anti-Icing     ¦    ¦    ¦ aircraft is not operated in known     ¦ ¦     Master Switch         ¦    ¦    ¦ or forecast icing conditions.         ¦

¦ 9.  Propeller Anti-     C ¦ 4  ¦ 0  ¦ May be inoperative provided         | ¦ ¦     Icing System          ¦    ¦    ¦ aircraft is not operated in known   | ¦ ¦     (Includes Spinner     ¦    ¦    ¦ or forecast icing conditions.       | ¦ ¦     Front Section and     ¦    ¦    ¦                                     | ¦ ¦     Propeller           B ¦ 4  ¦ 0  ¦ (M)May be inoperative provided:     | ¦ ¦     Afterbody)            ¦    ¦    ¦     a) An accepted procedure for    | ¦ ¦     (Except C-130 with    ¦    ¦    ¦        the application and          | ¦ ¦     Aeroproducts          ¦    ¦    ¦        reapplication of ICEX        | ¦ ¦     Propellers)           ¦    ¦    ¦        is established and used, and | ¦ ¦                           ¦    ¦    ¦     b) An accepted procedure for    | ¦ ¦                           ¦    ¦    ¦        detection and cleaning of      ¦ ¦                           ¦    ¦    ¦        contaminated compressor        ¦ ¦                           ¦    ¦    ¦        blades is established and      ¦ ¦                           ¦    ¦    ¦        used each flight day.          ¦

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

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

¦ U.S. DEPARTMENT OF TRANSPORTATION                                           ¦

¦                                            MASTER MINIMUM EQUIPMENT LIST    ¦ ¦ FEDERAL AVIATION ADMINISTRATION                                             ¦ ¦ --------------------------------------------------------------------------- ¦ ¦ AIRCRAFT:                                ¦ REVISION NO: 19       ¦ PAGE:    ¦ ¦              L-382 (C-130)               ¦                       ¦          ¦ ¦                                          ¦ DATE: 10/29/2004      ¦ 30-4     ¦ ¦ --------------------------------------------------------------------------- ¦ ¦                        1. ¦ 2. NUMBER INSTALLED                             ¦ ¦ SYSTEM &                  ¦    -------------------------------------------- ¦ ¦ SEQUENCE          ITEM    ¦    ¦ 3. NUMBER REQUIRED FOR DISPATCH            ¦ ¦ NUMBERS                   ¦    ¦    --------------------------------------- ¦ ¦ ------------------------- ¦    ¦    ¦ 4. REMARKS OR EXCEPTIONS              ¦ ¦ 30  ICE AND RAIN          ¦    ¦    ¦                                       ¦ ¦     PROTECTION            ¦    ¦    ¦                                       ¦

¦ 10. Propeller De-Icing  C ¦ 4  ¦ 0  ¦ May be inoperative provided         | ¦ ¦     System (Includes      ¦    ¦    ¦ aircraft is not operated in known   | ¦ ¦     Blades, Spinner       ¦    ¦    ¦ or forecast icing conditions.       | ¦ ¦     Front and Rear        ¦    ¦    ¦                                     | ¦ ¦     Sections, and       B ¦ 4  ¦ 0  ¦ (M)May be inoperative provided:     | ¦ ¦     Spinner Fairing)      ¦    ¦    ¦     a) An accepted procedure for    | ¦ ¦    &