Revision:

19a

 

Date: 11/17/2008

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

DEPARTMENT OF TRANSPORTATION

 

 

 

 

 

FEDERAL AVIATION ADMINISTRATION

 

 

 

 

 

WASHINGTON , D.C.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

MASTER MINIMUM EQUIPMENT LIST

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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

 

 

 

 

 

 


 

SYSTEM

PAGE(S)

REVISION

DATE

Contents

I

19a

11/17/2008

Highlights of Change

II, III

19a

11/17/2008

Definitions

VII

19a

11/17/2008

Preamble

XIII

19a

11/17/2008

21 - Air Conditioning

21-1 Thru 21-9

19a

11/17/2008

22 - Auto Flight

22-1 Thru 22-2

19a

11/17/2008

23 - Communications

23-1 Thru 23-7

19a

11/17/2008

24 - Electrical Power

24-1 Thru 24-3

19a

11/17/2008

25 - Equipment/Furnishings

25-1 Thru 25-15

19a

11/17/2008

26 - Fire Protection

26-1 Thru 26-4

19a

11/17/2008

27 - Flight Controls

27-1

19a

11/17/2008

28 - Fuel

28-1 Thru 28-6

19a

11/17/2008

29 - Hydraulic Power

29-1

19a

11/17/2008

30 - Ice and Rain Protection

30-1 Thru 30-5

19a

11/17/2008

31 - Indicating/Recording Systems

31-1 Thru 31-2

19a

11/17/2008

32 - Landing Gear

32-1

19a

11/17/2008

33 - Lights

33-1 Thru 33-3

19a

11/17/2008

34 - Navigation

34-1 Thru 34-15

19a

11/17/2008

35 - Oxygen

35-1

19a

11/17/2008

36 - Pneumatic

36-1 Thru 36-2

19a

11/17/2008

38 - Water/Waste

38-1 Thru 38-2

19a

11/17/2008

46 - Information Systems

46-1 Thru 46-2

19a

11/17/2008

49 - Airborne Auxiliary Power

49-1

19a

11/17/2008

52 - Doors

52-1

19a

11/17/2008

56 - Windows

56-1

19a

11/17/2008

61 - Propellers

61-1

19a

11/17/2008

72 - Engine

72-1

19a

11/17/2008

73 - Engine Fuel & Control

73-1

19a

11/17/2008

77 - Engine Indicating

77-1

19a

11/17/2008

79 - Engine Oil

79-1

19a

11/17/2008

80 - Engine Starting

80-1

19a

11/17/2008

 

 


 

EFFECTIVE ABOVE DATE, the L-382 (C-130) Master Minimum Equipment List has been COMPLETELY revised. Please replace ALL pages for a complete up-to-date MMEL. SEE NOTES BELOW FOR IMPORTANT INFORMATION ABOUT THIS REVISION.  Retain this sheet with your MMEL until the next revision is issued.

 

NOTE 1 : Pages WILL NOT be itemized in a CONTROL PAGE for individual revisions. Rather, the ATA section will contain the applicable number of pages and revision number. Any changes to any item within an ATA section will result in the entire section receiving a revision number. To find any revised item within the section see the list below.

 

NOTE 2 : The “Table of Contents” has been replaced with a “Contents” page having System, Pages, and Revision Numbers.

 

ATA

System/Sequence Number

 

Remarks

 

 

 

 

21

Air Conditioning

 

 

 

 

 

 

 

21-3

 

Added “Normal” to proviso.

 

 

 

 

 

21-3   1)

 

Added provisos for A/C with Alternate Manual Temperature Control System installed.

 

 

 

 

 

21-4  1)

 

Added sub item 1).

 

 

 

 

 

21-4  2)

 

Added sub item 2), a), b), c).

 

 

 

 

 

21-5

 

Added “Normal” to proviso.

 

 

 

 

 

21-5  1)

 

Added sub item 1).

 

 

 

 

 

21-6  1)

 

Added sub items 1)

 

 

 

 

 

21-6  2)

 

Added sub item 2), a), b), c).

 

 

 

 

 

21-11  3)

 

Revised title to more accurately describe system.

 

 

 

 

 

21-11  4)

 

Added sub items 4)

 

 

 

 

 

21-22  3)

 

Added item for A/C with SB 382-36-4.

 

 

 

 

 

21-22  4)

 

Renumbered item.

 

 

 

 

 

21-25

 

Deleted “is considered inoperative” per PL 25.

 

 

 

 

 

21-26

 

Deleted “is considered inoperative” per PL 25.

 

 

 

 

22

Auto Flight

 

 

 

 

 

 

 

22-2

 

Deleted “is considered inoperative” per PL 25.

 

 

 

 

 

22-3

 

Updated to current PL-093. Deleted “is considered inoperative” per PL 25.

 

 

 

 

 

22-5

 

Deleted “is considered inoperative” per PL 25.

 

 

 

 

 

22-6

 

Deleted “is considered inoperative” per PL 25.

 

 

 

 

23

Communications

 

 

 

 

 

 

 

23-4

 

Updated to current PL-106.

 

 

 

 

 

23-9

 

Updated to current PL-117.

 

 

 

 

24

Electrical

 

 

 

 

 

 

 

24-7  1) and 2)

 

Deleted “is considered inoperative” per PL 25.

 

 

 

 

25

Equipment / Furnishings

 

 

 

 

 

 

 

25-2

 

Updated to current PL-120.

 

 

 

 

 

25-3

 

Updated to current PL-097.

 

 

 

 

 

25-6

 

Updated to current PL-079.

 

 

 

 

 

25-8

 

Updated to current PL-116.

 

 

 

 

 

25-11

 

Updated to current PL-073.

 

 

 

 

 

25-15

 

Updated to current PL-104.

 

 

 

 

 

25-16

 

New item per PL-122.

 

 

 

 

26

Fire Protection

 

 

 

 

 

 

 

26-2

 

Deleted “is considered inoperative” per PL 25.

 

 

 

 

 

26-4

 

Corrected typo, “Overhead” to “Overheat”.

 

 

 

 

30

Ice and Rain

 

 

 

 

 

 

 

30-08   1) and 2)

 

Added relief for Prop and Engine Anti-Icing Master Switch INOP.

 

 

 

 

 

 

 

 

31

Indicating / Recording

 

 

 

 

 

 

 

31-2

 

Updated to current PL-087.

 

 

 

 

33

Lights

 

 

 

 

 

 

 

33-8  1)

 

Added item for A/C with STC #ST01162LA.

 

 

 

 

34

Navigation

 

 

 

 

 

 

 

34-11  1)

 

Updated to current PL-067.

 

 

 

 

 

34-13  1)

 

Updated to current PL-076.

 

 

 

 

 

34-21

 

Updated to current PL-054.

 

 

 

 

 

34-28

 

Updated to current PL-032.

 

 

 

 

 

34-31

 

Added relief for second MFD with Five Display Unit System installed.

 

34-34, 1), 2), 3), 4)

 

Change number installed to “-“.

 

 

 

 

35

Oxygen

 

 

 

 

 

 

 

35-1

 

Deleted “is considered inoperative” per PL 25.

 

 

 

 

46

Information Systems

 

 

 

 

 

 

 

46-1

 

Added relief for EFB.

 

 

 

 

77

Engine Indicating

 

 

 

 

 

 

 

77-1

 

Change title from Torque Indicators to Torque Indications.

 

 

 

 

79

Engine Oil

 

 

 

 

 

 

 

79-1

 

Changed title from Low Oil Pressure Warning Light, to Engine Low Oil Pressure Warning Indications.

 

 

 

 

 

79-2

 

Changed title from Oil Quantity Indicators, to Oil Quantity Indications.

 

 

 

 

 

79-3

 

Added additional relief for Engine Low Oil Quantity Indicating Systems for those aircraft with Engine Instrument Display Systems.

 

 

 

 

 

79-4

 

Changed title of Oil Cooler Flap Position Indicator, to Oil Cooler Flap Position Indications.

 

 

 

 

 

79-5 2)

 

Deleted word “manual” from proviso.

 

 

 

 

 

 

 

 

 

 

 

 

80

Starting

 

 

 

 

 

 

 

80-1

 

Changed title of Start Push Button Light, to Start Valve Open Light (Start Push Button Light).

 

 


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 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 (ETOPS) which has a type design approval for ER operations (ETOPS) 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 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 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 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.

 

NO CUSTOMIZED DEFINITIONS OF FAULT ALERTING ARE APPLICABLE TO THE LOCKHEED L-382 MMEL.

 


 

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

 

28.  “Considered Inoperative”, as used in the provisos means that item must be treated for dispatch, taxi and flight purposes as though it were inoperative.  The item shall not be used or operated until the original deferred item is repaired.  Additional actions include:  documenting the item on the dispatch release (if applicable), placarding, and complying with all remarks, exceptions, and related MMEL provisions, including any (M) and (O) procedures and observing the repair category.

 

29.  “Is not used” in the provisos, remarks or exceptions for an MMEL item may specify that another item relieved in the MMEL “is not used.”  In such cases, crewmembers should not activate, actuate, or otherwise utilize that component or system under normal operations.  It is not necessary for the operators to accomplish the (M) procedures associated with the item.  However, operational requirements must be complied with, and an additional placard must be affixed, to the extent practical, adjacent to the control or indicator for the item that is not used to inform crewmembers that a component or system is not to be used under normal operations.

 


 

30.  Nonessential equipment and furnishings (NEF) are those items installed on the aircraft as part of the original certification, supplemental type certificate, or engineering order that have no effect on the safe operation of flight and would not be required by the applicable certification rules or operational rules.  They are those items that if inoperative, damaged or missing have no effect on the aircraft’s ability to be operated safely under all operational conditions.  These nonessential items may be installed in areas including, but not limited to, the passenger compartment, flight deck area, service areas, cargo areas, crew rest areas, lavatories, and galley areas.  NEF items are not items already identified in the MEL or CDL of the applicable aircraft.  They do not include items that are functionally required to meet the certification rule or for compliance with any operational rule.  Operator’s NEF process shall not provide for deferral of items within serviceable limits identified in the manufacturer’s maintenance manual or operator’s approved maintenance program such as wear limits, fuel/hydraulic leak rates,

oil consumption, etc.  Cosmetic items that are fully serviceable but worn or soiled may be deferred under an operator’s NEF process.

 

 

 

 


 

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.

 

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

 

 

 

 

 

 


span style='font-size:11.0pt;font-family:Arial'

AIR CONDITIONING

 

 

 

 

 

 

 

 

 

 

 

 

1.

Air Conditioning Systems

C

2

1

(M) One may be inoperative provided 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 Diverter Valve (Airplanes prior to Serial Number 4653)

C

1

0

(M) May be inoperative provided Valve is secured OPEN.

 

 

 

 

 

 

 

 

3.

Cargo Compartment Automatic Temperature Control System

C

1

0

May be inoperative provided Cargo Compartment Normal Manual Temperature Control System is operative.

 

|

 

 

 

 

 

 

 

 

 

 

C

1

0

May be inoperative provided Cargo Compartment Air Conditioning System is considered inoperative.

 

 

 

 

 

 

 

 

1)

Airplanes with SB 382-21-10 (Alternate Manual Temperature Control System) Installed

C

1

0

May be inoperative provided:

a)          Cargo Compartment Alternate Manual Temperature Control System is operative, and

b)          Cargo Compartment Alternate Manual Temperature Control Duct Overheat Indication is operative.

|

|

|

|

|

|

|

 

 

 

 

 

 

 


21

AIR CONDITIONING

 

 

 

 

 

 

 

 

 

 

 

 

4.

Cargo Compartment Manual Temperature Control Systems

 

 

 

 

|

|

|

 

 

 

 

 

 

 

1)

Normal Manual Temperature Control System

C

1

0

May be inoperative provided Cargo Compartment Air Conditioning System is considered inoperative.

|

|

|

 

 

 

 

 

 

 

2)

Airplanes with SB 382-21-10 (Alternate Manual Temperature Control System) Installed

 

 

 

 

|

|

|

|

|

 

 

 

 

 

 

 

a)

Normal Manual Temperature Control System

C

1

0

May be inoperative provided:

a)          Cargo Compartment Alternate Manual Temperature Control System is operative, and

b)          Cargo Compartment Alternate Manual Temperature Control Duct Overheat Indication is operative.

|

|

|

|

|

|

|

 

 

 

 

 

 

 

b)

Alternate Manual Temperature Control System

C

1

0

May be inoperative provided normal Cargo Compartment Manual Temperature Control System is operative.

|

|

|

|

 

 

 

 

 

 

 

c)

Alternate Manual Temperature Control Duct Overheat Indication

C

1

0

May be inoperative provided normal Cargo Compartment Manual Temperature Control System is operative.

|

|

|

|

 

 

 

 

 

 

 


21

AIR CONDITIONING

 

 

 

 

 

 

 

 

 

 

 

 

5.

Flight Station Automatic Temperature Control System

C

1

0

May be inoperative provided Flight Station Normal Manual Temperature Control is operative.

 

|

 

 

 

 

 

 

 

 

 

 

C

1

0

May be inoperative provided Flight Station Air Conditioning System is considered inoperative.

 

 

 

 

 

 

 

 

1)

Airplanes with SB 382-21-10 (Alternate Manual Temperature Control System) Installed

C

1

0

May be inoperative provided:

a)          Flight Station Alternate Manual Temperature Control System is operative, and

b)          Flight Station Alternate Manual Temperature Control Duct Overheat Indication is operative.

|

|

|

|

|

|

|

 

 

 

 

 

 

 

6.

Flight Station Manual Temperature Control Systems

 

 

 

 

 

 

|

 

 

 

 

 

 

 

1)

Normal Manual Temperature Control System

C

1

0

May be inoperative provided Flight Station Air Conditioning System is considered inoperative.

|

|

|

 

 

 

 

 

 

 

2)

Airplanes with SB 382-21-10 (Alternate Manual Temperature Control System) Installed

 

 

 

 

|

|

|

|

 

 

 

 

 

 

 

a)

Normal Manual Temperature Control System

C

1

0

May be inoperative provided:

a)          Flight Station Alternate Manual Temperature Control System is operative, and

b)          Flight Station Alternate Manual Temperature Control Duct Overheat Indication is operative.

|

|

|

|

|

|

|

 

 

 

 

 

(Continued)

 


21

AIR CONDITIONING

 

 

 

 

 

 

 

 

 

 

 

 

6.

Flight Station Manual Temperature Control Systems (Cont’d)

 

 

 

 

 

 

 

 

 

 

 

 

2)

Airplanes with SB 382-21-10 (Alternate Manual Temperature Control System) Installed (Cont’d)

 

 

 

 

 

 

 

 

 

 

 

 

b)

Alternate Manual Temperature Control System

C

1

0

May be inoperative provided normal Flight Station Manual Temperature Control System is operative.

|

|

|

 

 

 

 

 

 

 

c)

Alternate Manual Temperature Control Duct Overheat Indication

C

1

0

May be inoperative provided normal Flight Station Manual Temperature Control System is operative.

|

|

|

|

 

 

 

 

 

 

 

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 Pressurization Control System

C

1

0

May be inoperative provided:

a)          Manual Pressure Control 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 Pressurization Control System

C

1

0

(M) May be inoperative provided:

a)          Manual Pressurization Cam is NEUTRAL, and

b)          Automatic Pressurization System is operative.

 

 

 

 

 

 

 

 


21

AIR CONDITIONING

 

 

 

 

 

 

 

 

 

 

 

 

10.

GTC Function of Air Conditioning Master Control Switch (Airplanes prior to Serial Number 4653)

C

1

0

 

 

 

 

 

 

 

 

 

11.

Cargo Compartment Air Conditioning Shutoff Switch (Except C-130A)

 

 

 

 

 

 

 

 

 

 

 

 

1)

Airplanes Prior to Serial Number 4653 Without bleed Air Divider Valve

C

1

0

May be inoperative provided:

a)          Both Wing Isolation Valves are operative, and

b)          Aircraft is not operated in known or forecast icing conditions.

 

 

 

 

 

 

 

 

2)

Airplanes Prior to Serial Number 4653 With Bleed Air Divider Valve

C

1

0

May be inoperative provided Right Wing Isolation Valve and Bleed Air Divider Valve are operative.

 

 

 

 

 

 

 

 

3)

Airplanes Prior to Serial Number 4653 With Bleed Air Divider Valve
(SB 382-36-4 Incorporated)

C

1

0

May be inoperative provided:

a)          No. 3 and 4 Bleed Air 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.

|

|

|

|

|

|

|

|

 

 

 

 

 

 

 

4)

Airplanes Serial Number 4653 and Subsequent

C

1

0

May be inoperative provided:

a)          No. 3 and 4 Bleed Air 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.

|


21

AIR CONDITIONING

 

 

 

 

 

 

 

 

 

 

 

 

12.

Flight Station Air Conditioning Flow Control and Shutoff Valve System

 

 

 

 

 

 

 

 

 

 

 

 

1)

Airplanes Prior to Serial Number 4653

C

1

0

May be inoperative provided Flow Control and Shutoff Valve Override is operative

 

 

 

 

 

 

 

 

2)

Airplanes Serial Number 4653 and Subsequent

C

1

0

May be inoperative provided:

a)          No. 1 and 2 Bleed Air 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-Climb Indicator

C

1

0

May be inoperative provided:

a)          Cabin Altimeter is operative, and

b)          Differential Pressure Gauge is operative.

 

 

 

 

 

 

 

 

14.

Differential Pressure Gauge

C

1

0

(O) May be inoperative provided:

a)          Cabin Altimeter is operative, and

b)          A chart is available for the Flight Engineer to convert Cabin Altitude to Differential Pressure.

 

 

 

 

 

 

 

 


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 Underfloor Heating

C

1

0

 

 

 

 

 

 

 

 

 

17.

Emergency Depressurization Switch

C

1

0

May be inoperative provided Emergency Depressurization Handle is operative.

 

 

 

 

 

 

 

 

18.

Emergency Depressurization Handle

 

 

 

 

 

 

 

 

 

 

 

 

1)

Airplanes Equipped with Bleed Air Shutoff Valves

C

1

0

(O) May be inoperative provided aircraft is operated unpressurized.

 

 

 

 

 

 

 

 

2)

Airplanes Equipped with Bleed Air Pressure Regulating and Shutoff Valves

C

1

0

 

 

 

 

 

 

 

 

 

19.

Safety Valve

C

1

0

(M)(O) May be inoperative provided:

a)          Outflow Valve is secured OPEN, and

b)          Aircraft is operated unpressurized.

 

 

 

 

 

 

 

 

20.

Cargo Compartment Auxiliary Vent Valve

C

1

0

(M) May be inoperative provided:

a)          Affected Valve is secured CLOSED, and

b)          Flight Station Auxiliary Vent Valve is operative.

 


21

AIR CONDITIONING

 

 

 

 

 

 

 

 

 

 

 

 

21.

Flight Station Auxiliary Vent Valve

C

1

0

(M) May be inoperative provided:

a)          Affected Valve is secured CLOSED, and

b)          Cargo Compartment Auxiliary Vent Valve is operative.

 

 

 

 

 

 

 

 

22.

Cargo Compartment Flow Control and Shutoff Valve

 

 

 

 

 

 

 

 

 

 

 

 

1)

Airplanes Prior to Serial Number 4653 Without Bleed Air Divider Valve

C

1

0

May be inoperative provided:

a)          Both Wing Isolation Valves are operative, and

b)          Aircraft is not operated in known or forecast icing conditions.

 

 

 

 

 

 

 

 

2)

Airplanes Prior to Serial Number 4653 With Bleed Air Divider Valve

C

1

0

May be inoperative provided Right Wing Isolation Valve and Bleed Air Divider Valve are operative.

 

 

 

 

 

 

 

 

3)

Airplanes Prior to Serial Number 4653 With Bleed Air Divider Valve
(SB 382-36-4 Incorporated)

C

1

0

May be inoperative provided:

a)          No. 3 and 4 Bleed Air 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.

|

|

|

|

|

|

|

|

 

 

 

 

 

 

 

4)

Airplanes Serial Number 4653 and Subsequent

C

1

0

May be inoperative provided:

a)          No. 3 and 4 Bleed Air 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.

|

 

 

 

 

 

 

 


21

AIR CONDITIONING

 

 

 

 

 

 

 

 

 

 

 

 

23.

Flight Station Flow Control and Shutoff Valve

 

 

 

Moved to 21-12, Revision 19.

 

 

 

 

 

 

 

 

24.

Cargo Compartment Recirculation Fan System

C

1

0

 

 

 

 

 

 

 

 

 

25.

Cargo Compartment Refrigeration Overheat Warning Light

C

1

0

May be inoperative provided Cargo Compartment Air Conditioning System is not used.

|

|

|

 

 

 

 

 

 

 

26.

Air Conditioning Anti-Ice Overtemp Warning Light System/AIR COND HOT Light System (Airplanes Serial Number 4653 through 4946 Not Modified by Service Bulletin 382-21-12/82-503)

C

2

1

May be inoperative provided associated Air Conditioning System is not used.

|

|

|

 

 

 

 

 

 

 

 

 

C

2

0

(O) May be inoperative provided both Air Conditioning Systems are not used.

|

|

 

 

 

 

 

 

 

27.

Cargo Compartment Air Conditioning Pack Overheat Warning System

 

 

 

Moved to 21-25, Revision 19.

 

 

 

 

 

 

 

 


22

AUTO FLIGHT

 

 

 

 

 

 

 

 

 

 

 

 

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 Navigation Modes (NAV/LOC, HDG)

C

-

0

May be inoperative provided enroute operations or approach minimums do not require their use.

 

 

 

 

 

 

 

 

 

 

 

 

 

NOTE: Any mode that operates normally may be used.

 

 

 

 

 

 

 

 

2)

Vertical Navigation Modes (ALT, ALT SEL, VS, IAS)

C

-

0

May be inoperative provided enroute operations or approach minimums do not require their use.

 

 

 

 

 

 

 

 

 

 

 

 

 

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 Coupler

C

-

0

May be inoperative provided approach minimums do not require its use.

 

 

 

 

 

 

 

 


22

AUTO FLIGHT

 

 

 

 

 

 

 

 

 

 

 

 

2.

AUTOPILOT OFF or AP DISENG Light

C

2

1

 

 

 

 

 

 

 

 

 

 

 

B

-

0

May be inoperative provided autopilot is not used.

|

|

 

 

 

 

 

 

 

3.

Autopilot Release Switch, Wheel Mounted

C

2

1

One may be inoperative provided:

a)          Autopilot is not used below 1,500 feet AGL, and

b)          Approach minimums do not require the use of the autopilot.

|

|

|

|

|

 

 

 

 

 

 

 

 

 

B

2

0

May be inoperative provided autopilot is not used.

|

|

 

 

 

 

 

 

 

4.

Radio Beam Coupler

 

 

 

Moved to 22-1, Revision 19.

 

 

 

 

 

 

 

 

5.

Autopilot Trim Indices (E-4)

B

3

0

May be inoperative provided autopilot is not used.

|

|

 

 

 

 

 

 

 

6.

Yaw Damper (AP105)

B

1

0

May be inoperative provided autopilot is not used.

|

|

 

 

 

 

 

 

 


23

COMMUNICATIONS

 

 

 

 

 

 

 

 

 

 

 

 

1.

Crewmember Interphone System

 

 

 

 

 

 

 

 

 

 

 

 

1)

Flight Station to Cargo Compartment, Cargo Compartment To Flight Station Function

C

1

0

(O) May be inoperative provided alternate Normal and Emergency Procedures and/or operating restrictions are established and used.

 

 

 

 

 

 

 

 

 

 

 

 

 

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 to Ground Function

C

1

0

(O) May be inoperative provided alternate procedures are established and used.

 

 

 

 

 

 

 

 

 

 

D

1

0

May be inoperative provided procedures do not require its use.

 

 

 

 

 

 

 

 

3)

Flight Station to Passenger Cabin, Passenger Cabin to Flight Station Function (Combi Aircraft Only)

C

1

0

(O) May be inoperative provided:

a)          Public Address System is operative, and

b)          Alternate procedures are established and used.

 

 

 

 

 

 

 

 

 

 

 

 

 

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

 

 

 

 

 

 

 

 

 

 

D

1

0

May be inoperative provided procedures do not require its use.

 

 

 

 

 

 

 

 


23

COMMUNICATIONS

 

 

 

 

 

 

 

 

 

 

 

 

2.   ***

Public Address (PA) System

 

 

 

 

 

 

 

 

 

 

 

 

1)

Passenger/Combi Configuration

B

1

0

(O) May be inoperative provided:

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 Speaker

C

1

0

(O) May be inoperative provided alternate procedures are established and used.

 

 

 

 

 

 

 

 

2)

Cargo Configuration

C

1

0

(O) May be inoperative provided 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 Speaker

C

1

0

(O) May be inoperative provided alternate procedures are established and used.

 

 

 

 

 

 

 

 

 

 

D

1

0

May be inoperative provided procedures do not require its use.

 

 

 

 

 

 

 

 


23

COMMUNICATIONS

 

 

 

 

 

 

 

 

 

 

 

 

3.

Communication Systems (VHF, UHF)

D

-

-

Any in excess of those required by FAR may be inoperative provided Communications Systems powered by Isolated DC Bus are operative.

 

 

 

 

 

 

 

 

1)

VHF Comm Control Panels

 

 

 

 

 

 

 

 

 

 

 

 

a)

Frequency Transfer Lights

C

-

0

 

 

 

 

 

 

 

 

 

b)

Frequency Transfer Switch

C

-

0

 

 

 

 

 

 

 

 

 

c)

Frequency Selector Knob

C

-

2

 

 

 

 

 

 

 

 

 

d)

Frequency Indication

C

-

2

 

 

 

 

 

 

 

 

 


23

COMMUNICATIONS

 

 

 

 

 

 

 

 

 

 

 

 

4.

High Frequency (HF) Communication Systems

D

-

-

Any in excess of those required by FAR may be inoperative.

 

 

 

 

 

 

 

 

 

 

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)          If Inmarsat codes are not available while using SATCOM voice, prior coordination with the appropriate ATS facility is required.

 

 

 

 

 

 

 

 

 

|

|

|

|

 

 

 

 

 

 

 

 

 

 

 

 

 

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.

 

 

 

 

 

 

 

 


23

COMMUNICATIONS

 

 

 

 

 

 

 

 

 

 

 

 

6.

Boom Microphones

 

 

 

 

 

 

 

 

 

 

 

 

1)

Cockpit Voice Recorder Equipped to Record Boom Microphone per FAR 121.139 (e), 135.151 (d), or 125.227 (e)

A

-

0

May be inoperative provided:

a)              Flight Data Recorder (FDR) is operative, and

b)              Repair is made within three flight days.

 

 

 

 

 

 

 

 

2)

Cockpit Voice Recorder Not Equipped to Record Boom Microphone

D

-

0

 

 

 

 

 

 

 

 

 

7.

Megaphones

 

 

 

Moved to 25-9, Revision 19.

 

 

 

 

 

 

 

 

8.

Cockpit Voice Recorder (CVR)

A

1

0

May be inoperative provided:

a)              Flight Data Recorder (FDR) is operative, and

b)              Repair is made within three flight days.

 

 

 

 

 

 

 

 

9.  ***

Selective Call System (SELCAL)

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.

 

 

 

 

 

 

 

 

1)

Channels

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.

|

|

 

 

 

 

 

 

 


23

COMMUNICATIONS

 

 

 

 

 

 

 

 

 

 

 

 

10.

Radio Management Unit (RMU) (STC#ST01162LA)

B

2

1

(O) May be inoperative provided:

a)              Cross-side tuning function of the operative RMU operates normally, and

b)              Radio tuning function of both FMS CDUs operate normally.

 

 

 

 

 

 

 

 

11.

Intercom Control Panel (ICS)

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.

 

 

 

 

 

 

 

 

12.

Satellite Communications System (SATCOM)

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.

 

 

 

 

 

 

 

 

13.

Data Link System

C

-

0

(O) May be inoperative provided alternate procedures do not require its use.

 

 

 

 

 

 

 

 

 

 

D

-

0

May be inoperative provided procedures do not require its use.

 

 

 

 

 

 

 

 

14.

Push-to-Talk Switches (PTT)

 

 

 

 

 

 

 

 

 

 

 

 

1)

Control Wheel Switches

C

2

1

(M) May be inoperative provided:

a)          Associated audio control panel PTT or hand microphone operates normally, and

b)          Failed switch is verified failed open.

 

 

 

 

 

 

 

 

 

 

 

 

 

(Continued)

 

 

 

 

 

 

 

 


23

COMMUNICATIONS

 

 

 

 

 

 

 

 

 

 

 

 

14.

Push-to-Talk Switches (PTT) (Cont’d)

 

 

 

 

 

 

 

 

 

 

 

 

2)  ***

Engineer’s Push-to-Talk Switch (Includes Foot Switch)

C

-

1

(M) May be inoperative provided:

a)          Associated audio control panel PTT or hand microphone operates normally, and

b)          Failed switch is verified failed open.

 

 

 

 

 

 

 

 

3)

Other Stations Switches

C

-

-

(M) May be inoperative provided:

a)          Associated audio control panel PTT or hand microphone operates normally, and

b)          Failed switch is verified failed open.

 

 

 

 

 

 

 

 

15.  ***

Headphones/Hand Microphones

D

-

-

Any in excess of those required by FAR for flight deck crewmembers may be inoperative or missing.

 

 

 

 

 

 

 

 


24

ELECTRICAL POWER

 

 

 

 

 

 

 

 

 

 

 

 

1.

Frequency Meter System

C

1

0

May be inoperative provided all 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.

 

 

 

 

 

 

 

 


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 Transformer Rectifier (Except C-130A)

C

2

1

 

 

 

 

 

 

 

 

 

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.

 

 

 

 

 

 

 

 


24

ELECTRICAL POWER

 

 

 

 

 

 

 

 

 

 

 

 

7.

AC Loadmeter (40 KVA Generator)

 

 

 

 

 

 

 

 

 

 

 

 

1)

C-130A

B

3

2

May be inoperative provided associated generator is not used.

|

|

 

 

 

 

 

 

 

2)

Except C-130A

C

5

-

May be inoperative provided associated generator is not used.

|

|

 

 

 

 

 

 

 

8.

AC Instruments and Engine Fuel Control Inverter (2500 VA) (Except C-130A)

B

1

0

May be inoperative provided AC electrical power is available for engine start.

 

 

 

 

 

 

 

 

9.

Co-Pilot’s AC Instruments Inverter (250 VA) (Except C-130A)

 

 

 

Deleted, Revision 19.

 

 

 

 

 

 

 

 

10.

Inverter (500 VA) Pilot’s (C-130A)

B

1

0

May be inoperative provided both AC Generators are operative.

 

 

 

 

 

 

 

 

11.

Inverter (100 VA) Copilot’s (C-130A)

B

1

0

May be inoperative provided both AC Generators are operative.

 

 

 

 

 

 

 

 

12.

DC Generators (C-130A)

B

4

3

May be inoperative provided associated voltmeter and ammeter are operative.

 

 

 

 

 

 

 

 

13.

Transformer Rectifier (C-130A)

B

2

1

 

 

 

 

 

 

 

 

 


25

EQUIPMENT/ FURNISHINGS

 

 

 

 

 

 

 

 

 

 

 

 

1.

Crewmember Shoulder Harness

 

 

 

DELETED in Revision 18.

 

 

 

 

 

 

 

 

2.    ***

Emergency Locator Transmitter (ELT)

 

 

 

 

|

|

 

 

 

 

 

 

 

 

Survival Type ELTs

D

-

-

Any in excess of those required by FAR may be inoperative or missing.

|

|

 

 

 

 

 

 

 

 

Fixed ELTs

A

-

0

May be inoperative or missing provided repairs are made within 90 days.

|

|

 

 

 

 

 

 

 

 

 

D

-

-

Any in excess of those required by FAR may be inoperative or missing.

|

|

 

 

 

 

 

 

 


25

EQUIPMENT/ FURNISHINGS

 

 

 

 

 

 

 

 

 

 

 

 

3.

Flight Attendant Seat (Single or Dual Position)

 

 

 

 

 

 

 

 

 

 

 

 

 

Aircraft With Only One Flight Attendant Seat

A

1

0

(M)(O) May be inoperative provided:

a)          Affected seat is not 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)

 

 

 

 

 

 

 

 


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.

 

 

 

 

 

 

 

 

 

 

D

1

0

(M) May be inoperative provided:

a)          Flight Attendant is not required by FAR,

b)          Affected seat is not occupied, and

c)          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.

|

|

|

 

 

 

 

 

 

 

 

 

 

 

 

(Continued)

 

 

 

 

 

 

 

 


25

EQUIPMENT/ FURNISHINGS

 

 

 

 

 

 

 

 

 

 

 

 

3.

Flight Attendant Seat (Single or Dual Position) (Continued)

 

 

 

 

 

 

 

 

 

 

 

 

 

Aircraft With More Than One Flight Attendant Seat

 

 

 

 

 

 

 

 

 

 

 

 

1)

Required Flight Attendant Seats

B

-

-

(M)(O) One seat or assembly (dual 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 adjacent flight attendant seat or the passenger seat which is more 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)

 

 

 

 

 

 

 

 


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)

 

 

 

 

 

 

 

 


25

EQUIPMENT/ FURNISHINGS

 

 

 

 

 

 

 

 

 

 

 

 

3.

Flight Attendant Seat (Single or Dual Position) (Continued)

 

 

 

 

 

 

 

 

 

 

 

 

 

Aircraft With More Than One Flight Attendant Seat (Continued)

 

 

 

 

 

 

 

 

 

 

 

 

2)

Excess Flight Attendant Seats

C

-

-

(M) May be inoperative provided:

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 Configuration

D

-

-

May be inoperative provided affected seat or seat assembly is not occupied.

 

 

 

 

 

 

 

 

4.

Flight Attendant Seat Lap Belt

 

 

 

Moved to 25-3, Revision 19.

 

 

 

 

 

 

 

 


25

EQUIPMENT/ FURNISHINGS

 

 

 

 

 

 

 

 

 

 

 

 

5.

Observer Seat(s)

 

 

 

 

 

 

 

 

 

 

 

 

1)

Primary Observer Seat (Including Associated Equipment)

A

-

-

May be inoperative provided:

a)          A passenger seat in the passenger cabin is made available to an FAA 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)