C130_PWS_UDLM_PDM_App_A_C130HJ_Work_Spec_FY20_dtd_12Sep19.pdf

PWS APPENDIX A

C-130H & C-130J

Work Specification (WS) Combined File

FY20

DEPARTMENT OF THE AIR FORCE

Work Spec: FY20 Final

MDS: AC130H, AC130U, C130E, EC130H, HC130N, HC130P, LC130H, MC130E,

MC130H, MC130P, AC130W, WC130H, C130H 83+, HC130N/P 64-69, C130H

78-82, C130H 73-74, C130H 83-99, C130H, HC130(H)N 88-93

27/06/2019

1.0 - (Changed) General

1.1 - (Changed) Information

1.1.1 - (Changed) This Work Specification establishes the minimum work requirements for Program Depot

Maintenance (PDM), modification, flight test and preparation for delivery of C-130 type aircraft by organic depot facilities and returns C-130 type aircraft to a serviceable but not like new condition.

NOTE: This project is unclassified; however, no data, technical or otherwise concerning this project, shall be released through publication or in any manner except with specific written authorization by AFLCMC /WLN.

AC130U

AC130W

C130H 73-74

C130H 78-82

C130H 83+

HC130(H)N 88-93

HC130N/P 64-69

LC130H

MC130H

MC130P

WC130H

Assigned MDS(s)

1.1.2 - (Changed) The aircraft shall be returned to the assigned organization in the same configuration as received, with the same type components, accessories, and special equipment installed except as modified, removed, or added by requirements of this Work Specification. Specifically equipped or instrumented aircraft are subject to be worked under the requirements of this Work Specification . This paragraph shall also apply to special configured aircraft.

AC130U

AC130W

C130H 73-74

C130H 78-82

C130H 83+

HC130(H)N 88-93

HC130N/P 64-69

LC130H

MC130H

MC130P

WC130H

Assigned MDS(s)

1.1.3 - (Changed) Special tools and test equipment are required. Special tools and test equipment required to accomplish PDM are listed in paragraph 3.2.25 of this Work Specification.

Assigned MDS(s)

Page 1 of 379June 27, 2019

AC130U

AC130W

C130H 73-74

C130H 78-82

C130H 83+

HC130(H)N 88-93

HC130N/P 64-69

LC130H

MC130H

MC130P

WC130H

1.1.5 - (Changed) Discrepancies found which do not require correction by this specification shall be recorded in aircraft historical records IAW TO 00-20-1.

AC130U

AC130W

C130H 73-74

C130H 78-82

C130H 83+

HC130(H)N 88-93

HC130N/P 64-69

LC130H

MC130H

MC130P

WC130H

Assigned MDS(s)

1.1.6 - Only those systems worked by a specific requirement or disturbed by other requirements of this specification shall be made operational unless a safety of flight condition exists or it is an overseas requirement as required by Section 3.

AC130H

AC130J

AC130U

AC130W

C130E

C130H

C130H 73-74

C130H 78-82

C130H 83+

C130H 83-99

EC130H

HC130N

HC130N/P 64-69

HC130P

LC130H

MC130E

MC130H

MC130P

WC130H

Assigned MDS(s)

1.1.7 - (Changed) Any deviations from this Work Specification must be approved by C-130 engineering.

Page 2 of 379June 27, 2019

C130H 73-74

C130H 78-82

C130H 83+

HC130(H)N 88-93

HC130N/P 64-69

LC130H

MC130H

MC130P

WC130H

1.1.8 - (Changed) PDM shall include a corrosion control program as outlined in this Work Specification . For the purpose of this Work Specification, corrosion treatment is defined as cleaning, removal of corrosion and deteriorated coatings, chemical treatment of metals, repair and finishing IAW applicable technical orders.

Missing or deteriorated coating systems shall be considered a discrepancy.

AC130U

AC130W

C130H 73-74

C130H 78-82

C130H 83+

HC130(H)N 88-93

HC130N/P 64-69

LC130H

MC130H

MC130P

WC130H

Assigned MDS(s)

1.1.9 - (Changed) Aircraft shall be handled IAW instructions in the applicable OMMS manuals . Qualification of personnel handling and operating aircraft shall conform to AFI 11-218, AFI 11-205 and AFJI 10-220.

AC130U

AC130W

C130H 73-74

C130H 78-82

C130H 83+

HC130(H)N 88-93

HC130N/P 64-69

LC130H

MC130H

MC130P

WC130H

Assigned MDS(s)

1.1.11 - (Changed) Skin patches, battle damage, or other non-conforming repairs installed by the field shall be evaluated by C-130 Engineering.

Page 3 of 379June 27, 2019

C130H 73-74

C130H 78-82

C130H 83+

HC130(H)N 88-93

HC130N/P 64-69

LC130H

MC130H

MC130P

WC130H

1.1.12 - (Changed) Unless otherwise directed in this specification, TO 1C-130A-6, or approved on AFTO Form

103, time change or life limited accessories and components are the responsibility of the assigned organization..

AC130U

AC130W

C130H 73-74

C130H 78-82

C130H 83+

HC130(H)N 88-93

HC130N/P 64-69

LC130H

MC130H

MC130P

WC130H

Assigned MDS(s)

1.1.13 - (Changed) Accomplish painting IAW instructions in paragraph 3.2.29 to this Work Specification, TO

1-1-691 and 1C-130A-23 when applicable. Aircraft not receiving a complete depaint and paint IAW paragraph

3.2.29 of this Work Specification will receive only touch up paint or scuff/sand and overcoat as directed by the

PAO/ACO IAW paragraph 3.2.29.

AC130U

AC130W

C130H 73-74

C130H 78-82

C130H 83+

HC130(H)N 88-93

HC130N/P 64-69

LC130H

MC130H

MC130P

WC130H

Assigned MDS(s)

1.1.15 - (Changed) Shoring is required when major structural components require replacement as depicted in

TO 1C-130A-3.

Page 4 of 379June 27, 2019

C130H 73-74

C130H 78-82

C130H 83+

HC130(H)N 88-93

HC130N/P 64-69

LC130H

MC130H

MC130P

WC130H

1.1.15.1 - (Changed) Special jacking and shoring for structural repairs shall be determined by onsite depot engineering based on the work and repairs to be accomplished on a particular aircraft in lieu of TO

1C-130A-3, and shall be approved by AFLCMC/WLN.

AC130U

AC130W

C130H 73-74

C130H 78-82

C130H 83+

HC130(H)N 88-93

HC130N/P 64-69

LC130H

MC130H

MC130P

WC130H

Assigned MDS(s)

1.1.16 - (Changed) Accomplish Analytical Condition Inspection (ACI) when required IAW paragraph 3.2.24.

AC130U

AC130W

C130H 73-74

C130H 78-82

C130H 83+

HC130(H)N 88-93

HC130N/P 64-69

LC130H

MC130H

MC130P

WC130H

Assigned MDS(s)

1.1.17 - (Changed) Accomplish maintenance compression requirements IAW paragraph 3.2.27 when directed by the PAO/ACO.

Page 5 of 379June 27, 2019

C130H 73-74

C130H 78-82

C130H 83+

HC130(H)N 88-93

HC130N/P 64-69

LC130H

MC130H

MC130P

WC130H

1.1.18 - (Changed) Any discrepancies caused by the depot facility shall be corrected by the depot facility at no cost to the government.

AC130U

AC130W

C130H 73-74

C130H 78-82

C130H 83+

HC130(H)N 88-93

HC130N/P 64-69

LC130H

MC130H

MC130P

WC130H

Assigned MDS(s)

1.1.19 - (Changed) The depot facility shall provide ALL ENGINEERING SERVICES required to support the work requirements of this Work Specification. A. This limited engineering authority allows AFLCMC/WLN certified engineers to provide on-site engineering to resolve structural and mechanical discrepancies on secondary (non-primary) structure and to resolve non-safety of flight discrepancies by developing and implementing solutions for these discrepancies for any USAF C-130 aircraft without AFLCMC/WLN coordination. This authorization also grants authority to provide engineering for modification, design, material substitution, repairs, and technical manual deviations without AFLCMC/WLN approval for secondary

(non-primary) structure and non-safety of flight discrepancies. These engineering solutions will be provided to

WR-ALC in a timely manner. B. This limited engineering authority allows AFLCMC/WLN certified engineers to provide on-site engineering to resolve structural and mechanical discrepancies on primary structure and to resolve safety of flight discrepancies and by developing and implementing solutions for these discrepancies for any USAF C-130 aircraft with AFLCMC/WLN coordination by E-mail. Coordination is defined as providing detailed description of the damaged area(s), detailed repair sketches, and engineering analysis for

AFLCMC/WLN review and approval/disapproval prior to implementing the solution. This authorization also grants authority to provide engineering for modification, design, material substitution, repairs, and technical manual deviations for primary structure and safety of flight discrepancies with AFLCMC /WLN coordination by

E-mail prior to implementation. C. This limited engineering authority does not provide engineering authority to correct discrepancies with solutions not approved in current USAF technical data on the following aircraft systems and sub-components: main landing gear assemblies, nose landing gear assembly, engines and propellers.

Page 6 of 379June 27, 2019

C130H 73-74

C130H 78-82

C130H 83+

HC130(H)N 88-93

HC130N/P 64-69

LC130H

MC130H

MC130P

WC130H

1.1.20 - (Changed) The organic depot facility shall not accomplish O & I Level Maintenance or technical orders unless directed by AFLCMC/WLNA through PAO/ACO or specially directed by this Work Specification

AC130U

AC130W

C130H 73-74

C130H 78-82

C130H 83+

HC130(H)N 88-93

HC130N/P 64-69

LC130H

MC130H

MC130P

WC130H

Assigned MDS(s)

1.1.21 - (Changed) Any other discrepancies discovered during ACI or other PDM activity that are O & I Level discrepancies, unique access, or more economical to correct during PDM, will be approved by the PAO/ACO.

AC130U

AC130W

C130H 73-74

C130H 78-82

C130H 83+

HC130(H)N 88-93

HC130N/P 64-69

LC130H

MC130H

MC130P

WC130H

Assigned MDS(s)

1.1.22 - (Changed) Accomplish other negotiated special maintenance when requested by PAO/ACO on AFTO

Form 103.

Page 7 of 379June 27, 2019

C130H 73-74

C130H 78-82

C130H 83+

HC130(H)N 88-93

HC130N/P 64-69

LC130H

MC130H

MC130P

WC130H

1.2 - (Changed) Terms Explained

Page 8 of 379June 27, 2019

1.2.1 - (Changed) ADMINISTRATIVE CONTRACTING OFFICER (ACO): The Government contracting officer who is responsible for Government contracts administration.

AIRCRAFT EXTERIOR: Aircraft outer skins and outer skins of components, such as flaps, ailerons, elevators, rudder, ramp, cargo door, nose gear doors, and main landing gear doors.

ACCESSIBLE: Applies to areas of equipment that may be inspected or worked without disassembly other than required by this specification.

ACCESSORY: A mechanism or device employed in conjunction with a major item of equipment or installed as part of a system.

AIRFRAME: The structural components of an airplane including the framework and skin of such parts as the fuselage, empennage, wings, and engine mounts (does not include landing gear and engine).

ANALYTICAL CONDITION INSPECTION (ACI): The systematic disassembly and inspection of aircraft or specific portions and parts thereof as specified in the work requirement to locate, analyze, and project the effects of defects (deteriorating conditions, corrosion, fatigue and overstress, failures, etc.). Reference paragraph 3.2.24.

BENCH CHECK: Visual inspection, physical test, and functional check using shop facilities, equipment, procedures, and test parameters, as set forth in applicable technical publications to determine the exact condition.

CALIBRATION: A comparison between two instruments, one of which is a standard of known accuracy, to detect and correlate or adjust any variation in accuracy of the instrument being compared.

COMPONENT: A separate identifiable part of an end item which performs a function within the system or subsystem and is necessary for the proper operation of that end item.

CORRECT DISCREPANCIES: The accomplishment of all necessary work and testing to restore the part, component or aircraft to a serviceable condition status.

DATA: All management, scientific engineering, and logistics information, reports and documentation which are required.

DEPOT FIELD TEAM (DFT): A group of Depot Maintenance personnel who are provided with Government furnished special tools, equipment and supplies to accomplish Maintenance/modification on site at operational bases. The work involves depot level and organizational and intermediate level tasks.

DEPOT LEVEL MAINTENANCE FACILITY: An industrial type facility established to perform overhaul functions or modification and maintenance in support of field and using organizations. This includes AFMC assigned installations and commercial contractors who are engaged in performing depot level work on weapon systems or equipment under contracts issued and managed by AFMC.

DETERIORATED FINISH: When the finish no longer provides the protection for which it was intended.

DISASSEMBLY: Teardown of the item or parts sufficient to permit the type and amount of inspection and work required.

DISCREPANCY, CRITICAL: A discrepancy that impacts safety of flight or could result in loss of life or serious injury, or impacts airworthiness or mission. (Ref: T.O. 00-35D-54)

DISCREPANCY, MAJOR: A discrepancy that results in safety of operation or potential for minor injury ; Foreign

Objects; inoperable systems, defective, or damaged components or other discrepancies that are suspected as non-conformance to applicable specifications, drawings, standards, agreements, technical orders, work

Page 9 of 379June 27, 2019 packages, etc., resulting from workmanship or incomplete/incorrect processes; inoperable systems or other mission limiting discrepancies that are suspected as non-conformance to applicable specifications, drawings, standards, agreements, technical orders, work packages, etc., resulting from workmanship or incomplete/incorrect processes; paint or corrosion discrepancies involving greater than 25 man hours to correct; incomplete, missing or incorrect historical documents. (Ref: T.O. 00-35D-54)

DISCREPANCY, MINOR: A discrepancy that is not sufficiently urgent or dangerous to warrant grounding or discontinued use of the aircraft and corrective action is less than 25 man hours to correct (excluding time to facilitate other maintenance). These may include but are not limited to: loose/missing hardware, paint or corrosion discrepancies, damaged, but serviceable components, equipment document discrepancies not minor administrative errors or those involving historical Documents). (Ref: T.O. 00-35D-54)

DISTURBED SYSTEM: Any system of which the whole or component part has been removed, disassembled, repaired, adjusted, modified, disconnected, or altered.

ECONOMICAL REPAIR: The correction of any discrepancy found, that because of access to that discrepancy during PDM, or because of availability of tools or spares required to correct the discrepancy, is more economical to accomplish during PDM.

END ITEM: A recoverable article of equipment listed in a procuring activity supply catalog .

ENGINE: The complete basic engine as specified in applicable technical order (TO) handbooks listed in the work specification.

ENGINE ACCESSORIES: All external items contained in the fuel, ignition, and control systems that are normally removed for rework or replaced without disassembly of the engine.

FUNCTIONAL CHECK: A check or test of the designed function operation of a specified unit using equipment procedures and limits specified in applicable TOs.

IAW: The abbreviation for: In Accordance With

INSPECT OR CHECK: An examination of an item to determine identity, condition and proper installation.

ISOCHRONAL INSPECTION: A searching inspection, consisting primarily of checking certain components, areas and systems of the aircraft which due to their function shall be accomplished upon the accrual of a specified number of flying hours or as determined by the owning command.

This inspection shall be accomplished as directed by AFTO 103 and approved by AFLCMC/WLNA. This inspection shall be accomplished to determine that no condition exists which, if not corrected, could result in failure of a component or a system malfunction prior to the next scheduled inspection.

LOOSE FASTENER: In the no-load condition, a loose fastener will be physically loose. A black ring around the head of the fastener does not constitute looseness. A black ring may be the result of the wet installation, as indicated by TO 1C-130A-3, 51-40-00 part 3 and 51-40-06.

MAINTENANCE COMPRESSION: A maximum all-out production of selected war mission aircraft and missiles undergoing PDM, modification, or area support within AFMC maintenance facilities. It entails actions which include suspension of routine PDM and modification work and reassembly of aircraft and missiles by accomplishment of only essential safety of flight maintenance and minimum acceptable war configuration mods, realignment of work stations, extension of work week and work day, redistribution of existing labor force, and cannibalization of aircraft on hand.

MDS: Mission Design Series.

MODIFICATION: A change in the physical configuration or in the functional characteristics of system or

Page 10 of 379June 27, 2019 equipment.

N/A: Not Applicable.

NONDESTRUCTIVE INSPECTION (NDI): Methods for investigating the quality, integrity, properties and dimensions of material and components without damaging or impairing their serviceability.

OVERSEAS: Outside the North American Continent.

O & I: Organizational and Intermediate Level Maintenance.

OVERHAUL: The disassembly, cleaning, inspection, repair or replacement of parts or components, reassembly and test of any item or accessory IAW applicable TOs, directives, or authorized manufacturer's publications to provide an operationally safe, serviceable and reliable item.

PARTS: Essential elements, components, or subassemblies of an item.

PREVENTIVE MAINTENANCE: The normal inspection, upkeep and lubrication of equipment required to maintain the serviceability of equipment subjected to usage, wear and deterioration.

PRODUCT AUDIT: An inspection and evaluation of repaired or modified items for the purpose of Government verification that all work directed fully complies with contractual requirements.

PROGRAMMED DEPOT MAINTENANCE (PDM): Depot level maintenance normally applied to aerospace vehicle schedule on a time cycle basis.

PROJECT ADMINISTRATION OFFICE (PAO): The responsible system management (SM) or item management (IM) representative who makes the management and technical decisions to make sure that the negotiated work package is accomplished in organic facilities. The duties are comparable to those of an ACO in contract programs.

RECLAMATION: The process of recovering serviceable or reparable spare parts.

REINSTALL: The reinstallation of a part or component on an aircraft after it has been removed to facilitate inspection, repair, or for military security purposes.

REPAIR: The restoration or replacement of parts or components of an item as necessitated by wear and tear, damage or failure of part in order to maintain the specific item in serviceable condition.

REPAIR FINISH: The coating system which is required to be applied to an area after replacement of components or accomplishment of any work which deteriorates the corrosion protection of the area after inspection shows coatings to be nonexistent or deteriorated.

REPARABLE: An unserviceable item that can be repaired and restored to a serviceable condition.

REPLACE: The replacement of items that are determined by the Government to be beyond economical repair, or as otherwise specifically directed.

SAFETY OF FLIGHT: A failure or malfunction that would present a hazardous condition to equipment or personnel during pre-flight, in-flight, or thru-flight operations.

SERVICEABLE: Capable of meeting the requirement and performing the function for which designed or modified, and meets all test requirements established by the work specifications.

SPECIAL INSPECTION: As used herein shall be interpreted to mean those inspections performed as required

IAW applicable TO 1C-130A-6.

Page 11 of 379June 27, 2019

TECHNICAL ORDERS (TO): A publication that gives specific technical directives and information with respect to the inspection, storage, operation, and maintenance of given items and equipment. Reference to TOs herein will include supplements and latest published changes.

TIME COMPLIANCE TECHNICAL ORDER (TCTO): An authorized directive issued to provide instructions for accomplishing 'one-time' changes, modifications, installation of new equipment, or inspection of equipment.

TOUCH-UP: The repainting of a local area or marking to provide legibility or protection and to meet quality standards.

VISUAL INSPECTION: Consists of visually inspecting for cracks, distortion, corrosion, fastener security, pulled rivets, and undue wear and damage. When inspecting items for corrosion, particular attention must be given to areas of dissimilar metal-to-metal contact (bushing, fasteners, etc.)

WORKBOOK: A listing of aircraft serial numbers, the equipment or systems to be modified, work to be accomplished and provisions for indicating that the work has been accomplished.

AC130U

AC130W

C130H 73-74

C130H 78-82

C130H 83+

HC130(H)N 88-93

HC130N/P 64-69

LC130H

MC130H

MC130P

WC130H

Assigned MDS(s)

1.3 - (Changed) Data

1.3.1 - (Changed) Maintenance Records, Forms and Publications

AC130U

AC130W

C130H 73-74

C130H 78-82

C130H 83+

HC130(H)N 88-93

HC130N/P 64-69

LC130H

MC130H

MC130P

WC130H

Assigned MDS(s)

1.3.1.1 - (Changed) The depot facility shall maintain the forms and publications listed in subparagraph

1.3.1.3 below. If records are not received or are illegible, the Depot shall obtain them from the using command or initiate new records in accordance with the applicable directive set forth in subparagraph

1.3.1.3 below. Maintain applicable forms listed in Column 1 IAW applicable directives listed in Column 3.

Page 12 of 379June 27, 2019

C130H 73-74

C130H 78-82

C130H 83+

HC130(H)N 88-93

HC130N/P 64-69

LC130H

MC130H

MC130P

WC130H

1.3.1.2 - (Changed) Record each technical order compliance in the aircraft historical records furnished with each aircraft IAW TO 00-20-1.

AC130U

AC130W

C130H 73-74

C130H 78-82

C130H 83+

HC130(H)N 88-93

HC130N/P 64-69

LC130H

MC130H

MC130P

WC130H

Assigned MDS(s)

1.3.1.3 - (Changed) These forms and publications shall be maintained from the date the aircraft is received until the date the aircraft departs.

Form Numbers Form Title Applicable Directives

DD 365 Series Record of Weight & Balance TO 1-1B-50

AF 2692 Acft/Missile Equip Transfer/Shipping Listing AFI 21-103

AFTO 58 Structural Repair/Corrosion Tracking Record TO 1C-130A-23

AFTO 95 Significant Historical Data TO 00-20-1

AFTO l7l C-l30 Inspection Tracking Record TO 1C-130A-36

AFTO 781 Series Aerospace Vehicle Flight Data Documents TO 00-20-1

AC130U

AC130W

C130H 73-74

C130H 78-82

C130H 83+

HC130(H)N 88-93

HC130N/P 64-69

LC130H

MC130H

MC130P

WC130H

Page 13 of 379June 27, 2019

1.3.1.4 - (Changed) GH - AFTO Form 95 Entries

A. A notation shall be made in the Significant Historical Data Column of AFTO Form 95, indicating the day, month, year and aircraft time and facility that PDM was accomplished IAW T.O. 00-20-1 and 00-20-2. This shall certify that prescribed requirements of this Work Specification were accomplished .

B. A notation of paint application shall be made as directed by paragraph 3.2.29.

C. AFTO 95 entries are required for the following:

1. PDM/UDLM accomplishment,

2. ISO accomplishment,

3. TCTO accomplishment,

4. A/C paint application,

5. MLG track replacement,

6. Rudder support bearing replacement,

7. Fuel foam replacement (each tank) or fuel boost or dump pumps replacement;

8. Installation of TO 1C-130A-3 repair figures 53-199-14 and 53-40-67

9. A/C critical structure-removed and replaced

10. A/C critical structure-damage repair

11. Accomplishment of TO 1C-130A-6WC-12/13/14/15 work cards

12. Accomplishment of ACI and/or CIE inspections

13. Severe corrosion

14. Special service test equip-installed/ removed

15. Aircraft alignment and symmetry results

16. Removed vertical & horizontal stabilizers

17. Wing removals

18. Added drain holes fwd of FS 245 and in ramp

19. Replaced FS 737 longeron fitting

20. Replaced sloping longeron

21. Replaced FS 1041 fittings

22. Replaced throttle & condition cables

23. Removed engines

24. Replaced struts

25. Replaced ballscrews

26. Removed flight controls

27. Accomplished wing bolt inspection

28. Accomplished bleed air checks

29. Removed bladder cells

30. Removal of bolts at the following locations: FS 245 and 737 splice fittings, FS 737 and 1041 longeron end fittings, and FS 477 and 617 upper tension tie fitting

31. Truss mount replacement

32. MLG vertical beam replacement

33. Installation of FS 517,528,577 and 588 MLG vertical beam splice repairs

34. Any new flapper drain valves installed and the specific FS and BL locations

Page 14 of 379June 27, 2019

AC130H

AC130J

AC130U

AC130W

C130E

C130H

C130H 73-74

C130H 78-82

C130H 83+

C130H 83-99

EC130H

HC130(H)N 88-93

HC130N

HC130N/P 64-69

HC130P

LC130H

MC130E

MC130H

MC130P

WC130H

1.3.1.5 - GH - TO 1C-130A-6 ASIP and Special Inspections and all T0 1C-130A-36 inspections accomplished under requirements of this Work Specification shall be recorded on applicable forms of the aircraft historical records.

AC130H

AC130J

AC130U

AC130W

C130E

C130H

C130H 73-74

C130H 78-82

C130H 83+

C130H 83-99

EC130H

HC130(H)N 88-93

HC130N

HC130N/P 64-69

HC130P

LC130H

MC130E

MC130H

MC130P

WC130H

Assigned MDS(s)

1.3.2 - (Changed) Reporting Requirements

Page 15 of 379June 27, 2019

C130H 73-74

C130H 78-82

C130H 83+

HC130(H)N 88-93

HC130N/P 64-69

LC130H

MC130H

MC130P

WC130H

1.3.2.1 - GH - Engine Status Report (AF FORM 1534). Furnish receipt, change in status and shipment of

AF owned engines T.O. 00-25-254-1.

AC130H

AC130J

AC130U

AC130W

C130E

C130H

C130H 73-74

C130H 78-82

C130H 83+

C130H 83-99

EC130H

HC130(H)N 88-93

HC130N

HC130N/P 64-69

HC130P

LC130H

MC130E

MC130H

MC130P

WC130H

Assigned MDS(s)

1.3.2.2 - GH - Aircraft/Missile Maintenance Status Report (AMREP). AFMCI 21-118 and implementing AFI

21-103.

Page 16 of 379June 27, 2019

AC130U

AC130W

C130E

C130H

C130H 73-74

C130H 78-82

C130H 83+

C130H 83-99

EC130H

HC130(H)N 88-93

HC130N

HC130N/P 64-69

HC130P

LC130H

MC130E

MC130H

MC130P

WC130H

1.3.2.3 - GH - Maintenance Data Documentation (MDD), as required by T.O. 00-20-2, TCTO compliance and status, and repair/replacement actions will be entered into the PPS module of the Reliability &

Maintenance Information System (REMIS) IAW TO 00-20-2.

AC130H

AC130J

AC130U

AC130W

C130E

C130H

C130H 73-74

C130H 78-82

C130H 83+

C130H 83-99

EC130H

HC130(H)N 88-93

HC130N

HC130N/P 64-69

HC130P

LC130H

MC130E

MC130H

MC130P

WC130H

Assigned MDS(s)

1.3.2.4 - GH - Repairable Item Processing Tag IAW TOs 00-20-2 and 00-20-3.

Page 17 of 379June 27, 2019

AC130U

AC130W

C130E

C130H

C130H 73-74

C130H 78-82

C130H 83+

C130H 83-99

EC130H

HC130(H)N 88-93

HC130N

HC130N/P 64-69

HC130P

LC130H

MC130E

MC130H

MC130P

WC130H

1.3.2.5 - GH - Defective or inadequate Parts/Specification Notification IAW TO 00-35D-54.

AC130H

AC130J

AC130U

AC130W

C130E

C130H

C130H 73-74

C130H 78-82

C130H 83+

C130H 83-99

EC130H

HC130(H)N 88-93

HC130N

HC130N/P 64-69

HC130P

LC130H

MC130E

MC130H

MC130P

WC130H

Assigned MDS(s)

1.3.2.6 - (Changed) - GI/GJ - ICARR Reporting - Comply with the Inspection, Crack/Corrosion And Repair

Reporting (ICARR-3D) requirements IAW 1C-130A-6, 1C-130A-36.

Page 18 of 379June 27, 2019

AC130U

AC130W

C130E

C130H

C130H 73-74

C130H 78-82

C130H 83+

C130H 83-99

EC130H

HC130(H)N 88-93

HC130N

HC130N/P 64-69

HC130P

LC130H

MC130E

MC130H

MC130P

WC130H

1.3.2.8 - GH - For each aircraft send one copy of completed AFTO Form 95 to C-130 ASIP Manager, AFLCMC/WLNEB, 235 Byron St Suite 19A, Robins AFB GA, 31098-1647. (N/A to ACI and CIE aircraft)

AC130H

AC130J

AC130U

AC130W

C130E

C130H

C130H 73-74

C130H 78-82

C130H 83+

C130H 83-99

EC130H

HC130(H)N 88-93

HC130N

HC130N/P 64-69

HC130P

LC130H

MC130E

MC130H

MC130P

WC130H

Assigned MDS(s)

1.3.2.9 - GH - The depot facility shall enter TCTO status (start date, completion date, and man-hours used) into the WR-ALC Program Management Support System (PMSS).

Page 19 of 379June 27, 2019

AC130U

AC130W

C130E

C130H

C130H 73-74

C130H 78-82

C130H 83+

C130H 83-99

EC130H

HC130(H)N 88-93

HC130N

HC130N/P 64-69

HC130P

LC130H

MC130E

MC130H

MC130P

WC130H

1.3.3 - (Changed) Technical Data

AC130U

AC130W

C130H 73-74

C130H 78-82

C130H 83+

HC130(H)N 88-93

HC130N/P 64-69

LC130H

MC130H

MC130P

WC130H

Assigned MDS(s)

1.3.3.1 - (Changed) The removal, disassembly, inspection, repair, adjustment, modification, test, assembly, and re-installation of components and equipment shall conform to the basic maintenance instruction manuals and other applicable TOs listed in Section 5 of this Work Specification.

AC130U

AC130W

C130H 73-74

C130H 78-82

C130H 83+

HC130(H)N 88-93

HC130N/P 64-69

LC130H

MC130H

MC130P

WC130H

Assigned MDS(s)

1.3.3.1.1 - (Changed) Structural repairs installed while accomplishing the requirements of this Work Specification shall conform to TO 1C-130A-3, 1C-130A-23, and AFLCMC/WLN instructions as directed by PAO/ACO.

Page 20 of 379June 27, 2019

C130H 73-74

C130H 78-82

C130H 83+

HC130(H)N 88-93

HC130N/P 64-69

LC130H

MC130H

MC130P

WC130H

Assigned MDS(s)

1.3.3.2 - (Changed) Replacement parts and materials used in the repair of the aircraft or any other equipment shall be those authorized in USAF approved publications.

AC130U

AC130W

C130H 73-74

C130H 78-82

C130H 83+

HC130(H)N 88-93

HC130N/P 64-69

LC130H

MC130H

MC130P

WC130H

Assigned MDS(s)

1.3.3.3 - (Changed) Obtain and use approved torque values and safety methods from publications listed below.

AC130U

AC130W

C130H 73-74

C130H 78-82

C130H 83+

HC130(H)N 88-93

HC130N/P 64-69

LC130H

MC130H

MC130P

WC130H

Assigned MDS(s)

1.3.3.3.1 - (Changed) OMMS manuals and TO 1C-130A-3 structural repair manual.

Page 21 of 379June 27, 2019

C130H 73-74

C130H 78-82

C130H 83+

HC130(H)N 88-93

HC130N/P 64-69

LC130H

MC130H

MC130P

WC130H

1.3.3.3.2 - (Changed) If not listed in OMMS or TO 1C-130-3 manuals, refer to accessory maintenance manuals.

AC130U

AC130W

C130H 73-74

C130H 78-82

C130H 83+

HC130(H)N 88-93

HC130N/P 64-69

LC130H

MC130H

MC130P

WC130H

Assigned MDS(s)

1.3.3.3.3 - (Changed) If not listed in 1.3.3.3.1 or 1.3.3.3.2 above see TO 1-1A-1, and 1-1A-8.

AC130U

AC130W

C130H 73-74

C130H 78-82

C130H 83+

HC130(H)N 88-93

HC130N/P 64-69

LC130H

MC130H

MC130P

WC130H

Assigned MDS(s)

1.3.3.4 - (Changed) Identification, installation, and replacement of flexible hose and fittings shall conform to

TOs 1-1A-1, 1-1A-8, 42E1-1-1 and 44H3-1-3. Low pressure hose having radial cracks on the end, minor cracks or lack of manufacturer's date shall not be rejected unless found unserviceable.

Page 22 of 379June 27, 2019

C130H 73-74

C130H 78-82

C130H 83+

HC130(H)N 88-93

HC130N/P 64-69

LC130H

MC130H

MC130P

WC130H

1.3.3.5 - (Changed) Inspection and replacement of vibration isolators (other than engine mounts) shall be

IAW TO 1-1-19.

AC130U

AC130W

C130H 73-74

C130H 78-82

C130H 83+

HC130(H)N 88-93

HC130N/P 64-69

LC130H

MC130H

MC130P

WC130H

Assigned MDS(s)

1.3.3.6 - (Changed) Color coding of new tubing shall be IAW the basic maintenance handbook for applicable aircraft and TO 1-1-8.

AC130U

AC130W

C130H 73-74

C130H 78-82

C130H 83+

HC130(H)N 88-93

HC130N/P 64-69

LC130H

MC130H

MC130P

WC130H

Assigned MDS(s)

1.3.3.7 - (Changed) All fluids, fuel, oils, grease, and compounds used in servicing the aircraft shall be specified in the individual work book for each C-130 aircraft.

Page 23 of 379June 27, 2019

C130H 73-74

C130H 78-82

C130H 83+

HC130(H)N 88-93

HC130N/P 64-69

LC130H

MC130H

MC130P

WC130H

1.3.3.8 - (Changed) Use of replacement synthetic rubber parts or assemblies containing synthetic rubber parts are subject to the restrictions IAW Department Of Defense (DOD) 4140.27-M.

AC130U

AC130W

C130H 73-74

C130H 78-82

C130H 83+

HC130(H)N 88-93

HC130N/P 64-69

LC130H

MC130H

MC130P

WC130H

Assigned MDS(s)

1.3.3.9 - (Changed) Non-Destructive Inspections

AC130U

AC130W

C130H 73-74

C130H 78-82

C130H 83+

HC130(H)N 88-93

HC130N/P 64-69

LC130H

MC130H

MC130P

WC130H

Assigned MDS(s)

1.3.3.9.1 - (Changed) Requirements for NDI shall be obtained from TO 1C-130A-36.

AC130U

AC130W

C130H 73-74

C130H 78-82

C130H 83+

HC130(H)N 88-93

HC130N/P 64-69

LC130H

MC130H

MC130P

WC130H

Page 24 of 379June 27, 2019

1.3.3.9.2 - (Changed) Nondestructive Inspection (NDI) methods, TOs 33B-1-2 and 1C-130A-36 shall be utilized when:

A. Directed by TOs or this Work Specification

B. Questionable indications of defects are noted

C. Parts that require rework in any way that could adversely affect the quality such as milling , welding, machining, plating, grinding, and heat treating

AC130U

AC130W

C130H 73-74

C130H 78-82

C130H 83+

HC130(H)N 88-93

HC130N/P 64-69

LC130H

MC130H

MC130P

WC130H

Assigned MDS(s)

1.3.3.9.3 - (Changed) Magnetic particle inspection shall be accomplished as directed by TO 33B-1-2, ASTM-E1444 and TO 1C-130A-36. Procedures specified in the General TO and specification shall not supersede those of the overhaul handbook unless so stipulated .

AC130U

AC130W

C130H 73-74

C130H 78-82

C130H 83+

HC130(H)N 88-93

HC130N/P 64-69

LC130H

MC130H

MC130P

WC130H

Assigned MDS(s)

1.3.3.9.4 - (Changed) When the condition of metal parts and material indicates unserviceability, such parts and material shall be inspected using methods and equipment prescribed in MIL-HDBK-6870A.

AC130U

AC130W

C130H 73-74

C130H 78-82

C130H 83+

HC130(H)N 88-93

HC130N/P 64-69

LC130H

MC130H

MC130P

WC130H

Assigned MDS(s)

1.3.3.9.5 - (Changed) Fluorescent penetrant inspection shall be accomplished IAW TOs 1C-130A-36, 33B-1-2, and ASTM-E1417-95A.

Page 25 of 379June 27, 2019

C130H 73-74

C130H 78-82

C130H 83+

HC130(H)N 88-93

HC130N/P 64-69

LC130H

MC130H

MC130P

WC130H

1.3.3.9.6 - (Changed) Radiographic inspection shall be accomplished IAW TOs 33B-1-1, 1C-130A-36 and MIL-STD-453 or equivalent standard.

Procedures specified in the general TO and specification shall not supersede those of the overhaul handbooks unless so stipulated .

AC130U

AC130W

C130H 73-74

C130H 78-82

C130H 83+

HC130(H)N 88-93

HC130N/P 64-69

LC130H

MC130H

MC130P

WC130H

Assigned MDS(s)

1.3.3.9.7 - (Changed) When inspection techniques not listed in TO 1C-130A-36 are used, they shall be reported using AFTO Form 242 IAW TO 33B-1-2.

The information reported shall be sufficient to enable maintenance personnel with training in the use of NDI to accomplish the reported inspection.

AC130U

AC130W

C130H 73-74

C130H 78-82

C130H 83+

HC130(H)N 88-93

HC130N/P 64-69

LC130H

MC130H

MC130P

WC130H

Assigned MDS(s)

1.3.3.10 - (Changed) Shot and Rotary peening shall be accomplished IAW T.O. 1-1-691 and T.O.

1C-130A-23.

Page 26 of 379June 27, 2019

C130H 73-74

C130H 78-82

C130H 83+

HC130(H)N 88-93

HC130N/P 64-69

LC130H

MC130H

MC130P

WC130H

1.3.3.11 - (Changed) Cadmium plating, anodizing, and ion vapor deposition shall be accomplished IAW TO

1C-130A-23 and specification listed there in.

AC130U

AC130W

C130H 73-74

C130H 78-82

C130H 83+

HC130(H)N 88-93

HC130N/P 64-69

LC130H

MC130H

MC130P

WC130H

Assigned MDS(s)

1.3.3.12 - (Changed) Abrasive blasting shall be accomplished IAW MIL-STD-1504 or equivalent standard.

AC130U

AC130W

C130H 73-74

C130H 78-82

C130H 83+

HC130(H)N 88-93

HC130N/P 64-69

LC130H

MC130H

MC130P

WC130H

Assigned MDS(s)

1.3.3.13 - (Changed) Heat treat of steel alloys shall be accomplished IAW SAE-AMS-H-6875 or equivalent specification. Heat treat of aluminum alloys shall be accomplished IAW SAE-AMS-H-6088 or equivalent specification.

Page 27 of 379June 27, 2019

C130H 73-74

C130H 78-82

C130H 83+

HC130(H)N 88-93

HC130N/P 64-69

LC130H

MC130H

MC130P

WC130H

1.3.3.14 - (Changed) All deviations from technical and engineering data must be approved by certified onsite engineering.

AC130U

AC130W

C130H 73-74

C130H 78-82

C130H 83+

HC130(H)N 88-93

HC130N/P 64-69

LC130H

MC130H

MC130P

WC130H

Assigned MDS(s)

1.4 - (Changed) Security

1.5 - (Changed) Quality Control Requirements

1.5.1 - (Changed) The Depot Facility inspection system requirements shall be IAW TO 33B-1-1 and TO

33B-1-2. (Paragraphs 3.1 and 3.2 N/A to North American Depot Facilities)

AC130U

AC130W

C130H 73-74

C130H 78-82

C130H 83+

HC130(H)N 88-93

HC130N/P 64-69

LC130H

MC130H

MC130P

WC130H

Assigned MDS(s)

1.5.2 - (Changed) Non-Destructive Inspection Requirements

Page 28 of 379June 27, 2019

C130H 73-74

C130H 78-82

C130H 83+

HC130(H)N 88-93

HC130N/P 64-69

LC130H

MC130H

MC130P

WC130H

1.5.2.1 - (Changed) Personnel performing the nondestructive inspections required by this Work

Specification must have had formal training in the usage of the inspection equipment and shall possess certification of such training. NDI inspectors shall meet the training standards and/or qualifications per NAS

410 Level II.

AC130U

AC130W

C130H 73-74

C130H 78-82

C130H 83+

HC130(H)N 88-93

HC130N/P 64-69

LC130H

MC130H

MC130P

WC130H

Assigned MDS(s)

1.5.2.2 - (Changed) NDI inspections shall be performed utilizing NDI equipment authorized for use IAW TO

1C-130A-36.

AC130U

AC130W

C130H 73-74

C130H 78-82

C130H 83+

HC130(H)N 88-93

HC130N/P 64-69

LC130H

MC130H

MC130P

WC130H

Assigned MDS(s)

1.5.2.3 - (Changed) It shall be certified that the NDI techniques performed on each structural item have been performed successfully under the conditions and circumstances specified in TO 1C-130A-36.

Page 29 of 379June 27, 2019

C130H 73-74

C130H 78-82

C130H 83+

HC130(H)N 88-93

HC130N/P 64-69

LC130H

MC130H

MC130P

WC130H

1.6 - (Changed) Condemnation & Repair

1.6.1 - (Changed) The depot shall not repair items where the cost of parts and labor exceeds 75% of the acquisition cost of the item unless authorized by the PAO and with the concurrence of the item manager .

Repairs and/or overhauls are limited to base level repair restrictions as determined by appropriate item manager, Source, Maintainability, Recoverability (SMR) code, and/or Expendability, Recoverability, Reparability, Capability (ERRC) code.

AC130U

AC130W

C130H 73-74

C130H 78-82

C130H 83+

HC130(H)N 88-93

HC130N/P 64-69

LC130H

MC130H

MC130P

WC130H

Assigned MDS(s)

1.6.2 - (Changed) No item is to be repaired as job routed if serviceable assets are available.

AC130U

AC130W

C130H 73-74

C130H 78-82

C130H 83+

HC130(H)N 88-93

HC130N/P 64-69

LC130H

MC130H

MC130P

WC130H

Assigned MDS(s)

1.6.3 - (Changed) Except for access doors and plates, ensure all repairs and removed structural members of skin are installed, replaced, or reinstalled with all fasteners wet with sealant and faying surface sealed IAW

1C-130A-3. For wet installation of fasteners, the sealant may be applied either to the hole or to the fastener.

When applying sealant to the hole, wet the entire surface.

Page 30 of 379June 27, 2019

C130H 73-74

C130H 78-82

C130H 83+

HC130(H)N 88-93

HC130N/P 64-69

LC130H

MC130H

MC130P

WC130H

1.7 - (Changed) Accessory and Component Reuse, Repair and Replacement

1.7.1 - (Changed) When determined from inspection, operational test, or bench check that overhaul is required to insure serviceability, items shall be replaced with serviceable accessories or components. In the event serviceable accessories or components cannot be provided by the item manager in sufficient time to avoid work stoppages, the depot facility may repair or overhaul reparable accessories or components only to the extent required to preclude work stoppages, and as approved by the PAO/ACO. PAO/ACO shall coordinate with AFLCMC/WLNA for repair and overhaul instructions.

AC130U

AC130W

C130H 73-74

C130H 78-82

C130H 83+

HC130(H)N 88-93

HC130N/P 64-69

LC130H

MC130H

MC130P

WC130H

Assigned MDS(s)

1.7.2 - (Changed) Cannibalization of parts, components, and accessories required to prevent schedule slippage is authorized, as approved by the PAO/ACO.

AC130U

AC130W

C130H 73-74

C130H 78-82

C130H 83+

HC130(H)N 88-93

HC130N/P 64-69

LC130H

MC130H

MC130P

WC130H

Assigned MDS(s)

1.7.3 - (Changed) No item is to be repaired as job routed if serviceable assets are available, and/or if estimated delivery date does not affect production critical path .

Page 31 of 379June 27, 2019

C130H 73-74

C130H 78-82

C130H 83+

HC130(H)N 88-93

HC130N/P 64-69

LC130H

MC130H

MC130P

WC130H

1.8 - (Changed) Fuel Tank Storage/Preservation

1.8.1 - (Changed) Internal preservation of tanks and systems is not required except when the aircraft is being prepared for extended storage IAW TO 1C-130A-17. Bladder cells shall be treated with a light coat of oil IAW

TO 1-1-3 or approved purging fluid

AC130H

AC130J

AC130U

AC130W

C130E

C130H

C130H 73-74

C130H 78-82

C130H 83+

C130H 83-99

EC130H

HC130(H)N 88-93

HC130N

HC130N/P 64-69

HC130P

LC130H

MC130E

MC130H

MC130P

WC130H

Assigned MDS(s)

1.9 - (Changed) Other

1.9.1 - (Changed) POLLUTION PREVENTION PROGRAM: The depot facility shall implement a Hazardous

Material Management and Pollution Prevention Programs, IAW National Aerospace Standard (NAS) 411 or local government rules and regulations if those rules and regulations are more restrictive than NAS 411 requirements, that integrates all pollution prevention efforts. The depot facility shall document their approach for managing hazardous materials, pollutants and potential pollutants associated with activities specified in this Work Specification. All of this information shall be provided in a Hazardous Material Management Plan

(HMMP).

Page 32 of 379June 27, 2019

C130H 73-74

C130H 78-82

C130H 83+

HC130(H)N 88-93

HC130N/P 64-69

LC130H

MC130H

MC130P

WC130H

2.0 - (Changed) Receipt of Aircraft at Facility

2.1 - (Changed) Handling and Safety

2.1.1 - AA - Upon receipt of aircraft at maintenance facility, accomplish a receiving inspection to identify

Foreign Object Damage (FOD) on all jet engines as follows: Visually inspect air inlet guide vanes and first stage compression rotor blades for damage. Results of this inspection shall be referred to the PAO/ACO for certification and disposition.

AC130U

AC130W

C130H 73-74

C130H 78-82

C130H 83+

HC130(H)N 88-93

HC130N/P 64-69

LC130H

MC130H

MC130P

WC130H

Assigned MDS(s)

1A1A - Incoming FOD Inspection, Engines Assigned Tasks

2.1.2 - AD - Perform incoming operational test of pitot static system IAW TO 1C-130H-2-34JG-10-1, 34-11-01, 34-11-02, 34-11-03, 11-24-06 or 1C-130H-2-34JG-10-2, 34-12-03, as applicable.

AC130U

AC130W

C130H 73-74

C130H 78-82

C130H 83+

HC130(H)N 88-93

HC130N/P 64-69

LC130H

MC130H

MC130P

WC130H

Assigned MDS(s)

1A1D - Fuselage Pressurization/Decay Test/Pitot Static Leak Check (Incoming) Assigned Tasks

2.1.3 - AD - Perform incoming ground pressurization decay tests IAW TO 1C-130H-2-21JG-30-1. If airframe and seals are leaking write up areas to receive special attention when the aircraft goes into dock work.

Page 33 of 379June 27, 2019

C130H 73-74

C130H 78-82

C130H 83+

HC130(H)N 88-93

HC130N/P 64-69

LC130H

MC130H

MC130P

WC130H

Assigned MDS(s)

1A1D - Fuselage Pressurization/Decay Test/Pitot Static Leak Check (Incoming) Assigned Tasks

2.1.4 - AF - Defuel aircraft on arrival. Handle and store fuel according to TOs 00-25-172, 42B-1-1, 42B1-1-14, and MIL-STD-1518. All drained fuel shall be credited to the procuring activity. (If aircraft forms are removed before defueling, assure that the fuel to be removed is recorded and usable fuel is placed in proper storage).

AC130U

AC130W

C130H 73-74

C130H 78-82

C130H 83+

HC130(H)N 88-93

HC130N/P 64-69

LC130H

MC130H

MC130P

WC130H

Assigned MDS(s)

1A1F - Incoming Defuel Assigned Tasks

2.1.4.1 - AG - All aircraft fuel tanks, fuel bladder cells, and plumbing shall be drained and purged IAW TO

1C-130A-17 and TO 1-1-3.

AC130U

AC130W

C130H 73-74

C130H 78-82

C130H 83+

HC130(H)N 88-93

HC130N/P 64-69

LC130H

MC130H

MC130P

WC130H

Assigned MDS(s)

1A1G - Purge and Perform Explosive Meter Check Assigned Tasks

2.1.5 - AE - Liquid and gaseous oxygen used for aviator`s breathing purposes shall be drained and handled

IAW T.O. 42B6-1-1 and T.O. 1C-130H-2-35JG-00-1.

Page 34 of 379June 27, 2019

C130H 73-74

C130H 78-82

C130H 83+

HC130(H)N 88-93

HC130N/P 64-69

LC130H

MC130H

MC130P

WC130H

1A1E - Drain Oxygen Assigned Tasks

2.1.6 - AB - De-Arm and remove the engine fire extinguisher squibs IAW TO 1C-130H-2-26JG-20-1. De-arm and remove in-flight refueling guillotine squibs (HC-130H/P/N and MC-130P aircraft only) IAW T.O.

1C-130H-2-28JG-20-2 28-26-11.

AC130U

AC130W

C130H 73-74

C130H 78-82

C130H 83+

HC130(H)N 88-93

HC130N/P 64-69

LC130H

MC130H

MC130P

WC130H

Assigned MDS(s)

1A1B - De-arm Aircraft, IFR Guillotine, Emergency Egress System /Battery removal and storage Assigned Tasks

2.1.6.1 - QP - Remove fire extinguisher bottles for time change.

AC130U

AC130W

C130H 73-74

C130H 78-82

C130H 83+

HC130(H)N 88-93

HC130N/P 64-69

LC130H

MC130H

MC130P

WC130H

Assigned MDS(s)

1D1A - Time Change/Calendar Inspections Only (Fire extinguisher / In-Flight refueling guillontine squibs) Assigned Tasks

2.1.7 - AI - Tow aircraft as required to complete PDM process.

Page 35 of 379June 27, 2019

C130H 73-74

C130H 78-82

C130H 83+

HC130(H)N 88-93

HC130N/P 64-69

LC130H

MC130H

MC130P

WC130H

1A1I - Towing through PDM process Assigned Tasks

2.2 - (Changed) Inventory

2.2.1 - AC - Inventory jointly with the aircraft commander or his designated representative each aircraft against property listed in aircraft property records AF 2692. Inventory should be accomplished upon receipt of aircraft at maintenance facility. Record and process inventory in accordance with AFI 21-103. The same AF 2692 equipment removed from an aircraft shall be reinstalled prior to departure.

NOTE: Annotate missing insulation in aircraft records. Depot facilities are not required to replace missing insulation.

AC130U

AC130W

C130H 73-74

C130H 78-82

C130H 83+

HC130(H)N 88-93

HC130N/P 64-69

LC130H

MC130H

MC130P

WC130H

Assigned MDS(s)

1A1C - Incoming AF Form 2692 Inventory and Storage Assigned Tasks

2.2.2 - AC - Aircraft received from overseas/offshore bases and that are scheduled to return overwater shall have survival equipment, life rafts, pyrotechnics pistols, and life vests inventoried.

AC130U

AC130W

C130H 73-74

C130H 78-82

C130H 83+

HC130(H)N 88-93

HC130N/P 64-69

LC130H

MC130H

MC130P

WC130H

Assigned MDS(s)

1A1C - Incoming AF Form 2692 Inventory and Storage Assigned Tasks

Page 36 of 379June 27, 2019

2.3 - (Changed) Preservation

2.3.1 - AH - Accomplish engine preservation IAW TO 1C-130H-2-00GE-00-1.

AC130U

AC130W

C130H 73-74

C130H 78-82

C130H 83+

HC130(H)N 88-93

HC130N/P 64-69

LC130H

MC130H

MC130P

WC130H

Assigned MDS(s)

1A1H - Preservation 4 ea Engines and APU/GTC Assigned Tasks

2.3.2 - AB - Remove aircraft storage battery, impact light batteries and INS/SCNS battery if installed, store, and maintain as directed in TO 8D2-1-31 or TO 8D2-3-1.

AC130U

AC130W

C130H 73-74

C130H 78-82

C130H 83+

HC130(H)N 88-93

HC130N/P 64-69

LC130H

MC130H

MC130P

WC130H

Assigned MDS(s)

1A1B - De-arm Aircraft, IFR Guillotine, Emergency Egress System /Battery removal and storage Assigned Tasks

2.3.3 - GM- Treat the aircraft as directed in TOs 1-1-17 and 1C-130A-17 when storage is anticipated. Drained fluids shall be disposed of or reused as follows:

AC130U

AC130W

C130H 73-74

C130H 78-82

C130H 83+

HC130(H)N 88-93

HC130N/P 64-69

LC130H

MC130H

MC130P

WC130H

Assigned MDS(s)

1B20N2A - Hazardous Material and Handling: WR-ALC 1B20N2B - Hazardous Material and Handling: OO-ALC

Page 37 of 379June 27, 2019

2.3.3.1 - AF - Serviceable fuel shall be recorded on AFTO Form 781H and credited to the aircraft when reservicing.

AC130U

AC130W

C130H 73-74

C130H 78-82

C130H 83+

HC130(H)N 88-93

HC130N/P 64-69

LC130H

MC130H

MC130P

WC130H

Assigned MDS(s)

1A1F - Incoming Defuel Assigned Tasks

2.3.3.2 - GM - Hydraulic fluid drained for any reason shall be disposed of as condemned property and need not be accounted for.

AC130U

AC130W

C130H 73-74

C130H 78-82

C130H 83+

HC130(H)N 88-93

HC130N/P 64-69

LC130H

MC130H

MC130P

WC130H

Assigned MDS(s)

1B20N2A - Hazardous Material and Handling: WR-ALC 1B20N2B - Hazardous Material and Handling: OO-ALC

Assigned Tasks

2.3.3.3 - AH - Drained engine oil shall be disposed of as condemned property and need not be accounted for.

AC130U

AC130W

C130H 73-74

C130H 78-82

C130H 83+

HC130(H)N 88-93

HC130N/P 64-69

LC130H

MC130H

MC130P

WC130H

Assigned MDS(s)

1A1H - Preservation 4 ea Engines and APU/GTC Assigned Tasks

2.3.3.4 - GM - Fuel used for flushing the fuel system, detection of fuel leaks, or that may be contaminated from other sources shall be checked IAW TOs 42B-1-1 and 42B1-1-1.

Page 38 of 379June 27, 2019

C130H 73-74

C130H 78-82

C130H 83+

HC130(H)N 88-93

HC130N/P 64-69

LC130H

MC130H

MC130P

WC130H

1B20N2A - Hazardous Material and Handling: WR-ALC 1B20N2B - Hazardous Material and Handling: OO-ALC

Assigned Tasks

2.3.4 - AH - Accomplish required internal preservation and cap off open ports IAW TOs 44H3-1-3 and

1C-130A-17 when required.

AC130U

AC130W

C130H 73-74

C130H 78-82

C130H 83+

HC130(H)N 88-93

HC130N/P 64-69

LC130H

MC130H

MC130P

WC130H

Assigned MDS(s)

1A1H - Preservation 4 ea Engines and APU/GTC Assigned Tasks

2.3.5 - AJ - Wash aircraft exterior IAW TO 1C-130A-23CL-1. (Complete exterior wash is required on those aircraft known to require complete depaint/paint).

AC130U

AC130W

C130H 73-74

C130H 78-82

C130H 83+

HC130(H)N 88-93

HC130N/P 64-69

LC130H

MC130H

MC130P

WC130H

Assigned MDS(s)

1A1J - Wash Aircraft and Lubricate Assigned Tasks

2.3.5.1 - (Changed) AJ - Clean interior wheel wells, flap wells, and Jet Assisted Take Off (JATO) wells IAW

TO 1-1-691 and 1C-130A-23 prior to accomplishing work requirements in Section III of this Work

Specification.

Page 39 of 379June 27, 2019

C130H 73-74

C130H 78-82

C130H 83+

HC130(H)N 88-93

HC130N/P 64-69

LC130H

MC130H

MC130P

WC130H

1A1J - Wash Aircraft and Lubricate Assigned Tasks

2.3.6 - AG - Internal preservation of tanks and systems is not required except when the aircraft is being prepared for extended storage IAW TO 1C-130A-17. Bladder cells shall be treated with a light coat of oil IAW

TO 1-1-3 or approved purging fluid.

AC130U

AC130W

C130H 73-74

C130H 78-82

C130H 83+

HC130(H)N 88-93

HC130N/P 64-69

LC130H

MC130H

MC130P

WC130H

Assigned MDS(s)

1A1G - Purge and Perform Explosive Meter Check Assigned Tasks

3.0 - (Changed) Work Requirements

3.1 - (Changed) General Aircraft

3.1.1 - (Changed) Items listed below shall be accomplished as directed by the PAO/ACO.

AC130U

AC130W

C130H 73-74

C130H 78-82

C130H 83+

HC130(H)N 88-93

HC130N/P 64-69

LC130H

MC130H

MC130P

WC130H

Assigned MDS(s)

3.1.1.1 - (Changed) Accomplishment of work not specifically directed in this Work Specification.

Page 40 of 379June 27, 2019

C130H 73-74

C130H 78-82

C130H 83+

HC130(H)N 88-93

HC130N/P 64-69

LC130H

MC130H

MC130P

WC130H

3.1.1.2 - QV - Correction of Safety of Flight discrepancies shall be accomplished as approved by

PAO/ACO.

AC130U

AC130W

C130H 73-74

C130H 78-82

C130H 83+

HC130(H)N 88-93

HC130N/P 64-69

LC130H

MC130H

MC130P

WC130H

Assigned MDS(s)

1E1A - Over and Above WSC: QS/QT/QU/QV/NQ/QI Assigned Tasks

3.1.1.3 - QU - Items listed on the AFTO Form 103 as approved by AFLCMC/WLNA and directed by

PAO/ACO.

AC130U

AC130W

C130H 73-74

C130H 78-82

C130H 83+

HC130(H)N 88-93

HC130N/P 64-69

LC130H

MC130H

MC130P

WC130H

Assigned MDS(s)

1E1A - Over and Above WSC: QS/QT/QU/QV/NQ/QI Assigned Tasks

3.1.1.4 - (Changed) The depot facility shall accomplish depot level TCTOs when approved by

AFLCMC/WLNA and directed by PAO/ACO through the AFTO Form 103.

Page 41 of 379June 27, 2019

C130H 73-74

C130H 78-82

C130H 83+

HC130(H)N 88-93

HC130N/P 64-69

LC130H

MC130H

MC130P

WC130H

3.1.1.4.1 - (Changed) QU - Remove and replace NLG Drag Brace IAW TO 1C-130-2150 if not PCW , AFTO 103 not required.

AC130U

AC130W

C130H 73-74

C130H 78-82

C130H 83+

HC130(H)N 88-93

HC130N/P 64-69

LC130H

MC130H

MC130P

WC130H

Assigned MDS(s)

1E1A - Over and Above WSC: QS/QT/QU/QV/NQ/QI

2G - REMOVE AND REPLACE NLG DRAG BRACE (TCTO2150)

Assigned Tasks

3.1.1.5 - QR - Accomplish Safety TCTOs requiring completion prior to PDM output.

AC130U

AC130W

C130H 73-74

C130H 78-82

C130H 83+

HC130(H)N 88-93

HC130N/P 64-69

LC130H

MC130H

MC130P

WC130H

Assigned MDS(s)

1D1B - Safety TCTOs Assigned Tasks

3.1.1.6 - QU - Correct other discrepancies that, because of unique access due to PDM activity or the unique availability of tools or spare parts, are more economical to accomplish during that PDM activity as approved by the PAO/ACO. All other discrepancies found during inspection shall be corrected as approved by the

PAO/ACO unless otherwise directed by this Work Specification.

Page 42 of 379June 27, 2019

C130H 73-74

C130H 78-82

C130H 83+

HC130(H)N 88-93

HC130N/P 64-69

LC130H

MC130H

MC130P

WC130H

1E1A - Over and Above WSC:…