Attch_2_-_PWS_Appendix_A_Work_Specification_F-15C_-_FA8505-17-R-0004.pdf

DEPARTMENT OF THE AIR FORCE

Work Spec: FY18 Final

MDS: F015C

8/16/2016

Work Spec: FY18 Final

MDS: F015C

DEPARTMENT OF THE AIR FORCE

1.0 - General

1.1 - Information

1.1.1 - This Work Specification (WS) (Appendix A) establishes the requirements for receipt, inspection, maintenance, modification, functional testing and delivery of F-15C/D/E aircraft input for Programmed Depot

Maintenance (PDM) at Source of Repair (SOR). The aircraft shall be received and reassigned to Air Force

Material Command (AFMC) in accordance with (IAW) AFI 21-103. The aircraft shall be returned to the assigned organization in the same configuration as received. The aircraft shall contain the same type components, accessories, and special equipment installed except as modified, removed, or added by requirements of this WS. No attempt shall be made to standardize aircraft on which previous non-standard system or structure installations have been made. Class II modifications (orange wire/orange structure) shall not be disturbed during maintenance. If Class II modifications must be disturbed, contact F-15 Engineering for disposition.

1.1.2 - New work requirements, deletion of work requirements or a scope change to requirements of this WS will not be put into effect without prior approval of the System Program Office (SPO). All amendments previously stated will be managed through the Engineering Requirement Review Process (ERRP) IAW

AFMAN 63-143. Prior to non-performance of a WS requirement the SOR shall notify F-15 Engineering.

1.1.3 - Disassembly of aircraft shall be limited to the extent necessary to accomplish the inspection and work required by this specification.

1.1.4 - Maintenance outside of the WS may be accomplished by the SOR but only with approval from the

PAO/ACO.

1.1.5 - During closing inspection, inspect the entire aircraft/systems after all maintenance has been completed to be sure all tools/foreign objects have been removed and there are no loose parts.

1.1.6 - A sign-off sheet and/or an in process inspection sheet shall be maintained for closeout inspections by access panels or areas where there is, at present, no requirement for quality control listed in technical manuals.

1.1.7 - Any maintenance generated defects, (Example: Dents caused by work stands, misdrilling of sheet metal, etc.) shall be corrected by the SOR without cost to the project.

1.1.8 - All applicable work outlined in this WS, including all TABs, must be completed for a PDM aircraft to be considered ‘sold’. THIS INCLUDES PROPER DOCUMENTATION OF ALL PDM TASKS (REMOVAL, INSPECTION, REPAIR, INSTALL, OPS CHECKOUT, SERVICING, ETC.) IAW TO 00-20-2.

1.1.9 - System checkout because of removal and reinstallation of a Line Replaceable Unit (LRU) or panel to gain access for other work shall require checkout IAW applicable Technical Order (TO).

CAUTION

Extreme caution must be taken in reinstallation of connections and cannon plugs to ensure that the connections are not damaged.

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1.1.10 - Complete an Air Force Technical Order (AFTO) Form 238 for all wing, horizontal stabilator, or landing gear removal and installations. Include the component serial number, aircraft serial number and date of removal and/or installation. Use TO 1F-15-101 for instructions on how to complete the AFTO Form 238. A copy of the AFTO Form 238 shall be furnished to F-15 Engineering immediately.

1.1.11 - Electrical wiring found to be misrouted will be brought to the attention of applicable SPO engineer and

PAO/ACO for disposition and permission to repair or leave in current configuration. Misrouted electrical wiring that presents a SOF/unsafe condition shall be corrected. Wiring not corrected shall be returned to the user in the condition received and documented on AFTO Form 781A as such.

1.1.12 - Engines on PDM aircraft shall have only those Safety of Flight (SOF) conditions corrected which are within the capabilities of the SOR. SOF conditions which cannot be corrected shall be cause to return the engine to using command for replacement. Engines with Non-SOF items shall be returned to the user in the condition received under the appropriate red diagonal/red dash condition symbol.

NOTE

Engines damaged as a result of Foreign Object Damage (FOD) and/or negligence while in possession of AFMC at the SOR shall be replaced by AFMC without impact upon the using command.

Engines requiring return to overhaul for any reason other than stated above shall have a replacement engine furnished by the using command.

1.1.13 - All flight checks shall be accomplished by qualified United States Air Force (USAF) pilots.

1.1.14 - All SOF systems required for functional check flight (FCF) or ferry mission must be airworthy. Other systems disturbed for repair, adjustment or alteration shall be checked in sufficient depth to insure operational reliability IAW basic TO. Modified components shall be operationally checked in accordance with applicable

Time Compliance Technical Order (TCTO) instructions. Systems not disturbed or not required for FCF and ferry mission may be returned to the using activity in the same condition as received, unless otherwise directed in this specification or by separate negotiation.

1.1.15 - All 103 delayed discrepancies shall be reviewed and considered by the Maintenance Review

Team/Project Administrative Office/Administrative Contracting Officer (MRT/PAO/ACO) and only corrected if approved. Discrepancies not approved for work shall be entered on AFTO Form 781K and returned to the using activity for corrective action.

1.1.16 - Incoming AFTO Form 781 write-ups shall be approved/disapproved for work during predock conference. Correct all approved write-ups.

1.1.17 - A TCTO implementation shall be accomplished within thirty days after receipt of formal publications, and supportability for negotiated workload is available at the maintenance facility. Incorporation shall be as negotiated.

1.1.18 - Organization and Intermediate Maintenance (O&I) level TCTOs that have less than 60 days to rescission date shall be accomplished after approval of the PAO/ACO, provided parts and kits are available.

1.1.19 - AFTO Form 103 requests for work shall be IAW TO 00-25-4.

1.1.20 - Furnish F-15 Engineering a copy of Predock minutes.

1.1.21 - Accomplish maintenance compression requirements when directed by the SPO IAW AFI 21-102 and

AFMCI 21-118 as defined in TAB B of this WS.

1.2 - Terms Explained

1.2.1 - See Attachment 1.

Attachment 1.pdf

Attachments

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1.3 - Data

1.3.1 - Maintenance Records, Forms and Publications

1.3.1.1 - The applicable forms and records listed in Table 1 shall be maintained IAW the listed directives listed during the time the aircraft is at the facility. Publications delivered with the aircraft shall be maintained

IAW TO 00-5-1.

Table 1

1.3.1.2 - Deficiency Reports (DRs) shall be submitted as necessary IAW TO 00-35D-54.

1.3.1.3 - All maintenance actions shall be documented IAW AFI 21-101, TO 00-20-2 and applicable -06 code manuals. Locally devised processing of forms and workbooks may be used in lieu of AFTO Form 349. Key punch cards for AFTO Forms will be processed IAW AFI 21-101.

1.3.1.4 - The aircraft records are to be maintained as described in the WS. This includes maintaining the weight and balance record on the aircraft. The table of maintenance records includes TOs 1-1B-40, 1-1B-50 and 1F-15C/E-5.

1.3.2 - Reporting Requirements

1.3.2.1 - The SOR shall prepare the following reports as applicable.

1.3.2.1.1 - Special Delinquent Progress Report, 6-LOG-K7, IAW AFMCR 65-46.

1.3.2.1.2 - Aircraft Transfer IAW AFI 21-103.

1.3.2.1.3 - Aircraft Delivery IAW AFI 21-103.

1.3.2.1.4 - RCS 8, HAF-V39 AMREP IAW AFMCI 21-118 - DI-L-7023D.

1.3.2.1.5 - AFMC Form 200 IAW AFMCI 21-125 (C1).

1.3.2.1.6 - Reporting of F100PW220/229 Comprehensive Engine Management System (CEMS) Data.

1.3.2.1.7 - The applicable forms and records listed in Table 2 shall be used IAW the directives listed during the time the aircraft is at the SOR and just after departure to transmit data requested by this WS and TOs.

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Table 2

1.3.2.1.8 - The applicable forms listed in Table 3 shall be used IAW the directives listed during the time the aircraft is at the SOR to request technical assistance, report technical data problems, and obtain general information to help process parts for delivery and storage.

Table 3

1.3.3 - Technical Data

1.3.3.1 - Specific TOs, publications, and directives are specified in Section 5 of this WS (does not include

TCTOs).

1.3.3.2 - Structural repairs accomplished by the SOR shall conform to TOs 1F-15C/E-3-1, 1F-15C/E-3-2, 1F-15C/E-3-3, 1F-15C/E-3-4, 1F-15C/E-3-5, 1F-15C/E-3-6, 1F-15C/E-3-7, 1F-15C/E-3-8, 1F-15-3, 1-1A-8, 1-1A-1 or other authorized directives as specified by F-15 Engineering.

1.3.3.3 - Replacement parts, materials, equipment and components used in the repair of the aircraft or any component of the aircraft shall be those authorized by the Air Force in approved publications. Any substitution shall be approved by appropriate Prime Air Logistics Complex Engineering.

1.3.3.4 - Engineering and maintenance procedures not covered by specific TOs shall conform to the following general TOs: TO 1-1-3 Preparations, Inspections and Repair of Fuel Cells, TO 1-1-8 Applications of Organic Coatings, Aerospace Equipment, TO 1-1-689 Corrosion Prevention & Control, Comprehensive

Engine Management System (CEMS) Equipment, TO 1-1-691 Aircraft Weapons Systems Cleaning and

Corrosion Control, TO 1-1A-1 General Manual for Structural Repair, TO 1-1A-8 Aircraft Structural Manual, TO 1-1A-9 Aircraft Metals, TO 1-1A-12 Maintenance and Repair of Plastics, TO 1-1A-14 Installation

Practices for Electric and Electronic Wiring, TO 1F-15A-2-00-WD-20-1 General Wiring and Repair

Procedures.

1.3.3.5 - Anti-friction bearings removed for maintenance shall be maintained IAW TOs 44B-1-2, 44B-1-3 and

44B-1-102.

1.3.3.6 - Identification, inspection, installation and replacement of flexible/rigid hose and fittings shall conform to applicable basic TOs or instructions of TOs 1-1A-1, 1-1A-8, 44H3-1-3 and 42E1-1-1.

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1.3.3.7 - Obtain and use approved torque values and safety methods from the applicable JGs, -3 series

TOs or 1-1A-8.

1.3.3.8 - Aircraft weight and balance is specified in TO 1F-15C/E-5. Qualification of weight and balance personnel shall be IAW TO 1-1B-50.

1.3.3.9 - If welding is required, personnel shall be qualified IAW SAE-AMS-1595. Ref AFI 21-105 and TO

00-25-252.

1.3.3.10 - Inspection, test and replacement of vibration isolators (other than engine mounts) shall conform to

TO 1-1-19.

1.3.3.11 - Fluids, fuel, oil, grease and paint compounds used shall conform to specifications in TOs for this aircraft.

1.3.3.12 - Inspection, installation, and repair of electrical wiring, conduits, and connectors not specifically covered in the Basic Maintenance Instruction Manuals shall conform to TO 1-1A-14 and TO 8-1-1.

1.3.3.13 - The issue, storage, acceptance, and installation of synthetic rubber parts and other dated items shall be IAW TO 00-20K-1 and the Stock Number Users Directory (SNUD), as applicable. If time replacement interval conflicts between TO 00-20K-1 and SNUD, SNUD shall take precedence.

1.3.3.14 - The ACES II seat and cartridge/propellant actuated items of the emergency egress system shall be removed/installed by certified egress personnel IAW the basic TO 13A5-56-11 and AFI 21-112.

Explosive components shall be stored IAW TO 11P3-1-7 and AFMAN 91-201.

1.3.3.15 - Maintain landing gear wheel brakes IAW TOs 4B-1-1 and 4B-1-32.

1.3.3.16 - Aircraft wheels shall be maintained IAW the basic TO and TO 4W-1-61.

1.3.3.17 - Servicing, removal, installation and replacement of tires shall be IAW the basic TO and TO

4T-1-3.

1.3.3.18 - Hydraulic fluid used for servicing the aircraft and in-ground/test equipment shall conform to either

MIL-PRF-5606H or MIL-PRF-83282D, as applicable.

1.3.3.19 - Nondestructive Inspection (NDI) methods (TO 33B-1-1 and TO 1F-15A-36) shall be utilized when:

1.3.3.19.1 - Directed by TOs or this WS, where instructions are not stated in TO 1F-15A-36.

1.3.3.19.2 - Questionable visual indications of defects are noted.

1.3.3.19.3 - Parts are reworked in any way that could adversely affect the quality of parts such as routing, welding, machining, plating, grinding, heat treating, etc.

1.3.3.20 - Clean and treat transparent surfaces, canopies and windshield IAW the basic TO and TO

1-1A-12.

1.4 - Security

1.4.1 - The SOR shall comply with the security requirements of AFI 31-101.

1.5 - Quality Control Requirements

1.5.1 - The SOR inspection system shall be IAW AFMCI 21-108.

1.6 - Condemnation & Repair

1.6.1 - The SOR shall not repair items where the cost of parts and labor exceeds 75 percent of the replacement cost of the items IAW TO 00-20-3 unless directed by the PAO/ACO.

1.6.2 - The SOR shall have prior approval of the PAO/ACO before taking condemnation action.

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1.6.3 - All items condemned that contain precious metals/critical alloys and/or all precious metals/critical alloys bearing scrap shall be turned in to the nearest Defense Property Disposal Office in accordance with

DOD 4160.21M, Chapter XVIII unless other specific instructions are furnished by the PAO/ACO. Part numbers of precious metal/critical alloys such as beryllium, cobalt, nickel, titanium and tungsten are identified in TO 00-25-113.

1.6.4 - The SOR shall not inspect, repair or recondition expendable parts if the parts and labor are equal to or exceeds the Defense Logistics Agency (DLA) unit price.

1.6.5 - When a replacement part or authorized substitute is not available for any source, including local manufacture, in a timely manner resulting in aircraft flow slippage, the SOR shall submit an AFTO Form 202 to allow engineering evaluation of alternative parts and/or repair.

1.6.6 - If a replacement part requirement is filled outside the normal supply channel i.e. Form 202, local purchase, local manufacture, etc. the SOR shall submit a DHA and notify the source of supply IAW AFMCI

21-129, AFMCI 21-130 and AFMCI 21-133.

1.7 - Accessory and Component Reuse, Repair and Replacement

1.7.1 - Accessories and components removed solely for work accessibility shall not be replaced or routed for repair but shall be reinstalled on the aircraft.

1.7.2 - All removed parts and components held for reinstallation shall be inventoried, identified (tagged) with the aircraft serial number, protected and properly stored to prevent damage and/or loss.

1.7.3 - When inspection, operational check or bench check reveals that an item is defective and intermediate level maintenance will not correct the defect, accessories and components will be replaced with serviceable items. In the event serviceable accessories or components cannot be provided in sufficient time to avoid work stoppage, the SOR may overhaul repairable accessories or components only to the extent required to prevent work stoppage, providing such overhaul or repair is within the maintenance capability and is approved by the

PAO/ACO.

1.7.4 - Initial local manufacture (LM) items will not be manufactured and cost charged to aircraft without approval of the PAO/ACO. Recurring LM items will be IAW G005M System.

1.7.5 - Extreme caution must be taken in reinstallation of connections and cannon plugs to insure that the connections are not damaged.

1.7.6 - Only "A" conditioned assets will be installed on all aircraft, any deviations will be assessed and require authorization from F-15 Engineering.

1.8 - Fuel Tank Storage/Preservation

1.8.1 - All drained fuel cells and external and internal tanks shall be treated for storage IAW TOs 1-1-3, 1F-15A-17, and the basic TO.

1.8.2 - Temporary outside storage of aircraft and external tanks shall be IAW TOs 1-1-17 and 1F-15A-17.

1.8.3 - Turbo-jet oil and lubricating oil drained for any reason shall not be reused and shall be disposed of as administratively condemned property IAW TO 42B2-1-3. If there is a hydraulic purifier available, purify the hydraulic fluid for reuse. Otherwise, discard IAW TO 42B2-1-3.

1.8.4 - Engines which are to be shipped to another location will be preserved and prepared for shipment IAW

TO 2J-1-18 and TO 1F-15A-17.

1.9 - Other

1.9.2 - Tab B Maintenance Compression Requirements

1.9.2.1 - Scope

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1.9.2.1.1 - This Tab B establishes the maintenance compression requirements for F-15C/D/E aircraft in the event maintenance compression is directed by the System Program Office (SPO) Director. A current detailed plan will be maintained by the SOR. The plan is used to accelerate the shift of work or personnel immediately and shall replace the WS. Plans will be submitted to F-15 Engineering for evaluation.

1.9.2.1.2 - The aircraft shall be prepared for delivery to the owning Command to an operational status according to the requirements outlined herein.

1.9.2.1.3 - The requirements outlined herein shall be complied with for the duration that the maintenance compression is in effect.

1.9.2.1.4 - Replace defective components, unless only minor repair is necessary.

1.9.2.1.5 - Cannibalization will be from aircraft requiring excessive work only.

1.9.2.1.6 - Aircraft shall be processed in one of the following below conditions to permit expedite delivery to the owning Command at the earliest possible date.

1.9.2.1.6.1 - Condition "A": Aircraft in flight test status/outgoing that is painted.

1.9.2.1.6.2 - Condition "B": Aircraft incoming for shop work that are determined (by examination of the aircraft forms) to be in flyable status will be returned to service (turn around) after compliance with the work detailed below for Condition "B" aircraft.

1.9.2.1.6.3 - Condition "C": Aircraft that can be removed and "buttoned up" from initial PDM cells/stations (in work 4 to 6 workdays) with engines installed and basically satisfactory with minor expenditure of manhours.

1.9.2.1.6.4 - Condition "D": Aircraft in final PDM cells/gates/stations (after fuel system check with engines installed).

1.9.2.1.6.5 - Condition "E": Aircraft requiring major modification (including those in PDM flow already undergoing modification and those in permanent storage).

1.9.2.1.8 - Every effort shall be expended to accomplish required work and delivery of the aircraft to the

Government in the order of condition listed above. Aircraft requiring the least amount of work shall be processed first.

1.9.2.1.9 - The AF Forms 2691 and 2692, Air Force Technical Order (AFTO) Form 95 and AFTO Form

781 series for the work accomplished shall be maintained and completed IAW Technical Order (T.O.)

00-20 series. An entry shall be made under remarks on AFTO Form 95 to indicate that the aircraft was processed IAW Maintenance Compression work requirements. All systems that are authorized to be inoperative shall be listed on AFTO Form 781 as inoperative.

1.9.2.1.10 - All other aircraft records, forms and publications shall be brought up to date, unless otherwise directed, and shall be returned with the aircraft. For identity of other forms and applicable directives related thereto refer to WS, Section I, paragraph 1.3.1.

1.9.2.1.11 -

In order to provide a combat ready weapon system, aircraft systems/subsystems must be operational

IAW the requirements of the Minimum Essential Subsystem List (MESL) provided in the appropriate AFI

21-103 supplement addendum.

1.9.2.2 -

Specific Work Requirements

1.9.2.2.1 - Aircraft Condition "A"

1.9.2.2.1.1 - Accomplish preflight and Postflight inspections IAW applicable TOs and correct SOF discrepancies prior to delivery of the aircraft to the using Command.

1.9.2.2.2 - Aircraft Condition "B"

1.9.2.2.2.1 - Review the aircraft maintenance records to determine the status and flying condition of the aircraft.

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1.9.2.2.2.2 - Accomplish preflight and Postflight inspections IAW applicable TOs and correct SOF discrepancies and Red X items revealed during inspection or examination of the records prior to delivery of the aircraft to the using Command.

1.9.2.2.3 - Aircraft Condition "C"

1.9.2.2.3.1 - Reinstall all removed components IAW applicable TOs and visually inspect all affected areas before closing up.

1.9.2.2.3.2 - Perform fuel system pressure check IAW applicable TOs. NOTE The aircraft should be completely reassembled and be in Condition "D" status.

1.9.2.2.3.3 - Perform Condition "D" tasks as directed below.

1.9.2.2.4 - Aircraft Condition "D"

1.9.2.2.4.1 - Rig and operationally check landing gear, wheel brakes, aileron, rudder, stabilator, and flaps IAW applicable TOs.

1.9.2.2.4.2 - Perform fuel system leak/operational check IAW applicable TOs

1.9.2.2.4.3 - Perform Condition "A" tasks as directed above.

1.9.2.2.5 - Aircraft Condition "E"

1.9.2.2.5.1 - When compression action is directed, a repair status of the aircraft must be conducted to determine the major repair tasks that must be fully accomplished while others may be curtailed or omitted. Technical assistance in evaluation of repair requirements can be obtained from F-15

Engineering.

1.9.2.3 - Finishing of Aircraft

1.9.2.3.1 - Aircraft in Conditions "A", "C", "D", and "E".

1.9.2.3.1.1 - Inspect interior of aircraft and remove all loose debris, such as: filings, chips, loose hardware, etc..

1.9.2.3.1.2 - Apply aircraft insignia and call letters conforming with TOs 1-1-8 and 1F-15A-23, if removed. Touch-up if illegible. No other markings shall be required unless otherwise directed.

1.9.2.3.2 - Aircraft in Condition "B" (Turnaround) shall be returned as received.

1.9.2.4 - Weight and Balance

1.9.2.4.1 - Weigh aircraft and complete the weight and balance records IAW the provisions in TOs

1F-15C/E-5 and 1-1B-50 only when work accomplished affects weight and balance, when weighing of aircraft is necessary to ensure SOF, or when requested on an AFTO Form 103 and approved.

1.9.2.5 - Flight Test and Government Acceptance

1.9.2.5.1 - Aircraft in Conditions "A", "C", "D", and "E" shall have the following accomplished:

1.9.2.5.1.1 - If applicable, depreserve engines IAW TO 2J-1-18.

1.9.2.5.1.2 - If applicable, service all systems IAW applicable TOs.

1.9.2.5.1.3 - Accomplish a preflight launch and end of runway inspection IAW applicable TOs. Correct all discrepancies determined to affect SOF.

1.9.2.5.1.4 - Due to work assignment (Condition "A" through "E") of the aircraft, flight testing of each aircraft shall be as determined by the SPO. The SPO shall determine whether to utilize Air Force flight test pilots or pick-up pilots to accomplish flight testing as circumstances dictate. The SPO shall also determine if the pick-up pilot can perform the test flight in the local area and continue on to their destination if the aircraft is determined to be satisfactory.

1.9.2.5.1.5 - Accomplish thru-flight inspection IAW applicable TOs. Correct all discrepancies determined to affect SOF.

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1.9.2.5.1.6 - The inventory referenced in AFI 21-103 shall be held to MINIMUM combat readiness essentials on Conditions "A", "C", "D", and "E" aircraft. Every effort shall be made to accomplish inventory at the same time thru flight inspection is accomplished. Aircraft in Condition "B" shall not require inventory when they do not go into shops for maintenance and modification.

1.9.2.5.2 - Aircraft in Condition "B" shall not normally be test flown unless work performed falls under the provisions of TO 1-1-300 and 1F-15A/E-6.

1.9.2.6 - Technical Orders and Other AF Directive Requirements

1.9.2.6.1 - Immediate Action TCTOs shall be accomplished as applicable to Condition "A", "B", "C", "D", and "E" aircraft.

1.9.2.6.2 - Urgent Action TCTOs shall be accomplished as applicable to Condition "A", "C", "D", and "E" aircraft, except when the aircraft have progressed to completion and would require disassembly or constitute a delay that is contrary to the maintenance compression policy.

1.9.2.6.3 - Routine and Other TCTOs shall be subject to compliance only when time shall permit and when disassembly and work is to be accomplished on the item and is not cause for delaying the aircraft.

1.9.2.6.4 - Condition "B" aircraft should not be processed in work and therefore should not be delayed for

TCTO compliance other than Immediate Action TCTOs directed for compliance by the SPO.

1.9.2.6.5 - Applicable regulation is AFMCI 21-118, Aircraft and Missile Maintenance

Production/Compression Report (AMREP) System.

2.0 - Receipt of Aircraft at Facility

2.1 - Handling and Safety

2.1.1 - Render Safe

2.1.1.1 - Grounding for dissipation of static electricity shall be IAW TO 00-25-172.

1A1A - Safe and Dearm Assigned Tasks

2.1.1.2 - The following hazardous equipment shall be made safe and handled IAW cited TOs.

2.1.1.2.1 - Impulse cartridges for external stores MK-1 Mod 3, MK-2 Mod 1,ARD 446-1 and ARD 863-1 shall be removed IAW TO 11A-1-33,1F-15E-33-1-2, and stored IAW TO 11A18-7-7 and AFMAN 91-201.

Personnel shall be qualified IAW AFI 23-106 and AFI 21-112.

1A1A - Safe and Dearm Assigned Tasks

2.1.1.2.2 - Fire extinguisher cartridges shall be removed IAW TO 1F-15C/E-2-26JG-20-1

1A1A - Safe and Dearm Assigned Tasks

2.1.1.2.3 - If the gun is installed, make safe for maintenance. Check gun, install safety pin, no ammo in gun, gun bay, and cavity of door 45. Install clearing sector tool. Reference TO 1F-15C/E-2-05JG-10-1.

NOTE The cartridge/propellant actuated device items of the emergency egress system shall be removed/installed by qualified egress personnel IAW the basic TO and TO 13A5-37-2. Personnel handling explosive components will be qualified IAW AFI 21-112.

1A1A - Safe and Dearm Assigned Tasks

2.1.1.2.4 - Pylons shall be de-armed, removed and stored for reinstallation IAW TO

1F-15C/E-2-94JG-32-1 once external tanks are removed.

1A1O - De-Arm, Remove, and Store Pylons Assigned Tasks

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2.1.1.2.5 - Dearm and make safe all munitions and explosive devices. WARNING All munitions shall be removed by the using activity prior to aircraft input. Should munitions be found aboard aircraft, the maintenance facility shall notify the Explosives Safety Office (SEW) and the PAO/ACO.

1A1A - Safe and Dearm Assigned Tasks

2.1.1.2.6 - Transport munitions to and from approved munitions storage areas as required.

1A1AG - Transport Munitions Assigned Tasks

2.1.1.3 - Foreign Object Damage prevention to jet engines, tires and aircraft flight surfaces shall be IAW AFI

21-101.

2.1.1.4 - Drain/purge oxygen system IAW TOs 1F-15C-2-35JG-10-1, 1F-15E-2-35JG-11-1, 1F-15-3 and

15X-1-1.

1A1Y - Drain/Purge Oxygen System Assigned Tasks

2.1.2 - Parking, Towing, Jacking

2.1.2.1 - The SOR shall handle, park, service, tow, dock, jack and moor aircraft IAW TOs

1F-15C/E-2-07JG-00-1, 1F-15C/E-2-09JG-00-1, 1F-15C/E-2-10JG-00-1, 1F-15C/E-3-1 and 1F-15-3 as required. Comply with all aircraft ground safety instructions as directed in applicable TOs.

1A1P - Tow Aircraft (7 tows of 14) 1B1A - Dock Aircraft 1B1C2 - Jack and Level Aircraft (5.3 X 3) 1B1F - Tow Aircraft (3 tows of 14) 1B1Q - De-Dock Aircraft 1B1AG - Reposition Aircraft 1B21M - Tow Aircraft (3 tows of 14) 1G1L - Tow Aircraft (1 tows of 14)

Assigned Tasks

2.1.2.2 - Qualification of personnel operating or moving aircraft shall conform to AFI 11-218, AFI 11-205, and

AFMC Supplement 1 to AFI 11-218.

1A1P - Tow Aircraft (7 tows of 14) 1B1F - Tow Aircraft (3 tows of 14) 1B21M - Tow Aircraft (3 tows of 14) 1G1L - Tow Aircraft (1 tows of 14)

Assigned Tasks

2.1.2.3 - Quality control of gaseous and liquid aviators breathing oxygen shall be IAW MIL-PRF-27210.

2.1.2.4 - Aircraft placed in hangars shall conform to the requirements specified in Appendix C, Industrial

Safety and Health Requirements.

2.1.3 - Joint Oil Analysis Program

2.1.3.1 - Perform a Joint Oil Analysis Program (JOAP) sample within thirty minutes of engine shutdown after aircraft arrival IAW TO 1F-15C/E-2-05JG-00-2.

1A1B1 - Take Joint Oil Analysis Program (JOAP) Sample (1X) Assigned Tasks

2.1.3.2 - Perform the lab test of the JOAP sample IAW 33-1-37-1 thru -3.

1A1B2A - Lab Test for Joint Oil Analysis Program (JOAP) Samples Assigned Tasks

2.1.4 - Fuel

2.1.4.1 - Handle and store fuel according to TOs 00-25-172, 42B-1-1, 42B1-1-1, MIL-STD-1518C and

AFOSH 127-43.

2.1.4.2 - All personnel engaged in fuel system maintenance and repair shall be qualified IAW the basic TO and TO 1-1-3.

Page 10 of 91August 16, 2016

2.1.4.3 - Defuel, purge and perform an explosive vapor level check as required to include the Conformal

Fuel Tanks (CFTs) to insure the aircraft and CFTs are safe for work IAW TOs 1-1-3, 1F-15C/E-2-12JG-10-2, and 1F-15C/E-2-12JG-11-1. Serviceable fuel shall be recorded on AFTO Form

781-2 and credited to the aircraft when servicing.

1A1G - Perform Explosive Vapor Level Check 1A1M - Defuel and Purge Internal Tanks and Lines 1A1N - Remove, Purge and Store External Fuel Tanks 1A1AF - Remove Conformal Fuel Tanks (CFTs) - F-15E Model Only 1B18F - Planning

Assigned Tasks

2.1.4.4 - All drained external tanks including CFTs if installed shall be removed and treated for storage IAW

TOs 1-1-3, 1F-15A-17 and 1F-15C/E-2-05JG-00-1. Tanks shall be retained for installation.

1A1N - Remove, Purge and Store External Fuel Tanks 1A1AF - Remove Conformal Fuel Tanks (CFTs) - F-15E Model Only

Assigned Tasks

2.1.4.5 - Temporary outside storage of aircraft and external tanks shall be IAW TOs 1-1-17 and 1F-15A-17.

2.1.5 - Receiving Aircraft

2.1.5.1 - The SOR shall complete AFTO Form 290 IAW TO 00-20-1 acknowledging receipt of the aircraft.

1B18F - Planning Assigned Tasks

2.2 - Inventory

2.2.1 - Accomplish inventory inspection IAW AFI 21-103.

1A1C - Accomplish Inventory Inspection Assigned Tasks

2.2.2 - Remove all classified equipment and store IAW applicable TOs.

1A1D - Remove and Store All Aircraft Equipment Assigned Tasks

2.2.3 - Record and process inventory IAW TO 1F-15A-21. NOTE Verify 1F-15A-21 equipment received on-board aircraft with crew immediately upon arrival.

1A1C - Accomplish Inventory Inspection Assigned Tasks

2.2.4 - Loose equipment shall be inventoried, tagged with aircraft serial number, inspected and stored in a secure area and returned with the same aircraft in the condition as received.

NOTE

Notify PAO/ACO of shortages and advise if command should or should not ship shortages to SOR.

Shortages, except those which occur while aircraft is at the SOR shall not be made up.

1A1E - Tag and Store Removed/Loose Equipment Assigned Tasks

2.2.5 - Manufacture metal tags for all parts removed from the aircraft to identify the parts and indicate the aircraft serial number on the tag so the reinstallation of the part may be made to the same aircraft.

1A1E - Tag and Store Removed/Loose Equipment 1B1AE - Correct Defects

Assigned Tasks

2.3 - Preservation

2.3.1 - Remove and preserve engines and Jet Fuel Starter (JFS) IAW TOs 2J-1-18, 1F-15A-17, 1F-15C/E-2-71JG-01-1, 1F-15C-2-80JG-10-1 and other applicable TOs. Remove the AMAD driveshafts while removing the engines IAW TO 1F-15C/E-2-83JG-10-1.

Page 11 of 91August 16, 2016

1A1L - Preserve Engines and Jet Fuel Starter (JFS) 1B1I - Remove Engines 1B5D25 - Remove Left Airframe Mounted Accessory Drive (AMAD) Drive Shaft 1B5D27 - Remove Right Airframe Mounted Accessory Drive (AMAD) Drive Shaft 1B5E5 - Remove Jet Fuel Starter (JFS)

Assigned Tasks

2.3.2 - Turbo-jet oil and lubricating oil drained for any reason shall not be reused and shall be disposed of as administratively condemned property IAW TO 42B2-1-3. If there is a hydraulic purifier available, purify the hydraulic fluid for reuse. Otherwise, discard IAW TO 42B2-1-3.

2.3.3 - Engines which are to be shipped to another location shall be preserved and prepared for shipment IAW

TOs 2J-1-18 and 1F-15A-17.

3.0 - Work Requirements

3.1 - General Aircraft

3.1.1 - The following inspections and maintenance shall be accomplished in accordance with appropriate technical orders and Air Force publications listed in Section V of this Appendix A. These discrepancies noted as a result of this inspection shall be corrected to the degree which shall result in a serviceable condition. All items removed to facilitate inspection or other reasons shall be reinstalled unless replacement is otherwise directed.

NOTE

In the event work required by this specification cannot be accomplished, contact the PAO/ACO for assistance in resolving the problem.

3.1.2 - Sealant and coating systems shall be mechanically or chemically removed in accordance with TOs

1-1-691, 1-1-8, 1-1-3, and 1F-15A-23 as necessary to accomplish the inspection requirements of this WS.

3.1.3 - Accomplish the following Tabs as directed by this WS.

3.1.3.1 - Accomplish Analytical Condition Inspection (ACI) when required in accordance with TAB A of this

WS.

3.1.3.2 - Accomplish painting IAW TAB C of this WS.

3.1.3.3 - Accomplish maintenance compression requirements when directed by the SPO IAW AFI 21-102 and AFMCI 21-118 as defined in TAB B of this WS.

3.1.3.4 - Accomplish corrosion treatment requirements in accordance with TAB E of this WS.

3.1.4 - The following shops and offices shall be maintained to support the F-15 aircraft: Planning, Forward

Logistic Support, Sealant Shop, Oxygen/Nitrogen Shops, Lubricant Shop, Hazardous Material Handling, Tool

Crib, Aircraft Logistics Support, Local Manufacture, and Tire Shop.

1B18A - Planner 1B18B - Forward Logistic Support (FLS) 1B18C1 - Sealant Shop 1B18C2 - Oxygen/Nitrogen Shops 1B18C3 - Lubricant Shop 1B18C4 - Hazardous Material Handling 1B18D1 - Communications Security (COMSEC) Vault 1B18D2 - Special Tool Cage 1B18E - Aircraft Logistics Specialist (ALS) 1B18F - Planning 1B18G - Local Manufactured Parts 1B18H - Tire Shop

Page 12 of 91August 16, 2016

3.1.6 - Install rubber protection on aircraft doors, panels, and surfaces which pose a hazard to equipment and personnel IAW AFOSH 91-501.

1B1AH - Protective Covering Assigned Tasks

3.1.7 - Perform Lower Explosives Limit (LEL) check IAW TO 1F-15C/E-2-28GS-00-1 and TO 1-1-3 prior to beginning work on each shift.

1B1B - Lower Explosive Limit (L.E.L.) Checks Assigned Tasks

3.1.8 - Perform explosive vapor level check IAW TO 1-1-3 on each wing leading edge thru drain holes and wing tips using an R-2 combustible and toxic gas indicator or equivalent prior to applying electrical power at predock, after initial refueling and initially at functional test. If the fire safe reading contained in TO 1-1-3 cannot be obtained or if there is evidence of leakage, make repairs per applicable technical manuals.

1A1G - Perform Explosive Vapor Level Check Assigned Tasks

3.1.9 - In the event special condition items (such as: hard landings, landing gear removals, operation under extremely dusty conditions, etc.) are encountered during processing of aircraft and/or listed as outstanding discrepancies on 781 forms upon receipt of aircraft, the applicable inspection requirements of TO 1F-15A/E-6 shall be accomplished and corrective action taken as directed by the PAO/ACO.

1A1F - Aircraft General Condition Inspection 1B1AE - Correct Defects

Assigned Tasks

3.1.10 - Complete all Individual Aircraft Tracking (IAT) and 1F-15A/E-6 Section II Part B inspections below unless told otherwise. Input the results of all IAT and 1F-15A/E-6 Section II Part B inspection results into the

Boeing ECS WebSafe AFTO Form 3 link IAW TO 1F-15A/E-6. Document the repair and/or replacement actions taken with the P/N and/or hole numbers using the number system in TO 1F-15A-36. If the hole numbers do not exist, provide a description of the repair location. NOTE For aircraft stated to complete IAT when called out in TO 1F-15-15A/E-6S-xxxx, the IAT inspection shall be completed for the calendar quarters that the aircraft will be at the depot and for one quarter after delivery.

3.1.11 - Incoming repairs on accessible internal wing torque box structure, fuselage longerons, machined bulkheads or formers, and any aircraft structure with Class 1, 2, or 3 stress intensity as defined by

1F-15C/E-3-2 require an AFMC Form 202 for disposition except for repairs installed by TCTOs, which do not require an AFMC Form 202. In addition, FS 415 doubler repair and FS 626 bulkhead preventative repair do not require 202 submission. AFMC Form 202s shall also be submitted for non-standard or non-compliant

1F-15C/E-3 TO series structural repairs. Safety-of-Flight (SOF) conditions shall be corrected as determined and approved by F-15 Engineering. Any of these incoming repairs (SOF or non-SOF) that require action will be repaired as directed by the PAO/ACO.

1A1F - Aircraft General Condition Inspection 1B18F - Planning

Assigned Tasks

3.2 - Specific Work Requirements

3.2.1 - Part A Depot Maintenance

3.2.1.1 - Predock and Disassembly

3.2.1.1.1 - (Changed) Aircraft (including wings) shall be subjected to a general condition inspection

(visual) prior to disassembly and after depaint (especially looking in all corrosion prone areas IAW TO

1F-15A-23) to determine obvious discrepancies, deterioration (structures, inlets, paint, flight controls, landing gear, canopy, etc.) wear, tear, cleanliness, and SOF conditions. Skins shall be inspected for cracks, buckled skins, missing or loose fasteners and corrosion. if bulging skin or fretting of fasteners is found, fasteners must be removed for further inspection. Repair, remove and replace, or remove and route for repair as directed by the PAO/ACO those items identified as unserviceable or missing as a result of findings from the general condition inspection and approved for work by MRT/PAO.

Page 13 of 91August 16, 2016

1A1F - Aircraft General Condition Inspection

3.2.1.1.2 - Prior to depainting the aircraft, document the location of loose or working fasteners on the aircraft, (including intakes) and components (wing, stabilizers, ramps, CFT, etc.). Identify all fasteners with dark residue around fastener. In some cases, the residue streaks behind the fastener. This is an indication that there has been movement of the fastener in the structure. The documentation should have the bad fasteners clearly marked (preferably a photograph with the fasteners circled). Provide all documentation to F-15 Engineering. This condition must be repaired IAW TO 1F-15C/E-3-2. If no specific repair exists submit AFMC Form 202.

1A1F - Aircraft General Condition Inspection Assigned Tasks

3.2.1.1.3 - Install protective covers on canopies (inside and outside), L/R Engine Intake and Exhaust, Pitot

Probes, Angle of Attack Probes, and tape Plenum Chamber Holes IAW applicable TOs.

1B1AH - Protective Covering Assigned Tasks

3.2.1.1.4 - Inspect engines for Foreign Object Damage (FOD) and any other visible damage. FOD shall immediately be brought to the attention of F-15 Planning and F-15 PAO/ACO. Defects shall be worked that are within the capabilities of the SOR.

1A1F - Aircraft General Condition Inspection 1B18F - Planning

Assigned Tasks

3.2.1.1.5 - Extend Speedbrake and install Safety Strut, P/N 68D050011-1005 IAW

1F-15C/E-2-05JG-10-1.

1A1K - Extend Speedbrake/Install Safety Strut Assigned Tasks

3.2.1.1.6 - Temporarily remove canopy IAW TO 1F-15D-2-95JG-21-1 or 1F-15E-95JG-21-1 to accommodate aft seat removal and temporarily install canopy prior to depaint. Once aircraft is depainted, remove canopy IAW TO 1F-15C-2-95JG-20-1, 1F-15D-2-95JG-21-1 or 1F-15E-95JG-21-1.

1A1W - Remove Canopy 1B1V - Temporarily Install Canopy

Assigned Tasks

3.2.1.1.7 - Remove ejection seat(s) IAW TO 1F-15A-2-95JG-10-1 or 1F-15B-2-95JG-11-1. Ejection seats shall be transported on Ejection Seat Support Dolly, P/N 64A127J1-1.

1A1Q1 - Remove Forward Seat 1A1Q2 - Remove Aft Seat

Assigned Tasks

3.2.1.1.8 - Ensure necessary components are removed from the aircraft prior to depainting the aircraft and depaint the aircraft and removed components IAW TAB C of this WS.

3.2.1.1.8.1 - Remove left and right ailerons IAW 1F-15C/E-2-27JG-10-2. Inspect ailerons to determine if they are gridlock ailerons, P/N 68B170000. If ailerons are honeycomb, replace with gridlock ailerons

,P/N 68B170000101 L/H or 68B170000-102 R/H.

1B1Y - Remove/Install Ailerons Assigned Tasks

3.2.1.1.8.2 - Remove left and right aileron actuators IAW 1F-15C/E-2-27JG-10-2.

1B1AC - Remove/Install Aileron Actuators Assigned Tasks

3.2.1.1.8.3 - Remove left and right flaps IAW 1F-15C/E-2-27JG-50-1. Inspect flaps to determine if they are gridlock flaps, P/N 68B180000. If flaps are honeycomb, replace with gridlock flaps, P/N

68B180000-101 L/H or 68B180000-102 R/H.

1B1X - Remove/Install Flaps Assigned Tasks

3.2.1.1.8.4 - Remove left and right flap actuators IAW 1F-15C/E-2-27JG-50-1.

Page 14 of 91August 16, 2016

1B1AD - Remove/Install Flap Actuators

3.2.1.1.8.5 - Remove speedbrake IAW 1F-15C/E-2-27JG-60-1. Inspect speedbrake to determine if it is a machined speedbrake, P/N 68A360194-1001. If speedbrake is composite, replace with machined speedbrake, P/N 68A360194-1001.

1B1Z - Remove/Install Speedbrake Assigned Tasks

3.2.1.1.8.6 - Remove left and right horizontal stabilators IAW TO 1F-15C/E-2-27JG-40-2. Inspect horizontal stabilators to determine if there are honeycomb components excluding the main torque box.

If there are honeycomb components, requisition new left and right horizontal stabilators with gridlock components.

NOTE

If there are none available before the aircraft is sent to functional test, then requisition reworked stabilators with honeycomb components. Annotate aircraft AFTO Form 95 that

Horizontal Stabilators with honeycomb components were installed, date and aircraft flying hours when installed.

1B9A - Remove Horizontal Stabilators (Left and Right) Assigned Tasks

3.2.1.1.8.7 - Remove left and right rudder/rudder drive fitting assemblies IAW TO

1F-15C/E-2-27JG-20-3. Inspect rudders to determine if they are two-bolt configuration, P/N

68A240001-1019. If they are not, replace with two-bolt configuration, P/N 68A240001-1019, and rudder drive fitting.

1B1AB - Remove/Install Rudders Assigned Tasks

3.2.1.1.9 - Remove the ammo drum IAW 1F-15C/E-2-94JG-50-2 to facilitate other maintenance.

1B4A - Remove Ammo Drum Assigned Tasks

3.2.1.1.10 - Remove left and right wing IAW TO 1F-15C/E-3-6 and transport wings to wing backshop area

IAW TOs 1F-15-3 and 1F-15A/E-6 to complete wing maintenance. Complete an AFTO Form 238 for all removed wings, recording the wing serial number, aircraft serial number, flight hours of the aircraft and any other important information as required by this WS. Use TO 1F-15-101 for instructions on how to complete the form. Provide the form to F-15 Engineering and 402 CMXG/Wing Shop within one working day of removal of the wings from the aircraft. Wings removed from Flight Data Recorder (FDR) aircraft will be marked "FDR Wing." If a wing change has to be made due to long lead time parts, the new wing will be equipped with the appropriate equipment as per TO 1F-15C/E-3-6.

1B8A - WING REMOVAL

1B8B - Wing Preparation/Remove Fairing Panels etc.

1B18F - Planning

Assigned Tasks

3.2.1.1.11 - Remove the radome from the aircraft IAW TO 1F-15C/E-3-4. Retain the radome for reinstallation.

1B2A - Remove Radome Assigned Tasks

3.2.1.1.12 - Remove glideslope antenna from the radome IAW TO 1F-15C/E-2-34JG-30-1.

1B2F - Remove Glideslope Antenna Assigned Tasks

3.2.1.1.13 - Remove left and right main landing gear (MLG) IAW TO 1F-15C/E-2-32JG-10-1.

1B11J - Remove Main Landing Gear (MLG) (Left and Right) Assigned Tasks

3.2.1.1.14 - Remove nose landing gear (NLG) IAW TO 1F-15C/E-2-32JG-30-1.

Page 15 of 91August 16, 2016

1B11A - Remove Nose Landing Gear (NLG)

3.2.1.1.15 - Remove nose landing gear drag brace IAW TO 1F-15C/E-2-32JG-30-1.

1B11H - Remove Nose Landing Gear Drag Brace Assigned Tasks

3.2.1.1.16 - Remove all doors, covers, and removable panels for access into areas requiring work in accordance with this WS.

1B1R - Remove/Install All Access Panels Assigned Tasks

3.2.1.1.17 - Remove the left and right variable ramp inlet assembly IAW TO 1F-15C/E-2-71JG-60-2. Turn in the first and third ramps into supply and order serviceable ramps from supply. Retain the second variable ramp for reinstallation. Depaint and paint the second variable ramp IAW TO 1F-15A-23.

1B7A - Remove Left and Right Variable Ramp Assigned Tasks

3.2.1.1.18 - Remove the left and right diffuser ramps IAW TO 1F-15C/E-2-71JG-60-2. Turn diffuser ramps in to supply and order serviceable ramps from supply.

1B4N1 - Remove Left and Right Diffuser Ramps Assigned Tasks

3.2.1.1.19 - Remove left and right Utility Hydraulic pumps IAW TO 1F-15C/E-2-29JG-11-2.

1B5D5 - Remove Right Utility Hydraulic Pump 1B5D7 - Remove Left Utility Hydraulic Pump

Assigned Tasks

3.2.1.1.20 - Remove Power Control (PC) System 1 hydraulic pump IAW TO 1F-15C/E-2-29JG-10-1.

1B5D9 - Remove PC1 Hydraulic Pump Assigned Tasks

3.2.1.1.21 - Remove Power Control (PC) System 2 hydraulic pump IAW TO 1F-15C/E-2-29JG-10-2.

1B5D11 - Remove PC2 Hydraulic Pump Assigned Tasks

3.2.1.1.22 - Remove left and right Airframe Mounted Accessory Drive (AMAD) IAW TO

1F-15C/E-2-83JG-20-1.

1B5D1 - Remove Airframe Mounted Accessory Drive (AMAD) Assigned Tasks

3.2.1.1.23 - Remove left and right utility pump manifolds IAW TO 1F-15C/E-2-29JG-10-1.

1B5D13 - Remove Left Utility Pump Manifold 1B5D15 - Remove Right Utility Pump Manifold

Assigned Tasks

3.2.1.1.24 - Remove Power Control (PC) System 1 pump manifold IAW TO 1F-15C/E-2-29JG-10-1.

1B5D17 - Remove PC1 Pump Manifold Assigned Tasks

3.2.1.1.25 - Remove Power Control (PC) System 2 pump manifold IAW TO 1F-15C/E-2-29JG-10-2.

1B5D19 - Remove PC2 Pump Manifold Assigned Tasks

3.2.1.1.26 - Remove left and right Integrated Drive Generator (IDG) IAW TO 1F-15C/E-2-24JG-10-1.

1B5D21 - Remove Right Integrated Drive Generator (IDG) 1B5D23 - Remove Left Integrated Drive Generator (IDG)

Assigned Tasks

3.2.1.1.27 - Remove Central Gearbox (CGB) IAW TO 1F-15C/E-2-80JG-12-1.

1B5E1 - Remove Central Gearbox (CGB) Assigned Tasks

3.2.1.2 - Wings

Page 16 of 91August 16, 2016

3.2.1.2.2 - Visually inspect all bushings at F.S. 509.5 thru 626.9 for corrosion, correct inside diameter, galling, fretting, and any unsatisfactory condition that may exist.

3.2.1.2.2.3 - NDI all fuselage attach lugs IAW 1F-15A-36. This is IAT 1. Input the results to the Boeing

ECS WebSafe AFTO Form 3 link IAW TOs 1F-15A/e-6 and 1F-15-101 to report that the inspection was performed and report any discrepancies and/or repair actions. Alternatively, provide the AFTO

Form 3 to F-15 Engineering within 1 working day of completion of the inspections.

1B5C - Inspect Fuselage Attach Lugs (IAT 1 is accomplished, ref 1B19A1) 1B18F - Planning

Assigned Tasks

3.2.1.2.3 - Reserved.

3.2.1.2.4 - Transport wing to SOR backshop for remainder of the wing work.

1B8B - Wing Preparation/Remove Fairing Panels etc.

Assigned Tasks

3.2.1.2.5 - (Changed) Refer to TAB D for wing work on wing serial numbers A24-0001 and up.

Accomplish ACI on wings as necessary IAW Tab A.

3.2.1.2.5.1 - (Changed) TAB D Wing Work

3.2.1.2.5.1.1 - General:

3.2.1.2.5.1.1.1 - The information contained in this section is not intended to be all inclusive nor to distract from procedures outlined in technical orders, specifications, standards and drawings listed in Section V of the WS, except where specifically noted herein.

3.2.1.2.5.1.1.2 - Repair of the wing includes all actions necessary to return them to the output configuration set forth in section 3.4.

3.2.1.2.5.1.1.3 - All major structural repairs shall be performed with wing assembly installed in the wing vertical overhaul frame, P/N 168110001 or the modified vertical overhaul frame, P/N

X8526568 IAW TO 1F-15C-3-6 for work on the inboard and outboard torque box skins and ribs, and replacement of the outboard trailing edge box assembly. No other fixtures, frames or holding frames shall be used for this purpose.

1B8B - Wing Preparation/Remove Fairing Panels etc.

Assigned Tasks

3.2.1.2.5.1.1.4 - The SOR shall inspect all leading edge and trailing edge components. All wiring, tubing, and associated components in all open areas of the wing shall be visually inspected. All defective items shall be evaluated IAW applicable tech data and repaired or replaced as required

1B8AD - Correct Defects for Wings Assigned Tasks

3.2.1.2.5.1.1.5 - Any damage to the wings caused by the SOR shall be corrected by the SOR at no cost to the Government.

3.2.1.2.5.1.1.6 - Input the results to the Boeing ECS WebSafe AFTO Form 3 link for all IAT inspections, repair and/or replacement actions giving the aircraft serial no., base, flight hours, wing serial numbers, and locations. Use the remarks section of the form to record P/N of new installed part. Use the F-15 hole numbering system in the 1F-15A-36 to locate where repairs were installed. If the hole numbers do not exist, provide a description of the repair location.

1B18F - Planning Assigned Tasks

3.2.1.2.5.1.1.7 - Wings removed from aircraft having a Flight Data Recorder (FDR) will be marked

“FDR wing” and shall be reinstalled on the aircraft they were removed from. If a wing change has to be made due to long lead time parts, then the new wing will be equipped with the appropriate equipment as per TO 1F-15E-3-6 (see paragraph 3.6).

1B8B - Wing Preparation/Remove Fairing Panels etc.

Assigned Tasks

3.2.1.2.5.1.2 - Specific Work Requirements:

Page 17 of 91August 16, 2016

3.2.1.2.5.1.2.1 - The SOR shall accomplish a leak test (manometer pressure test IAW Drawing

200810782). All leaks shall be permanently repaired IAW TO 1-1-3, 1F-15C/E-3-5 and TO

1F-15C/E-3-6.

1B8C - Wing closure, Install fairings, panels and perform all pressure checks Assigned Tasks

3.2.1.2.5.1.2.2 - Permanently and legibly mark each repaired end item with the SOR identification.

This identification marking shall display the SOR name, the Air Force contract number, and date of repair. The wing “Identification Data Plate” located under door 58 L/R shall be maintained. If the plate is replaced, all data, including original serial number, shall be stamped on a new plate and the wing shall be identified IAW the latest incorporated TCTO. If the data plate is missing, search the inboard trailing edge box area under door 138 L/R for a “parts installed list” to obtain the serial number and contact the F-15 Engineering.