Attch_5_-_PWS_Appendix_A_Work_Specification_F-15D_Addendum_-_FA8505-17-R-0004.pdf

FILE NUMBER: AFLCMC/WWQEC/FY18 FINAL F-15DWORK SPEC BASIC 23 JUN 16 i

PREPARED BY: AFLCMC/WWQEC/CHAMBERS/DSN 497-5796 APPENDIX A ADDENDUM

AIR FORCE LIFE CYCLE MANAGEMENT CENTER

ROBINS AIR FORCE BASE GEORGIA

EAGLE DIVISION

235 BYRON STREET SUITE 19A ROBINS AIR FORCE BASE GA 31098-1670

AF CONTRACT NO:________________ APPENDIX A

PR NO: FD2060-15-95046 ADDENDUM

DATE: 23 JUN 16

REV: BASIC

ADDENDUM TO APPENDIX A, FY18 Final F-15D Work Spec

WORK SPECIFICATION

TYPE WORK: PROGRAMMED DEPOT MAINTENANCE

TYPE AIRCRAFT: F-15D

For Performance during FY18 to 19

This Addendum is to be paired with the FY18 Final F-15D Work Spec.

Distribution Statement E: Distribution authorized to the Department of Defense (DOD) only because this data is “Competition Sensitive,” 28 Oct 1998. Other requests shall be referred to AFLCMC/WWQEB, 235 Byron St. Suite 19A Robins AFB GA 31098-1670.

FILE NUMBER: AFLCMC/WWQEC/FY18 FINAL F-15DWORK SPEC BASIC 23 JUN 16 ii

PREPARED BY: AFLCMC/WWQEC/CHAMBERS/DSN 497-5796 APPENDIX A ADDENDUM

REVISIONS OF APPENDIX A ADDENDUM

BASIC 23 JUN 16

Paragraphs that were changed during this revision to this work specification:

List of effective pages:

FILE NUMBER: AFLCMC/WWQEC/FY18 FINAL F-15DWORK SPEC BASIC 23 JUN 16 1- 1

PREPARED BY: AFLCMC/WWQEC/CHAMBERS/DSN 497-5796 APPENDIX A ADDENDUM

1 – General

This addendum is written to provide deviations, alternate procedures, new timelines, and waivers for Contractor depot for inspection and repair of F-15 aircraft. The deviations and waivers of this addendum shall be used in place of the corresponding paragraph numbers and/or additions to paragraphs in the work specification Appendix A, FY18.

All reference to PAO/ACO shall be interpreted as being PCO/ACO for contract facilities. All references to Contract Field Team for the purpose of installation/checkout of classified systems shall be interpreted as qualified personnel for purposes of this contract.

Use the combined TOs that cover all models of Appendix A lists except F-15E specific TOs. All references to “the government” shall be interpreted as being the U.S. Government.

All repairs, component replacement, or additional material required shall be approved by the PAO/ACO. The PAO/ACO may direct other work to be performed in conjunction with the PDM.

Add Paragraph 1.1a PAO/ACO may direct and approval is required for:

Additional work while aircraft is at the SOR.

Any engine repair or replacement.

Any additional explosive vapor level check not directed in the WS.

Repair of incoming discrepancies documented in 781 forms, which are not included in the scope of WS Paragraph 1.1.18 Any repairs to internal or external fuel tanks Any repairs to pylons Any repairs to the vertical stabilizers Any repairs to the wing structure

Add Paragraph 1.1b The SOR shall route all reports, documents, or other communication with F-15 Engineering, through the PAO/ACO.

Add Paragraph 1.1c The SOR shall route all AFTO Form 202’s to the WR Kadena PDM Program Manager / Production Manager.

Replace Paragraph 1.1.20 Not Applicable

Add Paragraph 1.1.22 The SOR is not authorized to use these methods, procedures, or specifications to accomplish the work directed herein unless approved by the PAO/ACO. SOR methods and procedures, when approved, must meet the government standards as outlined in directives listed in Section V and other directives governing requirements of this contract.

Add Paragraph 1.1.23 The work sequence set up herein is not mandatory. Rearrangement of the work sequence may be necessary at the SOR to efficiently perform the work herein.

Add Paragraph 1.1.24 The SOR shall accomplish specific work and physical security protection required by this specification.

Add Paragraph 1.1.25 The SOR shall perform work, which is requested by the using command on AFTO Form 103s if said work is approved/authorized by the WR Kadena PDM Program Manager.

Add Paragraph 1.1.26 The SOR shall accomplish urgent action and immediate action technical orders that are received while the aircraft is at the SOR as directed by the PAO/ACO.

Add Paragraph 1.1.27 All discrepancies noted which are not related to the work directed herein shall be submitted to the PAO/ACO for disposition. These discrepancies shall be recorded in aircraft historical records IAW

TO 00-20-5.

FILE NUMBER: AFLCMC/WWQEC/FY18 FINAL F-15DWORK SPEC BASIC 23 JUN 16 1- 2

PREPARED BY: AFLCMC/WWQEC/CHAMBERS/DSN 497-5796 APPENDIX A ADDENDUM

Add Paragraph 1.1.28 Recommendations for additional work not specified in this WS and determined necessary for SOR accomplishment while the aircraft is undergoing modification/PDM/ACI/CC/repair shall be forwarded to the PAO/ACO for disposition.

Add Paragraph 1.1.29 Recommendations for deletions of work requirements as amendments to this WS shall be forwarded to F-15 Engineering through the PAO/ACO for disposition.

Add Paragraph 1.1.30 Corroded avionics equipment screws, which are attached to the structural member, shall be replaced with new ones and the old ones discarded. If new fasteners are unavailable, fasteners that were removed may be reused if they are properly cleaned and corrosion treated.

Add Paragraph 1.3.1.5The SOR shall maintain the status report on government furnished equipment (GFE). This report shall identify any excess GFE and be submitted to the DCMA Property Administrator. A copy shall be provided to AFLCMC/WWQA. (DI-MGMT-80269)

Replace Paragraph 1.3.1.6 All maintenance actions shall be documented IAW AFI 21-101, TO 00-20-2, and applicable 1F-15A-6 code manuals. AFTO Forms 349 and 350 shall be used for reporting purposes. SOR will maintain records and forms IAW the contract data requirements list (DD Form 1423), attached to, and made a part of the contract. (DI-MISC-82003)

Add Paragraph 1.3.1.7 If aircraft are received minus applicable forms, or the forms contain incomplete information, provisions of TO 00-20-1 on missing forms shall apply.

Replace Paragraph 1.3.2.1 Contractor’s Progress, Status and Management Report-DI-MGMT-80227.

Add Paragraph 1.3.2.9 The SOR shall provide any information necessary to compile such reports as may be required of the PAO/ACO by technical orders, regulations, or other Air Force directives.

Add Paragraph 1.3.2.10 The SOR shall advise the WR Kadena PDM Program Manager, PAO/ACO and the appropriate System Manager Supply Monitor when it is anticipated that a shortage of either SOR or GFE shall cause a production delay. Statement of shortage of government equipment shall be in duplicate and submitted only after every possible effort has been made by the SOR to obtain the property. In reporting a shortage, the statement shall include requisition number(s), NSN, P/N submitted by the SOR, USAF source of supply (SOS), requisition status, and indicate all actions taken by the SOR and the USAF SOS to make the item available. Estimated delivery date from SOS shall also be provided. (DI-MGMT-80269)

Add Paragraph 1.3.2.11 SOR shall provide any information requested for preparation of AFI 21-103 reports.

Add Paragraph 1.3.2.12 CAVAF Reporting: The SOR shall report using the COMMERCIAL Asset Visibility (CAVAF). (DI-MGMT-81634C. The SOR shall provide data related to the tasks and efforts conducted for each repairable unit. CAVAF reporting will begin with contract/delivery order (insert contract/delivery order). If CAVAF training is required, contact 402 SCMS/GUNAB, Robins AFB GA 31098; Phone 478-327-6602, for additional information. The SOR shall conduct production reporting on a daily or as transactions occur basis.”

Add Paragraph 1.4.1 Aircraft received at the SOR may or may not have all classified equipment removed. Upon aircraft arrival, qualified personnel will remove classified equipment. Defense Contract Management Agency (DCMA) will then inspect and verify that all classified equipment has been removed before the SOR takes possession of the aircraft. Qualified personnel will reinstall the classified equipment prior to aircraft departure. SOR will not have access to classified equipment and will not take possession of the aircraft until after classified equipment has been removed from the aircraft.

Add Paragraph 1.4.2 Security at the SOR for F-15 aircraft shall be the responsibility of U.S. Government cleared personnel, DCMA Classified material will be stored in the existing class “B” (vault-type) GSA approved security container managed by qualified personnel.

Replace Paragraph 1.5.1 The SOR’s quality management and quality assurance shall conform to ISO 9001:2000 AS9100 Revision B, no tailoring. This system shall be developed and be available for cognizant QAR review prior to beginning repair. This requirement includes the complete processing of deficiency reports (DRs) at no additional cost to the government. Investigations are to be accomplished within 30 days after receipt of the exhibit.

FILE NUMBER: AFLCMC/WWQEC/FY18 FINAL F-15DWORK SPEC BASIC 23 JUN 16 1- 3

PREPARED BY: AFLCMC/WWQEC/CHAMBERS/DSN 497-5796 APPENDIX A ADDENDUM

Add Paragraph 1.5.2 The inspection system shall include a clear and complete set of work instructions (workbook logs) for all maintenance required which shall assure specific and uniform step-by-step directions for accomplishing work accurately, economically and safely. Documents shall specify component removals, inspections, and reinstallations, which affect quality and shall include caution and warning notes where failure to follow prescribed procedures could result in damage to Air Force property or injury to personnel. Removal and reinstallation of items (including lines, fittings and components) when required to gain access to another component shall be listed as separate entries on the work documents. Quantitative criteria (dimensions and tolerances) shall be included in the work document. The document shall also include criteria essential for determining the acceptability of work performed. Work documents shall be maintained and reviewed on a systematic basis for accuracy, completeness, compliance, and revisions essential in preventing recurring deficiencies. Corrective/preventive actions shall extend to the performance of all suppliers and will be responsive to deficiency report forwarded from the users through the

PAO/ACO.

Add Paragraph 1.5.3 Calibration standard for all common and special support equipment used during the repair or acceptance phases shall be in accordance with Air Force TOs, and ANSI/NCSLZ540-1.

Replace Paragraph 1.7.4 Initial local manufacture (LM) items will not be manufactured and cost charged to aircraft without approval of the PAO/ACO.

Add Paragraph 1.7.7 When shortages of parts or components will delay aircraft delivery, serviceable parts, or components, which are readily exchangeable, may be removed from another aircraft by cannibalization or rob-back with PAO/ACO approval IAW AFI 21-101, and TO 00-20-2.

Add Paragraph 1.10 Government Furnished Precision Measuring Equipment (PME)

Add Paragraph 1.10.1 The SOR shall furnish all labor to repair and calibrate Government Furnished Precision Measuring Equipment (PME) up to the capability of the SOR for category II type items.

Add Paragraph 1.10.2 In the event repair or calibration of PME is beyond the SOR’s capability, in country services through other facilities shall be arranged by the SOR, with prior approval by the PAO/ACO, and such service charges shall be reimbursed by the government as approved by the PAO/ACO.

Add Paragraph 1.10.3 In all cases, the U.S. Government shall provide all necessary parts, materials, or components required for repair of PME.

Add Paragraph 1.11 Tool Control/Accountability/Traceability

Add Paragraph 1.11.1 The SOR shall implement a tool control and accountability program IAW provisions AFI 21- 101.

Add Paragraph 1.11.2 Procedures that establish control/accountability/traceability of all tools used to perform maintenance functions or functional tests on USAF aircraft must be published and adhered to.

Add Paragraph 1.11.3 The following are minimum requirements that must be used to ensure tools will not be lost or allowed to go unidentified and undetected during maintenance/test on an aircraft.

Add Paragraph 1.11.3.1 Tools will be identified by marking (etching/stamping) so that they will be traceable to SOR and individual responsible for the tool.

Add Paragraph 1.11.3.2 Each tool will be accountable to the tool crib or individual by an inventory list showing type and quantity.

Add Paragraph 1.11.3.3 A format to count tools in work will be used in accordance with SOR’s appropriate format approved by PAO/ACO, each time a tool is used. The format will show how many tools are removed from the toolbox, and after the work, shift or task is completed, whether they have been checked back into the toolbox.

FILE NUMBER: AFLCMC/WWQEC/FY18 FINAL F-15DWORK SPEC BASIC 23 JUN 16 1- 4

PREPARED BY: AFLCMC/WWQEC/CHAMBERS/DSN 497-5796 APPENDIX A ADDENDUM

Add Paragraph 1.11.3.4 Tools that are too small to identify will be contained in a manner so that they will be adequately controlled in the toolbox. The format will reflect the quantity. The same procedure shall be followed as that for any other tool when and after using.

Add Paragraph 1.11.3.5 Stringent tool controls must be enforced at all times and as a tool is known or reported to be lost, the USAF QAR shall be notified immediately. Information on the tool reported lost should state type tool, aircraft tail number, location tool was last used, time and date, and individual that was assigned the tool. Every effort must be made to ensure the reported tool is found before maintenance is resumed or an aircraft is released for flight/delivery.

Add Paragraph 1.11.3.6 The SOR’s quality control organization will be responsible for ensuring effectiveness of the tool control program.

FILE NUMBER: AFLCMC/WWQEC/FY18 FINAL F-15DWORK SPEC BASIC 23 JUN 16 2- 1

PREPARED BY: AFLCMC/WWQEC/CHAMBERS/DSN 497-5796 APPENDIX A ADDENDUM

2 - Receipt of Aircraft at Facility

Replace Paragraph 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-15D/E-2-05JG-00-1. Tanks shall be retained for installation. If aircraft is input with external tanks installed, the work related to them shall be accomplished as an over and above effort as directed by PAO/ACO.

NOTE

If fuel transfer system is not made operational, tanks and pylons shall be returned on aircraft they were received on without external fuel. Tanks and pylons shall not be interchanged to obtain serviceable assets unless approved by the PAO/ACO.

Add Paragraph 2.1.4.6 All drained fuel will be credited to the Government. (If aircraft forms are removed before defueling make sure that, the fuel to be removed is recorded and usable fuel is placed in proper storage). (DI-

MGMT-82021)

Add Paragraph 2.1.7.1 Immediately upon receipt of aircraft, park aircraft in arm/dearm area (point aircraft in direction of least hazard), inspect for explosives and safe aircraft. Notify the PAO/ACO of any ammunition that was not removed by using activity, and do not touch the aircraft until PAO/ACO's direction. No ammunition is to be removed by SOR.

Replace Paragraph 2.2.1.1 Removal, installation, and operational check of classified materials the sole responsibility of qualified personnel, and will not be performed by Contractor personnel.

Replace Paragraph 2.2.1.2 Not Applicable

Add Paragraph 2.2.2 Following are minimum Maintenance Safety and Protection Equipment (1F-15A-21 equipment) that shall be on-board aircraft input to SOR (notify the PAO/ACO/owning command of 1F-15A-21 equipment shortages and advise if command should or should not ship shortages to SOR).

NOMENCLATURE QUANTITY

1. Cockpit Safety Pin, 68D110001 1

2. Ejection Seat Safety Pin Assy, C114767 2

3. Aircraft Ground Safety Uplock Arresting Hook Pin, 68D320001 1

4. Aircraft Ground Safety Landing Gear Pin, 68D320002 3

5. Afterburner Protector, 68D050006 2

6. Pitot Static Probe Protector, 68D050009 2

7. Aircraft Ground Blade Antenna Cover, 68D050059 2

8. Aircraft Ground Primary Heat Exchanger Inlet Cover, 68D050060 2

9. Canopy Strut, 68D110008-1003 1

10. Air Inlet Protector, 68D050007-1001 2

11. Secondary Heat Exchanger Exhaust Protector, 68D50032-1001 1

12. Secondary Heat Exchanger Inlet Plug, 68D050034 2

13. Cockpit Safety Pins, "C" 68D110001 2

FILE NUMBER: AFLCMC/WWQEC/FY18 FINAL F-15DWORK SPEC BASIC 23 JUN 16 2- 2

PREPARED BY: AFLCMC/WWQEC/CHAMBERS/DSN 497-5796 APPENDIX A ADDENDUM

14. Cockpit Safety Pins, "D" 68D110001 3

15. Speed Brake Safety Strut 1

16. Aircraft Ground Primary Heat Exchanger Exhaust Cover, 68D050061 2

17. Clearing Sector Download Pin Assembly 167C1029 1

18. Engine Ramp Ckt Breaker Clip Assembly MDE321041 2

19. Solo Flight Sequence Selector Collar, 68D110041 1

Add Paragraph 2.2.3 Aircraft shall be input without any alternate mission equipment installed.

FILE NUMBER: AFLCMC/WWQEC/FY18 FINAL F-15DWORK SPEC BASIC 23 JUN 16 3-1

PREPARED BY: AFLCMC/WWQEC/CHAMBES/DSN 497-5796 APPENDIX A ADDENDUM

3 - Work Requirements

Add Paragraph 3.1.6.9 The following shall apply to all avionics equipment identified by AFI 11-202 V3 or in the paragraphs 3.8.9.1.1. through 3.8.9.1.22 as safety of flight or mission profile: When Built-In-Test (BIT) and aircrew write-up indicates a malfunction in the avionic system, which box or boxes shall be removed from the aircraft by SOR personnel and replaced by a serviceable unit furnished as GFM. All removed reparable items shall be returned to the using command. When the condition does not affect safety of flight, mission profile or is not required for operational check as a result of TCTO compliance, the repair shall not be made.

Add Paragraph 3.1.6.9.1 The following Work Unit Code/Systems are identified as safety of flight and shall be replaced with fully operational units as an over and above effort directed by the PAO/ACO. Removal, installation, and operational check of the Central Computer (CLASSIFIED) 57A00 is the sole responsibility of qualified personnel, and will not be performed by SOR personnel.

Replace Paragraph 3.1.7 Perform LEL check IAW TO 1F-15D-2-28GS-00-1 and TO 1-1-3 prior to beginning work on each shift. An additional LEL check is required any time the aircraft is moved, or as directed by the PAO/ACO.

Replace Paragraph 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 PAO/ACO who will contact DCMA safety officer who will notify 330th ASW/SE and the AFLCMC/WWQAA Program Manager. Defects shall be worked that are within the capabilities of the SOR.

Replace Paragraph 3.2.1.2.4 Transport wing, as necessary, to SOR’s wing work area for accomplishment of the wing work.

Add Paragraph 3.2.1.2.5.1.3.13.1.1 If rib upper flanges and webs are cracked, replace cracked rib. Remove Surge Box panel P/N 68A115154 to facilitate XW172 aft rib replacement. Clean, re-seal, and install IAW TO’s after rib installation. Use new nut strips/inserts (Do not re-use old nuts). Complete an AFTO Form 3 for repair and/or replacement actions.

Add Paragraph 3.2.1.2.5.1.3.13.1.2 If new beefed up ribs have already been installed and only the fastener holes are cracked in the rib, then crack may be repaired by oversizing to the 2nd oversize only. If cracks remain, contact PAO/ACO who will in turn contact F-15 Engineering for disposition.

Add Paragraph 3.2.1.2.5.1.3.13.1.3 If the ribs have not been replaced with beefed up ribs, then remove and replace outboard torque box ribs, P/N 68A115102, 68A115104, 68A115142, and 68A115103 with new beefed up ribs. Remove Surge Box panel P/N 68A115154 to facilitate XW172 aft rib replacement. Clean, re-seal, and install IAW TO’s after rib installation. Use new nut strips/inserts (Do not re-use old nuts). Complete an AFTO Form 3 for repair and/or replacement actions.

NOTE

Check the outboard main spar while ribs are removed to determine if the main spar needs replacing.

Replace Paragraph 3.2.1.2.5.1.3.46 Transport wing back to aircraft for installation.

Replace Paragraph 3.2.1.5.1 Buff the canopy as required to remove damaged areas IAW TO 1F-15D/E-3-4. If the damages are beyond TO limitation, then replace the canopy assembly as directed by the PAO/ACO.

Replace Paragraph 3.2.1.5.2 Remove and buff the windscreen as required to remove damaged areas IAW TO 1F- 15D/E-3-4. If the windscreen cannot be returned to a serviceable status, replacement shall be accomplished using the advanced design windscreen (ADW) as the preferred spare IAW 1F-15D/E-3-4. Correct defects to the canopy, windscreen, attaching hardware, and rigging found in these areas. If the damages are beyond TO limitation, then replace the windscreen as directed by the PAO/ACO.

Replace Paragraph 3.2.1.6.2.3 Remove the horizontal stabilator connecting link from the aircraft. Inspect the bushing for wear and loose condition. If bushing is worn or loose, remove and replace the bushing as directed by the PAO/ACO. Ream the new bushing to original size as per TO 1F-15D-3-4 as directed by the PAO/ACO.

FILE NUMBER: AFLCMC/WWQEC/FY18 FINAL F-15DWORK SPEC BASIC 23 JUN 16 3-2

PREPARED BY: AFLCMC/WWQEC/CHAMBES/DSN 497-5796 APPENDIX A ADDENDUM

Replace Paragraph 3.2.1.10.9 Replace fuselage foam in the following tanks. SOR shall cut foam, only as directed by the PAO/ACO, for installation in cells 1, 2, 3A, 3B, left and right auxiliary tanks IAW drawing numbers 68B580059-193, 68B580059-185, 68B580059-187, 68B580059-189, 68B580059-197, and 68B580059-191 respectively.

Add Paragraph 3.2.1.11.7 Accomplish Organizational, "O", level engine maintenance on all aircraft IAW Job Guide series 1F-15D-2-71JG, 1F-15D-2-72JG, 1F-15D-2-73JG, 1F-15D-2-74JG, 1F-15D-2-75JG, 1F-15D-2-76JG, 1F-15D-2-77JG, 1F-15D-2-78JG, and 1F-15D-2-79JG as directed by PAO/ACO.

Replace Paragraph 3.2.1.14.2 Inspection/removal/repacking of crew parachute/survival kits shall not be accomplished to perform inspections of the parachute and survival kits. If expiration date occurs during time aircraft is at SOR, Kadena AB will provide a replacement parachute/survival kit. Removal of the parachutes and survival kits to perform other inspection or repairs is authorized.

Add Paragraph 3.2.1.14.9 Life support Equipment shall be maintained by Kadena AB IAW AFMCI 11-301.

Add Paragraph 3.2.1.14.10 Remove and reinstall the life raft only if required to complete other maintenance.

Inspections and repairs of the life raft will be performed by Kadena AB. Replace the life raft only as directed by the

PAO/ACO.

Add Paragraph 3.2.1.14.11 Inspect and perform operational checks on the CRU-60P oxygen connector and oxygen regulator.

Replace Paragraph 3.2.1.15.8 Correct defects on doors/panels including associated stiffeners and other substructure components. Rework all elongated/damaged holes to 2nd oversize to clean up damage on all door, covers, and removable panels. If 2nd oversize will not obviously clean up damage, submit an AFMC Form 202 to the PAO/ACO who will submit it F-15 Engineering. On all fixed structure areas, contact PAO/ACO who will in turn contact F-15 Engineering, by phone or by submitting an AFMC Form 202 for disposition (such as vertical stabilizer forward, aft and main boxes, Individual Aircraft Tracked (IAT) locations, etc.).

Replace Paragraph 3.2.1.15.14 Complete all Individual Aircraft Tracking (IAT) inspections using Attachment 2 as reference for if an IAT is to be completed 100% or occurenced based upon TOs 1F 15A/E 6 and 1F 15A/E 6S xxxx even if TO 1F 15A/E 6S xxxx does not say it is due. If an IAT is not listed in Attachment 2 but is listed in 1F 15A/E 6S xxxx as being due, complete the IAT inspection. Input the results of all IAT 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.

Alternatively, if access to the Boeing ECS WebSafe AFTO Form 3 link is unavailable, results can be emailed to 830acsg.gfeab.asip@robins.af.mil.

Assigned Tasks 1B19 - Depot and Field Level Individual Aircraft Tracking (IATs) Inspections

Replace Paragraph 3.2.1.18.1.1 This work statement establishes requirements for corrosion treatment of the F-15 aircraft at the SOR. All corrosion will be documented by the SOR and verified by AFQA. Attaching (nonstructural) hardware that shows evidence of corrosion in inaccessible areas will remain untreated as long as the item in question is not severely corroded except where more economical repair can be accomplished or repair is deemed necessary by AFQA and AFPD. In each case, economical and/or necessary repairs shall be approved by the PAO/ACO. Attaching (nonstructural) hardware that shows evidence of moderate to severe corrosion in accessible areas shall be replaced or treated in accordance with technical orders.

Add Paragraph 3.2.1.18.2.3.2 Improper fasteners or fasteners that are found missing during Evaluation and Inspection shall be replaced. Loose fasteners shall be retorqued IAW applicable TO. Fasteners with damaged nutplates shall have new nutplates installed if fasteners and nutplates are available. Install all permanent fasteners wet with sealant IAW TO 1F-15A-23.

FILE NUMBER: AFLCMC/WWQEC/FY18 FINAL F-15DWORK SPEC BASIC 23 JUN 16 3-3

PREPARED BY: AFLCMC/WWQEC/CHAMBES/DSN 497-5796 APPENDIX A ADDENDUM

Replace Paragraph 3.2.1.18.3.6.3 Visually inspect all corrosion prone areas IAW TO 1F-15A-23 for corrosion.

NOTE

Avionics components contained in the nose barrel, door 3 L/R, 6 L/R and 10 L/R shall not be removed for inspection of pin/washer/web (nose barrel) and pin/washer/cover/support (doors 3 L/R, 6 L/R and 10 L/R) under this requirement.

Replace Paragraph 3.2.1.18.3.7.1 Visually inspect all accessible areas in cockpit/ (equipment bay five) for corrosion and/or deteriorating paint. Pay particular attention to floors, walls, and interior surfaces. Inspection areas should include, but not be limited to, the items described in Section II of the TO 1F-15A-23 for the “main structural assembly.” To determine the extent of corrosion or paint deteriorations, cockpit/ (equipment bay five) mounted accessories/components may require removal or shifting from their prescribed location. Egress seats must be removed prior to this inspection per applicable Technical Orders. The records addressed in the 36 month seat inspection, Item 5, Steps A through F, Page 2-A-008, 1F-15A-6 , shall be documented/updated prior to aircraft departure from the SOR.

Replace Paragraph 3.2.3 Part C Negotiated TCTOs Not applicable

Replace Paragraph 3.2.4 Part D Negotiated Maintenance Not applicable

Add Paragraph 3.2.6 Approved Local Manufactures Items

L/I Part Number Nomenclature L/I Part Number Nomenclature

FILE NUMBER: AFLCMC/WWQEC/FY18 FINAL F-15DWORK SPEC BASIC 23 JUN 16 4-1

PREPARED BY: AFLCMC/WWQEC/CHAMBERS/DSN 497-5796 APPENDIX A ADDENDUM

4 - Final Processing of Aircraft

Add Paragraph 4.7.6.1 Reapply markings IAW TOs 1F-15A-23, and PACAF Supplement 1 to AFI 21-105. If painting and marking instructions of TOs 1-1-4 and 1F-15A-23 conflict, TO 1F-15A-23 shall take precedence.

Exceptions: (1) Air and ground crew names not required; (2) Black unbroken stars will be used IAW TO 1-1-8, (3) Station numbers will be placed on aircraft IAW TO 1-1-8, NOTE

Decals may be used.

Replace Paragraph 4.6.1. Functional check flights performed after accomplishment of repair/modification shall be identified as acceptance/functional check flight. Requirements listed in TO 1F-15A-6 inspection manual and the TO 1F-15A-6CF-1 Acceptance/Functional Check Flight Procedures Manual shall be accomplished when acceptance check flights are required. Aircraft systems not worked/reworked under this WS shall be checked during the acceptance/functional check flight to insure the overall condition of the aircraft is safe for flight. Discrepancies found during flight check that affect systems that were disturbed during work accomplished by the SOR or that affect those systems identified in this WS as mission essential will be corrected prior to aircraft departure. This includes all safety of flight items as well as SOR induced non-safety of flight discrepancies. All non-safety of flight items shall be recorded in aircraft records.

Replace Paragraph 4.8.4 Installation of classified items shall be accomplished by qualified personnel.

FILE NUMBER: AFLCMC/WWQEC/FY18 FINAL F-15DWORK SPEC BASIC 23 JUN 16 5-1

PREPARED BY: AFLCMC/WWQEC/CHAMBERS/DSN 497-5796 APPENDIX A ADDENDUM

5 - Tech Orders & Other Directives

Replace Paragraph 5.1.1 General Compliance Information: The SOR shall maintain all Technical Orders and other Technical Directives, hereinafter listed, in an updated and current status according to TO 00-5-1. Routine review of TO and technical directive indexes shall be accomplished at 90 day intervals following contract award.

Routine review notwithstanding, within 10 days following receipt of a change to Technical Orders or Technical Directive, SOR shall submit to the PAO/ACO a written evaluation of those changes, including specific back up data for those changes which impact the performance of the SOR. Changes, which impact the SOR, shall not be implemented by the SOR until authorized by the PAO/ACO. All statements in the following references reading "may" or "should" shall be interpreted as "shall.” Compliance with all listed directives, government specifications and standards, drawings and technical orders is mandatory while performing the work required by this WS when the following are applicable:

Update Paragraph 5.3 Applicable Directives

AFMCI 21-108 Production Acceptance Certification (PAC) and Organic Depot Maint Quality is not applicable.

AFI 32-1024 Standard Facility Requirements is not applicable.

JP 3-02-2 Amphibious Embarkation is not applicable.

DODI 5000-2 Management of Contract Data is applicable.