Performance_Work_Statement_(PWS).pdf

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PERFORMANCE-BASED WORK STATEMENT (PWS)

FOR

PACAF A-10 IN-THEATER DEPOT

PURCHASE REQUEST NO.: F2DCAQ8324B001

22 February 2019

Prepared By Mr. Jerome Savikis

OCONUS Depot Program Manager A-10 System Program Office

(801) 777-4153 jerome.savikis@us.af.mil

A-10 System Program Office (WWA) Air Force Life Cycle Management Center (AFLCMC)

6058 Aspen Road, Bldg. 1285 Hill Air Force Base (AFB), UT 84056

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Record of Revisions

Revision Number Date Description Basic 22 February 2019

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TABLE OF CONTENTS

1. PERFORMANCE WORK STATEMENT (PWS) 5

2. DESCRIPTION OF SERVICES 5

2.1. Scope 5

2.2. General Contractor Requirements 5

2.3. Facilities for Government Use 6

2.4. Terms Explained 7

2.5. Condemnation and Limitation on Repair 8

2.6. Accessory and Component Reuse, Repair, and Replacement 9

2.7. Contractor’s Workbook 10

2.8. Receipt of Aircraft at Contractor Facility 10

2.9. General Work Requirements 13

2.10. Specific Work Requirements 13

2.11. Final Processing of Aircraft 18

2.12. Over and Above Work Procedures 19

3. DATA 20

3.1. Maintenance Records, Forms, and Publications 20

3.2. Reporting Instructions 21

4. TECHNICAL ORDERS (TOS) AND OTHER DIRECTIVES 23

4.1. Technical Data 23

4.2. Compliance with Listed Publications 24

4.3. Applicable TOs 24

5. SERVICES SUMMARY 25

6. MANAGEMENT OBJECTIVES 26

6.1. General Objectives 26

6.2. Program Status Reporting 27

6.3. Program Management Reviews 27

6.4. Program Kick-Off Meetings 28

6.5. Master Program Plan and Schedule 28

7. GENERAL INFORMATION 29

7.1. Security / Operations Security Requirements 29

7.2. Quality Control 30

7.3. Quality Assurance 30

7.4. Configuration Management 31

7.5. Environmental Controls 31

7.6. Government Observations 32

7.7. Safety Requirements 32

7.8. Training 32

7.9. Special Qualifications 33

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TABLE OF CONTENTS

7.10. Phase Out 34

7.11. Publications 34

7.12. Government Furnished Property and Services 35

7.13. Government Inspection and Acceptance of Deliverables 35

7.14. Data Ownership 35

APPENDIX 1 – ACRONYMS AND ABBREVIATIONS LIST 36

APPENDIX 2 – TECHNICAL ORDERS AND OTHER DIRECTIVES 39

APPENDIX 3 – A-10C STRUCTURAL COMPONENT S/N VERIFICATION 47

APPENDIX 4 – A-10C PAINT SPECIFICATIONS 48

APPENDIX 5 – A-10C SCHEDULED STRUCTURAL INSPECTION (SSI) 52

APPENDIX 6 – ENHANCED WING ASSEMBLY (EWA) 66

APPENDIX 7 – EIGHT YEAR CORROSION (8YC) 70

APPENDIX 8 – LEGACY WING SCHEDULED STRUCTURAL INSPECTION (SSI) 75

APPENDIX 9 – PYLON REWIRE 93

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PERFORMANCE WORK STATEMENT (PWS)

1. PERFORMANCE WORK STATEMENT (PWS)

1.1. This Performance Work Statement (PWS) is prepared in accordance with (IAW) the Defense Acquisition Guidebook (DAG) 14.3.1.5.

2. DESCRIPTION OF SERVICES

2.1. SCOPE: This PWS defines depot-level maintenance required to sustain United States Air Force (USAF) A-10 aircraft. The objective of this contract is to acquire in-theater Contractor Maintenance Support to accomplish the work requirements specified herein. This PWS is a binding agreement between the U.S. Government (USG) and the contractor. The scope of this contract remains in effect under the terms of the basic contract and all applicable modifications until completion of the contract’s duration or exhaustion of the contract ceiling. The following general tasks are to be completed under this effort:

2.1.1. Acronyms and Abbreviations List – Appendix 1

2.1.2. Technical Orders and Other Directives – Appendix 2

2.1.3. A-10C Structural Component S/N Verification – Appendix 3

2.1.3. A-10C Paint Specifications – Appendix 4

2.1.4. A-10C Scheduled Structural Inspection (SSI) – Appendix 5

2.1.5. Enhanced Wing Assembly (EWA) – Appendix 6

2.1.6. Eight Year Corrosion (8YC) – Appendix 7

2.1.7. Legacy Wing Scheduled Structural Inspection – Appendix 8

2.1.8. Pylon Rewire – Appendix 9

2.1.9. Additional depot-level inspection, repair, and modification programs may arise in the future. All additional work requirements will be negotiated or accomplished using over-and-above work procedures. Revisions or supplements to this PWS will be added as needed through bi-lateral contract modifications.

2.2. GENERAL CONTRACTOR REQUIREMENTS

2.2.1. The contractor shall provide all facilities, equipment, Contractor Furnished Equipment/Contractor Furnished Material (CFE/CFM), and manpower to accomplish all work activities.

2.2.2. The contractor facility shall be located at an airport capable of receiving and servicing A- 10C. Facility shall be located within 400 nautical miles of Osan Air Base, South Korea.

2.2.3. The contractor shall furnish all parts and materials except USAF managed items supplied as Government Furnished Equipment/Government Furnished Material GFE/GFM as authorized in Appendix B of the contract see Government Furnished Property and Services paragraph

7.13. CFE/CFM shall be requisitioned using the MILSTRIP system. When required parts/materials are not available in MILSTRIP, the contractor shall requisition the CFE/CFM from USG approved sources or local manufacture in accordance with the technical data package. The contractor shall be responsible for ensuring all aircraft (A/C) parts meet flight worthiness standards and certification.

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2.2.4. The contractor shall possess local manufacturing capability for material and support equipment necessary to complete work requirements in cases when such material/equipment is not available from USG approved sources and local manufacture is authorized by the Administrative Contracting Officer (ACO).

2.2.5 The contractor shall furnish all parts and materials except USAF managed items supplied as GFE/GFM as identified in Appendix B of the contract. CFE/CFM may be requisitioned using the MILSTRIP system. When required parts/materials are not available in MILSTRIP, the contractor shall requisition the CFE/CFM from USG approved sources or local manufacture in accordance with the technical data package. The contractor shall be responsible for ensuring all aircraft parts meet flight worthiness standards and certification. Local manufacture requests shall be submitted using the AFMC Form 202 process for parts listed in the Illustrated Parts Breakdown (IPB) with a Source, Maintenance, and Recoverability (SMR) Code of procurable with no assets available through MILSTRIP or surplus. For parts with an SMR Code of Manufacture (starting with MO, MF, MD or XC) an AFMC Form 202 is not required. Reference Technical Order (TO) 00-25-195 AF Technical Order System Source, Maintenance, and Recoverability Coding of Air Force Weapons, Systems, and Equipment for SMR code breakdown. Local manufacture requests shall be submitted using the Air Force Material Command (AFMC) Form 202 process IAW paragraph 4.1.3. Submission of additional 202 requests is not required on locally manufacture parts that have been approved with an AFMC Form 202 by the A-10 SPO Engineering Group during the current contract.

2.2.6. The contractor shall be capable of meeting all applicable requirements in order to accept first A/C induction and begin work within six (6) months of contract award. Minimum requirements include facility preparation/upgrade, equipment acquisition, technical order library, compliance with all personnel training and certification requirements, approved safety, security, quality, and management plans, and compliance with Ground and Flight Risk contract clause (252.228-7001). The contractor shall coordinate closely with the USG Program Manager to ensure required GFE/GFM is received and develop mitigation options for items not readily available.

2.3. FACILITIES FOR GOVERNMENT USE

2.3.1. The primary work site is the Contractor’s facility.

2.3.2. The Contractor grants to the U.S. Government the right to utilize office space, together with light, heat, office furniture, local telephone service, and other services required, for administrative purposes associated with this contract. All of the space, utilities, and services mentioned herein will be furnished at no additional cost to the U.S. Government.

2.3.3. The Contractor is responsible for all facility maintenance directly related to A-10 contract.

2.3.4. Government Plant Representatives/Government Ground Flight Representative (GGFR) Office: The Contractor shall make office and working spaces available to the Government for Contract Administration Services (CAS) functions at its aircraft and maintenance facility (if not already established), as follows:

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2.3.4.1. Custodial services to include trash removal, sweeping, vacuuming, mopping, dusting and waxing of floors surfaces. Custodial services provided shall coincide with Contractor’s daily schedule for similar services.

2.3.4.2. Telecommunication Services (Voice/Phone). The designated DCMA office will be provided voice/phone line service for calls that does not incur any costs such as emergency response (119 or equivalent), international toll-free connections, and local calls. The Contractor shall receive written approval from the PCO before incurring any costs associated with long-distance or international calling. For U.S. Government personnel outside of the DCMA agency that requires use of long-distance or international calling, the designated unit shall pay for incurred telecommunication service charges, as applicable.

2.3.4.3. Telecommunication Services (Data/Peripheral). The designated DCMA office will provide their own data/peripheral network connections in accordance with DCMA instructions.

If Contractor networks are available for use, DCMA personnel will exercise existing DCMA instructions to initially receive approval to connect to these networks. The Contractor shall receive written approval from the PCO before incurring any costs associated with data/peripheral services. For U.S. Government personnel outside of the DCMA Agency that require data connection to the Contractor’s network and applicable peripherals such as printing and facsimiles, the designated unit shall pay for incurred telecommunication service charges, as applicable.

2.4. TERMS EXPLAINED For the purpose of the work specification, the terms used herein are explained as follows:

2.4.1. Defect: Any nonconformance of a characteristic with specified requirements. The classes of defects are minor, major, and critical.

2.4.1.1. Minor Defect: A defect that is not likely to materially reduce the usability of the end item or part for its intended purpose, or is a departure from established standards.

2.4.1.2. Major Defect: A defect, other than critical, that is likely to result in failure, or materially reduce the usability of the end item or part for its intended purpose.

2.4.1.3. Critical Defect: A defect that judgment and experience indicate is likely to result in hazardous or unsafe conditions for individuals using, maintaining, or depending upon the end item or part.

2.4.2. Disturbed Systems: Any system, of which the whole or a component part has been removed, disassembled, repaired, adjusted, modified, disconnected, or altered.

2.4.3. Accessible Areas: Those areas of equipment that may be inspected or worked without disassembly other than that required by this work specification.

2.4.4. End Item: The specific Aircraft for which this work specification is written.

2.4.5. Limited Access Area: An area which would not normally be opened during organizational and intermediate level maintenance or during a phase inspection excluding riveted or stress panels.

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2.4.6. Maintenance Facility: A maintenance facility is determined as an organic or contract facility capable of performing depot level, technical maintenance.

2.4.7. Inspection or Check: An examination of an item to determine identity, condition, and proper installation.

2.4.8. Examination: Determining the conformance of an item or part to specific requirements by simple physical (i.e., visual, auditory, tactile, etc.) means, manipulation, gauging, or measurement without the use of special laboratory appliances or procedures.

2.4.9. Modification: A change in the physical configuration or in the functional characteristics of a system or equipment.

2.4.10. Operational Check: A functional test of an accessory, component or system accomplished in its installed environment to assure proper installation and operation.

2.4.11. Repair: The process to remove defects, restore strength or replace parts and components using authorized TO methods as necessitated by wear and tear, damage or failure of parts to maintain the specific item of material in efficient operating condition.

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

2.4.13. Serviceable: Capable of meeting the requirement and performing the function for which designed or modified.

2.4.14. Maintenance Paint: Touch-up painting as necessary, to provide adequate corrosion protection.

2.4.15. Nondestructive Inspection (NDI): Methods for investigating the quality, integrity, properties, and dimension of material and components without damaging or impairing their serviceability.

2.4.16. Critical Safety Item: Pertains to aircraft items whose absence or failure would likely result in the loss of and/or serious damage to the aircraft and/or serious injury or death to the occupants during pre-flight, flight, or post flight operations.

2.5. CONDEMNATION AND LIMITATION ON REPAIR

2.5.1. Condemnation: Any item deemed unserviceable by the Administrative Contracting Officer (ACO) shall be condemned administratively IAW the Equipment Repair Recoverability Code (ERRC) criteria in TO 00-25-195 and processed IAW Air Force Instruction (AFI) 23-101.

Contact the ACO for disposition on disposal or return of condemned items.

2.5.2. Limitation on Repair: When the estimated cost to the USG for repair of an item or part, including labor and material, is in excess of 75 percent of the new acquisition/ exchange cost, the maintenance facility shall not repair the item or part without approval of the ACO.

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2.6. ACCESSORY AND COMPONENT REUSE, REPAIR, AND REPLACEMENT CRITERIA

2.6.1. Reuse: Serviceable accessories and components removed solely for work accessibility shall be identified by A/C serial number, protected, and properly stored to prevent damages or loss. Such accessories and components shall be reinstalled on the same A/C unless otherwise authorized by the ACO.

2.6.2. Repair: Accessories and components that have defects shall be repaired provided the repair does not exceed the base level repair authorized by TO 1A-10C-6 and the maintenance facility has the necessary support equipment to accomplish the required repairs. Those accessories and components requiring repairs that exceed base level repair restrictions or for which the necessary support equipment is not available, shall be replaced with a serviceable like item.

2.6.3. Replacement: Unserviceable accessories and components shall be replaced with a serviceable like item, or by cannibalization IAW AFI 21-102 and AFI 21-101 para 9.23. when authorized by the ACO.

2.6.3.1. Replacement parts shall comply with "Usable on Code" contained in the applicable 1A-10C-4 series Illustrated Parts Breakdown (IPB) technical order.

2.6.3.2. Candidates for cannibalization shall be reviewed for TO changes and updated Time Compliance Technical Order (TCTO) requirements affecting the required item configuration.

Cannibalization actions must be approved by the ACO prior to the cannibalization action.

2.6.3.3. Any parts that are cannibalized or replaced that are serially controlled by 1A-10C- 06 Work Unit Code (WUC) Manual shall be documented in the aircraft records.

2.6.4. Time changes: Accessories and components installed on incoming A/C should have sufficient remaining time to exceed the number of days the A/C will be in depot. A/C received with accessories/components requiring time change replacement will be referred to the ACO.

2.6.4.1. Accessories/components becoming overdue for time change during depot possession due to original output date being exceeded will be referred to the ACO. The ACO will coordinate with the using command for disposition of the time change requirement.

2.6.4.2. Time change item replacements, if accomplished by the contract depot facility, shall be recorded in the affected A/C Work Control Document (WCD)/records immediately after installation of the item.

2.6.4.3. When Cartridge Actuated Device / Propellant Actuated Device (CAD/PAD) items come due during time of depot possession, the owning unit is responsible for providing serviceable replacements to the contractor for install.

2.6.4.4. Prior to departure of the A/C, all time change items recorded in the maintenance WCDs shall be transcribed to the A/C records.

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2.7. CONTRACTOR’S WORKBOOK The contractor shall develop and maintain a workbook to provide specific and uniform step-by-step instructions for accomplishing work accurately, economically, and safely.

2.7.1. Workbooks must specify component removals, inspections, and reinstallations that affect quality and must include warning and caution notes where failure to follow prescribed procedures could result in injury to personnel or damage to USG property. Removal and reinstallation of items (including lines, fittings, components, etc.), when required to gain access to another component, shall be listed as separate entries in the workbook.

2.7.2. Include quantitative criteria (dimensions and tolerances) in the workbook, either by actual values or by references to the drawing or TO.

2.7.3. Include criteria essential for determining the acceptability of work performed.

2.7.4. Maintain and retain workbooks and other pertinent records IAW the contract requirement.

Sufficient documentation must be maintained by the contractor until the A/C’s next induction, incident, or action to assist in any accident investigation that may be conducted by the USG.

Records remaining at the end of the contract shall be prepared and transferred to the USG or the follow-on contractor.

2.8. RECEIPT OF AIRCRAFT AT CONTRACTOR FACILITY

Aircraft Delivery/Induction Requirements:

2.8.1. Aircraft:

2.8.1.1. A/C engines that are removed shall be reinstalled in the same A/C unless an exception is authorized by the ACO. These engines should not have inspections or time change items due within the next 25 operating hours or equivalent cycles.

2.8.1.2. Aircraft Munitions: A/C should be delivered to depot with all munitions and externals stores removed. A/C weight and balance will be maintained by use of ballast. A/C should not be delivered to depot with spent casings loaded.

2.8.1.3. Survival Packs: When delivered with the A/C to depot, survival packs should have a minimum of 90 days remaining prior too due date of 180-day inspection requirement prescribed in TO 14S1-3-51.

NOTE: This requirement is waived for A/C inducted for SSI

2.8.1.4. External Tanks: A/C being input to depot should be delivered without external tanks unless previously negotiated with depot using Air Force Technical Order (AFTO) Form 103.

2.8.1.5. A/C Records: The using activity will ensure that required forms are complete prior to delivery of A/C to depot.

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2.8.1.6. Review of A/C records should include verification of TCTOs and Engineering Change Proposal (ECP). A thorough review of each A/C fuselage and wing AFTO Form 95s for engineering derived re-inspection requirements shall be accomplished and documented on appropriate WCD. Copies of required forms will be IAW TO 00-20-1. Include engine historical records containing last five (5) flights of take-off Trim Data (NF Trim).

2.8.2. Handling:

2.8.2.1. The contract depot maintenance facility shall service, tow, park, moor, and make the A/C safe for maintenance IAW the applicable sections of TO 1A-10C-2-4JG-1.

2.8.2.2. Accomplish spectrometric oil sampling of each engine (except Auxiliary Power Unit [APU]) IAW AFI 21-124, TO 33-1-37-1, -2, -3, and 1A-10C-2-12JG-1. A data collection sheet should arrive with the A/C forms. File the completed sheet with the A/C forms along with a copy of the laboratory results printout. In addition, provide an electronic copy of the laboratory results to the using organization unit within 15 days of A/C arrival IAW Contract Data Requirements List (CDRL) A/B/C/D/E/F/G/H/J/K 001, Oil Analysis Report.

2.8.2.3. Download Turbine Engine Monitoring System/Airborne Data Recorder TEMS/ADR data IAW TO 1A-10C-2-31JG-1 and provide data to the using organization within 15 days of A/C arrival IAW CDRL A/B/C/D/E/F/G/H/J/K 002, Turbine Engine Monitoring System.

2.8.3. Inventory:

2.8.3.1. Receipt of the A/C shall be acknowledged on AFTO Form 290, Aerospace Vehicle Delivery Receipt IAW TO 00-20-1.

2.8.3.2. Inventory each A/C to ascertain the accuracy of the equipment installed in the A/C and all -21 equipment IAW 1A-10C-21. Document inspection results using an AF Form 2692 and maintain with the A/C forms.

2.8.3.2.1. If a discrepancy is noted, notify the ACO within (1) hour. The ACO will contact the unit organization to determine whether the missing equipment warrants a Report of Survey or replacement. Where safety of flight is affected, the owning unit will be responsible for providing the missing equipment.

2.8.3.3. Accomplish an inventory inspection of disturbed system/areas using this work specification and TO 1A-10C-6 as a guide. Visual inspection will continue throughout the entire disassembly phase and be performed in all areas accessed in the accomplishment of this work specification.

2.8.3.4. Incoming A/C and serialized component AFTO 95, AFTO 44 shall be reviewed for engineering inspection requirements on A/C driven by previous depot inductions or field repairs. All engineering inspection requirements documented into AFTO 95 from previous maintenance activities shall be incorporated and documented into current maintenance activity.

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2.8.3.5. Record A/C major structural components IAW Appendix 3 of the PWS: A-10 Structural Component Serial Number Verification and provide information IAW CDRL A/B/C/D/E/F/G/H/J/K 003.

Note:

The NLign program will be used to record incoming serialized components and also to capture the outgoing aircraft configuration information. Delivery of the information back to SPO engineering will also be through the NLign program.

2.8.3.5.1. Record data as detailed below for each A-10 induction:

2.8.3.5.1.1. Configuration Status (incoming / outgoing)

2.8.3.5.1.2. Depot

2.8.3.5.1.3. Tail Number

2.8.3.5.1.4. Induction (arrival / departure)

2.8.3.5.1.5. A/C Hours (COT)

2.8.3.5.1.6. Serial Number

2.8.3.5.1.7. Left Nacelle

2.8.3.5.1.8. Right Nacelle

2.8.3.5.1.9. Horizontal Stabilizer

2.8.3.5.1.10. Left Vertical Fin

2.8.3.5.1.11. Right Vertical Fin

2.8.3.5.1.12. Wing Center Panel

2.8.2.5.1.13. Left Outer Wing Panel and type

2.8.2.5.1.14. Right Outer Wing Panel and type

2.8.2.5.1.15. Forward Main Fuel Foam (date replaced)

2.8.2.5.1.16. Aft Main Fuel Foam (date replaced)

2.8.2.5.1.17. Vent Fuel Foam (date replaced)

2.8.2.5.1.18. Main Wing Fuel Foam (date replaced)

2.8.3.5.2. Using the NLign program upload the information and deliver electronic file at time of induction process.

2.8.4. Preservation:

2.8.4.1. Remove A/C battery, store, maintain and perform capacitance check

IAW TO 8D2-3-1.

2.8.4.2. Defuel A/C and Purging/Draining of Fuel Cells/Tanks IAW TO 1A-10C-2-12JG-1 and

TO 1-1-3.

2.8.4.3. Preserve engines IAW TO 2J-TF34-101 Chapter 3 as required.

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2.9. GENERAL WORK REQUIREMENTS

2.9.1. Comply with urgent action, immediate action, and safety TCTOs which are due to rescind and are supportable with kits/parts (if applicable) that are outstanding or generated while the A/C is in work.

2.9.2. All A/C systems shall be returned to the using command in the same condition as received, or better as determined by USG acceptance inspection. The USG reserves the right to require the contractor to remedy these problems at the contractor’s expense before USG acceptance or at a later time if the defect is proven to be latent. Any item(s) missing or inoperable upon receipt, that is/are necessary to perform system checks, shall be installed for test purposes and removed prior to delivery, unless directed otherwise by the ACO. Missing Critical Safety Item will be replaced with items furnished by the using commands. System checks, if required, shall be accomplished as directed by TOs identified in Appendix 2.

Exceptions to the above paragraph are A/C requiring over water delivery routes. All required systems shall be made operational to the point of passing the system operational checks as specified in AFI 11-207.

2.9.3. Markings: The contractor shall be responsible for replacing all markings removed or otherwise affected during any maintenance task. Units will supply the required stencils for individual unit logos and any additional markings requested by AFTO Form 103. All markings shall comply with TO 1A-10C-23.

2.9.4. When aircraft components or equipment require shipment they will be packaged IAW the Special Packaging Instructions (SPI) developed for that specific component. SPIs are available at https://spires.wpafb.af.mil.

2.10. SPECIFIC WORK REQUIREMENTS

2.10.1. Depot Maintenance: After an A/C has been received and inducted into the depot facility, accomplish specific work requirements as specified by the task order. Specific work requirements for individual depot work packages are contained in Appendices 1 through 9 of this PWS.

2.10.1.1. Perform disassembly IAW applicable TO/maintenance manuals.

2.10.1.2. Recording of Defects: All noted defects which are not part of a project requirement shall be recorded in the affected A/C 781 series forms IAW TO 00-20-1. Any repaired defects should be annotated on the AFTO 95s and in the applicable Maintenance Systems

(MIS).

2.10.1.3. Corrosion Treatment and Painting: Treat corrosion IAW TOs 1-1-691 and 1A-10C-23. Painting shall be IAW TOs 1-1-691, 1-1-8, and 1A-10C-23 unless otherwise specified.

2.10.1.4. All panels, doors, and covers opened or removed for access or compliance with work requirements herein shall be reinstalled by the maintenance facility IAW applicable TOs.

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2.10.1.5. Functional Check: The contract depot maintenance facility shall accomplish an operational check of each disturbed system. Each disturbed system shall be repaired/adjusted to meet the operational parameters specified in the applicable A-10C A/C job guide manuals.

2.10.1.5.1. Operational tests of disturbed systems will be performed when support/test equipment becomes available.

2.10.1.6. Critical Safety Item Systems are:

1. All Flight Instrument and Standby Instrument Systems

2. All Engine Performance Instruments

3. Communication/Navigation

a. Head Up Display - (required for Low Altitude Safety and Targeting Enhancement System/Ground Collision Avoidance System (GCAS)/Autopilot)

b. Very High Frequency/Frequency Modulation Radio

c. Instrument Landing System

d. Embedded Global Positioning System/Inertial Navigation System (EGI) (required for GCAS)

e. Radar Altimeter (required for GCAS)

f. Ultra-High Frequency/Amplitude Modulation radio (Air Force/Navy/Airborne Radio

Communication (ARC) 164(V))

g. ARC-210 Radio #1 radio, ARC-210 Radio #2 if installed

h. Intercommunication (AIC 18)

i. Identification Friend-or-Foe (AN/APX 101)

j. Tactical Air Navigation (AN/ARN 118(V))

k. Control Display Unit

l. Multifunction Color Display

4. Egress System (Visual Check, by certified personnel)

5. Ground Safety Pin Assembly (pilot's emergency canopy release)

6. Pin, Ejection Seat Safety

7. Parachute (Visual Check)

8. Survival Kit (Visual Check)

9. Canopy Breaker Tool (Visual Check)

10. Circuit Breakers (Visual Check)

11. Auxiliary Power Unit

12. Oxygen Supply and Regulation

13. Pitot Heat

14. Lighting System

a. Landing

b. Taxi

c. Position

d. Strobe Anti-collision

e. Instrument and Cockpit

15. Flight Control System

a. Primary and Secondary Controls

b. Manual Reversion

c. Stability Augmentation System

d. Speed Brakes

e. Primary Trim Control System

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16. Environmental Control System

a. Cockpit Temperature Control (manual)

b. Canopy Defogging

c. Windshield Temp/Heat

d. Cabin Pressure

17. Fuel Quantity

18. Fuel Transfer and Vent System

19. Primary and Utility Hydraulic Pressure Indicating System

20. Normal and Anti-Skid Wheel Braking System

21. Nose Wheel Steering

22. Landing Gear Retraction

23. Overheat and Fire Detection

24. Electrical Power Supply and Controls

25. Low Altitude Safety and Targeting Enhancement System

2.10.1.7. All non-safety of flight defects, reflected in the incoming A/C records or as listed on the AFTO Form 103 shall be corrected only when authorized by the ACO.

2.10.2. Depot Modification:

2.10.2.1. Accomplishment of depot level modifications will be performed as negotiated between the depot facility and ACO.

2.10.2.2. If an A/C is received for SSI that has not previously been modified with the TEMS re-wire, Pylon re-wire, or TCTO 1A-10C-544/553/554/555/604 but is not specified as a required task by the Task Order, notify the ACO for disposition.

2.10.2.3. When specified by the Task Order, comply with the Enhanced Wing Assembly (EWA) installation on scheduled A/C with TCTO 1A-10C-520 and applicable program guidance. Specific instruction is provided in Appendix 6 of this PWS.

2.10.2.4. When specified by the Task Order, install the following modifications, listed by current, applicable TCTO, as part of the Consolidated Modification Installation. This modification package may be installed as a stand-alone effort as determined by USAF requirements.

Negotiated TCTO:

2.10.2.4.1. TCTO 1A-10C-520 – Replacement of Wing Assembly with Enhanced Wing Assembly

2.10.2.4.2. TCTO 1A-10C-544 – Replacement of Upper Longeron Plates, Crown Skin Fuselage Repairs

2.10.2.4.3. TCTO 1A-10C-553 – Installation of Repair Straps at FS 405

2.10.2.4.4. TCTO 1A-10C-554 – Installation of Fuselage Fuel Cavity Drain Tube

Assemblies

2.10.2.4.5. TCTO 1A-10C-555 – Installation of Upper Longeron Repair Straps at FS 268

2.10.2.4.6. TCTO 1A-10C-604 – Replacement of Left Hand Lower Longeron, Hydraulic

Drive Fittings, and Associated Brackets

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2.10.3. TCTO Accomplishment:

2.10.3.1. Accomplish all TCTO’s specified by the Task Order. Individual TCTO accomplishment will be negotiated separately or accomplished as over-and-above. If missing (unaccomplished) TCTO’s are discovered on an A/C, submit an AFMC Form 202 and notify the ACO for disposition.

2.10.4. Additional Maintenance Requirements:

2.10.4.1. AFTO Form 103 defects shall be corrected when authorized by the ACO, as feasible, without negative impact to the A/C schedule. If authorized, repair shall be accomplished under over-and-above work procedures. For AFTO Form 103 requests requiring upfront parts support, owning unit shall supply such parts.

2.10.4.2. For A/C discrepancies not covered by the PWS and referenced documents the contractor shall annotate AFTO Form 781A IAW TO 00-20-1 and notify the ACO for disposition.

2.10.4.3. From time-to-time, the using unit may request that an A/C part be cannibalized from an A/C while it is inducted at the contract depot facility. When directed by the ACO, the contractor shall remove the requested part and ship to the requesting unit. If special packaging instructions are not provided or directed, the contractor shall be responsible for ensuring proper packaging to prevent damage. Coordinate with using unit to ensure a replacement part is received. Shipping, packaging, and work effort for component removal and reinstallation shall be accomplished under over-and-above work procedures.

2.10.4.4. From time-to-time, A/C may be inducted for stand-alone number I or II Phase Inspections that are not in-conjunction with SSI. Accomplish Phase Inspection

IAW TO 1A-10C-6.

2.10.5. Special Depot Requirements:

2.10.5.1. Drop-in Maintenance: From time to time, the USG may request to drop in additional A-10C for emergency repair and maintenance. To the extent feasible, based on the contractor's facilities and experience, the contractor shall accept such A/C for repair and maintenance. The contractor shall obtain prior authority for such inputs from the ACO. The ACO shall, provided funds are available, authorize such preliminary work sufficient for the contractor to develop and submit an estimate for completion of the required repairs or maintenance. When sufficient funding is available and the Procuring Contracting Officer (PCO) grants authorization for completion of the work, the ACO shall authorize completion of the work by issuance of a funded over and above work request. The over and above rates of the contract shall apply to all such work.

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2.10.5.2. Surge Requirements: When PACAF or CONUS based A-10 aircraft or aircraft assemblies (i.e. wings, nacelles) are inducted into the depot facility for emergency drop-in repair and maintenance, the contractor shall coordinate with the ACO and the A-10 System Program Office (SPO) to establish workload priorities for drop-in aircraft / assemblies and aircraft already in-work (i.e. SSI). The surge requirement should also extend to the local manufacture of structural components or other parts that may need to be manufactured as determined by the requirement. When directed by the ACO, the contractor shall, to the maximum extent feasible, increase production rate and / or capacity to accomplish drop-in and / or other over-and-above work requirements IAW the USG’s delivery schedule objectives / requirements. The contractor shall take efforts to minimize delays to the delivery schedule of aircraft already in-work. In addition, the ACO may direct surge operations to accelerate delivery of in-work aircraft and / or induct additional aircraft above and beyond the standard induction schedule. Surge requirements will be negotiated on a case by case basis and will be billed to the CLIN X017 (SURGE Requirement) of the contract.

2.10.5.3. Contract Field Team (CFT): The contractor shall have the capability to deploy a CFT off-site to accomplish depot-level maintenance separate from their primary facility in cases where an A-10 is not safe for flight or when a Task order is negotiated to accomplish A/C modifications off-site. Repairs of this type are primarily for the purposes of allowing for a one-time flight back to the main contractor depot facility or to accomplish modifications on an A/C already in work by the CFT. The USG will request a proposal from the contractor prior to issuing a Task Order for CFT services.

2.10.5.3.1. The AFLCMC/WWAE Engineering will make the determination if a repair will require a CFT.

2.10.5.3.2. The AFLCMC/WWA Program Manager shall notify the AFLCMC/WWAK contract negotiator, Defense Contract Management Agency (DCMA) ACO, and the contractor of the requirement via email.

2.10.5.3.3. The contractor shall acknowledge receipt of the requirement within two (2) working days to the DCMA ACO, the Program Manager, and the PCO (or his/her delegate).

If the contractor requires further information, the contractor shall send this request to the DCMA ACO prior to travel.

2.10.5.3.4. The contractor shall coordinate with the operational unit, AFLCMC/WWAE Engineering, Pacific Air Forces (PACAF) Functional Manager, Program Manager and DCMA ACO, as required, until all technical and logistical issues are resolved, understood and in hand.

2.10.5.3.5. The contractor shall then provide the ACO a detailed written work proposal.

The ACO will then provide written authorization to the contractor for the CFT to proceed.

2.10.5.3.6. The contractor shall coordinate a start work date with the PACAF Functional Manager, the operational unit, and owning MAJCOM with emphasis being to commence work as soon as possible. The contractor shall inform the ACO of the start work date.

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2.10.5.3.8. Any suggested additions, deletions, or deviations from written work proposal shall be coordinated in writing with the ACO prior to any changes taking effect.

2.10.5.3.9. Once the CFT work is completed, the contractor shall then provide the ACO the detail of cost incurred, in such a way that the ACO can approve and allow for the issue of the proper invoicing of said CFT work.

2.11. FINAL PROCESSING OF AIRCRAFT

2.11.1. Finishing:

2.11.1.1. The contract depot maintenance facility shall clean the exterior and interior of the A/C in those areas opened for access/rework. Remove all filings, chips, loose hardware, debris, and trapped moisture. Also remove any moisture which has been trapped in any of the lower compartments of the A/C.

2.11.1.2. Accomplish maintenance painting IAW TOs 1-1-691, 1-1-8, and 1A-10C-23.

2.11.1.3. Environmental sealing, shall be accomplished IAW TOs 1A-10C-3-1 and 1A-10C-2-

27MS-1

2.11.1.4. White Area Closure Sealing shall be accomplished IAW TO 1A-10C-2-27MS-1

2.11.2. De-preservation: De-preserve engines IAW TO 1A-10C-2-71JG-2 if required.

2.11.3. Servicing:

2.11.3.1. The contract depot maintenance facility shall service all systems IAW TO 1A-10C-

2-12JG-1.

2.11.3.2. The contract depot maintenance facility shall install serviceable battery IAW

TO 1A-10C-2-24JG-3.

2.11.4. Weight and Balance: Accomplish weight and balance IAW TOs 1A-10C-2-4JG-1, 1A- 10C-5, and 1-1B-50 when required.

2.11.5. Preflight: The contract depot maintenance facility shall accomplish preflight inspection IAW TO 1A-10C-6WC-5. Correct all Critical Safety Item and critical defects. All functional checks performed shall meet operational procedures contained in applicable job guide manuals.

2.11.6. Functional Check Flight (FCF): An FCF, if required, shall be accomplished IAW TO 1A- 10C-6CF-1. A USAF FCF pilot will be furnished by the individual unit. Unit must be contacted at least 10 working days prior to scheduling FCF to arrange for travel. Notify unit immediately of all changes to FCF schedule. Coordinate all FCF arrangements with the ACO.

2.11.7. Post Flight: Accomplish Post Flight Inspection IAW TO 1A-10C-6WC-5. Provide Oil Sample analysis and TEMS/ADR data to owning units as specified in paragraph 2.7.2.2 and 2.7.2.3.

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2.11.8. Preparation for Ferry:

2.11.8.1. Service all systems IAW TO 1A-10C-2-12JG-1.

2.11.8.2. Reinstall/replace all loose equipment received with A/C.

2.11.8.3. Accomplish preflight/post flight inspections IAW TO 1A-10C-6WC-5.

2.11.8.4. A/C will not be accepted for delivery with equipment/parts shortages that affect Critical Safety Item.

2.11.9. Forms Preparation: Complete the AF Form 2692 IAW AFI 21-103. Equipment removed/relocated shall be recorded on AF Form 2692. If applicable, annotate the A/C records to reflect the phase inspection that was accomplished.

2.11.10. For the outgoing configuration, record the serial numbers for A/C major structural components IAW Appendix 3: A-10C Structural Component Serial Number Verification and provide data IAW CDRL A/B/C/D/E/F/G/H/J/K 003.

2.12. OVER AND ABOVE WORK PROCEDURES

2.12.1. Prior to first A/C induction, the contractor shall work with the USAF A-10 SPO and the ACO to develop a comprehensive Over and Above Management Procedure mutually acceptable to the contractor and the USG. It is the contractor’s responsibility to ensure that this procedure is developed. The intent of this procedure is to minimize the response time to over and above work requests.

2.12.2. Any additional tasks directed to be accomplished beyond those tasks covered in the negotiated work packages will be handled under the over and above work procedures. All over-and-above work requests must be authorized by the ACO prior to accomplishment. The USG shall not be held liable for reimbursement for any unauthorized work tasks.

2.12.3. Cannibalization: If parts or component shortages will delay delivery of A/C, serviceable parts or components which are readily exchangeable may be removed from another A/C by cannibalization. The ACO must authorize all such actions prior to removal. Compensation shall be limited to extra man-hours associated with cannibalizing when the required parts cannot be supplied in a timely manner and work stoppage would occur. No compensation shall be made for labor hours required to effect original removal or replacement action, nor to remove a part which would have required removal during the normal rework process, nor cannibalization as a result of fault or negligence of the contractor.

2.12.4. USAF engineering or System Program Manager (SPM) dispositions requiring repairs/replacement beyond negotiated program requirements will funded through Over and Above procedures. All such repairs/replacements must be authorized by the ACO in advance.

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3. DATA

3.1. MAINTENANCE RECORDS, FORMS, AND PUBLICATIONS. The contract depot maintenance facility shall maintain the forms listed below as applicable, during the time the A/C is at the facility:

Form Number Form Title Directive

DD Form 365 Series Record of Weight and Balance TO 1-1B-50 and 1A-10C-5

AF Form 2692 Aircraft/Missile Equipment Property Record

AFI 21-103

AFTO Form 44 Turbine Wheel Historical Record TO 00-20-5-1-2 AFTO Form 95 Significant Historical Data TO 00-20-Series AFTO 781 Series Aerospace Vehicle TO 00-20-1

3.1.1. AFTO Forms 350: The maintenance facility shall prepare and process AFTO Form 350, Repairable Items Processing Tag, IAW AFI 21-101, Aircraft and Equipment Maintenance Management, and 00-20-2 Series Technical Orders.

3.1.2. Record on AFTO Form 95 IAW TO 00-20-1 and the applicable Maintenance System

(MIS)

3.1.2.1. Enter the induction date and flight hours (COT) for each aircraft into the depot. Enter dates that maintenance was performed and the serial numbers for the following components if removed from A/C whether it will be installed onto original A/C or not:

1. Wing Center Panel (WCP)

2. Left Hand (LH) Wing Outer Panel (WOP)

3. Right Hand (RH) Wing Outer Panel (WOP)

4. LH Nacelle

5. RH Nacelle

6. LH Vertical Fin

7. RH Vertical Fin

Enter dates that maintenance was performed and the serial numbers for the following components if installed onto A/C:

1. Wing Center Panel (WCP)

2. Left Hand (LH) Wing Outer Panel (WOP)

3. Right Hand (RH) WOP

4. LH Nacelle

5. RH Nacelle

6. LH Vertical Fin

7. RH Vertical Fin

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3.1.2.2.1. Use AFTO Form 95 and 781 series forms to document all engineering generated re-inspection requirements for any repair to include but not limited to; bushings, oversize of fastener holes, repair straps. This must include exact location of repair, oversized or bushed holes, layers affected, material used to make bushings and/or straps and size of bushings and/or straps.

Close loop on every AFMC Form 202 for each A/C. Engineering shall be informed and AFTO Form 95 shall be documented with geometry and dimension of final maintenance actions used to repair A/C. Do not use max allowable values from the AFMC Form 202 engineering disposition unless it was the actual final value used to repair the A/C. Include final size of hole prior to any cold work. The statement “prior to any cold working” does not imply cold working is required, only that reported diameters after cold work processes have occurred are not required. Include data about bushed holes, i.e. number of the hole and/or its location, layers bushed, bushing size and material, etc. Document the exact fastener holes that were cold-worked and what repair option was used. Document areas where blends were used and the remaining thicknesses after blending procedures.

NOTE: AFTO Form 95s are required for each serialized component.

3.1.2.2. Each white area inspection completed by the contract depot maintenance facility shall be recorded to include the date, reason, and time of entry and closing.

3.1.2.3. Entries shall be made in the A/C records of date of paint Removal/repainted.

3.1.2.4. Entries shall be made for any maintenance accomplished IAW TOs 00-20-1, Aerospace Equipment Inspection, Documentation, Policy and Procedures and 00-20-2, maintenance Data Documentation.

3.1.2.5. Results of cabin pressurization testing will be annotated.

3.1.3. Record A/C major structural components IAW TO 1A-10C-36 Chapter 7. The data will be delivered to the A-10 ASIP Office using the NLign Program IAW CDRL A/B/C/D/E/F/G/H/J/K 003. C o m p o n e n t i n f o r m a t i o n shall be completed and sent for both incoming inspection and outgoing forms preparation. Incoming information shall be delivered no later than (NLT) 30 days after A/C induction to allow for ASIP review. Copies of the outgoing form shall be delivered to the gaining unit as part of the A/C documentation.

3.2. REPORTING INSTRUCTIONS:

3.2.1. Material Deficiency Reporting: The contract depot maintenance facility shall submit Material Deficiency Reports and Production Quality Deficiency Report (PQDR) IAW TO 00-35D-

54. Deficiency reports shall be submitted IAW CDRL A/B/C/D/E/F/G/H/J/K 006, Deficiency Report, and CDRL A/B/C/D/E/F/G/H/J/K 007, Teardown Deficiency Report.

3.2.2. AFTO Form 22: When inadequacies are found to exist in technical publications or engineering data specified herein, they shall be reported on AFTO Form 22, Technical Manual (TM) Change Recommendation and Reply, IAW TO 00-5-1. Reports shall be submitted IAW CDRL A/B/C/D/E/F/G/H/J/K 008, Technical Order Improvement Report.

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3.2.3. USAF Engineering Data Deficiencies: Whenever deficiencies are found on drawings or other engineering data provided, an AFMC Form 202 shall be submitted to USAF engineering.

For all other deficiencies in USG provided data including illegible, inconsistent, defective, non-usable, late, or otherwise non-delivered information that will prevent the contractor from proceeding with work, submit a deficiency report IAW CDRL A/B/C/D/E/F/G/H/J/K 009, Government Furnished Information Deficiency Report.

3.2.4. The contract depot maintenance facility shall maintain a system for reporting maintenance and operational status of all possessed A-10C aircraft. Reporting procedures shall be IAW Air Force Material Command Instruction (AFMCI) 21-118 paragraph 5.2.4. All reports shall be submitted IAW CDRL A/B/C/D/E/F/G/H/J/K 010, Maintenance Data Collection Record.

3.2.5. IAW TO 1A-10C-36 Chapter 7, as part of the SSI program, the contract depot maintenance facility shall:

3.2.5.1. Aircraft Structural Integrity Program: It is the responsibility of the contract depot maintenance facility personnel to fully understand how to use the NLign program and the data capture requirements. A fully detailed description and example of the data capture process is available in TO 1A-10C-36 chapter 7, and Appendix 3 of the PWS. For questions regarding data submission, contact A-10 ASIP Office via e-mail to HILL.A10.ASIP@US.AF.MIL

3.2.5.2. Using the NLign program, the contractor will provide the following information to SPO ASIP Engineering. NLign is to be used as the primary reporting system when sending data to SPO engineering.

3.2.5.2.1. Contractor will document the appropriate serial number for each serialized component inspected.

3.2.5.2.2. Contractor will document the incoming initial and pre-cold work “crack like” clean-up of oversized diameter holes, crack direction and affected layer/layers for all numerically labeled holes. The holes are uniquely identified and documented on the SSI illustration sheets. Diameter and crack direction data is required for holes oversized to clear “crack like” defects.

3.2.5.2.3. Contractor will document the estimated length and direction of all “crack like” defects for each uniquely identified and documented surface scan inspection region.

3.2.5.2.4. At completion of SSI inspections export the completed inspection information to the A-10 ASIP office for approval.

3.2.6. Contractor Manpower Requirement:

3.2.6.1. In accordance with FY11 NDAA Section 8108, the Contractor shall report ALL contractor labor hours (including subcontractor labor hours) required for performance of services provided under this contract for the A-10 System Program Office via a secure data collection site. The Contractor is required to completely fill in all required data fields at http://www.ecmra.mil.

mailto:%20HILL.A10.ASIP@US.AF.MIL http://www.ecmra.mil/

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3.2.6.2. Reporting inputs will be for the labor executed during the period of performance for each Government fiscal year (FY), which runs 1 October through 30 September. While inputs may be reported any time during the FY, all data shall be reported no later than 31 October of each calendar year. Contractors may direct questions to the Contractor Manpower Reporting Application (CMRA) help desk.

3.2.6.3. Uses and Safeguarding of Information: Information from the secure web site is considered to be proprietary in nature when the contract number and contractor identity are associated with the direct labor hours and direct labor dollars. At no time will any data be released to the public with the contractor name and contract number associated with the data.

3.2.6.4. User Manuals: Data for Air Force service requirements must be input at the Air Force CMRA link. However, user manuals for government personnel and contractors are available at the Army CMRA link at: http://www.ecmra.mil.

4. TECHNICAL ORDERS (TOs) AND OTHER DIRECTIVES

4.1. TECHNICAL DATA:

4.1.1. The contract depot maintenance facility shall accomplish removal, disassembly, inspection, repair, replacement, adjustment, modification, test, assembly and installation of accessories and equipment shall conform to directives and supplements listed in Appendix 2-1 of this PWS.

4.1.2. The following order of precedence shall apply when conflicting requirements exist in the listed TOs and other directives shown in Appendix 2 – I. of this PWS:

1. USAF TOs and USG Specifications.

2. This PWS.

3. USG Approved Contractor Publications.

4. USG Approved Commercial Publications.

5. USG Approved Commercial Practices.

4.1.3. All existing or proposed structural repairs which do not conform to TOs 1A-10C-3, 1A- 10C-3-1, 16C1-30-10-3, 16C1-30-12-3, or the USAF approved engineering standards shall be submitted to…