STATEMENT OF WORK (SOW)

F108 Turbine Assembly - Low Pressure Union Assemblies

MODULE #13/15 & 14 AIR FORCE & NAVY

REV. 3

PREPARATION DATE: 21 Nov 2025

PREPARING ORGANIZATION:

421st Supply Chain Management Squadron (SCMS)/GUMBA Air Force Sustainment Center (AFSC)

And

Air Force Life Cycle Management Center (AFLCMC)

F108 Technical Services Element (LPSBA)

TINKER AFB, OK 73145-3031

And

Navy E-6B FST Propulsion Engineering Team

Technical Element (Navy Code 45200) Tinker AFB OK 73145-3031

TABLE OF CONTENTS

Page

SECTION I

1.0 Introduction 2

1.1 SOW Updates 3

1.2 Quality System/Quality Assurance 3

1.3 Subcontractor and Vendor Management 3

1.4 Transition and Relocation Plan 3

1.5 Contractor Relocation 4

1.6 Safety 4

1.7 General Services and Material 4

1.8 Receiving 4

1.9 Disassembly 5

1.10 Remanufacture 5

1.11 Remanufacture Procedures 5

1.12 Remanufacture Deviations 9

1.13 Replacement Quality 10

1.14 Over and Above (O&A) 10

1.15 Schedule 10

1.16 Designated Engineering Representative Processes and Procedures 10

1.17 Parts Not Listed in the Illustrated Parts Catalogue 10

1.18 Re-installation of Life Limited Parts (LLP) 11

1.19 FAA Form 8130-3 11

1.20 Reference & Technical Manuals 11

1.21 Deficiency Report Investigation 11

1.22 Condemnation of Assets 11

1.23 Packaging and Handling 12

1.24 Preservation 12

1.25 Item Unique Identification (IUID) 12

1.26 Shipping and Transportation 13

1.27 Reporting 13

1.28 CAV AF CFM Reporting Requirements 15

1.29 Contractor Manpower Reporting 21

1.30 Document Storage 21

1.31 Contractor Identification to Government Employees 21

1.32 Mission Essential Services 22

SECTION II

2.0 GOVERNMENT PROPERTY 22

2.1 Government Furnished Material (GFM) 22

2.2 Government Furnished Property (GFP) 22

APPENDIX “A”

ACRONYMS 24

SECTION I

1.0 SCOPE

Introduction: This Statement of Work (SOW) defines the requirements necessary to ensure that delivered remanufactured F108-100 (CFM56-2B) Low Pressure Turbine Rotor and Frame Assembly Module 13/15 and Low Pressure Turbine Shaft Assembly Module 14, F108-200 (CFM56- 2A) Low Pressure Turbine Union of Assemblies Module and associated parts are restored as nearly as possible to original life expectancy consistent with Air Force (AF) and Navy requirements set forth or referenced herein per FAR22.1003-6 and 48 CFR§22.1003-6. Specifically, but not exclusive. This applies to the following National Stock Numbers (NSN) and Part Numbers (P/N):

LOW PRESSURE ROTOR AND FRAME ASSEMBLY MODULE #13/15 F108-100

(CFM56-2B)

Input P/N Output P/N Input NSN Output NSN

305-482-301-0 305-482-301-0 2840-01-229-5786PN 2840-01-229-5786PN

305-482-302-0 305-482-302-0 2840-01-229-5786PN 2840-01-229-5786PN

305-482-303-0 305-482-303-0 2840-01-229-5786PN 2840-01-229-5786PN

LOW PRESSURE ROTOR AND FRAME ASSEMBLY MODULE #13/15 F108-200

(CFM56-2A)

305-482-301-0- 305-482-301-0-2A

305-482-301-0-2A 305-482-301-0-2A

2840-01-484-3913PN

2840-01-484-3913PN

2840-01-484-3913PN

2840-01-484-3913PN

305-482-302-0 305-482-302-0-2A 2840-01-484-3913PN 2840-01-484-3913PN

305-482-302-0-2A 305-482-302-0-2A 2840-01-484-3913PN 2840-01-484-3913PN

305-482-303-0 305-482-303-0-2A 2840-01-484-3913PN 2840-01-484-3913PN

305-482-303-0-2A 305-482-303-0-2A 2840-01-484-3913PN 2840-01-484-3913PN

LOW PRESSURE TURBINE SHAFT ASSEMBLY MODULE #14 F108-100A

(CFM56-2B)

301-316-158-0 301-316-158-0 2840-01-189-2941PN 2840-01-189-2941PN

LOW PRESSURE TURBINE SHAFT ASSEMBLY MODULE #14 F108-200

(CFM56-2A)

301-316-158-0 301-316-158-0-2A

301-316-158-0-2A 301-316-158-0-2A

2840-01-483-8785PN

2840-01-483-8785PN

2840-01-483-8785PN

2840-01-483-8785PN

The Contractor shall perform remanufacture of engine components at a Federal Aviation Administration Part 145 facility rated for CFM56-2A and CFM56-2B engine components. Contractor shall have remanufacture capabilities to include appropriate technical data, documents and license agreements required to accomplish remanufacture of F108 Module 13/15 and Module 14. The Contractor is responsible for the remanufacture and scheduled delivery of a quality product.

1.1 SOW Updates: The Contractor shall provide updates and change recommendations to this SOW to the Procurement Contracting Officer (PCO) in writing (email is acceptable) but the Government shall maintain the SOW during the performance of this contract.

1.2 Quality System and Quality Assurance: Each F108 Module 13/15 and Module 14 shall be delivered to the Government defect free. Each F108 Module 13/15 and Module 14 will be inspected by Defense Contract Management Agency (DCMA) at the contractor’s facility to determine serviceability and quality.

The Contractor shall maintain a system that adheres to the requirements of International Standard Organization (ISO) 9001.2015/ANSI/ASQC Q92 or AS9100, Quality Systems Model for Quality Assurance in Design/Development, Production, Installation, and Servicing and supplement requirements imposed by this contract. Develop and implement procedures to properly maintain measuring and test equipment IAW ANSI/NCSL Z540-1. The quality system will include a clear and complete set of work documents for all maintenance required by this contract. The Contractor’s quality program shall be designed to promptly detect and correct conditions adverse to quality.

1.3 Subcontractor and Vendor Management: The Contractor shall maintain a system for the management of subcontractors and vendors IAW the provisions of this contract. The Contractor shall ensure that the subcontractor(s)/vendor(s) data, designs, and deliverables meet all F108 Module 13/15 and Module 14 engineering and technical requirements and shall fulfill the requirements of this contract. The Government personnel shall be provided with the opportunity to attend all subcontractor reviews and other problem-solving reviews as observers.

1.4 Transition and Relocation Plan: The Contractor shall maintain and execute a transition plan detailing a ramp up/ramp down process that will not impact on-going remanufacturing processes and scheduled deliveries of assets per contract. This plan shall include transition strategies and shall describe facilities needed to support the deliverable modules, including the required manpower and skills to support the transition, and a schedule of the transition from roll-out to full operational status. Fully operational capability must be remanufactured per contract.

1.5 Contractor Relocation: The Contractor shall coordinate the relocation schedule with the PCO to ensure no conflicts exist. In the event of a relocation, the Contractor shall continue to provide support for the F108 Module 13/15 at the new location IAW this contract. The Contractor shall be responsible for the security of F108 Module 13/15 and Module 14 areas/equipment during relocation.

1.6 Safety: The Contractor shall maintain and execute a safety program using MIL-STD-882E, AFI 91- 301 and AFI 91-204 as guides. The Contractor shall comply with all safety provisions and technical specifications listed in CFM56 Engine Shop Maintenance Manual (CMM).

All Contractor personnel and technicians shall comply with system safety engineering principles during all levels of remanufacturing.

While performing work under this contract the contractor shall comply with all applicable federal, state and local regulations regarding occupational safety and health. The contractor shall notify the PCO within eight (8) hours of any damage to government property where the dollar value exceeds $500,000.00 and within two workdays, for any damage to government property less than $500,000.00 during the execution of the contract.

Mishap notifications shall contain, as a minimum, the following information:

a. Contract, Contract Number, Name and Title of Person(s) Reporting

b. Date, Time and exact location of accident/incident

c. Brief Narrative of accident/incident (Events leading to accident/incident)

d. Cause of accident/incident, if known

e. Estimated cost of accident/incident (material and labor to repair/replace)

f. Nomenclature of equipment and personnel involved in accident/incident

g. Corrective actions (taken or proposed)

h. Other pertinent information

If requested by the designated PCO, the contractor shall immediately secure the mishap scene/damaged property and impound pertinent maintenance and training records, until it is released by the Procuring Safety Office.

1.7 General Services and Material: The Contactor shall provide all materials for the remanufacture processes required to execute this contract, except for the Government furnished modules sent to the Contractor for remanufacture.

1.8 Receiving: The Contractor shall perform a visual inspection upon receipt for any shipping or packaging damage. The Contractor shall report all received F108 Module 13/15 and Module 14 that are misidentified, misdirected, incomplete or missing parts to the PCO in writing (email is acceptable) for disposition instructions. The Contractor shall also perform a visual inspection upon receipt of the asset using CFM56 Engine Shop Maintenance Manual (CMM) 72-54-XX and 72-56-XX. The Contractor shall not destroy reusable shipping containers and will reuse them for return shipment. In the event that a shipping container is no longer usable, the contractor will contact the PCO for disposition instructions. In addition, the contractor shall submit SDRs related to shipment of misidentified items, variations in quantity, non-requisitioned items, lost or damaged parcel post, and items in dubious condition. These discrepancies shall be reported and resolved using the DoD web-based application WebSDR, located at:

https://www.transactionservices.dla.mil/daashome/websdr.asp . This system of reporting an SDR has been developed in compliance with DoD regulations 4140.1-R, Supply Chain Material Management Regulation and 4000.25-M, Defense Logistics Management System (DLMS) Supply Standards and Procedures, which requires automated SDR processing. The Prime Packaging Specialist may authorize exceptions to these requirements

(CDRL A006).

1.9 Disassembly: The Contractor shall disassemble each Module 13/15 and Module 14 to expose hardware requiring remanufacture or replacement due to cause or life limits. The Contractor shall inspect and remanufacture or replace, as necessary to meet United States Air Force (USAF) build requirements – CFM56- 2B ESM 72-54 and CFM56-2B ESM 72-56 and United States Navy build requirements – CFM-56-2A Engine Ship Manual (ESM), all additional hardware exposed during disassembly.

1.10 Remanufacture: Upon completion of the incoming inspection, the Contractor shall restore the module to original life expectancy in compliance with all applicable CFM56-2B Engine Shop Manual (ESM) and Service Bulletin/Airworthiness Directive Requirements. The Contractor shall perform all inspections, replacement of parts, remanufacture, reassembly, adjustments, calibrations, USAF approved modifications, testing and operational checks, correct all discrepancies and malfunctions, and verify adequate and proper like new condition of any component, system, or subsystem.

1.11 Remanufacture Procedures: Low Pressure Turbine (LPT) Rotor and Frame Assembly, Low Pressure Turbine (LPT) Shaft Assembly and component parts shall be remanufactured IAW the procedures outlined in the CFM56-2A ESM, ESM 72-54-00 through 72- 54-20 and 72-56-00 through 72-56-10 and ESM 72-55-00. This also includes Standard Practice Manual CFMI-TP-SP.2.

Contractor shall acquire all component parts from Air Force approved vendors, Government inventory, Original Equipment Manufacturer (OEM) approved vendors, or commercial inventories approved by the USAF and/or OEM. Life Limited Parts (LLP) shall be new and unused from Air Force and/or Navy approved sources or remanufactured from Government inventory. New and unused non-LLP components shall be from Air Force approved vendors, Government inventory, or OEM approved vendors. Non-LLP used serviceable commercial components shall be from used commercial inventories acquired originally from an Air Force or OEM approved vendors.

Stage 1 blades that cannot be returned to fully serviceable and like new condition by the contractor shall be replaced with new manufactured (OEM) blades. Blades can be purchased by contractor from Fedmall. The anticipated quantity of Stage 1 blades to be replaced on Module 13/15 are 105 each for the Air Force engine module and 141 each for the Navy engine module.

The Contractor shall not acquire non-LLP used commercial parts from supplier sources that have been subject to any violation, penalty, or disciplinary actions leading to FAA disapproval of its aircraft, engine maintenance or operations. The Contractor shall provide FAA Form 8130-3 documentation or Certificate of Conformance for each used component in a module at time of module delivery.

For both the Air Force and Navy Module 14, the Contractor shall, as applicable, comply with the latest revisions of the https://www.transactionservices.dla.mil/daashome/websdr.asp

Service Bulletins identified below as well as with any outstanding FAA Airworthiness Directives. For the remanufacture of Module 14, replacement of the No. 4 bearing will not be included in the normal remanufacture requirement. If it is determined that replacement of the No. 4 bearing is needed, it will be funded separately as an Over and Above work request IAW

DFARS 252.217-7028.

1.11.1 Module 13/15 Air Force Requirement

The Contractor shall ensure all four stages of LPT blades are either brand new or fully restored to “as new” condition. Inspection serviceable limits are only sufficient if there is no corresponding repair attached to the inspection. “As new” condition is defined as blades that have had all remanufacture processes performed. All knife edges and Z-notches are restored to full remanufacture limits per Technical Order (T.O.) guidance. Blend repairs on the airfoils are allowed to restore to “as new” condition. All LPT blades fully restored to “as new” condition must meet the following pre-twist angle requirements:

Stage 1 minimum pre-twist angle = 2.07 deg Stage 2 minimum pre-twist angle = 2.55 deg Stage 3 minimum pre-twist angle = 3.50 deg Stage 4 minimum pre-twist angle = 4.70 deg

The Contractor shall ensure that all abradable honeycomb seals are replaced with newly manufactured abradable honeycomb seals on all delivered Module 13/15.

1.11.2 Module 13/15 Navy Requirement

Level of Inspection: Component parts removed from rotor and frame assembly shall be inspected to piece part requirements outlined for that specific part in accordance with CFM56-2 ESM.

Air Seals: Repair 001, LPT rotating air seals (72-54-06), Repair 001, LPT inner stationary air seals (72- 54-

09) and Repair 001, LPT outer stationary seals (72-54-12) are to be accomplished 100% to restore seals to unworn condition.

LPT Blades: The Contractor shall ensure all four stages of LPT blades are either brand new or fully restored to “as new” condition. Inspection serviceable limits are only sufficient if there is no corresponding repair attached to the inspection. “As new” condition is defined as blades that have had all remanufacture processes performed. All knife edges and Z-notches are restored to full remanufacture limits per Technical Order (T.O.) guidance. Blend repairs on the airfoils are allowed to restore to “as new” condition. All LPT blades fully restored to “as new” condition must meet the following pre-twist angle requirements.

All blades used must meet the following pre-twist angle requirements (The pre-twist angle requirements do not apply to new, unused OEM blades):

Stage 1 minimum pre-twist angle = 2.07 deg Stage 2 minimum pre-twist angle = 2.55 deg Stage 3 minimum pre-twist angle = 3.50 deg

Stage 4 minimum pre-twist angle = 4.70 deg

Three evenly spaced “cutter blades” shall be incorporated in each of stages 1 thru 3 IAW CFM56-2B Service Bulletin SB 72-0365 and CFM56-2A SB 72-0228.

The Contractor shall ensure that all abradable honeycomb seals are replaced with newly manufactured abradable honeycomb seals on all delivered Module 13/15.

Module Inspection: In addition to the component piece part inspections all Modules returned to the Government shall meet the inspection criteria established in T.O. Reference CFM56 Engine Shop Manual Task 72-00-54-200-001 D “Low Pressure Turbine Rotor/Stator and Shaft Module Inspection” specifically with respect to:

Navy CFM56-2A Special Requirement: If it has not already been done, re-identify the remanufactured/reconditioned Module 14 Assembly by adding “-2A” to the assembly part number to read 301-316-158-0-2A depending on the original P/N of the unit. Permanently mark assembly using CFM International authorized method or equivalent with a -2A after the assembly part number in the location allowed by the blueprint.

The CFM56-2A assets will be shipped with a statement on the FAA 8130-3 Form or Certificate of Conformance required in paragraph 1.20 that states that the Source of Repair (SOR) complied or did not comply with the service bulletins of this paragraph. It is understood that some service bulletins may not apply. If a service bulletin was not applicable, this is to be stated on the serviceable tag or FAA document.

The contractor shall use non-life-limited Navy CFM56-2A assets, to include Navy CFM56- 2A assets that can be remanufactured per contract. When Module 14 cannot be remanufactured per the contract time frame, the contractor shall inform the PCO and request a stated additional amount of time to complete the remanufacture. If Navy assets are not available to replace those that have been condemned, the only assets available are commercial assets; commercial assets may be used provided that they are from Navy approved vendors or OEM approved vendors and meet serviceable inspection criteria and are interchangeable without alteration per CFM56-2A Engine Manual.

1) Circumferential looseness of blades at tip-shrouds.

2) Pre-twist gaps such that adjacent interlocks do not touch.

3) Shingled or unlatched blade tip-shrouds.

Adjusting Sleeve Considerations: The Turbine Frame Assembly is matched with the Low-Pressure Turbine Rotor Assembly through No. 5 bearing adjusting sleeve. The replacement of Turbine Frame or of the No. 5 bearing support cannot be done without rework of the adjusting sleeve per CFM56, ESM 72-00- 03 (Refer to caution in 72-00-56-20 turbine frame removal) after removal and disassembly of the Module.

During removal the parts must be identified, and match marked for inspection and installation operations.

Navy CFM56-2A Special Requirement: If it has not already been done, re-identify the remanufactured/reconditioned Module 13/15 Assembly by adding “-2A” to the assembly part number to read 305-482-301-0-2A, 305-482-302-0- 2A or 305-482-303-0-2A depending on the original P/N of the unit. Permanently mark assembly using CFM International authorized method or equivalent with a

-2A after the assembly part number in the location allowed by the blueprint.

The CFM56-2A assets will be shipped with a statement on the FAA 8130-3 Form or Certificate of Conformance required in paragraph 1.20 that states that the Source of Repair (SOR) complied or did not comply with the service bulletins of this paragraph. It is understood that some service bulletins may not apply. If a service bulletin was not applicable, this is to be stated on the serviceable tag or FAA document.

The contractor shall use non-life-limited Navy CFM56-2A assets, to include Navy CFM56- 2A assets that can be remanufactured per contract. When a Module 13/15 cannot be remanufactured per the contract time frame, the contractor shall inform the PCO and request a stated additional amount of time to complete the remanufacture. If Navy assets are not available to replace those that have been condemned, the only assets available are commercial assets; commercial assets may be used provided that they are from Navy approved vendors or OEM approved vendors and meet serviceable inspection criteria and are interchangeable without alteration per CFM56-2A Engine Manual.

Measure and record the following Module 13 features on DD Form 1574 (Serviceable Tag-Material) and on the FAA Form 8130-3 or Certificate of Conformance that accompany the assets back to supply:

1) LPT Case diameter D: 34.476-34.484 (serviceable) or 34.4803-34.4838 (remanufactured)

2) LPT 1st Stage Shroud Support (un-installed) diameter B: 34.653-34.665 (serviceable) or

34.6614- 34.665 (remanufactured) and diameter C: 34.468-34.480 (serviceable) no remanufacture.

3) LPT 1st Stage Shroud Support Diameter B while installed on the LPT case.

All Modules returned to the Air Force will meet the inspection criteria established in T.O. Reference CFM56-2A and CFM56-2B Engine Shop Manuals Task 72-00-54-200-001-D, paragraph 3.E. LOW

PRESSURE TURBINE ROTOR/STATOR MODULE INSPECTION.

Component parts removed from rotor and frame assembly shall be inspected to piece part requirements outlined for that specific part IAW CFM56- 2B ESM. Re-installed components shall be upgraded to the latest configuration required in the latest revision of CFM56-2A and CFM56- 2B service bulletin manuals. Contractor shall comply with the latest version of the following CFM56- 2A and CFM56-2B Service Bulletins (SB). SB compliance shall be recorded on DD Form 1574 (Serviceable Tag- Material) and on FAA Form 8130-3 that accompany the assets back to supply. All outstanding FAA Airworthiness Directives shall also be incorporated. Specific Service Bulletins (SB) requiring compliance include, but are not limited to:

CFM56-2A SB 72-0020 Rework of Conical Rotor Support CFM56-2A SB 72-0144 Increase in height of the Abradable Honeycomb on Stage 1 Outer

Stationary Air Seal CFM56-2A SB 72-0180 Intro of New LPT Case Assy CFM56-2A SB 72-0228 Introduction of 3 New Blades with Hardened Teeth for Each Set of

Stages 1, 2 and 3 LPT Blades CFM56-2B SB 72-0277 Increase in Height of the Abradable Honeycomb on Stage 1 Outer

Stationary Air Seal

CFM56-2A SB 72-0338 Re-identification of Low-Pressure Turbine (LPT) Conical Supports and LPT Stub shafts (Air Directive 96-18-16)

CFM56-2A SB 72-0356 Anti-Rotation lock replacement rework/re-identification of Stage 2 and 3 Stationary Air Seal Segments

CFM56-2B SB 72-0365 Introduction of 3 New Blades with Hardened Teeth for Each Set of Stages 1,2,3 LPT Blades

CFM56-2A SB 72-0372 Re-identification of conical supports CFM56-2B SB 72-0389 Modification of T495 Bracket and Ring Sector CFM56-2B SB 72-0476 Reidentification of LPT Conical Supports and LPT Stub Shafts CFM56-2B SB 72-0496 Antirotation Lock Replacement/Rework/Re-ID Stg 2 & 3 Stationary Air

Seal Segments CFM56-2B SB 72-0525 Accident Involved Hardware CFM56-2A SB 72-0541 Turbine Frame (72-56-00) Rework of the Old LPT Frame Assy to permit the removal of the Oil Supply Tube Elbow Assy on wing CFM56-2A SB 72-0602 Replacement of suspect Stage 1 LPT blades 301-330-114-0 and 301-

330-115-0 CFM56-2B SB 72-0745 Replacement of Stage 1 LPT Blade 301-330-114-0 and 301-330-115-0

NOTE: Cycle time of blades are not tracked and therefore may not match that of the module. Blades affected by SB 72-0745 need to be replaced regardless of cycle time shown.

Incorporate the following Service Bulletins 100% (USAF):

□ 72-0185 LPT Shaft Assy - Introduction of New Center Vent Tube Support Assemblies

□ 72-0409 LPT Shaft Assy - Introduction of a Thicker Center Vent Tube

□ 72-0605 Low Pressure Turbine Shaft (72-55-00) - Introduction of New Center Vent Tube Supports

□ 72-0649 Low Pressure Turbine Shaft (72-55-00) - Introduction of New N°4 Roller Bearings with New Outer Race Material

Incorporate the following Service Bulletins 100% (USN):

□ 72-0275 LPT Shaft Assy - Introduction of a Thicker Center Vent Tube

□ 72-0464 Low Pressure Turbine Shaft (72-55-00) - Introduction of New Center Vent Tube Supports

□ 72-0507 Low Pressure Turbine Shaft (72-55-00) - Introduction of New N°4 Roller Bearings with New Outer Race Material

NOTE: Currently the above-mentioned Service Bulletins require compliance. Should, in the future, additional Service Bulletin(s) be released and required to return a Module 13/15 and Module 14 to like new condition they will be addressed on a case-by-case basis and may be incorporated in this SOW via contract modification.

1.11.3 Testing & Evaluation: The Contractor shall conduct all testing IAW CFM56-2B guidance.

Government reserves the right to witness any and/or all tests conducted by the Contractor and/or subcontractors on a noninterference basis.

1.12 Remanufacture Deviations: Prior to Contractor’s deviations in remanufacturing of Module 13/15 and

Module 14 or component parts, the Contractor shall obtain written approval for deviations from the PCO as outlined in ESM 72-54-00 through 72-54-020, 72-55-00 and 72-56-00 through 72-56-010, or Service Bulletin authorized modifications. Requests for Deviations (RFD) will be sent to the PCO from the contractor, and an Air Force or Navy Propulsion Engineer will review the request. If the deviation is approved the Contractor will receive a signed RFD from the PCO.

1.13 Replacement Quality: The Contractor shall ensure that materials, parts and accessories used in remanufactured components are restored to original life expectancy or nearly so and are interchangeable without alteration per CFM56-2A Engine Manual.

1.14 Over and Above (O&A): Contracts for the remanufacture of Government assets generally do not contain O&A work requirements except for missing components or for components damaged due to causes unrelated to the normal use of the end item. O&A work is defined as work that is within the general scope of the contract; is not covered by the line item(s) for the basic work under the contract; and is necessary to satisfactorily complete the contract. Requests for O&A work will be processed IAW DFARS 252.217-7028.

O&A work requests shall be negotiated through the ACO/PCO prior to O&A work being performed.

It is understood that for purposes of this requirement, the replacement of the LPT Module 14 #4 bearing is not included as part of the remanufacture requirement described in this SOW. If replacement of the Module 14 #4 bearing is necessary to return the asset to a “like new” condition, the replacement of the Module 14 #4 bearing will be considered O&A work and will be separately funded on the appropriate O&A CLIN IAW DFARS 252.217-7028. The contractor shall submit an O&A work request for replacement of the Module 14 #4 bearing and receive ACO/PCO approval prior to replacement of the Module 14 #4 bearing.

1.15 Schedule: Any changes to contractual milestones shall be made only with Program Office coordination and written approval of the PCO (email is acceptable). The Contractor shall meet the following delivery schedule:

Air Force Module 13/15 - 12 each every 30 days after receipt of asset(s);

Navy Module 13/15 - 1 each every 60 days after receipt of asset(s);

Air Force Module 14 - 7 each every 30 days after receipt of asset(s);

Navy Module 14 - 1 each every 60 days after receipt of asset(s).

Production or delivery problems which have developed, or are developing, and have the potential to stop, interrupt or impact the production or delivery of contract end items will be reported to the Program Management Office via the PCO within 1 business day.

1.16 Designated Engineering Representative (DER) Processes and Procedures: Prior to Contractor’s use in the remanufacturing of Module 13/15 and Module 14 or component parts, the Contractor shall obtain written approval from the PCO for all DER processes and procedures (email is acceptable).

1.17 Parts Not Listed in the Illustrated Parts Catalogue (IPC): The Contractor shall identify the use and/or reuse of any part not listed specifically in the CFM56-2A and CFM56-2B Illustrated Parts IPC to the PCO (email is acceptable) for Air Force and Navy Propulsion Engineering authorization.

1.18 Re-installation of Life Limited Parts (LLP): The Contractor shall ensure all LLPs that were removed for a required inspection are assembled back into the same rotor unless Air Force or Navy Engineering authorization has been granted. The Contractor shall check records to ensure specified life cycles have not been exceeded; Air Force part must have 3500 cycles (Build Policy) remaining for the CFM56-2B components. Navy part must have 3000 cycles (Build Policy) remaining to max life limit for the CFM56-2A components. When a part exceeds max life cycle limit or has insufficient life cycles remaining, the Contractor shall ensure the replacement part selected for that rotor has equal or greater life cycles remaining than all other component parts in that rotor assembly. A LLP removed from a USAF F108-100/CFM56-2B and Navy F108- 200/CFM56-2A assembly will not be replaced with a component/part that has operated in any configuration other than a USAF F108- 100/CFM56-2B engine and Navy F108-200/CFM56-2A engine. The remanufacture source should expect a 0.16% replacement rate for all LLP’s.

LLP parts will not be co-mingled with or replaced by repaired/reconditioned commercial parts from any other sources or fleets. The Contractor shall provide completed documentation with each F108 Module 13/15 and Module 14 assembly that has been remanufactured with the intent of returning this assembly to like new condition. The documentation shall have correct part number or assembly part number and serial number and work accomplished annotated. The Contractor shall list all service bulletins that were complied with during the remanufacture of F108 Module 13/15 and Module 14.

1.19 FAA Form 8130-3: The Contractor shall provide a completed FAA Form 8130-3, Airworthiness Approval Tag and/or Certificate of Conformance, with each remanufactured assembly or remanufactured component part used therein prior to acceptance by the Government. In item 13 (remarks), list CFM56- 2B/2A Service Bulletins applied in reworking a part or assembly to an authorized output part number.

(Example: CFM56-2B, SB 72-0365).

1.20 Reference & Technical Manuals: In execution of this SOW, the Contractor shall apply processes, tools, and products in accordance with (IAW) CFM56 Engine Shop Maintenance Manual (CMM) 72-54- XX, 72-55- XX 2B/2A and 72-56-XX, CFM56-2B Service Bulletins, CFM56-2B Engine Shop Manual 72-54- 00, 72-55-00 and 72-56- 00 through 72-56-10, and CFMI-TP-SP.2. All modules returned to back to the Government will meet the inspection criteria established in T.O. reference CFM56-2B Engine Shop Manual Task 72- 00-54-200-001- D Low Pressure Turbine Rotor/Stator Module – Inspection and must comply with Service Bulletin 72- 0365.

1.21 Deficiency Report (DR) Investigation: When the Government finds a discrepancy at acceptance inspection, a DR will be submitted, and the Contractor shall investigate and submit findings to include root causes and a corrective action against all DRs submitted to Contractor against items remanufactured by this contract which are reported to be defective (CDRL A005). Each DR will be processed IAW Technical Order (T.O.) 00-35D- 54, USAF Material Deficiency Reporting System, in a timely manner to meet suspense dates assigned by the action agency. Reference CDRL A005.

1.22 Condemnation of Assets

1.22.1 Air Force The Contractor shall condemn, at the Contractor’s facility, any F108 Module 13/15 and Module 14 component parts that do not meet current inspection limits. The Contractor shall process all condemned assets through Plant Clearance Automated Reutilization Screening System (PCARSS). The Contractor shall also provide Government quantities by P/N and NSN of reparable components condemned and annotate on AFMC Contract Depot Maintenance (CDM) Production Report via the Contract Data Requirements List (CDRL A002) DD Form 1423. The Contractor shall report all condemned F108 Module 13/15’s via AFMC CDM Production Report (CDRL A002), Monthly Production Report and Commercial Asset Visibility for Air Force (CAVAF) System (CDRL A001). Condemnations shall be reported to 421 SCMS/GUMBA, Air Force Sustainment Center (AFSC) to establish usage rates and cost planning.

1.22.2 Navy Condemnation of F108–200 Module 13/15 components that are classified as high-cost (all LLP components plus the turbine frame and turbine case) that do not meet inspection and/or remanufacture limits, shall be coordinated with Navy engineering prior to actual condemnation Component condemnation and scrap disposal shall be in accordance with (IAW) FAR 46.605 and FAR 45.606 as well as DFARS 252.245-7004, Reporting, Reutilization, and Disposal. Disposal shall be through the Defense Reutilization and Marketing Office (DRMO). Utilization of contractor’s internal scrap procedures may be approved after receipt and approval of the contractor’s plan or Standard Operating Procedures (SOP) for condemnation and scrap process.

All scrap disposal shall be IAW Defense Logistics Agency Demilitarization (DMIL) Code requirements with coordination through DCMA Plant Clearance Officer on SF 1424. The contractor shall provide the government quantities by P/N, NSN, and S/N of condemned F108-200 13/15 parts and annotate on Contract Depot Maintenance (CDM) Production Report CDRL A002 DD Form 1423.

Tracked Parts/Components that have a remaining life of less than 3000 Maj Cycles (Navy Build Policy – para 1.19) require disposition from Navy Propulsion Engineer. The Navy may elect to use components that are within a few hundred cycles of meeting the Build Policy requirements. In such instances the Navy will provide written authorization to use the affected item.

1.23 Packaging and Handling: The Contractor shall properly package the F108 Module 13/15 and Module 14 IAW Air Force Material Command (AFMC) Form 158, Packaging Requirements. The Contractor shall place a serviceable tag, Department of Defense (DD) Form 1574 inside the package along with the pump as well as another completed DD Form 1574 to the outside of the package. In addition, all marking and labeling of unit and shipping containers shall be IAW MIL-STD-129R, Department of Defense Standard Practice, Military Marking for Shipment and Storage. Use additional guidance for preparation and shipment IAW T.O. 00-20-1, 00-20-3, MIL-STD-2073-1, MIL-STD- 129R, AFPAM 24-237 and AFMAN 24-206. This contract does not allow for commercial packaging.

1.24 Preservation: The contractor shall not destroy reusable shipping containers and will reuse them for return shipment. Contractor is authorized to utilize shipping containers as received, i.e., missing or broken latches. Contractor will continue to band the containers utilizing metal strapping. In the event that a shipping container is no longer usable, the contractor will contact the PCO for disposition instructions.

Units shall be packed IAW with T.O. 00-85B-3 using Special Packaging Instruction (SPI) F000003XA6.

1.25 Item Unique Identification (IUID): The contractor shall follow the latest DoD instructions to install IUID compliant marks. TOs and drawings will be complied with for any component where direction is currently called out in the TO or drawings. Unless otherwise directed, the following Number Structure will be used as the IUID, in the order specified, in accordance with UII Construct #2 specified in MIL-STD-130N

Table IV “UII construct business rules and supplemental data”. This number shall be incorporated into the box label, affixed or attached to the exterior of the item packaging, and shall not be affixed or attached to the part itself.

Issuing Agency Code (IAC), Enterprise Identifier (CAGE Code, DUNs number or DODAAC), Original Part Number and Serial Number.

1.26 Shipping and Transportation: Contractor shall meet the delivery schedule as outlined in the contract.

Contractor shall ship or transport applicable deliverables as appropriate in order to have the deliverables available to support the customer’s operational requirements and in accordance with the contract’s delivery schedule. The contractor shall not destroy reusable shipping containers and will reuse them for return shipment.

1.27 Reporting: Contractor shall provide completed FAA Form 8130-3 (Airworthiness Approval Tag) and/or Certificate of Conformance documentation with each F108 Module 13/15 and its component parts that have been remanufactured with the intent of returning these assemblies or component parts to service. This documentation shall have part number, serial number, work accomplished, Service Bulletins complied with, on serviceable tag, DD Form 1574. The Contractor shall ensure that all reporting as specified under the following CDRL is accomplished:

A001: Commercial Asset Visibility Air Force (CAVAF) End Item Reporting A002: Contract Depot Maintenance (CDM) Production Report A003: Comprehensive Engine Management System (CEMS) Reporting A004: Interim Contractor Support (ICS) Parts Usage and Maintenance Data Collection Report A005: Acquisition and Sustainment Data Package (ASDP) Deficiency Report (DR) A006: Report of Shipping (Item) and Packaging Discrepancy A007: Counterfeit Prevention Plan (CPP) Report A008: Government Property Inventory Report A009: Production Surge Plan (DI-MGMT-80969)

A001: CAVAF End Item Reporting CDRL – Contractor shall input the data IAW CAV AF and shall not be waived. For CAVAF reporting, the Contractor shall submit Discrepancy Reports (SDRs) when required and IAW CDRL DD Form 1423-1and SOW 1.30.4.

A002: Contract Depot Maintenance (CDM) Production Report CDRL – Data IAW the CDM report shall not be waived. The report format Source: https://assist.dla.mil – Downloaded: 2016- 04—12T17:42Z (sample form attached to CDRL). Data totals shall be as of the end of each month. Contractor’s format with the same data elements as found on the CDM report may be accepted if approved through the PCO and IAW CDRL DD Form 1423-1.

A003: CEMS Reporting CDRL – Each Serial Number F108 Module 13/15 assembly is loaded into Comprehensive Engine Management System (CEMS) system and all part number changes must have documentation accomplished. The point of contact for verification of part numbers and serial numbers for the Air Force NSN: 2840-01-229-5786PN (CII: HF108E0/HF108G0) is Frederick Gonzales, Equipment Specialist,

(405) 734-5021, AFLCMC/LPSBA email: frederick.gonzales@us.af.mil. The point of contact for verification of part numbers and serial numbers for the Navy NSN: 2840-01-484- 3913PN (CII: HG108E0/HG108G0) is https://assist.dla.mil/ mailto:frederick.gonzales@us.af.mil

Raymond Thomas, Equipment Specialist, (405) 734-5002, AFLCMC/LPSBA email:

raymond.thomas.7@us.af.mil.

A004: Interim Contract Support (ICS) Parts Usage and Maintenance Data Collection Report CDRL – Contractor shall input data on the Data Collection Form, and this shall not be waived. Contractor must use provided format with all the data elements. Data shall be reported to 421 SCMS/GUMBA, Air Force Sustainment Center (AFSC), to establish usage rates and cost planning by email: matthew.koerner@us.af.mil.

In addition, the Contractor shall submit Supply Discrepancy Reports (SDRs) when required IAW the contract’s SOW. Contractor shall process DRs when required IAW Section 1.6 and 1.30.4 of this SOW.

A005: Acquisition and Sustainment Data Package (ASDP) Deficiency Report (DR) – As defined by T.O. 00- 35D-54, submit a report whenever a material or quality deficiency occurs using SF 368 or equivalent.

A006: Report of Shipping (Item) and Packaging Discrepancy – Contractor will use WEBSDR to submit an electronic SF-364 (Standard Form) IAW TO 00-35D-54 upon discovery of discrepancies for items of supply received for: overage, wrong item, duplication of shipment, misdirected shipment, nonreceipt, damage, and/or improperly packaged shipment.

A007: Counterfeit Prevention Plan (CPP) Report (DI-MISC-81832)

A008: Government Property Inventory Report CDRL – This shall not be waived. This report enables the contractor to a 100% inventory listing of Government Property (i.e., both Government Furnished Property (GFP) and Contractor Acquired Property (CAP)) in the contractor’s possession (to include subcontractors) by contract IAW CDRL 1423-1.

A009: Production Surge Plan (DI-MGMT-80969) – Once surge operations are determined to be necessary, are implemented and high demand items are identified as contract items, the contracting office will execute a surge clause to meet the contingency requirements SURGE OPTION (DEC 2018)

(a) General. The Government has the option to Increase the quantity of supplies or services called for under this contract by no more than 150 percent and/or accelerate the rate of delivery called for under this contract, at a price or cost established before contract award or to be established by negotiation as provided in this clause.

(b) Schedule.

(1) When the Capabilities Analysis Plan (CAP) is included in the contract, the option delivery schedule shall be the production rate provided with the Plan. If the Plan was negotiated before contract award, then the negotiated schedule shall be used.

(2) If there is no CAP in the contract, the Contractor shall, within 30 days from the date of award, furnish the Contracting Officer a delivery schedule showing the maximum sustainable rate of delivery for items in this contract. This delivery schedule shall provide acceleration by month up to the maximum sustainable rate of delivery achievable within the Contractor's existing facilities, equipment, and subcontracting structure.

(3) The Contractor shall not revise the option delivery schedule without approval from the Contracting Officer.

mailto:raymond.thomas.7@us.af.mil mailto:bradley.brist@us.af.mil

(c) Exercise of option.

(1) The Contracting Officer may exercise this option at any time before acceptance by the Government of the final scheduled delivery.

(2) The Contracting Officer will provide a preliminary oral or written notice to the Contractor stating the quantities to be added or accelerated under the terms of this clause, followed by a contract modification incorporating the transmitted information and instructions. The notice and modification will establish a not-to- exceed price equal to the highest contract unit price or cost of the added or accelerated items as of the date of the notice.

(3) The Contractor will not be required to deliver at a rate greater than the maximum sustainable delivery rate under paragraph (b)(2) of this clause, nor will the exercise of this option extend delivery more than 24 months beyond the scheduled final delivery.

(d) Price negotiation.

(1) Unless the option cost or price was previously agreed upon, the Contractor shall, within 30 days from the date of option exercise, submit to the Contracting Officer a cost or price proposal (including a cost breakdown) for the added or accelerated items.

(2) Failure to agree on a cost or price in negotiations resulting from the exercise of this option shall constitute a dispute concerning a question of fact within the meaning of the Disputes clause of this contract. However, nothing in this clause shall excuse the Contractor from proceeding with the performance of the contract, as modified, while any resulting claim is being settled.

1.28 CAV AF CFM REPORTING REQUIREMENTS: Contract Depot Maintenance (CDM) guidance for contractor technical responsibilities and reporting requirements of the Commercial Asset Visibility Air Force (CAVAF) system. CAVAF shall be the primary system of record for providing daily status of all Government owned assets located at contractor repair facilities. Reporting within CAV AF shall not be limited to end items subject to repair but are to include assets stored at a contractor Inventory Control Point (ICP). Any CAVAF system down-time will be identified on the CAVAF home page banner. Contractors are responsible for ensuring current User Guides are utilized by their CAVAF reporters. NOTE: Contractor User’s Guide may be accessed from the CAVAF Homepage.

1.28.1 CAVAF FAMILIARIZATION TRAINING: Familiarization training for CAVAF reporting will be requested by the contractor via the applicable ICP CAVAF system administrator (SA). For assistance, guidance or questions to specific contract transactions reporting requirements may be addressed to the CAV AF contract monitor (CM). ICP CAVAF (SA and/or CM) points of contact (See Contractor Responsibility Item #4).

1.28.2 CONTRACTOR RESPONSIBILITY: Contractor CAVAF reporting requirements shall be accomplished daily and/or within one (1) business day of a maintenance action occurrence IAW the applicable CAVAF CDRL and CAVAF system, version 8.0.1 or higher. Accurate and timely reporting of maintenance transactions into CAVAF is critical to the management of repair requirements and the management of world- wide asset distribution. Contractor shall ensure asset record in CAVAF is an accurate reflection of physical assets on hand at all times.

1.28.2.1 Each CAVAF reporter shall submit a completed System Authorization Access Request, DD Form 2875, per instructions within 10 days after contract award date. All DD Form 2875(s) shall be digitally signed. There “must be two CAVAF reporters” for the contractual reporting requirements to ensure there is no possibility of a lapse in reporting coverage.

1.28.2.2 User(s) shall complete initial DoD Information Assurance (IA) Cyber Awareness Challenge training and submit a course completion certificate with the DD Form 2875. IA Cyber Awareness Challenge course completion certification shall be accomplished annually.

Users shall access IA training on the Cyber Awareness Challenge website, under the Department of Defense Employees section, click hyperlink; “Launch New Cyber Awareness Challenge Department of Defense Version” using the following website:

http://iase.disa.eta/cyberchallenge/launchPage.htm

1.28.2.2.1 First time CAV AF users will email initial IA Cyber Awareness Challenge course completion certificates, AF Form 4394, AF User Agreement Statement, and completed DD Form 2875 to point of contact at applicable ICP (see item #4).

1.28.2.2.2 All following annual course completion certificates shall be completed before lapse in certification occurs and will be emailed to respective ICP identified in paragraph 4a, 4b, and 4c below.

1.28.2.2.3 Product Functionality Caution: To meet technical functionality requirements, this awareness product was developed to function with Windows operating systems (Window 7, VISTA, and XP), when configured correctly) using either the Internet Explorer (IE) or Firefox browsers. Users employing either OS or browser may experience difficulties and may not be able to complete the training or print the certificate of completion. They Cyber Awareness Challenge course completion is a contractual requirement, and the contractor must comply.

1.28.2.3 Reporters requiring the default password or password resets should contact their applicable ICP CAV AF System Administrator POC listed below:

1.28.2.3.1 Robins AFB, GA, call (478) 327-6602 or 327-6603, or send email request to:

406scms.cav.af.ar@us.af.mil

1.28.2.3.2 Hill AFB, UT, call (801) 586-3736, or send email request to:

420scms.cdm@us.af.mil

1.28.2.3.3 Tinker AFB, OK, call (405) 622-7325 or (405) 736-7329 or send email request to:

420.scms.tinker.cdm.workflow@us.af.mil

1.28.2.4 To access the CAVAF system, contractor and subcontractor reporters shall follow “initial log-in procedures” as prescribed within the Contractors User’s Guide.

1.28.2.5 Contractor shall ensure accountability of all Government Furnished Property (GFP) within their Enterprise Resource Planning (ERP) or Commercial Off- the-Shelf (COTS) system, which must be reported accurately for same GFP records within CAVAF at all times.

http://iase.disa.eta/cyberchallenge/launchPage.htm mailto:420.scms.tinker.cdm.workflow@us.af.mil

1.28.2.6 Contractual Induction-at-Risk of end items is prohibited on all contracts.

1.28.2.7 Contract/Delivery Order Closure Disposition– Government will provide disposition instructions to contractor’s reporter. Contractor shall begin shipping assets within 10 days of receiving government disposition instructions and have completed all shipping actions 30 days thereafter. Contractor shall be fully responsible to ensure all corresponding CAVAF reporting actions associated with disposition occur within one (1) business day of related shipment action.

1.28.2.8 All NSNs identified as Nuclear Weapon Related Materiel (NWRM) shall require contractor CAVAF reporting for production management to track and report NWRM end items in repair with Serial Number identification within one (1) business day for asset visibility and serial number tracking. When receipted, Contractor’s reporter shall capture each NWRM asset’s Serial Number when reparable is received. Contractors shall follow all NWRM management requirements outlined in AFI 20-110, NWRM Management, to include, but not limited to packaging, marking, labeling, storage, transportation and receipt of all NWRM assets, with emphasis on Positive Inventory Control (PIC) and records management by the contractor and government to assure compliance. The successful application of these procedures requires the full cooperation of all personnel associated with the storage, shipping, transshipping and receiving of all NWRM assets.

1.28.3 SPECIFIC CAVAF CONTRACTOR TRANSACTIONAL REPORTING REQUIREMENTS:

1.28.3.1 “Not-on-Contract” (NOC) receipt transactions apply to assets which are associated to a contractor facility DoDAAC and not an active contract delivery order. Regardless of asset condition code status, Not-on-contract shall be used for the following reporting actions:

1.28.3.2 Discrepancy Items – Are identified as misrouted shipments, misidentified shipments, or damaged end items. Contractor’s reporter will verify resolution weekly to acquire resolution to discrepancy within 30-days of receipt transaction. The contractor shall comply with disposition instructions provided by the Government within 10-days and complete all associated reporting actions within same period. Contractor reporting actions shall be resolved using reversals of individual record control document numbers (RCDN) or may be accomplished utilizing a ‘bulk’ shipment action of RCDN.

1.28.3.3 Inventory Control Point Items – are identified as…