SOW for J85 Engine Repairs 10.08.26.docx

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DRAFT STATEMENT OF WORK FOR REVIEW: BQM-34S Engine Repair, Overhaul and Conversion
Solicitation number
RFI-N00019-242-25-076-SN
Issued by

About this file

This is a Statement of Work for J85 Engine Repairs related to a Department of the Navy Naval Air Systems Command draft solicitation for BQM-34S Engine Repair, Overhaul, and Conversion services. The Navy is releasing this SOW as a Special Notice (RFI-N00019-242-25-076-SN) to solicit industry feedback, questions, and recommendations prior to issuing a formal Request for Proposal. This is explicitly not a formal RFP, and the Government will not provide compensation for any information submitted in response to this notice.

Industry stakeholders are invited to review the SOW and submit all feedback, suggestions, and questions using a provided format to Contract Specialist Nikolas Kokolios (nikolas.a.kokolios.civ@us.navy.mil) or Contracting Officer Marianne Wild (marianne.g.wild.civ@us.navy.mil) no later than Friday, October 23, 2026, at 2:00 PM EST. All comments must reference the specific SOW page, section, and paragraph number being addressed. The draft SOW addresses engine repair, overhaul, and conversion requirements for BQM-34S engines, though the specific technical requirements, performance metrics, and contractual terms are contained within the referenced SOW document.

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STATEMENT OF WORK

FOR

J85 GENERAL ELECTRIC ENGINE

REPAIRS, OVERHAULS AND CONVERSIONS

08 October 2026 Prepared by:

PORTFOLIO ACQUISITION EXECUTIVE

FOR

AVIATION

AERIAL TARGETS PROGRAM OFFICE (PMX-208)

47123 BUSE ROAD

BUILDING 2272 PATUXENT RIVER MD 20670-1547

DISTRIBUTION STATEMENT D. Distribution authorized to the Department of Defense and U.S. DoD Contractors only: Controlled Technical Information December 2019. Other requests for this document must be referred to PMX-208, Portfolio Acquisition Executive for Aviation, Naval Air Systems Command, Patuxent River, MD 20670.Controlled by: Department of Navy Controlled by: NAVAIRSYSCOM; PAE- Aviation; PMX-208 CUI Category: Controlled Technical Information Distribution Statement D POC: PMX-208 Program Manager, 301-757-6812

Table of Contents

1. SCOPE1
1.1 Background1
2. REFERENCE1
3. REQUIREMENTS2
3.1 Program Management and Contract Status2
3.2 Government Furnished Equipment2
3.3 J85-GE-100A Repair2
3.3.1 J85-GE-100A Test, Teardown & Evaluation for Repair2
3.3.2 J85-GE-100A Repair Execution3
3.3.3 J85-GE-100A Performance Evaluation3
3.3.4 J85-GE-100A Preservation, Packaging & Return Shipment3
3.4 J85-GE-100A Overhaul3
3.4.1 J85-GE-100A Test, Teardown & Evaluation for Overhaul3
3.4.2 J85-GE-100A Overhaul Execution3
3.4.3 J85-GE-100A Performance Evaluation After Overhaul3
3.4.4 J85-GE-100A Preservation, Packaging & Return Shipment After Overhaul4
3.5 J85-GE-5 Repair and Conversion4
3.5.1 J85-GE-5 Test, Teardown & Evaluation for Repair and Conversion4
3.5.2 J85-GE-5 Repair and Conversion to J85-GE-100A Execution4
3.5.3 Performance Evaluation After Repair and Conversion4
3.5.4 Preservation, Packaging & Return Shipment After Repair and Conversion4
3.6 Quality Assurance Program4
3.6.1 Quality Control and Inspection Program4
3.7 Configuration Control5
3.7.1 Configuration and Data Management5
3.8 Program Protection5
3.8.1 Cybersecurity Maturity Model Certification Level5
3.8.2 Cybersecurity5
3.8.3 Operations Security5
3.8.4 Security Clearances5
4. ACRONYMS6
Appendix A,7
QEC Kit7

SCOPE

This Statement of Work (SOW) defines the requirements to perform repair, overhaul, and conversion of the J85-GE-5 and J85-GE-100A engines in support of the United States Navy (USN) BQM-34S Subsonic Aerial Target.

Background The BQM-34 Firebee Target was originally powered using a Continental J69 turbojet. When the Navy modernized the Firebee line in the mid-to-late 1980s, the J85-GE-100A was used. The J-85-100A engine is a modified variant of the J-85-5 engine. In general, the modification consists of removing the afterburner section, applying corrosion-resistant coatings to critical components, repositioning the accessory gearbox 180 degrees, fabricating new fuel and oil lines, and installing an inlet adapter ring and a non-afterburner exhaust cone. These modifications enable the J85-GE-100A engine to fit properly within the target nacelle while maintaining required performance and reliability. The J85-GE-100A provides the target with increased thrust up to 2,450 lbf, allowing the BQM-34S to operate at speeds up to Mach 0.9, reach altitudes up to 45,000 ft, and execute high-G maneuvers (up to 5G) to replicate modern tactical jet threats. The extra thrust also allows the BQM-34S to support heavier internal payloads.

The USN plans to procure a minimum of 100 new targets as part of the new production effort known as the BQM-34S Strengthen Target Inventory New Growth (STING) program. The STING program carries an inventory of J85-GE-100A and J85-GE-5 engines that require either repair, overhaul, and/or conversion.

REFERENCE

Unless otherwise noted elsewhere in the document, the latest version of the listed documents shall apply. When referenced document titles, revision letters, and dates of issue are omitted for brevity of reference, the short form reference shall be understood to be the specific issue identified in this section.

Number
Title
Date
01-J85-2
Intermediate Maintenance Manual, Turbojet Engine Model J85-100 Series
1 December 2019
PPC50
J85 Power Plant Change No. 50
TBD 2026
CMP I20800
Configuration Management Plan PMA-208 Aerial Target Systems
14 Mar 2023

REQUIREMENTS

Program Management and Contract Status The Contractor shall provide technical and administrative program management for quality, timely and cost-effective deliveries for all products/services ordered hereunder. The Contractor shall provide status reports in accordance with CDRL B001. These monthly reports shall include a schedule that delineates the planned schedule for all activities, events, and milestones associated with the tasks in this SOW. The schedule shall include programmatic and technical tasks and activities necessary to complete the work effort scoped within the SOW.

CDRL B001 - Contractor’s Progress and Status Report Government Furnished Equipment Engines provided under this contract shall consist of a complete J85-GE-100A or J85-GE-5 series engine, consisting of the following major components:

1. Air inlet section

2. Compressor section

3. Mainframe section

4. Combustion section

5. Turbine section

6. Exhaust section

7. Accessories section Every engine will have an Engine Logbook that shall remain with the engine to house maintenance repair records.

Two (2) J85-GE-100A Quick Engine Change (QEC) kits will be provided as Government Furnished Equipment (GFE) for use during testing of each J85-GE-100A engine. See Appendix A for itemized QEC. The J85-GE-100A QEC kits can be reused for each test.

All GFE will be delivered to the Contractor in reusable shipping containers. The Contractor shall return all GFE to the Government in the same reusable containers, properly packaged and secured.

J85-GE-100A Repair J85-GE-100A Test, Teardown & Evaluation for Repair The Contractor shall receive, induct, and perform a comprehensive Test, Teardown, and Evaluation (TT&E) on each Not-Ready for Issue (NRFI) J85-GE-100A engine, designated by serial number under this contract. The TT&E shall inspect hardware condition and identify the scope of work, parts/materials, labor hours, schedule, and total cost necessary to return the asset to Ready for Issue (RFI) condition in accordance with (IAW) Technical Manual 01-J85-2. The J85-GE-100A engines have an expected service life of 10 to 15 operating hours; all proposed repair actions must align with this operational limit. The Contractor shall document and deliver the TT&E findings and recommendations in accordance with CDRL A001.

CDRL A001 TT&E Results DI-NDTI-80809B NOT 3 J85-GE-100A Repair Execution Upon receipt of written approval and formal authorization from the Primary Contracting Officer (PCO), the Contractor shall furnish all labor, materials, tooling, support equipment, and test facilities necessary to execute the repair of each approved J85-GE-100A engine serial number IAW the accepted TT&E report and Technical Manual 01-J85-2. The Contractor shall add a repair record to the Engine Logbooks with the repair description and date.

J85-GE-100A Performance Evaluation After engine repair, overhaul, or conversion, the Contractor shall perform all quality inspections, balancing, a functional test, and performance evaluation – including test cell verification – to ensure operational compliance and repair quality. Testing shall be conducted IAW the ratings and limitations outlined in Technical Manual 01-J85-2 and sections 9-38 and Tables 9-7 and 9-8. The Contractor shall document and deliver a description of the work performed and the test results IAW CDRL A002 and in the Engine Logbook.

CDRL A002 Performance Evaluation Results DI-PSSS-80386A J85-GE-100A Preservation, Packaging & Return Shipment The Contractor shall prepare each RFI J85-GE-100A engine for shipment and long-term (more than 45 days) storage using the GFE storage container provided, and IAW Technical Manual 01-J85-2.

All containers shall be marked IAW MIL-STD-129.

J85-GE-100A Overhaul J85-GE-100A Test, Teardown & Evaluation for Overhaul The Contractor shall receive, induct, and perform a comprehensive TT&E on each NRFI J85-GE-100A engine marked for overhaul, designated by serial number under this contract. The TT&E shall inspect hardware condition and identify the scope of work, parts/materials, labor hours, schedule, and total cost necessary to return the asset to an RFI condition IAW Technical Manual 01-J85-2. The J85-GE-100A engines have an expected service life of 10 to 15 operating hours; all proposed overhaul actions must align with this operational limit. The Contractor shall document and deliver the TT&E findings and overhaul action recommendations in accordance with CDRL A001.

CDRL A001 TT&E Results DI-NDTI-80809B NOT 3 J85-GE-100A Overhaul Execution Upon receipt of written approval and formal authorization from the PCO, the Contractor shall furnish all labor, materials, tooling, support equipment, and test facilities necessary to execute the overhaul of each approved J85-GE-100A engine serial number IAW the accepted TT&E report and Technical Manual 01-J85-2. The Contractor shall add a repair record to the Engine Logbooks with the repair description and date.

J85-GE-100A Performance Evaluation After Overhaul Upon completion of a J85-GE-100A engine overhaul, the Contractor shall perform a performance evaluation IAW paragraph 3.3.3.

J85-GE-100A Preservation, Packaging & Return Shipment After Overhaul The Contractor shall preserve, package and ship the overhauled engines IAW paragraph 3.3.4.

J85-GE-5 Repair and Conversion J85-GE-5 Test, Teardown & Evaluation for Repair and Conversion The Contractor shall receive, induct, and perform a comprehensive TT&E on each NRFI J85-GE-5 engine, designated by serial number under this contract. The TT&E shall inspect hardware condition and identify the scope of work, parts/materials, labor hours, schedule, and total cost necessary to produce an RFI J85-100A engine IAW Technical Manual 01-J85-2 and PPC50. The J85-100A engines have an expected service life of 10 to 15 operating hours; all proposed repair actions must align with this operational limit. The Contractor shall document and deliver the TT&E findings and repair action recommendations in accordance with CDRL A001.

CDRL A001 TT&E Results DI-NDTI-80809B NOT 3 J85-GE-5 Repair and Conversion to J85-GE-100A Execution Upon written approval and formal authorization from the PCO, the Contractor shall furnish all labor, materials, tooling, support equipment, and test facilities necessary to execute the repair and conversion of each J85-GE-5 engine serial number IAW PPC50. The Contractor shall add a repair record to the Engine Logbooks with the repair description and date.

The Contractor shall perform the conversion and testing of the first converted unit in the presence of a Government Representative. This witnessed portion shall encompass PPC50 Sections TBD through Section TBD, concluding with the Performance Evaluation.

Performance Evaluation After Repair and Conversion Upon completion of the engine repair and conversion, the Contractor shall perform a Performance Evaluation IAW paragraph 3.3.3.

Preservation, Packaging & Return Shipment After Repair and Conversion The Contractor shall preserve, package and ship the converted engines IAW paragraph 3.3.4.

Quality Assurance Program The Contractor shall implement a Quality Assurance (QA) program that is compliant with the latest revision of SAE AS9100 Quality Management Systems – Requirements for Aviation, Space, and Defense Organizations. The Contractor shall flow down all applicable quality requirements to its suppliers and Subcontractors.

Quality Control and Inspection Program The Contractor shall implement an effective Quality Control (QC) and Inspection Program to ensure all products, services, and data delivered under this contract comply with all specified requirements.

Configuration Control Configuration and Data Management The Contractor shall conduct a Configuration and Data Management Program IAW CMP I20800 Configuration Management Plan PMA-208 Aerial Target Systems. The Contractor shall require Subcontractors to comply with the PMA-208 Configuration Plan.

Program Protection Cybersecurity Maturity Model Certification Level For the duration of the contract performance period, the Contractor shall enforce and maintain cybersecurity compliance with the NIST SP 800-171 Rev 2 standard through CMMC Level 2 self-assessments and participate in annual government-led assessments. The Contractor shall provide evidence of its current self-assessment and NIST SP 800-171 Rev 2 compliance status via email to the Technical Point of Contact (TPOC) upon request. The Contractor shall safeguard covered defense information in accordance with DFARS clause 252.204-7012. The requirements of DFARS clause 252.204-7012 and compliance with NIST SP 800-171 Rev 2 shall be flowed down to all applicable Subcontractors.

Cybersecurity The Contractor shall ensure appropriate protective measures are in place to safeguard Controlled Unclassified Information (CUI) processed, stored, or transmitted on the Contractor’s information systems. The Contractor shall report within 72 hours of discovery of any cyber incident that affects CUI processed, stored, or transmitted through the Contractor's information systems. The Contractor shall report cyber incidents to the DoD at https://dibnet.dod.mil. The Contractor shall preserve and protect data and information from all known affected information systems and all relevant monitoring or packet capture data for at least 90 days from the submission of the cyber incident report to allow DoD to request the media or decline interest. At DoD’s request, the Contractors shall provide DoD with access to additional information or equipment that is necessary to conduct a forensic analysis.

Operations Security The Contractor shall provide at all facilities an appropriate means of storage for controlled unclassified documents, equipment, and materials in accordance with Operations Security (OPSEC) requirements. The Contractor shall maintain the facility level OPSEC program in accordance with the Contractor’s existing OPSEC Plan and Government requirements to protect sensitive data. The Contractor is responsible for Subcontractor implementation of the OPSEC program requirements for this contract.

Security Clearances Performance of work under this contract will require access to sensitive (unclassified and controlled unclassified) information, systems and/or equipment. Specific Contractor personnel must be eligible to perform Non-Critical Sensitive work as defined by Secretary of the Navy Instruction (SECNAVINST) 5510.30C via the Non-National Industrial Security Program (Non-NISP). The Government’s Non-NISP requires specific Contractor personnel with a need to know to receive and maintain (e.g. self-reporting, foreign travel) a favorably vetted and adjudicated Tier-3 investigation by the Government Security Office and ultimately the Defense Counterintelligence and Security Agency (DCSA) Adjudication Vetting Services (AVS). The Government Security Office shall initiate the Contractor's electronic investigation questionnaire application (eAPP) and do a preliminary screening of the Contractor's eAPP and fingerprints for suitability and derogatory information prior to performance. The Contractor employee shall provide all requested information pursuant to the Privacy Act of 1974. Fingerprinting requirements for contractors located outside of the government security office’s local area shall be the responsibility of the Contractor.

The Contractor shall coordinate and ensure the provision of security badges required to allow Contractor personnel access to designated workspaces and materials; the Contractor shall comply with all applicable security requirements, abide by direction given by Military Police or other security personnel, and adhere to installation traffic laws.

ACRONYMS

Acronym
Definition
AVS
Adjudication Vetting Services (AVS).
CDRL
Contract Data Requirements List
CMMC
Cybersecurity Maturity Model Certification
CUI
Controlled Unclassified Information
DCSA
Defense Counterintelligence and Security Agency
DFAR
Defense Federal Acquisition Regulation Supplement
GE
General Electric
GFE
Government Furnished Equipment
IAW
In Accordance With
NRFI
Not Ready for Issue
OPSEC
Operations Security
PCO
Procuring Contracting Officer
PPC
Powerplant Change
QA
Quality Assurance
QEC
Quick Engine Change
RFI
Ready for Issue
SOW
Statement of Work
TT&E
Teardown, Test, and Evaluation
USN
United States Navy

Appendix A, QEC Kit

PART NUMBER
NOMENCLATURE
REQ QTY
124P524-1
SHROUD INSTALLATION
124P524-7
SHROUD-UPPER FWD ASSY
1
124P524-15
SHROUD-UPPER AFT ASSY
1
124P524-9
SHROUD-LOWER AFT ASSY
1
124P490-1
SUPPORT, SHROUD
7
53413-2118-SH
CLAMP
1
NAS6603-2
BOLT
24
AN960-10
WASHER
24
124P468-1
MOUNT INSTALLATION AFT
124P468-3
BEAM
2
124P468-5
HANGER
1
124P468-7
HANGER
1
6749CV-10-9
JUMPER, BONDING`
1
MS24665-302
PIN, COTTER
2
AN310-6
NUT
3
NAS1306-15D
BOLT
2
AN960C10L
WASHER
6
AN960-616
WASHER
2
AN960C10
WASHER
6
NAS620C10
WASHER
12
NAS1003-10A
BOLT
12
MS21043-3
NUT
6
124P468-9
MOUNT INSTALLATION AFT
NAS1306-15D
BOLT
1
AN960-616
WASHER
3
124P529-1
THROTTLE ACTUATOR INSTALLATION
124P529-1
ACTUATOR
1
124P542-1
KEY-WOODRUFF
1
124P526-1
BRACKET ASSY
1
124P540-1
BELLCRANK-ACTUATOR
1
124P528-1
BELLCRANK-FUEL CONTROL
1
124P527-1
ROD-ASSY
1
NA1581A3R3
BOLT
5
124P529-1
THROTTLE ACTUATOR INSTALLATION
AN4-7A
BOLT
3
AN3-11A
BOLT
1
NAS6603-8
BOLT
2
AN960-416
WASHER
6
MS21042L4
NUT
6
AN960-10L
WASHER
10
MS21042L3
NUT
3
NAS1352-06-16
SCREW
1
AN960-6L
WASHER
2
MS21042L06
NUT
1
124N387-3
PLATE INSTALLATION
124N387-9
PLATE ASSY
4
NAS517-3-5
SCREW
8
MS21042-3
NUT
8
124N387-5,-6,-7,-8
BLEED AIR DUCT ASSY
4
MS35276-260
SCREW
8
124E1216-1
WIRING HARNESS INSTALLATION
SDLA0002-1
IGNITION LEAD ASSY
1
124E1162-1
THERMOCOUPLE CABLE ASSY
1
124E361-7
ENG DISC TO ENG GRD WIRING HARNESS
1
124E360-7
BR,ENG DISC TO ENG ACCESSORIES WIRING HARNESS
1
124E337-7
PWR ELEC GEN TO EXT
1
124E359-7
BR PWR ELEC GEN TO EXT PWR RCPT
1
124E335-1
CONN,IGNITION DISC BRKT
1
MS20995C20
LOCK WIRE
AR
MS35207-264
SCREW
1
MS35207-263
SCREW
4
MS24693-S4
SCREW
4
MS21043-3
NUT
5
MS21042L04
NUT
4
NAS1149C0332
FLAT WASHER
5
MS21919WDG3
CLAMP
1
MS21919WDG18
CLAMP
1
MS21919WDG12
CLAMP
1
MS21919WDG6
CLAMP
3
124E1216-1
WIRING HARNESS INSTALLATION
MS21919WDG5
CLAMP
1
MS21919WDG10
CLAMP
3

MISC INSTALLATION COMPONENTS

124N388-1
BRACKET
2
124N388-3
SHIM
2
124P533-1
TIE DOWN FITTING
2
6752CV-2-13
JUMPER
1
6752CV-10-9
JUMPER
1
646110-40120 (ALT. 156R005-450120)
HOSE ASSY, OIL
1
601051K0244
HOSE ASSY, FUEL
1
359 1/2 -4D-0024
HOSE ASSY, DRAIN
1
12459-66-1
STARTER GENERATOR
1
MS9136-01
GASKET, STARTER GENERATOR
1
MS27196-12-16
GASKET, FUEL HOSE
1
STRYP5963-1
SEALANT
1 TUBE
MS9556-10
BOLT
6
NAS6604H6
BOLT
4
NAS6604H8
BOLT
4
MS20995C32
LOCKWIRE
3FT
MS21046C6
NUT
6
MS35266-59
SCREW
6
MS24693S272
SCREW
4
MS3506-267
SCREW
2
MS35206-248
SCREW
1
MS24694S56
SCREW
2
MS21042L3
NUT
4
MS21043-3
NUT
21
AN960C616L
WASHER
6
AN960-416
WASHER
8
AN960-10L
WASHER
4
RY500F2217
IDENTIFICATION PLATE
1

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