1. QF-16 Engine Mgmt Agmt_Pass 6_FINAL.pdf
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- Attached to
- Aerial Targets III FY23
- Solicitation number
- FA489021R0012
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This memorandum of agreement outlines the roles and responsibilities for engine management and sustainment activities supporting the QF-16 Full Scale Aerial Target program. The agreement is between the Air Force Life Cycle Management Center, 53rd Weapons Evaluation Group, 848th Supply Chain Management Group, and the Propulsion Sustainment Division regarding the use of F100 and F110 engines on QF-16 aircraft. Key responsibilities include regenerating and providing engines to support QF-16 production quantities, coordinating engine repairs and transportation, developing engine plans and budgets, and ensuring parts availability. The agreement establishes concepts of operation for engine usage on QF-16 aircraft and defines engine requirements to support the program through fiscal year 2022.
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FOR OFFICIAL USE ONLY 1
QF-16 FULL SCALE AERIAL TARGET (FSAT)
ENGINE MANAGEMENT AGREEMENT
BETWEEN
PROPULSION SUSTAINMENT DIVISION (AFLCMC/LPS)
TINKER AFB, OK
AND
53D WEAPONS EVALUATION GROUP (53 WEG)
TYNDALL AFB, FL
848th SUPPLY CHAIN MANAGEMENT GROUP (848 SCMG)
TINKER AFB, OK
AIR FORCE LIFECYCLE MANAGEMENT CENTER (AFLCMC)
TEST AND TRAINING DIVISION (AFLCMC/EBY)
EGLIN AIR FORCE BASE, FL
VERSION 2.0
23 APRIL 2015
DISTRIBUTION E: Distribution authorized to the Department of Defense (DoD) Components only due to information requiring protection against premature dissemination and due to critical technology as of 18 Feb 2014. Other requests shall be referred to AFLCMC/EBYA, 207 West D Ave, Suite 214, Eglin Air Force Base (AFB), FL 32542-6844.
WARNING: This document contains technical data whose export is restricted by the Arms Export Control Act (Title 22, U.S.C., Sec 2751, et seq.)
Violations of these export laws are subject to severe criminal penalties. Disseminate in accordance with provisions of DoD Directive 5230.25.
DESTRUCTION NOTICE: Destroy by any method that will prevent disclosure of contents or reconstruction of this document.
FOR OFFICIAL USE ONLY 2
SIGNATURES
PAUL C. WAUGH, GS-15, DAF (Date)
Chief, Propulsion Sustainment Division
SCOTT L. WARD, Colonel, USAF (Date)
Commander, 53d Weapons Evaluation Group (WEG)
________________________________________________ 27 April 2015___
C. MCCAULEY VONHOFFMAN, Colonel, USAF (Date)
Chief, Systems Support Division, ACC/A4M
____________________________________________ ___3 June 2015__
ROD B. BLOKER, Colonel, USAF (Date)
Commander, 848th Supply Chain Management Group
MICHELE A. HAFERS, GS-15, DAF (Date)
Senior Materiel Leader, Test and Training Division
FOR OFFICIAL USE ONLY 3
RECORD OF PREVIOUS DOCUMENTS/CHANGES
Version Date Revision Reason for Change
1.0 18 Feb 2014 Initial
2.0 23 Apr 2015 1 Incorporate 848th Roles, Responsibilities
This document supersedes the MOA dated 6 Dec 2010 between EBY and 848 SCMG. Refer questions concerning this agreement to AFLCMC/EBYA, 207 West D Avenue, Suite 214, Eglin AFB, FL 32542-6853. This agreement will be reviewed on a bi-annual basis, with significant changes resulting in re-coordination and signature.
POINTS OF CONTACT
Organization Name Contact Info Phone AFLCMC/EBYA Mrs. Maria White
Materiel Leader maria.white.1@us.af.mil (850) 883-5381
DSN 875
AFLCMC/EBYA Mr. Kypp Wetmore Aerial Targets Chief EN kypp.wetmore@us.af.mil (850) 883-3397
DSN 875
AFLCMC/EBYA Mr. Stephen Pratt QF-16 Program Manager stephen.pratt.4@us.af.mil (850) 883-0413
DSN 875
AFLCMC/EBYA Mr. Kenneth Hislop QF-16 Operations PM kenneth.hislop@us.af.mil (850) 883-3367
DSN 875
AFLCMC/EBYA Mr. Larry Bates QF-16 Deputy PM lawrence.bates.4@us.af.mil (850) 883-3454
DSN 875
AFLCMC/EBYA Mr. Eric Alber QF-16 Financial Specialist eric.alber.1@us.af.mil (850) 883-0356
DSN 875
AFLCMC/EBYA Mr. Phillip N. Arnts QF-16 Engine Manager phillip.arnts.1.ctr@us.af.mil (850) 883-3047
DSN 875
53 WEG/CM Lt Col Tim Harbor Dep Commander, Maintenance timmy.harbor@us.af.mil (850) 523-2190
ACC/A5TT Mr. William (Kelly) Adams Chief, Test & Evaluation Branch william.adams.2@us.af.mil (757) 764-7597
DSN 574
ACC AMIC Mr. Keith Miller ACC O&M Prog Manager james.miller.137@us.af.mil (757) 764-9399
DSN 574
AFLCMC/LPSA Mr. Dewey Ezzell F100 Engine Manager dewey.ezzell.1@us.af.mil (405) 734-8719
DSN 884
AFLCMC/LPSB Neal Hollingshead F110 Engine Manager neal.hollingshead@us.af.mil (405) 734-4809
DSN 884
309 AMARG Michael Simpson QF-16 Workloader michael.simpson.23@us.af.m il
(520) 228-8649
DSN 228
ACC/A4MP Mr. Scott Holland ACC Engine Manager scott.holland.1@us.af.mil (757) 764-5142
DSN 574
SCMS/GUMA
Mr. Dave Barna Chief, F100 Engine Flight david.barna.1@us.af.mil
405) 734-8786
DSN 884
SCMS/GUMC
Mr. Steve Bailey Chief, F110 Engine Flight steven.bailey@us.af.mil (405) 736-3979
53 WEG Mr. Stephen Smith Unit Engine Manager stephen.smith.107.ctr@us.af.
mil
(850) 283-3091
DSN 523
mailto:William.Adams@langley.af.mil mailto:Dewey.M.Ezzell@tinker.af.mil mailto:david.barna.1@us.af.mil
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1.0 EXECUTIVE SUMMARY
The intent of this agreement between AFLCMC/LPS, 53 WEG, 848 SCMG, and AFLCMC/EBY (herein referred to as the “Program Office”) is to define and formalize the QF-16 Full Scale Aerial Target (FSAT) engine stakeholder responsibilities and establish a QF-16 concept of operations (CONOPS) and parts supportability for the F100 and F110 engine regeneration effort required to satisfy overall QF-16 program requirements. This agreement is effective upon the signature of all parties and will remain in effect for the duration of the QF-16 acquisition process or until dissolved as mutually agreed by all parties. This agreement is to be reviewed biennially, and any substantial changes will be re-coordinated for signature.
2.0 STAKEHOLDERS
2.1 Air Force Life Cycle Management Center (AFLCMC)/Armament Directorate (AFLCMC/EB) is responsible for cradle-to-grave management of United States Air Force (USAF) air-to-air and air-to-ground weapon systems. The Director of AFLCMC/EB is the AF Program Executive Officer (PEO) for Weapons, and reports to the Assistant Secretary of the Air Force for Acquisition (SAF/AQ) on acquisition matters.
2.2 Within the Test and Training Division (AFLCMC/EBY) is the QF-16 Program Office, and acts as the single point of contact for the development, procurement, and sustainment of QF- 16s for the USAF, US Navy (USN), and US Army (USA). The AFLCMC/EBY Senior Materiel Leader is designated as the System Program Manager (SPM) for the QF-16 Program, is responsible for the overall Operational Safety, Suitability & Effectiveness (OSS&E) certification of the QF-16, and reports directly to the AF PEO for Weapons.
2.3 The Aerial Targets Branch (AFLCMC/EBYA) is a subordinate branch of AFLCMC/EBY and is responsible for execution responsibilities of the QF-16 Full Scale Aerial Target.
2.4 The Propulsion Sustainment Division (AFLCMC/LPS) acts as the single manager for all propulsion sustainment issues within the USAF by providing support of assigned aircraft engines operated by the USAF and multiple foreign countries. AFLCMC/LPS has OSS&E responsibility and provides core life cycle management, program management, financial, contract and support for F100 and F110 series engines.
2.4.1 F100/TF33/F119/F117 Branch (AFLCMC/LPSA): Provides engine system logistics and sustainment support for F100 series engines.
2.4.2 F101/F108/F110/F118 Branch (AFLCMC/LPSB): Provides engine system logistics and sustainment support for F110 series engines.
2.5 The 53d Weapons Evaluation Group (53 WEG) (Operations) conducts the USAF air-to-air Weapon System Evaluation Program (WSEP), known as Combat Archer, and the Air Force air-to-ground WSEP, known as Combat Hammer. Unit personnel operate and maintain all USAF aerial targets that support Combat Archer and Title 10 testing.
2.6 The Air Combat Command (ACC) Systems Support Division (ACC/A4M), Propulsion Branch (ACC/A4MP) acts as MAJCOM point of contact for (53 WEG) engine retrograde and resupply requisitions.
2.7 412th Test Wing (TW) (Edwards AFB, CA): Provides engine repair, represervation, and regeneration capabilities for both F100 and F110 series engines.
2.8 183d Centralized Repair Facility (CRF) (Springfield Air National Guard (ANG), IL): Provides engine repair, represervation, and regeneration capabilities for F110 series engines.
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2.9 159th Maintenance Group (MXG) CRF (New Orleans ANG, LA): Provides engine repair, represervation, and regeneration capabilities for F100 series engines.
2.10 96 MXG (Eglin AFB, FL): Provides engine repair, represervation, and regeneration capabilities for the F100-PW-200D engine.
2.11 The 309th Aerospace Maintenance and Regeneration Group (AMARG) at Davis-Monthan AFB, AZ is a subordinate unit of the 309th Maintenance Wing at Hill AFB, UT and provides engine preservation (F110 only), and long-term storage of F100 and F110 series engines.
2.12 The 848th Supply Chain Management Group (848 SCMG) sustains weapon systems world-wide by providing Supply Chain Management life cycle support to include developing enterprise demand/supply plans, developing/implementing sourcing strategies, executing the supply plan, and executing cognizant design to meet customer requirements for assigned engines.
2.12.1 The 421st Supply Chain Management Squadron (421 SCMS) will plan requirements and procure AFSC-managed engine components for follow-on support of QF-16 F100 and F110 series engines.
3.0 ASSUMPTIONS
3.1 The Combat Air Forces (CAF) Mean Time Between Removal (MTBR) Rate is 500 cycles for F110-GE-100B engines and 400 cycles for F100-PW-220B/F engines based on a 4-quarter rolling average computed quarterly.
3.2 QF-16 flight hour expectations are anticipated to consist of approximately 95 percent manned flight hours, with the remaining 5 percent flown unmanned (Not Under Live Local Operator (NULLO)) based on current program projections. This expectation is subject to change in accordance with user requirements and funding availability.
3.3 QF-16 attrition is anticipated to start 1QFY16, with an eventual attrition rate of 22 per year.
This rate is directly correlated to the stand-down of the QF-4 fleet.
3.4 The post-delivery servicing Jet Engine Intermediate Maintenance (JEIM) business agreements will be coordinated between the 53 WEG, ACC/A4MP Command Engine Management Section and respective JEIMs.
4.0 CONCEPT OF OPERATIONS
4.1 F-16s will be regenerated at AMARG and then ferried to Cecil Field, FL for target modification. The modified aircraft will then be ferried to Tyndall AFB, FL and accepted via DD 250 by the USAF as QF-16 FSATs.
4.2 Block 15 and 25 Aircraft (F100-PW-220B/F and F100-PW-200D)
4.2.1 Block 15 and 25 aircraft require an F100-PW-220B/F for manned operations. These engines will be regenerated at a servicing JEIM location and then shipped to AMARG for installation into F-16s. The F100-PW-220 is not authorized for attrition; therefore, the F100-PW- 220 engine will be removed and replaced by an F100-PW-200D for NULLO operations.
4.2.2 F100-PW-100C engines will be converted into F100-PW-200D engines IAW TCTO (Time Compliance Technical Order) 2J-F100-971 at a servicing JEIM location and distributed to Tyndall AFB or Holloman AFB for installation in NULLO-designated QF-16s. F100-PW-200D
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engines are only authorized for unmanned missions. Figure 1 illustrates F100 engine CONOPS at Tyndall AFB, FL and Holloman AFB, NM.
Figure 1 F100 Engine CONOPS at Tyndall AFB, FL and Holloman AFB, NM
4.3 Block 30 Aircraft (F110-GE-100B)
Block 30 aircraft will require an F110-GE-100B for manned and NULLO operations. The Block 30 does not require an engine swap upon NULLO designation unless more than 600 Total Accumulated Cycles Remain (TACR) on the engine. If more than 600 TACR, the engine shall be swapped out with an on-site low cycle engine. Figure 2 illustrates F110 CONOPS at Tyndall AFB, FL and Holloman AFB, NM.
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Figure 2 F110 Engine CONOPS at Tyndall AFB, FL and Holloman AFB, NM
4.4 AFLMCM/LPS Engine Disposition Coordination. The 53 WEG will coordinate disposition of F100-PW-220 and F110-GE-100B (>600 TACR) engines removed for NULLO operations with ACC/A4MP and AFLCMC/EBYA. ACC/A4MP will offer AFLCMC/EBYA the first right of refusal for reutilization of these engines in future QF-16 production lots. The 53 WEG will be responsible for cost of shipping the engine to location as directed by ACC/A4MP.
4.4.1 Engines removed for NULLO operations and subsequently accepted by AFLCMC/EBYA for reutilization shall be shipped to a servicing JEIM as directed by ACC/A4MP within 15 days of removal.
4.5 Engine Spares
4.5.1 AFLCMC/EBYA will initially provide both Tyndall AFB and Holloman AFB three (3) engines each per engine configuration (F100-PW-220, F100-PW-200D, F110-GE-100B) for a total of nine (9) spares total at each location.
4.5.2 Due to the limited supply of F110 engines with greater than or equal to 900 TACR, there will be low cycle F110 engines available for Block 30 attrition. An F110 low cycle engine will be provided by the Program Office, as directed by the QF-16 Engine Manager, in coordination with the 53 WEG UEM. Deliveries will be based on scheduled NULLO modification start dates.
4.5.3 Engine spare sustainment will be the responsibility of the 53 WEG through individual agreements established with respective servicing JEIM locations.
4.5.4 Each Block 15 and 25 aircraft will have an F100-PW-200D engine ground transported to Tyndall AFB or Holloman AFB prior to a NULLO mission (kill authorization). The delivery schedule will be coordinated by the 53 WEG and AFLCMC/EBYA.
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5.0 SPECIFIC ROLES AND RESPONSIBLITIES
5.1 AFLCMC/EBY (through AFLCMC/EBYA) will:
5.1.1 Be responsible for the QF-16 Program to include all direct reporting and execution of program element (PE) 35116F to AFPEO/WP and SAF/AQP, as required.
5.1.2 Serve as the QF-16 Chief Engineer with overall engineering authority for the development and integration of the drone unique package for the QF-16 system.
5.1.3 Support all QF-16 engine specific TO requirements. Participate in TO development, certification, and verification of all QF-16 engine TOs.
5.1.4 Be responsible for the identification and accomplishment of required engine TCTOs prior to DD 250 of QF-16 aircraft to ACC. Engines delivered to 53 WEG will have at least 12 months useful life remaining before a TCTO would ground the engine. The 12-month life limit does not apply when TCTOs are fielded after a regenerated engine has been delivered to AMARG for aircraft installation.
5.1.5 Provide the 53 WEG initial bed down spares with high cycles remaining (>600 for F100 and >900 for F110). AFLCMC/EBYA will not deliver Block 30 aircraft with engines below 300 TACR (feasibility based on current inventory) unless a high-cycle engine was removed from an aircraft prior to attrition and is available to be installed in a newly delivered aircraft.
5.1.6 Provide a QF-16 Engine Manager to be the primary point of contact for engine related issues affecting QF-16 Program execution.
5.1.7 Provide technical support to Unit Engine Manager (UEM), as required.
5.1.8 Consult AFLCMC/LPSA (F100) and AFLCMC/LPSB (F110) for Engineering Dispositions for Nonconforming Technical Problems Beyond Published Authority (TO 00-25-107) for F-16 common support as requested.
5.1.9 Develop an engine regeneration schedule to include engine serial number selections, dates for regeneration, JEIM facilities performing maintenance, and engines requiring containerization once they are regenerated and preserved.
5.1.10 Function as a voting member of the F110 Maintenance Planning Working Group. The QF-16 Program has equal priority with the CAF as long as war-ready spares are categorized as “green”.
5.1.11 Coordinate with 53 WEG quarterly to obtain WSEP and weapons testing mission schedule to ensure -200D engines availability.
5.1.12 Provide funding for engine transportation until the asset is transferred to ACC via Comprehensive Engine Management System (CEMS).
5.1.13 Plan, program and budget adequate funding for the procurement, logistics support, and storage of uninstalled engines assigned to the QF-16 program (including required repair and maintenance of Government Furnished Property (GFP) to support QF-16 engine transfer requirements).
5.1.14 Develop and maintain 3 year engine production schedule and provide to LPSA and LPSB as requested.
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5.2 AFLCMC/LPS (through AFLCMC/LPSA and AFLCMC/LPSB) will:
5.2.1 Define, approve, document, and maintain the configurations for both the manned and unmanned QF-16 aircraft engines. AFLCMC/LPSA is responsible for F100 engines (F100-PW- 100/200D and F100-PW-220) and AFLCMC/LPSB is responsible for F110 (F110-GE-100B) engines.
5.2.2 Develop and maintain QF-16 engine build procedures for manned and unmanned aircraft engines.
5.2.3 Provide engine program office engineering technical support.
5.2.4 Communicate with ACC/A4MP and AFLCMC/EBYA to identify engines and earmark engines available for use on the QF-16 program.
5.2.5 Work with 421 SCMS to ensure all AFSC-managed components and parts for follow-on support of QF-16 engines are programmed and/or retained.
5.2.6 Provide sustainment support of QF-16 engines. Assist the QF-16 Program Office in identifying and submitting requests for retention of applicable F100 and F110 parts by maintaining an official parts retention list.
5.2.7 Retain engineering authority for QF-16 engine configurations and maintain OSS&E responsibility for these configurations.
5.2.8 Support AFLCMC/EBYA by providing necessary QF-16 engine documentation and information to support the overarching QF-16 OSS&E.
5.2.9 Assist the QF-16 Program Office in the development of applicable planning, programming, and budgeting requirements for the QF-16 program.
5.2.10 Participate in QF-16 Program Management Reviews (PMR) as requested.
5.3 53 WEG will:
5.3.1 Ensure O&M contract maintains requirement for an on-site UEM, ensuring best utilization of engines in accordance with the QF-16 engine management strategy. The UEM will perform engine management duties prescribed by AFI 21-101 Aircraft and Equipment Maintenance Management, TOs 00-25-254-1 and 00-25-254-2 CEMS Engine Management System Reporting Procedures.
5.3.2 Coordinate logistics of transporting engines to servicing JEIMs, manage engine swap outs matching engine TACR to life remaining on aircraft, manage scheduled/unscheduled maintenance, and coordinate with ACC/A4MP and AFLCMC/LPS for all engine disposition instructions.
5.3.3 In the event an engine becomes damaged by a foreign object (FOD) or is assessed as non-repairable at the organizational level, the 53 WEG will coordinate with the appropriate JEIM shop for the repair of the engine. Replenishment spares will be repaired using O&M funding.
5.3.4 Provide funding for engine transportation after engine transfer from AFLCMC/EBYA to ACC. The 53 WEG will pay transportation costs for retrograde engines shipped to servicing JEIMs for repair. If the engine is to be returned back to the unit, 53 WEG will pay for shipment of the engine from the servicing JEIM. When an engine is being dispositioned back to the QF-
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16 Program Office, the 53 WEG will only pay for transportation of the engine to the location as directed by ACC/A4MP.
5.3.5 When an unserviceable F100 or F110 engine is determined Not Repairable This Station (NRTS) or a serviceable engine requires shipment from the JEIM or unit to unit, utilize the following procedures: Obtain control number from ACC/A4MP. The unit will send an e-mail to ACC/A4MP Engine Management requesting engine disposition instructions. The supplied control number request document will include the following information: Unit, From (requester's name), Phone Number, Date, Engine Type, Engine Serial Number, Current Engine Operating Time, Time Remaining, and Detailed Discrepancy.
5.3.6 Report engine loss via CEMS upon target attrition and provide documentation to the appropriate Tinker AFB F100 or F110 engine inventory manager. The responsibility of the engine loss transaction and uploading of supporting documentation to the CEMS database will be performed by the operating base Stock Record Account Number (SRAN) engine manager or equivalent at the time of attrition. The transaction will finalize the life of the engine and include deletion from the USAF inventory.
5.3.7 Coordinate directly with AFLCMC/LPSA engineering on -200D trim issues (waiver requests) using the propulsion waiver template. Request a template from the following address:
AFLCMC.LPSA.LLO.Liaison@us.af.mil.
5.3.8 Coordinate with AFLCMC/EBYA to conduct a quarterly engine management review to ensure stock levels and production of -200D engines are adequate to meet demand.
5.3.9 Coordinate with AFLCMC/EBYA and request delivery of -200D engines or F110 low cycle engines 60 days prior to aircraft NULLO modification start date.
5.3.10 Be responsible for any engine TCTOs fielded after DD 250 of the QF-16 aircraft. The 53 WEG will utilize O&M funding for newly fielded TCTOs on all delivered engines.
5.3.11 Provide funding for trailer, hardback, and sway bracket transportation and maintenance after delivery and transfer from AFLCMC/EBYA.
5.4 848 SCMG (through 421 SCMS) will:
5.4.1 Plan requirement, procurement, and repair of Air Force managed components for sustainment of QF-16 F100 and F110 engines.
5.4.2 Ensure sufficient availability to include lead time of engine spare parts to support the engine regeneration schedule (Table 7.2).
5.4.3 Ensure sufficient availability of engine spare parts to support the operation and maintenance of 60 earmarked F100-PW-220s, and 128 F110-GE-100Bs through 2025.
5.4.4 The operational program for the 60 earmarked F100-PW-220 engines will be represented by newly established Program Execution (PE) Code 1144 Block 15/25 aircraft flying hours for use on NSNs applicable to the F100-PW-220 at 100% application.
5.4.5 The F100-PW-100C (-200D) is not an active USAF operational program. The F100-PW- 200D will be installed in QF-16 near the end of the aircraft life cycle, so no repair or generation of components is expected; therefore, no projection of requirements in D200 is necessary.
mailto:AFLCMC.LPSA.LLO.Liaison@us.af.mil
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6.0 FUNDING
6.1 AFLCMC/EBYA, with AFLCMC/LPS and 421 SCMS support, will support the POM process for QF-16 engine modification, refurbishment, and sustainment costs.
6.2 AFLCMC/LPSA and AFLCMC/LPSB will work with AFLCMC/EBYA, 53 WEG and other agencies as required in support of the POM process for QF-16 engine sustainment activities throughout the life cycle of the QF-16 program.
6.3 Personnel: Each organization will staff requirements for manpower authorizations to support this MOA through their applicable HQ for resourcing.
7.0 REQUIREMENTS
7.1 QF-16 production aircraft quantities are listed in Table 7.1 below and are based on the
FY16 PB.
Table 7.1 Overall QF-16 Production Quantities as of FY16 PB
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7.2 QF-16 Engine Requirements. The current QF-16 engine plan is shown in Table 7.2 below.
*NOTE: 5 each Navy funded aircraft will be added to Lots 4 & 5. Types Blocks TBD
Table 7.2 Overall QF-16 Engine Requirements
Notes/Assumptions:
1. -220 and -100B based on min. # of engines required to support Blk 15, 25, and 30 production aircraft quantities.
2. -200D based on sum of projected Blk 15 and 25 production aircraft quantities (1 ea. -200D required for each Blk15 and 25 NULLO mission.
3. Initial fielding of spares is 3 ea. -100B, -220, -200D at Tyndall AFB (Lot 1); 3ea. -100B and -220 at AMARG (Lot 1) and 3 ea. -100B, -220, -200D at Holloman AFB (Lot 3).
4. Allocation of -220s is limited to 60. Engines will be recycled to achieve program requirement of 112.
5. Allocation of F100-PW-100C (-200D) is limited to 140.
6. **IMPORTANT** Based on # of cycles needed (≥600 cycles for -220 and ≥900 cycles for -100B) vs. # of cycles available on QF-16 allocated engines is driving a larger quantity of engines required and/or increased regeneration costs to QF-16 program. F100 and F110 BSL draw downs and unknown condition of future engines will result in fluctuations of quantities listed in this table.
8.0 SUPPORT AGREEMENTS
8.1 The QF-16 Program Office has the following support agreements required for the execution of the QF-16 Program:
8.1.1 412th Test Wing (Edwards AFB, CA) Statement of Capabilities (SOC): Provides engine repair, represervation, and regeneration capabilities for both F100 and F110 engine configurations for the QF-16 Program. The SOC is dated 12 February 2014 and the period of performance is 1 September 2013 through 30 September 2015.
8.1.2 159th Maintenance Group CRF (New Orleans ANG, LA) Memorandum of Agreement (MOA): Provides engine repair, represervation, and regeneration capabilities for F100 engine configurations required for the QF-16 Program. The MOA is dated 16 June 2014.
8.1.3 183d Centralized Repair Facility (CRF) (Springfield Air National Guard (ANG), IL MOA:
Provides engine repair, represervation, and regeneration capabilities for F110 engine configuration required for the QF-16 Program. The MOA is dated 27 January 2014 and the period of performance is through 27 January 2023.
8.1.4 96th Maintenance Group (Eglin AFB, FL) SOC: Provides engine repair, represervation, and regeneration capabilities for the F100-PW-200D engine configuration required for the QF- 16 Program. The period of performance for the SOC is 1 October 2014 through 30 September 2018.
QF-16 Lot 1 2 3 4 5 6 7 8 9
Engine Deliveries Complete FY14 FY15 FY16 FY17 FY18 FY19 FY20 FY21 FY22 Totals
GE Engines (F110-GE-100B)
BLK 30 Prime Engines 6 10* 12 15** 18** 14 13 13 17 118
Spares 7*** 3 10
Total Required 13 10 15 15 18 14 13 13 17 128
PW Engines (F100-PW-220)
BLK 25 Prime Engines 2 4 13 15** 16** 14 13 13 90
BLK 15 Prime Engines 5 10** 15
Spares 6*** 3 9
Total Required 13 14 16 15 16 14 13 13 114
PW Engines (F100-PW-200D)
BLK 15/25 Unmanned Engines 7 14 13 15 16 14 13 13 105
Spares 3 3 6
Total Required 10 14 16 15 16 14 13 13 111
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8.1.5 AMARG Service Level Agreement (SLA) and Engine Statement of Work (SOW) attachment: Outlines the overall F-16 regeneration effort for the QF-16 Program as performed by AMARG. This document is dated 3 June 2013 which covers the Lot 1 performance period.
An updated Lot 2 SLA is currently in coordination, projected to be signed April 2015.
8.1.6 OC-ALC/848 SCMG & OC-ALC/GKG MOA: Outlines engine and supply chain management responsibilities. The MOA is dated 6 December 2010.
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ACROYMNS
ACC Air Combat Command
AFLCMC Air Force Life Cycle Management Center
AFMC Air Force Materiel Command
AFSC Air Force Sustainment Center
AMARG 309th Aerospace Maintenance and Regeneration Group
AMIC Acquisition Management Integration Center
CAF Combat Air Forces
CEMS Comprehensive Engine Management System
CONOPS Concept of Operations
CRF Centralized Repair Facility
DAF Department of the Air Force
FOD Foreign Object Damage
FSAT Full Scale Aerial Target
GFP Government Furnished Property
JEIM Jet Engine Intermediate Maintenance
MOA Memorandum of Agreement
MTBR Mean Time Between Removal
NRTS Not Repairable This Station
NULLO Not Under Live Local Operator
O&M Operations & Maintenance
OSS&E Operational Safety, Suitability & Effectiveness
PEO Program Executive Officer
POM Program Objective Memorandum
PE Program Execution
PM Program Manager
PMR Program Management Review
SAF Secretary of the Air Force
SCMG Supply Chain Management Group
SECDEF Secretary of Defense
SOC Statement of Capability
SPM System Program Manager
SRAN Stock Record Account Number
TACR Total Accumulated Cycles Remaining
TCTO Time Compliance Technical Order
TW Test Wing
UEM Unit Engine Manager
USA United States Army
USN United Stated Navy
WEG Weapons Evaluation Group
WSEP Weapon System Evaluation Program
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