Att_(1)_PWS_Highlighted.pdf

PERFORMANCE WORK STATEMENT

FOR

DEPOT-LEVEL REPAIR

OF

NAVAIR

KC-130J QUICK ENGINE CHANGE ASSEMBLIES

(AE2100D3 ENGINES)

13 September 2016

Solicitation Number N00019-16-R-0013

Approved by:

DISTRIBUTION STATEMENT A. Approved for public release

Performance Work Statement

PWS REVISION HISTORY

Original Draft…………………………………………………………………………………… 20 January 2015

Final ………………………………………………………………………………………………13 September 2016

Table of Contents

PWS REVISION HISTORY

1.0 SCOPE

1.1 Weapon System Description and Use

1.2 Support Concept

1.2.1 Operational Concept

1.2.2 Maintenance Concept

2.0 APPLICABLE DOCUMENTS

2.1 Government Documents

2.2 Kuwait Air Force Specific Documents

2.3 Other Documents

3.0 GENERAL REQUIREMENTS

3.1 Quality Management System

3.2 Operations Security

3.3 Project Management

3.3.1 Project and Risk Management

3.3.2 Project Manager

3.4 Hazardous Material and Waste

3.5 Package, Handling, Shipping, and Transportation

3.5.1 Shipping, Packaging, Storage, and Containers

3.5.2 Government Furnished Property Shipping

3.6 Export Control Licenses

3.7 Engine Transaction Reporting

3.8 Information Assurance

4.0 PROJECT REQUIREMENTS (CLINs 0X01 and 0X02)

4.1 Management Plan

4.2 Meetings and Reviews

4.2.1 Post-Award Conference

4.2.2 Project Manager

4.2.3 Agenda

4.2.4 Meeting Minutes

CDRLs A003, AA03, AB03, AC03, and AD03

4.3 Airworthiness and Configuration Management

4.3.1 Airworthiness Certification Authority

4.3.2 Configuration Changes

4.3.3 Technical Variances and Deviations

4.4 ENGINEERING INVESTIGATIONS AND TECHNICAL SERVICES (CLIN 0X19)

5.0 GENERAL REPAIR REQUIREMENTS

5.1 Repairs

5.1.1 QECA Repairs

5.1.2 Repair Materials

5.1.4 Work Performed Records

5.1.5 Engine Disks

5.1.6 Repair Action Report

5.1.7 Life Limited Components

5.1.8 Storage

5.1.9 Property Control

5.1.10 Preservation

5.1.11 Monthly Preservation Tasks

5.2 Security of Government Property

5.3 Cannibalization

5.4 Condemnation

5.5 Disposition of Material

6.0 INDUCTION, DISASSEMBLY, AND ASSEMBLY OF THE QECA (CLIN 0X03)

6.1 Receipt of QECAs

6.1.1 Receiving Inspections

6.1.2 Engine Transaction Reports

6.2 Processing of QECAs

7.0 QECK REPAIRS (CLINs 0X04, 0X05, 0X06, and 0X07)

7.1 Categorize Repair

7.2 Repair

7.3 Deviation Requests

8.0 POWER SECTION REPAIR (CLINs 0X08, 0X09, 0X10, 0X11, 0X12, and 0X13)

8.1 Categorize Repair

8.2 Repair

8.3 Reassemble

8.4 Operational Test

9.0 PROPELLER GEARBOX AND GEARBOX MOUNTED ACCESSORY DRIVE REPAIR (CLINs 0X14 and 0X15)

9.1 Categorize Repair

9.2 Repair

9.3 Operational Test

9.4 Request Disposition

10.0 ADDITIONAL REPAIRS (CLINs 0X16, 0X17, and 0X18)

10.1 Radiological Control

10.2 Engine Reassembly (CLIN 0X17)

10.3 QECK Reassembly (CLIN 0X18)

11.0 Shipping (CLINs 0X20, 0X21, 0X22, and 0X23)

11.1 Shipping Requirements QECAs and PGBs

APPENDIX A: KC-130J QUICK ENGINE CHANGE ASSEMBLY (QECA) SYSTEM DESCRIPTION

APPENDIX B: PROJECTED UTILIZATION RATES

APPENDIX C: METRICS

2.0 METRIC DEFINITIONS

2.1 QECA Repair Turn-Around Time

2.2 PGB and GMAD Turn-Around Time

2.3 RADCON Survey Turn-Around Time

APPENDIX D: APPROVED OEM SERVICE BULLETINS

1.0 RECEIPT AND PROCESSING

2.0 QECA REPAIRS - INDUCTION

3.0 CORE ENGINE TEARDOWNS

APPENDIX F: LIST OF ACRONYMS

1.0 SCOPE

This Performance Work Statement (PWS) defines the effort required for the Contractor to provide depot-level repair of KC-130J Quick Engine Change Assemblies (QECA) for the Naval Air Systems Command (NAVAIR) KC-130J aircraft utilized by the U.S. Marine Corps (USMC), U.S. Navy (USN), and NAVAIR-managed Foreign Military Sales (FMS) cases.

1.1 Weapon System Description and Use

The KC-130J aircraft performs USMC, USN, and Kuwait Air Force (KAF) peculiar mission requirements such as in-flight refueling for fixed and rotary wing aircraft, rapid ground refueling, and other tactical capabilities. The KC- 130J aircraft QECA consists of the Rolls-Royce AE2100D3 turboprop engine and the Lockheed Martin Quick Engine Change Kit (QECK). Additional descriptions of the propulsion system are outlined in Appendix A, KC- 130J Quick Engine Change Assembly (QECA) System Description.

1.2 Support Concept

This PWS details the QECA depot repair requirements and engineering and technical services required to meet the operational concept, maintenance concept, and support dates as defined herein with the repair capability meeting the Government’s annual engine operating hours outlined in Appendix B, Projected Utilization Rates. The Government manages engines as a propulsion package referred to as a “QECA”, which is comprised of the nacelle (QECK), core engine, and the necessary components attached to them in order to make the QECA a complete operational unit. As such, the Government will ship complete QECAs to the Contractor’s depot maintenance center for repair. Propeller Gearbox (PGB) and Gearbox Mounted Accessory Drive (GMAD) will also be shipped as individual components for repair. Attachment 2 to the contract, Engine Inventory, provides a list of all QECK and engines currently managed in the NAVAIR inventory and expected to be repaired by the Contractor under this PWS.

As the Government continues to procure aircraft and spare engines, this attachment will be updated to include any additions and deletions made to the inventory.

1.2.1 Operational Concept

The Government operates the KC-130J at sites within the continental United States and outside the continental United States. The sites are identified in Appendix B, Projected Utilization Rates.

1.2.2 Maintenance Concept

Government, FMS, and Government-contracted personnel maintain the propulsion system at the organizational-level (O-level) in accordance with the approved maintenance concept as described in the NAVAIR KC-130J Organizational Maintenance Manuals, KAF KC-130J Organizational Maintenance Manuals, NAVAIR Technical Directives (TDs), Naval Aviation Maintenance Program (NAMP), and other Government approved data. This support includes servicing, troubleshooting, scheduled and unscheduled maintenance actions, and preservation and packing of retrograde material. The Contractor is responsible for facilities, labor, parts, material, and test equipment for depot-level repair of QECAs. Additionally, the Contractor is responsible for effectively managing repair part inventories, which includes forecasting all material requirements and vendor contracts which results in all received material being returned to ready-for-issue (RFI) status.

2.0 APPLICABLE DOCUMENTS

These documents are for reference purposes only. Specific requirements are identified in the applicable PWS sections.

2.1 Government Documents

•NAVAIR KC-130J Organizational Maintenance Manuals •COMNAVAIRFORINST 4790.2B, The Naval Aviation Maintenance Program (NAMP) •NAVAIRINST 13700.15F, Decision Knowledge Programming for Logistics Analysis and Technical

Evaluation (DECKPLATE) Engine/Propulsion System Module (E/PSM) Management •Department of Defense (DoD) Manual 5220.22-M, National Industrial Security Program Operating Manual

(NISPOM)

•NAVAIRINST 4130.1D, Naval Air Systems Command Configuration Management Process •MIL-HDBK-516, Airworthiness Certification Criteria •JSSG-2007 Joint Services Specification Guide – Engines, Aircraft, Turbine •SECNAVINST 4140.2 Management of Aviation Critical Safety Items •NAVAIRINST 13100.15, Engineering Technical Review of Commercial-Derivative Aircraft Programs •National Aerospace Standard (NAS) 411 Hazardous Materials Management Program •Title 14 CFR Part 21, Certification Procedures for Products and Parts •Title 14 CFR Part 39, Airworthiness Directives •Title 14 CFR Part 145, Repair Station Requirements (European Aviation Safety Agency (EASA) Part 145 Certified Repair Station and Transport Canada Civil Aviation regulations IAW FAA AC 43-10C, United States- Canada Bilateral Aviation Safety Agreement Maintenance Implementation Procedures are acceptable equivalents to 14 CFR Part 145) •NAVAIRINST 00-25-300, NAVAIR Technical Directives System •DoD 4160.21-M, Defense Materiel Disposition Manual •DoD 4160.28, Defense Demilitarization: Program Administration

• DoDI 8520.02 dated 24 May 2011 Public Key Infrastructure (PKI) and Public Key (PK) Enabling

• NAVAIR 01-75GAJ-6 Periodic Maintenance Information Manual (PMIC)

2.2 Kuwait Air Force Specific Documents

•KAF KC-130J Organizational Maintenance Manuals •Kuwait Aviation Maintenance Program 4790.2B

2.3 Other Documents

•AE 2100D3 Maintenance Manual (MM) (CSP 34042) •AE 2100D3 Engine Manual (EM) (CSP 31013) •AE Series Standard Practices Manual (SPM) (CSP 40000) •AE 2100D3 Service Bulletins (SB) (CSP 34043) •AE 2100D3 Operations Manual (CSP30004) •AE 2100D3 Illustrated Parts Catalog (CSP33004) •AE 2100D3 Fault Isolation Manual (CSP34063)

3.0 GENERAL REQUIREMENTS

This section establishes the requirements for the Contractor to execute this PWS. These requirements apply to all contract line item numbers (CLINs). The Contractor shall use best commercial practices unless otherwise specified.

The Contractor shall meet the metrics as defined in Appendix C, Metrics.

3.1 Quality Management System

The Contractor's project management efforts shall satisfy the requirements of this PWS. The Contractor shall provide and use a commercial quality system that demonstrates a systems approach for managing quality, safety, and compliance with all contractual requirements in accordance with Title 14 CFR Part 145 Requirements (European Aviation Safety Agency (EASA) Part 145 Certified Repair Station and Transport Canada Civil Aviation (TCCA) regulations IAW FAA AC 43-10C, United States-Canada Bilateral Aviation Safety Agreement Maintenance Implementation Procedures are acceptable equivalents to 14 CFR Part 145). The Contractor is accountable for all sub-contractors and vendors, and as such, shall be required to implement a quality system achieving control of the quality of the services and supplies. The Government reserves the right to perform any necessary inspections, verifications, and evaluations of the Contractor’s repair facilities at any time during contract performance to ascertain the adequacy of the quality system. For safety related visits, the Government will give the Contractor no less than 5 working days’ notice. The Government will give the Contractor no less than 30 working days’ notice for all other visits.

3.2 Operations Security

The Contractor shall establish and maintain a security program with policies and procedures that are in compliance with the requirements of the NISPOM DODM 5220.22-M.

3.3 Project Management

3.3.1 Project and Risk Management.

The Contractor shall provide project management to meet the performance requirements of the PWS. The Contractor shall establish and maintain a risk management program for the purpose of early identification and mitigation of program risks as to not negatively impact contract performance.

3.3.2 Project Manager.

The Contractor shall designate a single point of contact responsible for the overall management and performance of the contract requirements. The Contractor shall provide, in writing, the name and contact information of the designee to the Procurement Contract Officer (PCO) within ten working days of contract award. Any change of Project Manager shall be submitted to the PCO within five business days.

3.4 Hazardous Material and Waste

The Contractor shall implement hazardous material handling procedures that comply with local, state, and federal laws and regulations concerning the use of Class I Ozone Depleting Compounds and Ozone Depleting Substances identified in NAS411-1.

3.5 Package, Handling, Shipping, and Transportation

3.5.1 Shipping, Packaging, Storage, and Containers.

The Contractor shall preserve and package for transport all Government property in accordance with the Original Equipment Manufacturer (OEM) Repair Manuals. The primary method for shipping engines and components will be as part of QECAs. Components shall be shipped to and from the Contractor in approved shipping containers. In the event engines are shipped for repair on Government engine stands, the Contractor shall ensure Government engine stands and adapters are fully accounted for and returned to the Government in RFI condition.

3.5.2 Government Furnished Property Shipping.

The Contractor shall ship all Government Furnished Property at the request of the COR.

3.6 Export Control Licenses

The Contractor shall have export licenses for all components, parts, and materials that are International Traffic in Arms Regulation controlled no later than 30 days after contract award.

3.7 Engine Transaction Reporting

The Contractor shall comply with the E/PSM reporting procedures in accordance with NAVAIRINST 13700.15F as changes in custody, status, or conditions occur. The Government will authorize the Contractor access to the DECKPLATE Engine Management database.

3.8 Information Assurance

The Contractor shall ensure that personnel accessing information systems have the proper and current certifications to access DOD information systems for the purpose of performing IA functions. Public Key Infrastructure (PKI) encryption is the chosen compliant Department of Defense (DoD) standard for protecting Controlled Unclassified Information (CUI) during transmission. CUI encompasses For Official Use ONLY (FOUO) and Sensitive Information. Failure to encrypt CUI during electronic transmission is considered a security weakness and must be reported to the Information Assurance Officer (IAO) and Program Security Manager (PSM) via the Contractor’s responsible individual. The Contractor shall require their personnel to adhere to the required PKI policies stated herein when transmitting CUI. The Contractor shall implement DoD PKI policy per DODI 8520.02. The Contractor shall obtain and utilize PKI certificates issued by approved External Certificate Authority (ECA), for the purposes of protecting all CUI. A substitute to utilizing approved PKI ECA certificates is for the Contractor to become a member of the Federal Bridge Certification Authority in order to issue approved Contractor issued PKI certificates with trust relationships to the DoD PKI. Approved PKI will be utilized by the Contractor and their subcontractors when transmitting CUI via electronic means. A temporary written waiver for such requirements may be granted by the government provided that the Contractor submits a waiver request in writing.

4.0 PROJECT REQUIREMENTS (CLINs 0X01 and 0X02)

4.1 Management Plan

The Contractor shall create and maintain a Management Plan to provide processes for providing project management, QECA and component repair, and engineering and technical services required under this PWS. The Contractor shall submit the Management Plan in accordance with Contract Data Requirements Lists (CDRLs) A001, AA01, AB01, AC01, and AD01.

4.2 Meetings and Reviews

4.2.1 Post-Award Conference.

The Contractor shall host a post-award conference with the Government at the Contractor’s facility no later than 45 days after contract award. This meeting will cover the topics as set forth in FAR Subpart 42.5, Post-award Orientation. Additionally, the Contractor shall demonstrate its management procedures, provide progress assessments, review technical and other specialty area status, and schedule dates for near-term critical meetings and actions.

4.2.2 Project Manager.

The Contractor’s Project Manager shall attend and participate in the meetings listed below. Meetings will be scheduled by the Government with at least 30 days advance notice.

4.2.2.1 The Contractor shall host semi-annual Program Management Reviews (PMRs) at the Contractor’s facility.

4.2.2.2 The Contractor shall provide weekly status reports to the COR of all QECAs at the depot via weekly teleconference.

4.2.2.3 The Contractor shall host and conduct monthly meetings by telephone or video teleconference to provide status on all open actions, performance metrics status, engine status highlights, QECA Deficiency Trends, engineering and logistical emergent issues, risks, the potential impacts, and mitigation approaches.

4.2.3 Agenda.

The Contractor shall prepare an Agenda for the PMRs and submit the Agenda in accordance with CDRLs A002, AA02, AB02, AC02, and AD02.

4.2.4 Meeting Minutes.

The Contractor shall prepare Meeting Minutes for the PMR and submit the Meeting Minutes in accordance with CDRLs A003, AA03, AB03, AC03, and AD03.

4.2.5 Government Furnished Equipment.

Spare core engines will be provided as Government Furnished Equipment (GFE) in accordance with Attachment 2 to the contract. These GFE items will be utilized only when authorized by the COR. The Contractor shall store the USMC or FMS owned spare core engines and shipping containers in a secure storage area. The Contractor shall utilize OEM methods and procedures for maintaining the engines in a preserved and ready-for-installation state and will provide status of all GFE items during monthly meetings. The monthly preservation tasks shall include:

a) Perform general container maintenance;

b) Ensure cleanliness and legible stenciling;

c) Ensure all fasteners are in place and properly torqued;

d) Inspect for damage to the outer surface of the container;

e) Examine the external shock sensors;

f) Monitor humidity;

g) Reclaim atmosphere (as needed) and;

h) Maintain preservation documentation.

4.3 Airworthiness and Configuration Management

4.3.1 Airworthiness Certification Authority.

NAVAIR is the airworthiness certification authority for the KC-130J aircraft. NAVAIR’s airworthiness certification for KC-130J propulsion system leverages the Federal Aviation Administration (FAA) type certification and civil airworthiness standards as a baseline in accordance with MIL-HNDBK-516, JSSG-2007, and NAVAIRINST

13100.15. The current depot maintenance manuals, illustrated parts breakdown, and formal TDs form the baseline certification for airworthiness of depot-repaired engines.

4.3.2 Configuration Changes.

The Contractor shall review the engine logbooks for NAVAIR TDs requiring incorporation during repair and document the compliance of the TD upon completion. Applicable NAVAIR TDs are available for download from the Naval Aviation Technical and Engineering Services Command's (NATEC) website www.natec.navy.mil. The current maintenance manuals, Illustrated Parts Breakdown (IPB), Approved OEM Service Bulletins (Appendix D), and Formal Technical Directives form the baseline configuration of the KC-130J QECA.

4.3.3 Technical Variances and Deviations.

http://www.natec.navy.mil/

The Contractor shall provide a copy of the FAA approved technical variance (TV) via the WIS when the Contractor deviates from the authorized configuration and or use of unauthorized parts or components to all AE2100D3 engines repaired under this PWS. A TV is defined as any deviation or variance that is outside the approved configuration, tolerances, or limits defined in the OEM repair manuals. Additionally, the Contractor shall make available all relevant data, analysis, and assumptions for review by NAVAIR technical authority experts to document the nature of the change, support why the change is needed, what testing was completed to ensure safety, and if the change is permanent or temporary.

4.4 ENGINEERING INVESTIGATIONS AND TECHNICAL SERVICES (CLIN 0X19)

4.4.1 Engineering Investigation, Analytical Condition Inspection, and Product Quality Deficiency Report.

The Contractor shall provide, at the request of the Government and with COR approval, support investigations of items designated special interest. These tasks are Engineering Investigations (EIs)/Analytical Condition Inspection (ACI)/ Product Quality Deficiency Report (PQDR). The Fleet Support Team (FST) engineering personnel will coordinate with the Contractor on the induction of EI, ACI or PQDR items and provide specific disassembly, inspection, and data recording instructions. The Contractor shall research component history to include hours/cycles accrued, serviceability, repairs, and installations/removals, at a minimum. Disposition instructions and release of the EI, ACI, or PQDR item will be provided by FST engineering upon completion of the EI, ACI, and PQDR. The time required to support the EI, ACI, shall not be counted against the Contractor's TAT. The Contractor shall compile analysis and test data and submit in accordance with CDRLs B001, BA01, BB01, BC01, and BD01.

5.0 GENERAL REPAIR REQUIREMENTS

5.1 Repairs

The following requirements shall apply to all repairs performed under sections 6 through 10 of this PWS:

5.1.1 QECA Repairs.

The Contractor shall perform all unscheduled and scheduled repairs, maintenance actions, restoration, tests, FAA-approved airworthiness directives in accordance with Title 14 CFR Part 39, and configuration changes in accordance with the baseline configuration, established in section 4.3.2 of this PWS. Future service bulletins will be addressed in accordance with the FAR 52.212-4(c) Contract Terms and Conditions -- Commercial Items (May 2015).

5.1.2 Repair Materials.

The Contractor shall ensure the safety and quality of all materials used in repairs and ensure that all new, repaired, or refurbished parts are FAA-certified (or equivalent TCCA or EASA), in accordance with Title 14 CFR Part 21 and accompanied by a copy of the work order, FAA Form 8130-3 or an equivalent Contractor Certificate of Conformance (COC), and FAA Form 8110-3 or an equivalent Certificate of Release, Test, and Conformity.

5.1.3 Perform Repairs. The Contractor shall provide all labor, parts, and material necessary to perform repairs.

5.1.4 Work Performed Records.

The Contractor shall provide documentation to certify all work was accomplished in accordance with Federal Aviation Regulation Part 145, Repair Stations (or equivalent TCCA or EASA), and in accordance with current policies and procedures; and record all maintenance, modifications, and component life information into the applicable NAVAIR/KAF logbook, commercial logbook, and record for all contractor work performed.

5.1.4.1 The Contractor shall ensure that all work accomplished has been certified as airworthy and properly documented on FAA Form 8130-3 or an equivalent Contractor Certificate of Conformance (COC) and FAA

Form 8110-3 or an equivalent Certificate of Release, Test, and Conformity, and DD250.

5.1.4.2 The Contractor shall provide notification of any issue concerning a CSI part to the COR and FAA (or equivalent TCCA or EASA) via email within Two Working Days.

5.1.5 Engine Disks.

The Contractor shall update engine data disks for all work performed by the Contractor.

5.1.6 Repair Action Report.

The Contractor shall compile all repair data and submit a Repair Action Report on repaired QECAs, engines, modules, and components in accordance with CDRLs A004, AA04, AB04, AC04, and AD04.

5.1.7 Life Limited Components.

The contractor shall replace all life limited components referenced in the KC-130J PMIC, with less than 800 cycles life remaining per the recorded cycles in Engine Logbook.

5.1.8 Storage.

The Contractor shall, upon Government direction, provide indoor storage for up to two NAVAIR or FMS-owned spare core engines and two shipping containers.

5.1.9 Property Control.

Core engines and containers stored at the Contractor’s facility shall be managed under the Contractor’s Government-approved property control system. The Contractor shall keep any property received under this contract separate from other property.

5.1.10 Preservation.

The Contractor shall use approved OEM methods and procedures for maintaining the engines in a preserved and RFI state.

5.1.11 Monthly Preservation Tasks.

The Contractor shall perform the following monthly preservation tasks:

5.1.11.1 Perform general container maintenance

5.1.11.2 Ensure cleanliness and legible stenciling

5.1.11.3 Ensure all fasteners are in place and properly torqued

5.1.11.4 Inspect for damage to the outer surface of the container

5.1.11.5 Examine the external shock sensors

5.1.11.6 Monitor humidity

5.1.11.7 Reclaim atmosphere (as needed)

5.1.11.8 Update preservation documentation (as needed)

5.2 Security of Government Property

All property received under this contract shall be in an enclosed and covered area accessible only to authorized personnel and protected against loss, damage, and theft.

5.3 Cannibalization

The Contractor shall request, in writing, approval from the COR to cannibalize repairable parts, components, or modules from other QECAs. Cannibalization approval by the Government shall not constitute grounds to extend the TAT of the QECA from which the parts were cannibalized. If the Government fails to provide disposition within three working days, the TAT will stop until disposition is provided.

5.4 Condemnation

Parts, components, and modules shall be considered for condemnation if their repair exceeds the repairable limits specified in the applicable OEM manuals. The Contractor shall not repair condemned parts unless authorized in writing by the COR. All condemned parts shall be reported in the Master Repair Document (MRD) and the Contractor shall request the Government provide disposition guidance for all condemned parts. The Government may choose to recycle some or all of unusable materials.

5.5 Disposition of Material

The Contractor shall include in its NAVAIR approved Management Plan the process for disposal of Government property and shall include the requirements stipulated in the FAR Part 45, Government Property; DoD 4160.21-M, Defense Material Disposition Manual; and DoD 4160.28, Defense Demilitarization: Program Administration. The Contractor shall dispose of all removed Government property in accordance with the Management Plan.

6.0 INDUCTION, DISASSEMBLY, AND ASSEMBLY OF THE QECA (CLIN

0X03)

6.1 Receipt of QECAs

The Contractor shall receive and induct all QECAs that have identified discrepancies requiring partial or full disassembly.

6.1.1 Receiving Inspections.

The Contractor shall perform a receiving inspection of the QECA and notify the COR of findings within three working days of receipt at the Contractor’s facility.

6.1.2 Engine Transaction Reports.

The Contractor shall submit Engine Transaction Reports (ETR) via DECKPLATE Engine Management on all engines or components in accordance with NAVAIRINST 13700.15E. Lost or missing maintenance records shall not prevent the reporting of receipt of engines or components in DECKPLATE. In the case of lost or missing maintenance records, the ETR entries shall identify what records were not received.

6.1.3 Records Protection. The Contractor shall protect all maintenance records from damage or loss.

6.2 Processing of QECAs

The Contractor shall perform receiving, inspection, removal of core engine, minor repair of QECK, reinstallation of the core engine, final inspections, report preparations, and logbook and record card update actions to return the QECA to RFI condition as outlined in Appendix E, Repair Processes.

7.0 QECK REPAIRS (CLINs 0X04, 0X05, 0X06, and 0X07)

A QECK depot-level repair encompasses the structural components, all attaching components, wiring, ducts, and tubing of the QECA that are not part of the core engine. Repairs of the QECA Transport Dollies/Stands and the QECA protective bag/cover will be included in the QECK repair effort. The QECK repairs shall be classified, as outlined below, based on the number of flight hours acquired since the last depot shop visit. Flight hours are defined as the amount of hours on the QECK since the last shop visit, as recorded by the Government in Naval Aviation Flight Records (NAVFLIR).

7.1 Categorize Repair

The categories of repair are defined as follows:

•CLIN 0X04 - Category 1 Repair: 0-750 hours since last shop visit •CLIN 0X05 - Category 2 Repair: 751 – 1500 hours since last shop visit •CLIN 0X06 - Category 3 Repair: 1501 – 2250 hours since last shop visit •CLIN 0X07 - Category 4 Repair: 2251 – or more hours since last shop visit

7.2 Repair

Upon receipt of executed Task Order, the Contractor shall repair the QECK.

7.3 Deviation Requests

The Contractor shall obtain NAVAIR approval, in writing via the COR, for any change to or deviation from QECK and subcomponents of the QECK prescribed repair procedure or test specification(s) in approved OEM and Government Maintenance manuals. NAVAIR will provide disposition within five working days. If the Government fails to provide disposition within three working days, the TAT will stop until disposition is provided.

8.0 POWER SECTION REPAIR (CLINs 0X08, 0X09, 0X10, 0X11, 0X12, and 0X13) Modules are defined below and are inclusive of all attaching components, wiring harnesses, tubing, and ducting.

Repairs are inclusive of all disassembly, inspections, repairs, component testing, reassembly of Power Section and Torque meter, and operational testing of the core engine. The engine repairs shall be classified, as outlined below, based on the reason for removal.

1. Power Section

2. Torque meter

3. Power Unit Accessory Drive

8.1 Categorize Repair

•CLIN 0X08 - Category 1 Repair: Performance •CLIN 0X09 - Category 2 Repair: Metal in Oil •CLIN 0X10 - Category 3 Repair: Oil Leak/Pressure Issues •CLIN 0X11 - Category 4 Repair: External Engine Damage •CLIN 0X12 - Category 5 Repair: FOD •CLIN 0X13 - Category 6 Repair: Vibration

The category of repair will be determined by the Government using the maintenance download and/or fleet inspection information. In the event that additional repairs are identified by the Contractor during induction, the Contractor shall notify the PCO within three working days.

8.2 Repair

Upon receipt of executed Task Order, the Contractor shall repair the engine.

8.3 Reassemble

Upon repair of the module(s), the Contractor shall reassemble the Power Section and Torquemeter.

8.4 Operational Test

Upon reassembly of a core engine, the Contractor shall perform an operational test of the engine to certify as RFI.

All engines repaired by the Contractor shall have a maximum measured gas temperature (MGT) value of 1366°F to produce a 100% shaft horse power (SHP) rating of 4637 SHP at Sea Level, Static, Standard Day conditions in order to be considered RFI.

9.0 PROPELLER GEARBOX AND GEARBOX MOUNTED ACCESSORY DRIVE

REPAIR (CLINs 0X14 and 0X15)

This section applies to the AE2100D3 PGB and GMAD units that are received by the Contractor either installed in a QECA or as stand-alone units. The PGB and GMAD repairs shall be classified, as outlined below, based on the number of flight hours acquired since the last depot shop visit. Flight hours are defined as the amount of hours on the PGB and GMAD since the last shop visit, as recorded by the Government in NAVFLIR.

9.1 Categorize Repair

•CLIN 0X14 – Category 1 Repair: 0-2,000 hours since last shop visit •CLIN 0X15 – Category 2 Repair: 2,001– or more hours since last shop visit

9.2 Repair

Upon receipt of executed Task Order, the Contractor shall repair the PGB and GMAD.

9.3 Operational Test

Upon repair of the PGB and GMAD, the Contractor shall perform an operational test of the units to certify as RFI.

9.3.1 For PGB and GMAD units received installed, the operational test should be accomplished once installed on the core engine.

9.3.2 For PGB and GMAD units received as standalone assets, the test may be completed using a standalone test platform or as an installed unit on a core engine.

9.4 Request Disposition

Upon successful completion of the operational test, the Contractor shall request Government disposition from the COR for the PGB and GMAD.

10.0 ADDITIONAL REPAIRS (CLINs 0X16, 0X17, and 0X18)

The Contractor shall perform repairs under this section in conjunction with the repairs listed in Sections 7 and 8 of this PWS. The intent of this section is to provide for repairs considered beyond the scope of sections 7 and 8 of this PWS. All additional repairs shall be accomplished using the same process outlined in all repair sections of the PWS.

Additional repairs are:

10.1 Radiological Control

(RADCON) QECA Survey (CLIN 0X16). Under this CLIN, the Contractor shall disassemble, survey, inspect, and decontaminate a radiation contaminated QECA IAW contract AE2100 RADCON Engine Teardown Inspection

Plan (Attachment 3) complying with all local laws and regulations, and the following:

a) The Contractor shall make the radiological survey facility available for Government site survey within 30 days of contract award.

b) The Contractor shall perform up to three decontamination attempts if the component is found above the limits. If there is less than a 10% reduction in radioactivity between the initial survey and the first decontamination attempt, and the component remains above limits, the item shall be quarantined. If the component remains above limits after the third decontamination attempt, the component shall be quarantined.

c) The Contractor shall retain all quarantined components at the radiological survey facility until the Government provides disposition instructions.

d) The Contractor shall complete and submit all Survey Plan Appendices and associated documentation completely, correctly, and within the guidelines provided in the survey plan. The Contractor shall submit the appendices for each QECA survey as each appendix is completed.

e) The Contractor shall retain all QECAs at the radiological survey facility until the component is cleared for release.

All QECAs surveyed under this CLIN will be reviewed and cleared by the Government prior to release for reassembly. This release shall be provided by the Government via Naval message. The Contractor shall perform reassembly of the QECA under CLIN 0X16 or 0X17 as appropriate.

10.2 Engine Reassembly (CLIN 0X17).

Under this CLIN, the Contractor shall inspect and reassemble an engine received in a disassembled state. These engines were disassembled during RADCON survey and have been cleared for reassembly by NAVSEA. The Contractor shall perform the reassembly under this CLIN concurrently with the repair procedures performed under one of the following CLINs: 0X08, 0X09, or 0X10, as outlined in Section 8 of this PWS necessary to restore the engine to RFI condition.

10.3 QECK Reassembly (CLIN 0X18).

Under this CLIN, the Contractor shall inspect and reassemble a QECK received in a disassembled state. These QECKs were disassembled during RADCON survey and have been cleared for reassembly by NAVSEA. The Contractor shall perform the reassembly under this CLIN concurrently with the repair procedures performed under one of the following CLINs: 0X04, 0X05, or 0X06, as outlined in Section 7 of this PWS necessary to restore the QECK to RFI condition.

11.0 Shipping (CLINs 0X20, 0X21, 0X22, 0X23, 0X24, and 0X25)

11.1 Shipping Requirements QECAs and PGBs.

The Contractor shall coordinate and ship QECAs and components as directed by the COR. Transportation costs for shipment of the QECAs and components from the Government site to the Contractor’s facility are the responsibility of the Government. The Contractor will be responsible to ship QECAs and PGBs from the Contractor’s facility to the Government designated CONUS, Japan, or KAF location determined by the COR. The below listed destinations and supported activities are provided as standard shipping locations but are not all inclusive as other events may require shipments to alternate destinations to support fleet requirements.

CONUS (CLIN 0X20 QECA, 0X21PGB) - The following geographical areas are utilized to support USMC, USMCR, activities that are based or operating within the Continental US.

CONUS DESTINATIONS Activity Supported

Cherry Point , NC VMGR-252

Patuxent River, MD VX-20 Newburgh, NY VMGR-452 Fort Worth, TX VMGR-234 San Diego, CA VMGR-352

Japan (CLIN 0X22 QECA, 0X23 PGB) - The following geographical area is utilized to support USMC, USMCR, activities that are based or operating outside of the Continental US.

Japan DESTINATIONS Activity Supported Iwakuni, Japan VMGR-152

KAF (CLIN 0X24 QECA, 0X25 PGB) – QECAs and PGBs shall ship to one of the following locations of the Contractor’s choice in support of KAF activities that are based or operating outside of the Continental US.

DESTINATIONS Activity Supported Jamaica, NY Kuwait (Freight Forwarding Activity)

TBD, United Kingdom Kuwait (Freight Forwarding Activity) Hamburg, Germany Kuwait (Freight Forwarding Activity)

APPENDIX A: KC-130J QUICK ENGINE CHANGE ASSEMBLY (QECA)

SYSTEM DESCRIPTION

QECA SYSTEM DESCRIPTION

The KC-130J propulsion system is comprised of the AE2100D3 turboprop engine manufactured by Rolls-Royce and the nacelle (commonly referred to as “QECK”) assembly manufactured by Lockheed Martin. The QECA is maintained as a complete ready to install and operate assembly.

AE2100D3 TURBOPROP ENGINE DESCRIPTION

The Rolls-Royce AE2100D3 engine is comprised of five major modules:

1. Power Section

2. Torque meter

3. Power Unit Accessory Drive

4. Gearbox Mounted Accessory Drive

5. Propeller Gearbox (PGB)

Each engine includes the below listed major components and Line Replaceable Units (LRU):

1. Starter 11. Starter control valve 21. Torque meter pick-ups

2. Compressor inlet pressure sensors

12. Compressor inlet temperature sensors

22. Thermocouples

3. Full authority digital electronic control

(FADEC) (2)

13. Indicating magnetic plugs 23. Fuel pump metering unit

4. Compressor variable geometry actuator

14. Anti-ice valve 24. Permanent magnetic alternator

5. Igniters 15. Ignition exciters 25. Fuel cooled oil cooler

6. NP harness 16. NP speed sensor 26. Power Section lube and scavenge pump

7. Fuel nozzles 17. NG speed sensors 27. PGB lube and scavenge pump

8. Bleed control valve 18. All engine tubing 28. Prop shaft flange adapter

9. FADEC A harness 19. FADEC B harness 29. Compressor bleed valves

10. EMS harness 20. Fuel flow meter

KC-130J NACELLE DESCRIPTION

The Lockheed Martin KC-130J Nacelle is comprised of the following:

1. Nacelle structure 8. Engine and aircraft pneumatic system

2. Engine mounts 9. Engine and aircraft electrical system

3. Electric generator 10. Engine fuel system

4. Propeller pitch control unit 11. Engine control and indicating systems

5. Propeller over-speed governor 12. Engine oil system

6. Engine exhaust nozzle 13. Engine starting system

7. Brush block and bracket 14. Engine hydraulic system

The above lists are intended to detail only the major modules and components of the engine; they are not all-inclusive. A thorough breakdown of the engine that includes all parts, repairable as well as consumable, can be found in the Rolls-Royce AE2100D3 Illustrated Parts Catalog or the NAVAIR KC-130J Organizational Maintenance Manuals.

APPENDIX B: PROJECTED UTILIZATION RATES

Projected KC-130J Distribution by Site and Projected Flight Hours:

USMC and USN Activities FY17 FY18 FY19 FY20 FY21 Active Squadron VMGR-152 / Iwakuni Japan 15 15 15 15 15 VMGR-252 / Cherry Point, NC 15 15 15 15 15 VMGR-352 / Miramar, CA 15 15 15 15 15 Projected Active Aircraft Flight Hours 20,993 21,563 20,758 21,021 20,246

Reserve Squadron

VMGR-452 / TBD 0 0 0 2 5

VMGR-234 / Fort Worth, TX 7 8 10 12 12 Projected Reserve Aircraft Flight Hours 2,500 2,500 2,500 2,500 5,200

Test Squadron VX-20 / Patuxent River, MD 1 1 1 1 1 Projected Test Aircraft Flight Hours 120 120 120 120 120

Total Aircraft USMC and USN 53 54 57 60 62 FMS Activities Kuwait (KAF) 3 3 3 3 3 Projected Total Aircraft Flight Hours 2,200 2,200 2,200 2,200 2,200

APPENDIX C: METRICS

1.0 METRIC INTRODUCTION

1.1 This Appendix defines the metrics selected to measure the Contractor’s performance effectiveness in meeting the requirements established in the Performance Work Statement. The Contractor shall be held responsible for meeting established metrics in accordance with clause H-1 Liquidated Damages and any other remedies available under this contract. These metrics were selected in order to institute a program that provides Government operating forces with the QECA readiness necessary to meet their worldwide national security commitments.

1.2 Throughout the contract period, Contractor performance to metrics will be continually monitored per the Quality Assurance Surveillance Plan (QASP). Formal reviews of performance will be held at each Program Management Review. At each semi-annual review the cause and corrective actions associated with non-performance to metrics will be discussed and addressed.

1.3 In cases of non-performance to metrics, the following causes and results will be addressed by the NAVAIR and Contractor program management group:

•Validity of metric and measurements or data feeding the metric •Impact on fleet readiness and operation due to the metric infraction or non-attainment •Reason or cause for the metric infraction; both Government-caused and Contractor-caused •Corrective action taken and results (metric performance due to timing associated with corrective action implementation)

1.4 The Metrics for performance monitoring and management are:

Metric Name Metric

QECA Repair Turn-Around Time (TAT) 100 Days PGB and GMAD TAT (Stand Alone) RADCON Survey TAT

45 Days 90 Days

QECA Repair Turn-Around Time (TAT) For induction in first 6 months of contract award

140 Days

2.0 METRIC DEFINITIONS

2.1 QECA Repair Turn-Around Time

The QECA Repair TAT conveys the Government’s requirements for repair responsiveness. The Contractor can use this metric to help determine the proper capacity of its repair facilities, repair part inventories, and subcontract requirements. The TAT starts once the Government issues a task order for repair of a QECA and the Contractor receives the QECA. TAT ends when the Contractor provides copies of repair documentation and notifies the COR that the QECA is RFI and ready for shipment.

Date RFI – Date task order issued and QECA received = Total Days TAT

2.2 PGB and GMAD Turn-Around Time

The PGB and GMAD TAT convey the Government’s requirements for repair responsiveness. The Contractor can use this metric to help determine the proper capacity of its repair facilities, repair part inventories, and subcontract requirements. The TAT starts once the Government issues a task order for repair of a specific module and the Contractor receives the specific module. TAT ends when the Contractor provides copies of repair documentation and notifies the COR that the module is RFI and ready for shipment.

Date RFI – Date task order issued and PGB received = Total Days TAT

2.3 RADCON Survey Turn-Around Time

The RADCON Survey TAT conveys the Government’s requirements for survey responsiveness. The Contractor can use this metric to help determine the proper capacity of its radiological survey facility. The TAT starts once the Government issues a task order for survey of a QECA and the Contractor receives the QECA. TAT ends when the Government authorizes the QECA for release or disposition.

Date the Government authorizes the QECA for release or disposition – Date task order issued and QECA received = Total Days TAT

APPENDIX D: APPROVED OEM SERVICE BULLETINS

NOTE: All data acquired from ETS, including compliance.

Service Bulletin Number

Title

USMC KAF

Compliance Compliance

AE 2100D3-72-005 New Compressor Stages 1-5 Borescope Plug 100.0% 100.0% AE 2100D3-72-006 1st stage compressor wheel retrofit 100.0% 100.0% AE 2100D3-72-007 New 11th and 12th Stage Compressor Wheels and 9th - 13th Stage

Compressor Vanes 100.0% 100.0%

AE 2100D3-72-011 Replace the Bearing-Outer-Race Locking Key 100.0% 100.0% AE 2100D3-72-012 Replace the 6th- and 7th-Stage Compressor Wheels 100.0% 100.0% AE 2100D3-72-013 Introduction of New 8th-14th-Stage Compressor Blades and Wheels 100.0% 100.0% AE 2100D3-72-014 Rework the Accessory Gearbox Housing Assembly 100.0% 100.0% AE 2100D3-72-015 Aluminum Actuator Ring Clevis 100.0% 100.0% AE 2100D3-72-016 New Gas-Generator Case Baffle Assembly 100.0% 100.0% AE 2100D3-72-017 Revised Balance Procedure 100.0% 100.0% AE 2100D3-72-018 New 1st-Stage Gas Generator Turbine Wheel Assembly 100.0% 100.0% AE 2100D3-72-019 New Turbine 3rd-Stage Vane-and-Seal Assembly 100.0% 100.0% AE 2100D3-72-020 New 1st- and 2nd-Stage Turbine Wheels 100.0% 100.0% AE 2100D3-72-021 1st-Stage Gas-Generator Turbine Vanes 100.0% 100.0% AE 2100D3-72-022 New 4th-Stage Turbine Blades 100.0% 100.0% AE 2100D3-72-023 Inspection and Installation of Air Sensing Tip on Air Inlet Housing 100.0% 100.0% AE 2100D3-72-026 Life-Limited Torquemeter Shafts 100.0% 100.0% AE 2100D3-72-029 Turbine Rotor Assemblies Identification Markings 100.0% 100.0% AE 2100D3-72-031 Introduction of Turbine 1st-Stage Vane-and-Support Assembly 100.0% 100.0% AE 2100D3-72-035 Additional Testing Requirements 100.0% 100.0% AE 2100D3-72-036 Type Certified Identification Plates 100.0% N/A AE 2100D3-72-039 New 6th- thru 14th-Stage Compressor Vanes N/A N/A AE 2100D3-72-041 New Metal Cover Plate for the Diffuser 100.0% 100.0% AE 2100D3-72-042 New Front Sump Hardware 100.0% 100.0% AE 2100D3-72-044 1st-Stage Compressor Wheel Assembly 100.0% 100.0% AE 2100D3-72-045 Modify the Rear Engine-Mount Bracket N/A N/A AE 2100D3-72-047 Replace the PGB/Strut Grounding Strap 100.0% 100.0% AE 2100D3-72-048 Compressor-Rotor-Replace the Self-Locking Bearing Nut

(23039898) 100.0% 100.0%

AE 2100D3-72-050 PGB Drain Plug N/A N/A AE 2100D3-72-051 Change the Routing/Clamping of the Electrical Harnesses 100.0% 100.0% AE 2100D3-72-054 PGB Strut-Fitting Eccentric Pins 100.0% 100.0% AE 2100D3-72-056 Gearbox-Drive Bearing Housing N/A N/A AE 2100D3-72-057 New 3rd-Stage Turbine Blades 99.6% 100.0% AE 2100D3-72-059 Replace the Threaded Oil Nozzle in the Gearbox-Mounted

Accessory Drive 100.0% 100.0%

AE 2100D3-72-061 Power Turbine Rotor Assembly Identification Markings 100.0% 100.0% AE 2100D3-72-063 Rework the GMAD Housing N/A N/A AE 2100D3-72-064 Remove the NO. 2 - Bearing Front-Sump Impeller N/A N/A

AE 2100D3-72-065 Gas-Generator Case-and-Vane Assembly 100.0% 100.0% AE 2100D3-72-067 Rear Engine-Mount Bracket 100.0% 100.0% AE 2100D3-72-068 New 1st--Stage Compressor Wheel Assembly 50.0% N/A AE 2100D3-72-070 Compressor-Air-Inlet-Housing Dowel Pin 100.0% N/A AE 2100D3-72-073 New Compressor-to-Turbine Shaft and Liner with Locking Spiral

Retaining Ring 100.0% N/A

AE 2100D3-72-074 New Center-Sump Housing Assembly and Center-Sump Forward Stationary Seal

100.0% 100.0%

AE 2100D3-72-076 New Position for the PGB Grounding Straps N/A N/A AE 2100D3-72-080 New Anti-Ice-Manifold Support Bracket 100.0% 100.0% AE 2100D3-72-082 Chem-Milled Diffuser 99.2% 100.0% AE 2100D3-72-086 New 1st-Stage Turbine Blade Tracks and Gasifier Turbine Inner

Casing 100.0% 100.0%

AE 2100D3-72-089 New Propeller Gearbox Planet Oil-Supply-Tube Assembly 100.0% N/A AE 2100D3-72-091 Rework the Compressor-to-Turbine Shaft 100.0% 100.0% AE 2100D3-72-099 1st- thru 5th-Stage Compressor Inner-Ring Segment End Gap 100.0% N/A AE 2100D3-72-102 No. 6 Carbon Seal Assembly with Steel Sleeve 99.6% 100.0% AE 2100D3-72-105 New No. 2 Ball Bearing (23066402) 44.4% N/A AE 2100D3-72-107 Front-Sump Housing Assembly - Rework 77.8% N/A AE 2100D3-72-110 New Compressor Vane Assembly Nuts 100.0% 100.0% AE 2100D3-72-125 New Center-Sump Housing 100.0% 100.0% AE 2100D3-72-140 Replace the Split Inner-Race Ball Bearing 100.0% N/A AE 2100D3-72-143 PGB-to-Power Section Strut Assembly - Repair 98.3% 100.0% AE 2100D3-72-145 New 2nd-Stage Gas-Generator Turbine Blade Track (23070945) 99.2% 100.0% AE 2100D3-72-151 New Torquemeter Shaft 100.0% 100.0% AE 2100D3-72-153 New 1st-Stage Gas-Generator Turbine Blades 96.7% 100.0% AE 2100D3-72-157 3rd-Stage Power Turbine Wheel - Shot Peening 92.6% 100.0% AE 2100D3-72-158 New Effusion-Cooled Combustion Liner Assembly 88.0% 100.0% AE 2100D3-72-159 New 4th and 5th-Stage Inner Ring Segment Assemblies 96.3% 100.0% AE 2100D3-72-160 New 2nd-Stage Gas-Generator Turbine Blade (23072136) 94.6% 100.0% AE 2100D3-72-162 New 3rd-Stage Power Turbine 2-Span and 5-Span Coverplates 96.7% 100.0% AE 2100D3-72-167 New No. 4 Carbon Seal (23070366 or 23071880) 100.0% 100.0% AE 2100D3-72-168 New #4 Teflon Seal 99.2% 100.0% AE 2100D3-72-172 New High Pressure Thrust Bearing Retainer Assembly (23073145) 98.8% 100.0% AE 2100D3-72-174 New Inlet Housing Hub Flowpath Extension (23073167) 98.8% 100.0% AE 2100D3-72-180 Remove the 2nd-Stage Gas-Generator Turbine Wheel Balance

Weights 93.4% 100.0%

AE 2100D3-72-181 New Compressor-Rear Air Seal (23073881) 95.5% 100.0% AE 2100D3-72-184 New Teflon (Omniseal) Seals 98.7% 100.0% AE 2100D3-72-185 New Teflon Seal (23073975) 98.3% 100.0% AE 2100D3-72-188 New No. 5 Carbon Seal (23073831) 97.5% 100.0% AE 2100D3-72-195 New 1st-Stage Compressor Blade Rear Retainer 89.3% 100.0% AE 2100D3-72-198 No. 6 Carbon Seal Assembly Test 95.5% 100.0% AE 2100D3-72-199 New No. 4 Bearing Spanner Nut (23074208) 95.5% 100.0% AE 2100D3-72-204 Install the 2nd-Stage Gas-Generator Turbine Wheel Balance

Weights (23038853) 94.6% 100.0%

AE 2100D3-72-206 New 6th thru 13th Stage Chrome Carbide Coated Knife Seal Comp

Wheels & Honeycomb Vanes 77.7% 100.0%

AE 2100D3-72-207 New Power Turbine Shaft Plug (23073072) 86.4% 100.0% AE 2100D3-72-214 New Center-Sump Rear Stationary Seal 94.2% 100.0% AE 2100D3-72-215 New Teflon Seal for Front Sump 95.0% 100.0% AE 2100D3-72-220 New Compressor Case Assembly with XPT blade Track Coating-

Rework 88.4% 100.0%

AE 2100D3-72-221 No. 4 Ball Bearing Inspection 79.3% 100.0% AE 2100D3-72-222 1st Stage Turbine Vane, Rail Hole Cooling 93.0% 100.0% AE 2100D3-72-223 1st Stage Gas Generator Turbine Blade-Rework 71.6% N/A AE 2100D3-72-228 New Compressor Rotor Assembly 74.0% 100.0% AE 2100D3-72-237 New Front Sump Oil Transfer Tube Assembly (23079312) 93.4% 100.0% AE 2100D3-72-238 Power Unit Accessory Drive-Bevel Spur Starter-Drive-Gearshaft-

Rework 100.0% 100.0%

AE 2100D3-72-239 Bevel Pinion Gearbox - Rework 90.1% 100.0% AE 2100D3-72-240 4th Stage Turbine Vane and Seal - Baffle Removal 92.1% N/A AE 2100D3-72-241 New Glass-Peened 1st-Stage Compressor Blade (23079367) 80.6% 100.0% AE 2100D3-72-244 New 2nd-Stage Gas-Generator Turbine Single Crystal Blade

(23079108) 88.8% 100.0%

AE 2100D3-72-287 Propeller Gearbox Main Diaphragm -Tapered Pin Removal 50.4% 100.0% AE 2100D3-73-003 New CVG-Actuator Drain Fuel Tube N/A N/A AE 2100D3-73-005 Fuel Pump and Metering Unit Upgrade 100.0% 100.0% AE 2100D3-73-009 Return Fuel Nozzles for Rework N/A N/A AE 2100D3-73-011 Clearance Hole for the Fuel-Flowmeter Support Bracket 100.0% 100.0% AE 2100D3-73-017 Replace the Test FCOC Tubes 100.0% 100.0% AE 2100D3-73-020 New Fuel-and-Metering Unit (FPMU 106) 100.0% N/A AE 2100D3-73-025 Introduction of New FCOC Tubes and Support…