DRAFT_SOW_12_May.docx

STATEMENT OF WORK (SOW)

F108 Low Pressure Turbine Assembly

MODULE 13/15

PURCHASE REQUEST NUMBER: FD2030-13-02133

REV. 0

PREPARATION DATE: 12 MAY 2014

PREPARING ORGANIZATION:

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

And

Air Force Life Cycle Management Center (AFLCMC) F108 Technical Services Element (LPSBAA)

TINKER AFB, OK 73145-3031

Table of Contents

SECTION I

1.0 Scope

This Statement of Work (SOW) defines the requirements necessary to ensure that delivered remanufactured F108-100 (CFM56-2B) Low Pressure Turbine Rotor and Frame Assembly Modules 13/15 and associated parts are restored as nearly as possible to original life expectancy consistent with AF requirements set forth or referenced herein. This SOW applies to the following National Stock Numbers (NSN) and Part Numbers (P/N):

LOW PRESSURE ROTOR AND FRAME ASSEMBLY MODULE #13/15

F108-100 (CFM56-2B)

The instructions stipulated are brief, concise statements providing general requirements for delivered remanufactured F108 Modules 13/15. All performance, with respect to the delivered remanufactured F108 Modules 13/15 and module components, shall be performed at a Contractor owned or operated Federal Aviation Administration Part 145 certified facility rated for CFM56-2B engine components that performs remanufacture using manufacturing processes similar to those used in the original manufacture of Modules 13/15. See FAR 22.1003-6(a)(1). Contractor shall have remanufacture capabilities to include required technical data, repair documents, and license agreements to accomplish remanufacture of F108 Modules 13/15 strictly in accordance with Government requirements and scheduled delivery of a quality product.

1.1 SOW Updates:

The Contractor shall not make any changes to the requirements in this SOW without written approval of the Procurement Contracting Officer (PCO). Contractor recommended changes shall be in writing (email is acceptable), but the Government shall maintain the SOW during the performance of this contract and ensure all changes are necessary and consistent with the requirement of FAR 22.1003-6(a)(1) prior to approval and performance.

1.2 Quality Control/Quality Assurance Plan:

The contractor shall develop, implement, and maintain an integrated Quality Control (QC)/Quality Assurance (QA) plan for the purpose of providing and maintaining confidence in contractor performance, product delivery, and data integrity throughout the life of the contract. Quality shall be ensured throughout the program in all areas of remanufacture, assembly inspection testing, and shipping.

The QC/QA plan shall be developed IAW AFPD 63-5, Quality Assurance and AFI63-501, Air Force Acquisition Quality Program, or an ISO 9000 certified plan to ensure quality across all aspects of the remanufacturing processes used, product assurance, reliability, maintainability, and supportability.

The Air Force reserves the right to verify the effectiveness of the QA program through reviews and audits of work in progress at the Contractor owned or operated facilities.

1.3 Subcontractor and Vendor Management:

The Contractor shall maintain a system for the management of subcontractors and vendors IAW the provisions of this contract. The Contractor shall ensure that all manufacturing processes, data, designs, and deliverables meet all F108 Modules 13/15 engineering and technical requirements, are in accordance with this SOW, and shall fulfill the requirements of this contract and FAR 22.1003-6(a)(1).

1.4 Transition and Relocation Plan:

The Contractor shall maintain and execute a transition plan detailing a ramp up/ramp down process that will not impact on-going remanufacturing processes as prescribed in FAR 22.1003-6(a)(1). This plan shall include transition strategies and shall describe the contractor own or operated facilities needed to support the deliverable modules, including the required manpower and skills to support the transition, and a schedule of the transition from roll-out to full operational status.

1.5 Contractor Relocation:

In the event relocation becomes necessary, the Contractor shall prepare a relocation plan and make available upon request to the Government. This plan shall include a listing of all completion dates of the steps required in the performance of the move and shall address on-site pre-teardown requirements, on-site re-assembly requirements, discrepancy correction, and transition security. The Contractor shall be responsible for the security of F108 Modules 13/15 Government Furnished Property (GFP) during relocation.

The Contractor shall coordinate the relocation schedule with the PCO/QAR to ensure no conflicts exist. In the event of relocation, the Contractor shall continue to provide support for the F108 Modules 13/15 at the new location IAW this SOW.

1.6 Safety:

The Contractor shall maintain and execute a safety program using MIL-STD-882D, AFI 91-301 and AFI 91-204 as guides. The Contractor shall comply with all safety provisions and technical specifications listed in CFM56 Engine Shop Maintenance Manual (CMM). All Contractor personnel and technicians shall comply with system safety engineering principles during all levels of remanufacturing.

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

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

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

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

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

d. Cause of accident/incident, if known

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

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

g. Corrective actions (taken or proposed)

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

1.7 General Services and Material:

The Contactor shall provide all materials for the manufacturing processes required to execute this contract. In exchange, in part, for each remanufactured module ordered, the Government will provide, on a one to one basis, degraded or inoperable GFP F108 13/15 modules free of meaningful damage inconsistent with aircraft engine usage.

1.8 Receiving:

The Contractor shall perform a visual inspection upon receipt for any shipping or packaging GFP damage. The Contractor shall report all Government delivered F108 Modules 13/15 GFP that are misidentified, misdirected, incomplete or missing parts to the PCO in writing (email is acceptable) for disposition instructions. The Contractor shall also perform a visual inspection upon receipt of GFP using CFM56 Engine Shop Maintenance Manual (CMM) 72-54-XX and 72-56-XX. The Contractor shall not destroy reusable shipping containers, and will reuse them for return shipment. In addition, the contractor shall submit SDRs related to shipment of misidentified items, variations in quantity, lost or damaged parcel post, and meaningful damage to GFP inconsistent with aircraft engine usage. These discrepancies shall be reported and resolved using the DoD web-based application WebSDR, located at:

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

1.8.1 Deficiency Report (DR) Investigation:

At the Government’s request, the Contractor shall investigate and submit findings to include root causes and a corrective action against all DRs submitted to Contractor against delivered remanufactured Modules 13/15 through this contract, which are returned as defective.

1.8.2 Condemnation of Assets:

The Contractor shall condemn, at the Contractor’s facility, any F108 Modules 13/15 component parts that do not meet Build Policy life cycle limits, or do not meet ESM “Serviceable Limits” and cannot be reworked per ESM guidance, before those components lose their identities as GFP and become contractor property. The Contractor shall process all condemned assets through Plant Clearance Automated Reutilization Screening System (PCARSS). The Contractor shall also provide Government quantities by P/N and NSN of components condemned and annotate on AFMC Form 413 Monthly Production Report via the Contract Data Requirements List (CDRL) DD Form 1423.

The Contractor shall report all condemned F108 Module 13/15’s via AFMC Form 413 (CDRL A002), Monthly Production Report and Commercial Asset Visibility for Air Force (CAVAF) System (CDRL A001). Condemnations and usage quantities shall be reported to 421 SCMS/GUMBA, Air Force Sustainment Center (AFSC) via Interim Contract Support (ICS) Parts Usage and Maintenance Data Collection Report (CDRL A004).

1.8.3 Supply Discrepancy Report (SDR):

The Contractor shall submit SDRs when required IAW the contract’s CAVAF Statement of Work, Section 7. Contractor shall process DRs when required IAW Section 1.6 of this SOW.

1.9 Remanufacture:

Remanufactured modules shall be restored to original life expectancy of at least 3500 cycles, in compliance with all applicable CFM56-2B Engine Shop Manual (ESM) and Service Bulletin/Airworthiness Directive Requirements. The Contractor shall perform all inspections, parts usage, manufacturing processes, assembly, adjustments, calibrations, testing and operational checks, correct all discrepancies and malfunctions, and verify acceptable ESM condition of any component, system, or subsystem.

1.9.1 Remanufacture Procedures:

F108 Modules 13/15 shall be remanufactured and component parts shall be reworked, rehabilitated, and/or altered IAW the procedures outlined in ESM 72-54-00 through 72-54-20 and 72-56-00 through 72-56-10, which includes the Standard Practice Manual CFMI-TP-SP.2.0. Delivered remanufactured Modules 13/15 shall only contain hardware meeting the requirements of this SOW. The Contractor shall inspect all components to ensure that they meet United States Air Force (USAF) build requirements.

The Contractor shall acquire component parts from vendors approved by the Air Force, vendors approved by the Original Equipment Manufacturer (OEM), Government inventory, or commercial inventories approved by the USAF and/or OEM. Life Limited Parts (LLP) shall be either new and unused from sources approved by the Air Force, or sourced from government F108/CFM56-2B engine configurations. The Contractor shall check records for all non-new LLPs to ensure component life cycle limits have not been exceeded. In addition, the Contractor shall ensure that all non-new LLPs have a minimum of 3500 cycles (Build Policy) remaining for use in remanufactured Modules 13/15. LLPs assembled in delivered remanufactured F108 Modules 13/15 shall not have been replaced by repaired/reconditioned commercial parts or be sourced from commercial fleets. The Contractor shall provide certification of the remaining life of each LLP assembled in all delivered remanufactured Modules 13/15, and have records (subject to inspection by the government) that will confirm all LLPs have a minimum of 3500 cycles remaining.

New and unused non-LLP components shall be from vendors approved by the Air Force, vendors approved by the OEM, or Government inventory. Non-LLP used commercial components assembled in remanufactured modules delivered to the Government shall be from used commercial inventories acquired originally from vendors approved by the Air Force or OEM. The Contractor shall not acquire non-LLP used commercial parts from supplier sources that have been subject to any violation, penalty, or disciplinary actions leading to FAA disapproval of its aircraft, engine maintenance, or operations. The Contractor shall provide FAA Form 8130-3 documentation for each used component in a module at time of module delivery.

The Contractor shall ensure all four stages of LPT blades are either new and unused or fully restored per ESM guidance. ESM “Serviceable Limits” are sufficient to determine LPT blade usability only when there is no corresponding repair attached to the inspection. All knife edges and Z-notches shall be fully restored per ESM guidance. Blending per ESM guidance is allowed for airfoil restoration. All LPT blades used must meet the following pre-twist angle requirements:

Stage 1 minimum pre-twist angle = 2.07 deg Stage 2 minimum pre-twist angle = 2.55 deg Stage 3 minimum pre-twist angle = 3.50 deg Stage 4 minimum pre-twist angle = 4.70 deg The Contractor shall ensure that all abradable honeycomb seals are replaced with newly-manufactured abradable honeycomb seals on all delivered Modules 13/15.

All remanufactured Modules delivered will meet the inspection criteria established in T.O. Reference CFM56-2B Engine Shop Manual Task 72-00-54-200-001-D, paragraph 3.E. LOW PRESSURE TURBINE ROTOR/STATOR MODULE-INSPECTION and must comply with Service Bulletin 72-0365. Rotor and frame assembly component parts used shall be inspected to piece part requirements outlined for that specific part IAW CFM56-2B ESM. All remanufactured components shall comply with the latest revision of all CFM56-2B service bulletins, along with any outstanding FAA Airworthiness Directives.

Each remanufactured Turbine Frame Assembly shall be matched to its Low Pressure Turbine Rotor Assembly through #5 bearing adjusting sleeve. Remanufactured Turbine Frames and #5 bearing supports shall include rework of the adjusting sleeve per CFM56-2B, ESM 72-00-03 (Refer to caution in 72-00-56-20 turbine frame removal). Remanufactured parts must be identified and match-marked for inspection and assembly operations.

1.9.2 Testing & Evaluation:

The Contractor shall conduct all testing IAW CFM56-2B guidance. The Government reserves the right to witness any and/or all tests conducted by the Contractor and/or subcontractors on a noninterference basis.

1.9.3 Remanufacture Deviations:

Manufacturing and inspection processes used shall be in accordance with ESM 72-54-00 thru 72-54-020 and 72-56-00 thru 72-56-010, Service Bulletin requirements, and comply with FAR 22.1003-6(a)(1)(iv). Prior to Contractor’s effecting deviations in manufacturing or inspection processes for Modules 13/15 or component parts, the Contractor shall obtain written approval for deviations from the PCO.

1.9.4 Deliverables Quality:

The Contractor shall ensure that materials, parts, and accessories used in remanufactured components are restored to original life expectancy or nearly so, and are interchangeable without alteration.

1.9.5 Designated Engineering Representative (DER) Processes and Procedures:

The Contractor shall obtain written approval from the PCO for all DER manufacturing processes and procedures (email is acceptable), prior to using those DER manufacturing processes and procedures in the remanufacture of F108 Modules 13/15 or component parts.

1.9.6 Parts Not Listed in the Illustrated Parts Catalogue (IPC):

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

1.9.7 Documentation and Certification of Remanufacture:

The Contractor shall provide completed documentation with each delivered remanufactured F108 Module 13/15. The documentation for delivered remanufactured Modules 13/15 shall have correct part numbers and/or assembly part numbers and serial numbers, as well as certification that the delivered modules strictly comply with this SOW. The Contractor shall identify and list all service bulletins applied during the remanufacture of delivered F108 Modules 13/15.

1.10 FAA Form 8130-3:

The Contractor shall provide a completed FAA Form 8130-3, Airworthiness Approval Tag, with each remanufactured assembly or remanufactured component part used therein prior to acceptance by the Government. In item 13 (remarks), list CFM56-2B Service Bulletins applied in reworking a part or assembly to an authorized output part number. (Example: CFM56-2B, SB 72-0365).

1.11 Quality System and Quality Assurance:

Each remanufactured F108 Module 13/15 shall be delivered to the Government defect free. The Contractor shall maintain a system that adheres to the requirements of International Standard Organization (ISO) 9001.2000/ANSI/ASQC Q92, Quality Systems Model for Quality Assurance in Design/Development, Production, Installation, and Servicing and supplement requirements imposed by this contract. Develop and implement procedures to properly maintain measuring and test equipment IAW ANSI/NCSL 2340-1. The quality system will include a clear and complete set of work documents for all manufacturing and inspection processes required by this contract. The Contractor’s quality program shall be designed to promptly detect and correct conditions adverse to quality.

1.12 Packaging and Handling:

The Contractor shall be responsible for the preservation and packaging of the delivered F108 Module 13/15 IAW the Special Packaging Instructions specified on AFMC Form 158, Packaging Requirements. The Contractor shall place a serviceable tag, Department of Defense (DD) Form 1574, inside the package along with the assembly as well as outside the package. In addition, all marking and labeling of unit and shipping containers shall be in accordance with Mil-Std-129P, Department of Defense Standard Practice, Military Marking for Shipment and Storage. Use additional guidance for preparation and shipment IAW T.O. 00-20-1, 00-20-3, MIL-STD-2073-1, MIL-STD-129, AFPAM24-237, and AFMAN 24-206. Contractor shall not use Commercial Packaging.

1.13 Schedule:

Any changes to contractual milestones shall be made only with Program Office coordination and written approval of the PCO (email is acceptable). Production or delivery problems which have developed, or are developing, and have the potential to stop, interrupt, or otherwise impact the production or delivery of remanufactured F108 Modules 13/15 will be reported to the Program Management Office via the PCO within 7 calendar days of discovery.

1.14 Shipping and Transportation:

The Contractor shall meet the delivery schedule as outlined in Schedule B of the contract. The Contractor shall ship or transport applicable contractor supplies and materials as appropriate in order to have the contractor supplies and materials available to support the customer’s operational requirements and IAW the contract.

1.15 Document Storage:

All records and reports outlined in this SOW shall be prepared for each part and a copy kept on file by the Contractor for five (5) years after contract completion. The Government Technical Representative reserves the right to request and view any records at any time.

1.16 Mission Essential Services:

N/A

1.17 Contractor Identification to Government Employees:

Contractor employees shall identify themselves as Contractor personnel by introducing themselves or being introduced as Contractor personnel and displaying distinguishing badges or other visible identification for meetings with Government personnel. In addition, Contractor personnel shall appropriately identify themselves as Contractor employees in telephone conversations and in formal and informal written correspondence.

SECTION II

2.0 Applicable Documents

2.1 Reporting:

The Contractor shall meet the delivery schedule. Contractor shall provide completed FAA Form 8130-3 with each remanufactured F108 Module 13/15 and component parts. This documentation shall have part number, serial number, work accomplished, and Service Bulletins applied, on a DD Form 1574 tag. The Contractor shall ensure that all reporting as specified under the following CDRL is accomplished:

2.2 Reference & Technical Manuals:

In execution of this SOW, the Contractor shall apply manufacturing processes, tools, and products as prescribed in FAR 22.1003-6(a)(1)(iv) and in accordance with (IAW) CFM56 Engine Shop Maintenance Manual (CMM) 72-54-XX and 72-56-XX, CFM56-2B Service Bulletins, CFM56-2B Engine Shop Manual 72-54-00 and 72-56-00 through 72-56-10, and CFMI-TP-SP.2. All remanufactured modules must meet the inspection criteria established in T.O. reference CFM56-2B Engine Shop Manual Task 72-00-54-200-001-D Low Pressure Turbine Rotor/Stator Module –Inspection and must comply with Service Bulletin 72-0365.

SECTION III

3.0 REQUIREMENTS

3.1 Government Furnished Material (GFM):

None. Contractor shall furnish all material, support equipment, tools, test equipment and services. Government Furnished Material will not be provided.

Contractor furnished material used for replacement components shall be parts specified in ESM CFM56-2B Engine Shop Manual. Any deviations shall have written approval from Propulsion Engineering, AFLCMC/LPSBAA and AFLCMC/LPSBAB through the PCO.

3.2 Government Furnished Property (GFP):

GFP shipped to the contractor ceases to be GFP at the point identified in FAR 22.1003-6(a)(1)(v), except as specified in SOW Section 1.8.

APPENDIX “A”

ACRONYMS

File No: FD2030-13-02133

File No: FD2030-13-02133 image1.emf

Interim Rpt ERRC N Non Reparable NSNs DLA,IPV.xlsx 13-15 ERRC T (Work Package)

F108 Module 13/15 ERRC T, REPARABLE NSNs WITH WORK PACKAGE

Module Serial Number:

Nomenclature NSN PN Work Package Repair Quantity in TO Repairs Performed Quantity Condemned Quantity

001 002 003 004 005 006 007 008 009 010 011 012 013 014 015 016 017

LPT Rotor Blades, Stage 1 2840-01-466-7430 Unknown 72-54-01 7

LPT Rotor Blades, Stage 2 2840-01-466-7140 Unknown 72-54-02 11

LPT Rotor Blades, Stage 3 2840-01-187-8239 301-330-321-0 11

LPT Rotor Blades, Stage 4 2840-01-189-2914 301-330-438-0 11

LPT Rotor Disk 2840-01-185-6489 301-331-126-0

LPT Rotor Disks, Stage 1 2840-01-856-6489 301-331-126-0 72-54-03 0

LPT Rotor Disks, Stage 2 2840-01-856-6490 301-331-227-0 0

LPT Rotor Disks, Stage 3 2840-01-185-6491 301-331-322-0 0

LPT Rotor Disks, Stage 4 2840-01-185-6492 301-331-427-0 0

LPT Shroud Support 2840-01-185-6427 301-555-227-0 72-54-04 8

LPT Rotor Support Unknown Unknown 72-54-05 3

LPT Rotating Air Seals Unknown Unknown 72-54-06 4

LPT Case 2840-01-185-6488 Unknown 72-54-07 13

LPT Nozzle Segment, Stage 2 2840-01-344-3233 305-390-/308/311-0 72-54-08 17

LPT Nozzle Segment, Stage 3 2840-01-341-0050 305-390-705-0 17

LPT Nozzle Segment, Stage 4 2840-01-187-3198 305-390-904-0 17

LPT Inner Stationary Air Seal Unknown Unknown 72-54-09 3

LPT Thermal Insulation Blanket Unknown Unknown 72-54-10 1

LPT Cooling Air Tube Assembly Not Applicable Not Applicable 72-54-11 2

LPT Outer Stationary Air Seal Unknown Unknown 72-54-12 5

LPT Cooling Air Manifolds Not Applicable Not Applicable 72-54-13 4

13-15 ERRC T (No Work Package)

F108 Module 13/15 ERRC T, REPARABLE NSNs WITHOUT WORK PACKAGE

Nomenclature NSN PN Quantity Replaced

Turbine Frame 2840-01-139-4018PN 301-316-869-0

Turbine Conical Support 2840-01-185-6424PN 305-056-116-0

Turbine Assembly 2840-01-211-0178PN 301-412-083-0

Air Seal, Stage 4 2840-01-417-6409PN 335-040-606-0

Turbine Assembly 2840-01-211-0178PN 301-412-083-0

Aircraft Seal 2840-01-185-6426PN 301-332-016-0

Turbine Disk, Stage 4 2840-01-185-6492PN 301-331-429-0

Seg Seal, Stage 4 2840-01-417-6409PN 335-040-606-0

Air Seal 2840-01-189-2631PN 301-317-621-0

Nozzle Segment, Stage 4 2840-01-187-3158PN 305-391-003-0

Air Seal 2840-01-185-6425PN 301-331-923-0

Turbine Blade, Stage 3 2840-01-372-5896PN 301-330-325-0

Turbine Disk, Stage 3 2840-01-185-6491PN 301-331-322-0

Air Seal 2840-01-187-3046PN 335-040-505-0

Seg Seal, Stage 3 2084-01-187-3179PN 301-317-923-0

Seg Seal, Stage 3 2084-01-187-3179PN 301-317-927-0

Nozzle Segment, Stage 3 2840-01-341-0068PN 305-390-805-0

Rotating Air Seal, Stage 2 2840-01-185-6423PN 301-331-820-0

Blade, Stage 2 2840-01-187-8239PN 301-330-221-0

Blade, Stage 2 2840-01-466-7740PN 301-330-222-0

LPT Disk, Stage 2 2840-01-185-6490PN 301-331-227-0

Aircraft Seal 2840-01-341-9081PN 305-040-407-0

Air Seal 2840-01-185-6429PN 301-317-826-0

Nozzle Segment, Stage 2 (CD) 2840-01-345-4795PN 305-390-518-0

Nozzle Segment, Stage 2(CD) 2840-01-340-9213PN 305-390-408-0

Rotating Air Seal, Stage 1 2840-01-185-6422PN 301-331-721-0

Blade, Stage 1 2840-01-466-7141PN 301-330-115-0

Seg Seal, Stage 1 2840-01-212-1035PN 301-317-321-0

LPT Rear Case Assembly 2840-01-455-7988PN 305-078-653-0

Ring-Sector Support 2840-01-262-8042PN 305-386-609-0

15 ERRC T (Work Package)

F108 Module 15 ERRC T, REPARABLE NSNs WITH WORK PACKAGE

Nomenclature NSN PN Work Package Repair Quantity in TO Repairs Performed Quantity Condemned Quantity

001 002 003 004 005 006 007 008 009 010 011 012 013 014 015 016 017

LPT Frame Unknown Unknown 72-56-01 14

No 5 Bearing Support Assy 2840-01-192-5345 Unknown 72-56-02 6

Oil Sump Assy 2840-01-196-6004 Unknown 72-56-03 4

Midstream Fairing 2840-01-206-9820 Unknown 72-56-04 2

Oil Inlet Cover 2840-01-189-2857 Unknown 72-56-06 3

Flame Arrestor Assy Not Applicable Not Applicable 72-56-08 1

Flange 4730-01-181-1064 Unknown 72-56-09 1

Turbine Frame Hardware Unknown Unknown 72-56-10 1

13-15 ERRC N (DLA, IPV)

ERRC N, NON-REPARABLE NSNs (DLA, IPV)

Nomenclature NSN PN Quantity Replaced Replacement %

Rivet 5320005504055SX AN123322

Bolt 5306005389046NY J644P04D

Plug 5342011848596PN 301-595-102-0

Packing Assembly 5330014236747SX 305-483-202-0

Pipe Flange 4730011811069SX 305-380-401-0

Packing Assembly 5330014236744SX 305-482-802-0

Tube Assembly 4710011759254 305-379-804-0

Machine Bolt 5306010056711NY J643P06A

Loop Clamp 5340012594151SX J1220G06

Self-Lock Nut 5310011797823SX J979P05

Machine Bolt 5306005108553NY J645P17A

Support 5340-011780034 305-050-106-0

Oil Sump 2840014301109SX 305-046-922-0

Abraidable Liner 2840012392726PN 301-285-112-0

Abraidable Liner 2840012392727PN 301-287-711-6

Pipe Flange 4730013433108SX 301-413-313-6

Tube Assembly Unknown 305-951-901-0

Half-Case Unknown 334-007-019-0

Nozzle Unknown 305-369-105-6

Tube Sleeve 2840011873028PN 305-377-813-6

Support 2840011925345PN 301-321-270-0

Insert 5325015025850SX SRWK258L0024

Insert 5325013424893SX SRK258L0024

Nipple Unknown 305-376-903-6

Machine Bolt 5306005263990NY J644P07A

Fairing 2840012069820PN 301-321-612-0

Rivet 5320-011910175 21217TC2406

Anchor Nut 5310-996172377 AS46726

Self-Lock Nut 5310-014945830 J979P04

Bolt 5306000977307SX J644P12A

Bearing Support 2840011892857PN 335-071-002-0

Frame Assembly Unknown 335-014-620-0

Bushing Unknown 334-007-080-0

Self-Lock Nut Unknown 649-785-258-0

Self-Lock Nut Unknown 649-785-259-0

Stud 5307011907225SX 301-568-711-0

Elbow 4730-013260750 305-980-005-6

Pin 5315008840180SX R261P06

Nut 4730008212468SX R260P06L

Tube Assembly 4710012676815SX 301-559-705-6

Nipple 4730012676816SX 305-981-002-6

Sleeve Bushing 3120-012703878 334-007-066-0

Sleeve Bushing Unknown 334-007-082-0

Sleeve Bushing Unknown 334-007-081-0

Swivel Wire Unknown R261P12

Connector Nut Unknown R260P12L

Nipple Unknown J385P12

Nut 4730009162005SX MS919712

Nut 5310011753711JF J980P04

Bolt 5306011774989JF J814P02A

Borescope Plug 6650014240967TG 305-381-303-0

Retaining Hook 2840012517753PN 301-328-701-0

Strip Cover 2840012517754PN 301-328-101-0

Aircraft Strip 2840014219369SX 334-007-330-0

Bushing 2840014219371SX 334-007-198-0

Bolt-Slabbed 5306-011832120 9115M80P07

LPT Str Shroud Shield 2840011873194PN 301-324-504-0

Insert 5342011835092SX 305-056-201-0

Honeycomb Liner 2840012620472PN 334-007-033-0

Honeycomb Liner 2840012719160PN 334-007-042-0

Stop 2840012517758PN 301-595-702-6

Strip Cover 2840012517752PN 301-318-310-0

Plate-Rein, Stage 3 2840014219365SX 301-318-620-0

Strip-Steel, Stage 3 2840014219372SX 334-007-208-0

Strip (Plate-Preinserted) 2840014219361SX 334-007-229-0

LPT Str Shroud Shield 2840013538259SX 301-324-304-0

Retainer Blade, Stage 2 2840011873001PN 301-332-207-0

Anti Wear Shield 2840011892860PN 305-415-601-0

Honeycomb Liner 2840012633297PN 334-007-030-0

Sealing Sleeve 4730-011834903 301-581-007-0

Strip Cover 2840012517751PN 301-318-411-0

Plate-Rein, Stage 2 2840014219373SX 301-318-520-0

Plate-Rein, Stage 2 2840014219367SX 334-007-195-0

Support Strip 2840014373389SX 334-007-207-0

Heat Shield 2840011873193PN 301-324-110-0

Dee Bolt 5306-011875288 649-779-057-0

Retainer Blade, Stage 1 2840011873044PN 301-332-108-0

Deflector 5340011892569PN 301-567-701-0

Anti Wear Shield 2840011873043PN 305-385-102-0

Retaining Hook 2840012517759PN 301-327-103-0

Central Lip 2840012517757PN 301-518-904-0

Strip Cover 2840012517756PN 305-365-302-0

Strip Cover 2840012517755PN 305-365-401-0

Ring 5365012620471PN 334-007-036-6

Screw-Machine Flat Hd 53050010103683SX NAS1102E3-12

Threaded Bushing Unknown 334-007-085-0

Rivet 5320016384921SX AN123639

Rivet 5320013553562SX 21217TC3214

Bracket 5342012682585SX 305-482-601-0

Bracket 5342012687604SX 305-402-504-0

Bracket 5340014498374SX 305-402-404-0

Bracket 5342012696110SX 305-404-503-0

Rivet 5320002057768SX 21217TC3209

Rivet 5320-011904437 21217TC3210

Screen Collar 2840014486110SX 305-386-309-0

Screen Collar Unknown 305-386-408-0

Rivet 5320002791282SX AN123371

Rivet 5320013556675SX 21215TC5614

Ring-Sector Support 2840012711625PN 305-386-506-0

Ring-Sector Support 2840012639339PN 305-386-708-0

Ring-Sector Support 2840012619956PN 305-386-805-0

Bracket-Angle 5340012665861SX 305-387-302-0

Bracket-Angle 5340012687690SX 305-070-005-0

Insulation Blanket 2835012619979PN 305-389-402-0

Insulation Blanket 2835012619980PN 305-393-902-0

Blade Retainer 2840011873045PN 301-332-313-0

Insulation Blanket 2840011873211PN 305-390-001-0

Insulation Blanket 2840011873212PN 305-390-101-0

Insulation Blanket 2840011873214PN 305-389-301-0

Insulation Blanket 2840011873215PN 305-389-401-0

Insulation Blanket 2840011873216PN 305-385-202-0

Insulation Blanket 2840011892656PN 305-389-701-0

Insulation Blanket 2840011892657PN 305-390-201-0

Insulation Blanket 2840011892658PN 305-389-901-0

Insulation Blanket 2840011892660PN 305-389-601-0

Insulation Blanket 2840011892661PN 305-389-801-0

Insulation Blanket 2840011892662PN 305-394-001-0

Insulation Blanket 2840011892669PN 305-393-901-0

Insulation Blanket 2840012517749PN 305-394-202-0

Insulation Blanket 2840012619976PN 305-389-002-0

Insulation Blanket 2840012619977PN 305-389-102-0

Insulation Blanket 2840012619978PN 305-389-202-0

Insulation Blanket 2840012629597PN 305-393-802-0

Counter Balance Weight 3040011873121PN 301-332-446-0

Counter Balance Weight 3040011873122 301-332-454-0

Counter Balance Weight 3040011873123 301-332-455-0

Counter Balance Weight 3040011873127PN 301-332-448-0

Counter Balance Weight 3040011873128PN 301-332-449-0

Counter Balance Weight 3040011873129PN 301-332-450-0

Counter Balance Weight 3040011873130 301-332-451-0

Counter Balance Weight 3040011873131 301-333-452-0

Counter Balance Weight 3040011873132 301-333-453-0

Counter Balance Weight 3040011873133 301-332-456-0

Counter Balance Weight 3040011873126PN 301-332-447-0

Sleeve Bushing 3120011872708 305-074-104-0

Sealing Sleeve 4730011834903 301-581-006-0

Machine Screw 5305012189768SX NAS1102E3-3

Machine Bolt 5306011624738SX J644P07B

Machine Bolt 5306011774989JF J814P020A

Dee Bolt 5306011833911SX 649-779-056-0

Self-Lock Nut 5310010363814NY J979P03

Self-Lock Nut 5310011753711JF H50185-4

Self-Lock Nut 5310011787518JF J980P05

Plain Washer 5310011868919SX 649-341-010-0

Retaining Ring 5325012106838SX J206P0051

Strip Seal 5330011834905SX 301-325-503-0

Strip Seal 5330011834906SX 301-329-003-0

Nonmetallic Seal 5330011837116SX 301-325-404-0

Nonmetallic Seal 5330011837117SX 301-325-203-0

Nonmetallic Seal 5330011837118SX 301-325-303-0

O-Ring 5331011837091SX 301-325-107-0

Deflector 5340011892569PN 301-567-701-0

Bushing 5365011848541SX 301-557-402-0 image2.emf

Interim Rpt ERRC T NSNs NO Work Pckg.xlsx 13-15 ERRC T (Work Package)

F108 Module 13/15 ERRC T, REPARABLE NSNs WITH WORK PACKAGE

Module Serial Number:

Nomenclature NSN PN Work Package Repair Quantity in TO Repairs Performed Quantity Condemned Quantity

001 002 003 004 005 006 007 008 009 010 011 012 013 014 015 016 017

LPT Rotor Blades, Stage 1 2840-01-466-7430 Unknown 72-54-01 7

LPT Rotor Blades, Stage 2 2840-01-466-7140 Unknown 72-54-02 11

LPT Rotor Blades, Stage 3 2840-01-187-8239 301-330-321-0 11

LPT Rotor Blades, Stage 4 2840-01-189-2914 301-330-438-0 11

LPT Rotor Disk 2840-01-185-6489 301-331-126-0

LPT Rotor Disks, Stage 1 2840-01-856-6489 301-331-126-0 72-54-03 0

LPT Rotor Disks, Stage 2 2840-01-856-6490 301-331-227-0 0

LPT Rotor Disks, Stage 3 2840-01-185-6491 301-331-322-0 0

LPT Rotor Disks, Stage 4 2840-01-185-6492 301-331-427-0 0

LPT Shroud Support 2840-01-185-6427 301-555-227-0 72-54-04 8

LPT Rotor Support Unknown Unknown 72-54-05 3

LPT Rotating Air Seals Unknown Unknown 72-54-06 4

LPT Case 2840-01-185-6488 Unknown 72-54-07 13

LPT Nozzle Segment, Stage 2 2840-01-344-3233 305-390-/308/311-0 72-54-08 17

LPT Nozzle Segment, Stage 3 2840-01-341-0050 305-390-705-0 17

LPT Nozzle Segment, Stage 4 2840-01-187-3198 305-390-904-0 17

LPT Inner Stationary Air Seal Unknown Unknown 72-54-09 3

LPT Thermal Insulation Blanket Unknown Unknown 72-54-10 1

LPT Cooling Air Tube Assembly Not Applicable Not Applicable 72-54-11 2

LPT Outer Stationary Air Seal Unknown Unknown 72-54-12 5

LPT Cooling Air Manifolds Not Applicable Not Applicable 72-54-13 4

F108 Module 13/15 ERRC T, REPARABLE NSNs WITHOUT WORK PACKAGE

Nomenclature NSN PN Quantity Replaced

Turbine Frame 2840-01-139-4018PN 301-316-869-0

Turbine Conical Support 2840-01-185-6424PN 305-056-116-0

Turbine Assembly 2840-01-211-0178PN 301-412-083-0

Air Seal, Stage 4 2840-01-417-6409PN 335-040-606-0

Turbine Assembly 2840-01-211-0178PN 301-412-083-0

Aircraft Seal 2840-01-185-6426PN 301-332-016-0

Turbine Disk, Stage 4 2840-01-185-6492PN 301-331-429-0

Seg Seal, Stage 4 2840-01-417-6409PN 335-040-606-0

Air Seal 2840-01-189-2631PN 301-317-621-0

Nozzle Segment, Stage 4 2840-01-187-3158PN 305-391-003-0

Air Seal 2840-01-185-6425PN 301-331-923-0

Turbine Blade, Stage 3 2840-01-372-5896PN 301-330-325-0

Turbine Disk, Stage 3 2840-01-185-6491PN 301-331-322-0

Air Seal 2840-01-187-3046PN 335-040-505-0

Seg Seal, Stage 3 2084-01-187-3179PN 301-317-923-0

Seg Seal, Stage 3 2084-01-187-3179PN 301-317-927-0

Nozzle Segment, Stage 3 2840-01-341-0068PN 305-390-805-0

Rotating Air Seal, Stage 2 2840-01-185-6423PN 301-331-820-0

Blade, Stage 2 2840-01-187-8239PN 301-330-221-0

Blade, Stage 2 2840-01-466-7740PN 301-330-222-0

LPT Disk, Stage 2 2840-01-185-6490PN 301-331-227-0

Aircraft Seal 2840-01-341-9081PN 305-040-407-0

Air Seal 2840-01-185-6429PN 301-317-826-0

Nozzle Segment, Stage 2 (CD) 2840-01-345-4795PN 305-390-518-0

Nozzle Segment, Stage 2(CD) 2840-01-340-9213PN 305-390-408-0

Rotating Air Seal, Stage 1 2840-01-185-6422PN 301-331-721-0

Blade, Stage 1 2840-01-466-7141PN 301-330-115-0

Seg Seal, Stage 1 2840-01-212-1035PN 301-317-321-0

LPT Rear Case Assembly 2840-01-455-7988PN 305-078-653-0

Ring-Sector Support 2840-01-262-8042PN 305-386-609-0

F108 Module 15 ERRC T, REPARABLE NSNs WITH WORK PACKAGE

Nomenclature NSN PN Work Package Repair Quantity in TO Repairs Performed Quantity Condemned Quantity

001 002 003 004 005 006 007 008 009 010 011 012 013 014 015 016 017

LPT Frame Unknown Unknown 72-56-01 14

No 5 Bearing Support Assy 2840-01-192-5345 Unknown 72-56-02 6

Oil Sump Assy 2840-01-196-6004 Unknown 72-56-03 4

Midstream Fairing 2840-01-206-9820 Unknown 72-56-04 2

Oil Inlet Cover 2840-01-189-2857 Unknown 72-56-06 3

Flame Arrestor Assy Not Applicable Not Applicable 72-56-08 1

Flange 4730-01-181-1064 Unknown 72-56-09 1

Turbine Frame Hardware Unknown Unknown 72-56-10 1

ERRC N, NON-REPARABLE NSNs (DLA, IPV)

Nomenclature NSN PN Quantity Replaced Replacement %

Rivet 5320005504055SX AN123322

Bolt 5306005389046NY J644P04D

Plug 5342011848596PN 301-595-102-0

Packing Assembly 5330014236747SX 305-483-202-0

Pipe Flange 4730011811069SX 305-380-401-0

Packing Assembly 5330014236744SX 305-482-802-0

Tube Assembly 4710011759254 305-379-804-0

Machine Bolt 5306010056711NY J643P06A

Loop Clamp 5340012594151SX J1220G06

Self-Lock Nut 5310011797823SX J979P05

Machine Bolt 5306005108553NY J645P17A

Support 5340-011780034 305-050-106-0

Oil Sump 2840014301109SX 305-046-922-0

Abraidable Liner 2840012392726PN 301-285-112-0

Abraidable Liner 2840012392727PN 301-287-711-6

Pipe Flange 4730013433108SX 301-413-313-6

Tube Assembly Unknown 305-951-901-0

Half-Case Unknown 334-007-019-0

Nozzle Unknown 305-369-105-6

Tube Sleeve 2840011873028PN 305-377-813-6

Support 2840011925345PN 301-321-270-0

Insert 5325015025850SX SRWK258L0024

Insert 5325013424893SX SRK258L0024

Nipple Unknown 305-376-903-6

Machine Bolt 5306005263990NY J644P07A

Fairing 2840012069820PN 301-321-612-0

Rivet 5320-011910175 21217TC2406

Anchor Nut 5310-996172377 AS46726

Self-Lock Nut 5310-014945830 J979P04

Bolt 5306000977307SX J644P12A

Bearing Support 2840011892857PN 335-071-002-0

Frame Assembly Unknown 335-014-620-0

Bushing Unknown 334-007-080-0

Self-Lock Nut Unknown 649-785-258-0

Self-Lock Nut Unknown 649-785-259-0

Stud 5307011907225SX 301-568-711-0

Elbow 4730-013260750 305-980-005-6

Pin 5315008840180SX R261P06

Nut 4730008212468SX R260P06L

Tube Assembly 4710012676815SX 301-559-705-6

Nipple 4730012676816SX 305-981-002-6

Sleeve Bushing 3120-012703878 334-007-066-0

Sleeve Bushing Unknown 334-007-082-0

Sleeve Bushing Unknown 334-007-081-0

Swivel Wire Unknown R261P12

Connector Nut Unknown R260P12L

Nipple Unknown J385P12

Nut 4730009162005SX MS919712

Nut 5310011753711JF J980P04

Bolt 5306011774989JF J814P02A

Borescope Plug 6650014240967TG 305-381-303-0

Retaining Hook 2840012517753PN 301-328-701-0

Strip Cover 2840012517754PN 301-328-101-0

Aircraft Strip 2840014219369SX 334-007-330-0

Bushing 2840014219371SX 334-007-198-0

Bolt-Slabbed 5306-011832120 9115M80P07

LPT Str Shroud Shield 2840011873194PN 301-324-504-0

Insert 5342011835092SX 305-056-201-0

Honeycomb Liner 2840012620472PN 334-007-033-0

Honeycomb Liner 2840012719160PN 334-007-042-0

Stop 2840012517758PN 301-595-702-6

Strip Cover 2840012517752PN 301-318-310-0

Plate-Rein, Stage 3 2840014219365SX 301-318-620-0

Strip-Steel, Stage 3 2840014219372SX 334-007-208-0

Strip (Plate-Preinserted) 2840014219361SX 334-007-229-0

LPT Str Shroud Shield 2840013538259SX 301-324-304-0

Retainer Blade, Stage 2 2840011873001PN 301-332-207-0

Anti Wear Shield 2840011892860PN 305-415-601-0

Honeycomb Liner 2840012633297PN 334-007-030-0

Sealing Sleeve 4730-011834903 301-581-007-0

Strip Cover 2840012517751PN 301-318-411-0

Plate-Rein, Stage 2 2840014219373SX 301-318-520-0

Plate-Rein, Stage 2 2840014219367SX 334-007-195-0

Support Strip 2840014373389SX 334-007-207-0

Heat Shield 2840011873193PN 301-324-110-0

Dee Bolt 5306-011875288 649-779-057-0

Retainer Blade, Stage 1 2840011873044PN 301-332-108-0

Deflector 5340011892569PN 301-567-701-0

Anti Wear Shield 2840011873043PN 305-385-102-0

Retaining Hook 2840012517759PN 301-327-103-0

Central Lip 2840012517757PN 301-518-904-0

Strip Cover 2840012517756PN 305-365-302-0

Strip Cover 2840012517755PN 305-365-401-0

Ring 5365012620471PN 334-007-036-6

Screw-Machine Flat Hd 53050010103683SX NAS1102E3-12

Threaded Bushing Unknown 334-007-085-0

Rivet 5320016384921SX AN123639

Rivet 5320013553562SX 21217TC3214

Bracket 5342012682585SX 305-482-601-0

Bracket 5342012687604SX 305-402-504-0

Bracket 5340014498374SX 305-402-404-0

Bracket 5342012696110SX 305-404-503-0

Rivet 5320002057768SX 21217TC3209

Rivet 5320-011904437 21217TC3210

Screen Collar 2840014486110SX 305-386-309-0

Screen Collar Unknown 305-386-408-0

Rivet 5320002791282SX AN123371

Rivet 5320013556675SX 21215TC5614

Ring-Sector Support 2840012711625PN 305-386-506-0

Ring-Sector Support 2840012639339PN 305-386-708-0

Ring-Sector Support 2840012619956PN 305-386-805-0

Bracket-Angle 5340012665861SX 305-387-302-0

Bracket-Angle 5340012687690SX 305-070-005-0

Insulation Blanket 2835012619979PN 305-389-402-0

Insulation Blanket 2835012619980PN 305-393-902-0

Blade Retainer 2840011873045PN 301-332-313-0

Insulation Blanket 2840011873211PN 305-390-001-0

Insulation Blanket 2840011873212PN 305-390-101-0

Insulation Blanket 2840011873214PN 305-389-301-0

Insulation Blanket 2840011873215PN 305-389-401-0

Insulation Blanket 2840011873216PN 305-385-202-0

Insulation Blanket 2840011892656PN 305-389-701-0

Insulation Blanket 2840011892657PN 305-390-201-0

Insulation Blanket 2840011892658PN 305-389-901-0

Insulation Blanket 2840011892660PN 305-389-601-0

Insulation Blanket 2840011892661PN 305-389-801-0

Insulation Blanket 2840011892662PN 305-394-001-0

Insulation Blanket 2840011892669PN 305-393-901-0

Insulation Blanket 2840012517749PN 305-394-202-0

Insulation Blanket 2840012619976PN 305-389-002-0

Insulation Blanket 2840012619977PN 305-389-102-0

Insulation Blanket 2840012619978PN 305-389-202-0

Insulation Blanket 2840012629597PN 305-393-802-0

Counter Balance Weight 3040011873121PN 301-332-446-0

Counter Balance Weight 3040011873122 301-332-454-0

Counter Balance Weight 3040011873123 301-332-455-0

Counter Balance Weight 3040011873127PN 301-332-448-0

Counter Balance Weight 3040011873128PN 301-332-449-0

Counter Balance Weight 3040011873129PN 301-332-450-0

Counter Balance Weight 3040011873130 301-332-451-0

Counter Balance Weight 3040011873131 301-333-452-0

Counter Balance Weight 3040011873132 301-333-453-0

Counter Balance Weight 3040011873133 301-332-456-0

Counter Balance Weight 3040011873126PN 301-332-447-0

Sleeve Bushing 3120011872708 305-074-104-0

Sealing Sleeve 4730011834903 301-581-006-0

Machine Screw 5305012189768SX NAS1102E3-3

Machine Bolt 5306011624738SX J644P07B

Machine Bolt 5306011774989JF J814P020A

Dee Bolt 5306011833911SX 649-779-056-0

Self-Lock Nut 5310010363814NY J979P03

Self-Lock Nut 5310011753711JF H50185-4

Self-Lock Nut 5310011787518JF J980P05

Plain Washer 5310011868919SX 649-341-010-0

Retaining Ring 5325012106838SX J206P0051

Strip Seal 5330011834905SX 301-325-503-0

Strip Seal 5330011834906SX 301-329-003-0

Nonmetallic Seal 5330011837116SX 301-325-404-0

Nonmetallic Seal 5330011837117SX 301-325-203-0

Nonmetallic Seal 5330011837118SX 301-325-303-0

O-Ring 5331011837091SX 301-325-107-0

Deflector 5340011892569PN 301-567-701-0

Bushing 5365011848541SX 301-557-402-0 image3.emf

Interim Rpt ERRC T Reparable NSNs Work Pckg.xlsx 13-15 ERRC T (Work Package)

F108 Module 13/15 ERRC T, REPARABLE NSNs WITH WORK PACKAGE

Module Serial Number:

Nomenclature NSN PN Work Package Repair Quantity in TO Repairs Performed Quantity Condemned Quantity

001 002 003 004 005 006 007 008 009 010 011 012 013 014 015 016 017

LPT Rotor Blades, Stage 1 2840-01-466-7430 Unknown 72-54-01 7

LPT Rotor Blades, Stage 2 2840-01-466-7140 Unknown 72-54-02 11

LPT Rotor Blades, Stage 3 2840-01-187-8239 301-330-321-0 11

LPT Rotor Blades, Stage 4 2840-01-189-2914 301-330-438-0 11

LPT Rotor Disk 2840-01-185-6489 301-331-126-0

LPT Rotor Disks, Stage 1 2840-01-856-6489 301-331-126-0 72-54-03 0

LPT Rotor Disks, Stage 2 2840-01-856-6490 301-331-227-0 0

LPT Rotor Disks, Stage 3 2840-01-185-6491 301-331-322-0 0

LPT Rotor Disks, Stage 4 2840-01-185-6492 301-331-427-0 0

LPT Shroud Support 2840-01-185-6427 301-555-227-0 72-54-04 8

LPT Rotor Support Unknown Unknown 72-54-05 3

LPT Rotating Air Seals Unknown Unknown 72-54-06 4

LPT Case 2840-01-185-6488 Unknown 72-54-07 13

LPT Nozzle Segment, Stage 2 2840-01-344-3233 305-390-/308/311-0 72-54-08 17

LPT Nozzle Segment, Stage 3 2840-01-341-0050 305-390-705-0 17

LPT Nozzle Segment, Stage 4 2840-01-187-3198 305-390-904-0 17

LPT Inner Stationary Air Seal Unknown Unknown 72-54-09 3

LPT Thermal Insulation Blanket Unknown Unknown 72-54-10 1

LPT Cooling Air Tube Assembly Not Applicable Not Applicable 72-54-11 2

LPT Outer Stationary Air Seal Unknown Unknown 72-54-12 5

LPT Cooling Air Manifolds Not Applicable Not Applicable 72-54-13 4

F108 Module 13/15 ERRC T, REPARABLE NSNs WITHOUT WORK PACKAGE

Nomenclature NSN PN Quantity Replaced

Turbine Frame 2840-01-139-4018PN 301-316-869-0

Turbine Conical Support 2840-01-185-6424PN 305-056-116-0

Turbine Assembly 2840-01-211-0178PN 301-412-083-0

Air Seal, Stage 4 2840-01-417-6409PN 335-040-606-0

Turbine Assembly 2840-01-211-0178PN 301-412-083-0

Aircraft Seal 2840-01-185-6426PN 301-332-016-0

Turbine Disk, Stage 4 2840-01-185-6492PN 301-331-429-0

Seg Seal, Stage 4 2840-01-417-6409PN 335-040-606-0

Air Seal 2840-01-189-2631PN 301-317-621-0

Nozzle Segment, Stage 4 2840-01-187-3158PN 305-391-003-0

Air Seal 2840-01-185-6425PN 301-331-923-0

Turbine Blade, Stage 3 2840-01-372-5896PN 301-330-325-0

Turbine Disk, Stage 3 2840-01-185-6491PN 301-331-322-0

Air Seal 2840-01-187-3046PN 335-040-505-0

Seg Seal, Stage 3 2084-01-187-3179PN 301-317-923-0

Seg Seal, Stage 3 2084-01-187-3179PN 301-317-927-0

Nozzle Segment, Stage 3 2840-01-341-0068PN 305-390-805-0

Rotating Air Seal, Stage 2 2840-01-185-6423PN 301-331-820-0

Blade, Stage 2 2840-01-187-8239PN 301-330-221-0

Blade, Stage 2 2840-01-466-7740PN 301-330-222-0

LPT Disk, Stage 2 2840-01-185-6490PN 301-331-227-0

Aircraft Seal 2840-01-341-9081PN 305-040-407-0

Air Seal 2840-01-185-6429PN 301-317-826-0

Nozzle Segment, Stage 2 (CD) 2840-01-345-4795PN 305-390-518-0

Nozzle Segment, Stage 2(CD) 2840-01-340-9213PN 305-390-408-0

Rotating Air Seal, Stage 1 2840-01-185-6422PN 301-331-721-0

Blade, Stage 1 2840-01-466-7141PN 301-330-115-0

Seg Seal, Stage 1 2840-01-212-1035PN 301-317-321-0

LPT Rear Case Assembly 2840-01-455-7988PN 305-078-653-0

Ring-Sector Support 2840-01-262-8042PN 305-386-609-0

F108 Module 15 ERRC T, REPARABLE NSNs WITH WORK PACKAGE

Nomenclature NSN PN Work Package Repair Quantity in TO Repairs Performed Quantity Condemned Quantity

001 002 003 004 005 006 007 008 009 010 011 012 013 014 015 016 017

LPT Frame Unknown Unknown 72-56-01 14

No 5 Bearing Support Assy 2840-01-192-5345 Unknown 72-56-02 6

Oil Sump Assy 2840-01-196-6004 Unknown 72-56-03 4

Midstream Fairing 2840-01-206-9820 Unknown 72-56-04 2

Oil Inlet Cover 2840-01-189-2857 Unknown 72-56-06 3

Flame Arrestor Assy Not Applicable Not Applicable 72-56-08 1

Flange 4730-01-181-1064 Unknown 72-56-09 1

Turbine Frame Hardware Unknown Unknown 72-56-10 1

ERRC N, NON-REPARABLE NSNs (DLA, IPV)

Nomenclature NSN PN Quantity Replaced Replacement %

Rivet 5320005504055SX AN123322

Bolt 5306005389046NY J644P04D

Plug 5342011848596PN 301-595-102-0

Packing Assembly 5330014236747SX 305-483-202-0

Pipe Flange 4730011811069SX 305-380-401-0