16-00015_REV2_SOW_NonCm_6_0_Update_pdf.pdf

FD2030-16-00015 Page 1

STATEMENT of Work (SOW) for the

TF33 Vane and Shroud (Stators)

PURCHASE REQUEST NUMBER: FD2030-16-00015

REV:2

PREPARATION DATE: 31 Oct 2016

Request Date: 31 Oct 2016

PREPARING ORGANIZATION:

st Supply Chain Management Squadron SCMS/GUME

Oklahoma City Air Logistics

And

Air Force Life Cycle Management Center (AFLCMC)

Propulsion Sustainment Division (LPS)

TF33 Technical Services Flight (LPSEA)

TINKER AFB, OK 73145-3031

FD2030-16-00015 Page 2

TABLE OF CONTENTS Page

TABLE OF CONTENTS 2

SECTION I

1 General 3

1.1 Receiving 3

1.2 Cleaning 4

1.3 Inspection 4

1.4 Remanufacture 4

2.0 Quality System and Quality Assurance 5

3.0 Deficiency Report 5

4.0 Condemned Assets 5

5.0 Packaging and Handling 5

6.0 Reporting 5

7.0 Shipping and Transportation 5

8.0. Safety 5

SECTION II

3 GOVERNMENT PROPERTY 6

APPENDIX A

ACRONYMS 7

ATTACHMENT 1

Stator Parts 8

Contractor approved vane providers 14

FD2030-16-00015 Page 3

SECTION I

1. General: The purpose of this Statement of Work (SOW) is to define the remanufacture requirements for the TF33 Vane and Shroud (Stators) that apply to the following National

Stock Numbers (NSN) and Part Numbers (P/N):

See attachment (1):

The instructions stipulated are brief, concise statements providing general requirements for remanufacturing of the TF33 Vane and Shroud (Stators). These requirements are dependent upon the contractor having remanufacture capabilities to include appropriate technical data, manufacturing documents, and change in designs and testing equipment. The contractor shall use the most current revision of the technical data referenced in this document. An Initial

Product Evaluation (IPE) will be required only if the contractor facility has not remanufactured this component previously for the U.S. Air Force. If an IPE is required, (3) each N2 stators with

Nickel Braze and (2) each N1 stators will be required as part of the Source Approval Request before a contractor can be considered an approved source. Replacement vanes must be obtained from government approved sources. See attachment (1) for approved sources. The contractor is responsible for the production; remanufacture and scheduled delivery of a quality product (see attachment 1). Each TF33 Vane and Shroud (Stator) identified as serviceable shall be delivered to the Government defect free. The contractor shall meet the delivery schedule.

Mission Essential Services: N/A

1.1 Receiving: The contractor shall perform a receiving visual inspection upon receipt of each

TF33 Vane and Shroud (Stators) IAW T.O. 2J-TF33-53-6. Each item shall be inspected prior to placing in process to determine its condition and to ensure that item identification corresponds to that shown on the current schedule. Nonconforming end items shall be reported to the

Procurement Contracting Officer (PCO) or Production Management Specialist (PMS) representative within 30 days after receipt. The contractor shall obtain disposition instructions from the PCO or PMS. The contractor shall report the condemnation in accordance with the

CAV reporting requirements found in the reporting paragraph, 6.0. The contractor shall initiate a

Supply Discrepancy Report (SDR) for any assets received in other than the contracted packaging. The Contractor shall initiate a Supply Discrepancy Report (SDR) formerly called

Report of Discrepancy (ROD) for such shipments or any assets as describe above or received in packaging other than the contracted packaging requirements through WEB SDR. The WEB SDR is located at: https://www.transactionservices.dla.mil/daashome/websdr.asp. If applicable, the

Contractor shall provide the PCO, ES and PMS with an estimated parts list required should missing parts be determined. 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 and IAW Contractor Asset Visibility for the Air

Force (CAV AF) Statement of Work (SOW). The prime packaging specialist may authorize exceptions to these requirements.

https://www.transactionservices.dla.mil/daashome/websdr.asp

FD2030-16-00015 Page 4

1.2 Cleaning: Parts will be cleaned prior to inspection and rework IAW T.O.s 2-1-111 and

2J-TF33-53-5.

1.3 Inspection: Visually and dimensionally inspect parts for wear and serviceability per T.O.

2J-TF33-53-6. Any vane and shroud (stator) that has a previous rework/remanufacture that would cause the finished part to exceed present rework or inspection limits shall be held in a bond room for review by AFLCMC/LPSEA3 and provide disposition instructions. Identify and segregate all N2 vane and shrouds (stators) with previous partial vane replacements via silver braze. Identify, by part number (P/N) the correct blue print braze requirement. N2 vane and shrouds (stators) with silver braze be repaired using either gold nickel or nickel braze.

1.4 Remanufacture: Remanufacturing shall be accomplished IAW 2J-TF33-53 series

Technical Orders, T.O. 2-1-111 and attachment (1) of this SOW.

1.4.1 The uses of silver braze for remanufacture of the N2 vane and shrouds (stators) is not authorized. N2 vane and shrouds (stators) that were previously remanufactured using silver braze must have the silver braze materials stripped out. The joints must be re-brazed using nickel braze.

1.4.2 Gold nickel brazed vane and shrouds (stators) that are found to have cracks in one or more of the vane to shroud, braze joints must be remanufactured using nickel braze only.

1.4.3 All N2 vane and shroud (stators) will be output as the latest master P/N, NSN per attachment (1) reflecting out master output NSN.

1.4.4 Regardless of the original P/N braze specification, all 100% vane replacements will be done with nickel braze and 100% new and unused vanes.

1.4.5 N2 vane and shroud (stators) that are silver brazed assemblies per the blue print and stators that have been re-identified with a gold nickel or nickel braze P/N during a previous remanufacture, and are subsequently discovered during the remanufacture process to be silver, will be remanufactured using nickel braze.

1.4.6 All vane airfoils must have a surface finish of 35AA or smoother on 85% of the airfoil and 60AA or smoother on remaining 15% of the airfoil (adjacent to the inner and outer shroud.)

1.4.7 Stators must be produced with 100% non-blended vanes.

1.4.8 All tooling provided by SOR shall be approved by AFLCMC/LPSEA unless certified to have been built to the PWA drawing. Any modified tooling for inspection and test purposes will require approval prior to use.

1.4.9 All detailed and/or component parts required to accomplish remanufacture of van and shrouds (stators) to finished end item shall be contractor furnished.

1.4.10 Process all N1 vane and shrouds (stators) assemblies through final acceptance inspection as a matched set. All N1 vane and shroud (stators) assemblies sent to packaging prior to shipment to Tinker AFB shall be banded together as a matched set. Output NSN for part number of vane and shroud (stators) assembly will not change.

FD2030-16-00015 Page 5

2.0 Quality System and Quality Assurance: The contractor shall develop and maintain a system that adheres to the requirements of International Standard Organization (ISO) 9001, AS9100 and NATO AQAP 270.

3.0 Deficiency Report (DR): At the Government’s request, the contractor shall investigate and submit findings to include root causes and a corrective action against all Deficiency Reports submitted to contractor against items remanufactured by this contract which are reported to be defective.

4.0 Condemned Assets: TF33 Vane and Shrouds (Stators) that exceed present remanufacture and inspection limits shall be condemned at contractor’s facility and data provided to the Production Management Specialist with the 421 SCMS/GUME monthly on monthly production form AF form 413 (CDRL A001 – E0001).

All condemnations will be recorded in CAVAF within 24 hours from being deemed condemned.

See 6.0) Reporting.

5.0 Packaging and Handling: The contractor shall place a completed serviceable tag, Department of Defense (DD) Form 1574 inside the package along with the assembly. The contractor shall place another completed DD Form 1574 to the outside of the package.

6.0 Reporting: The contractor shall provide each month after the end of month production an AF form 413 or another format approved by the PMS of the monthly production, total assets received, produced and any assets condemned by order. The monthly production report is due to the Production Management Specialist no later than 7 business days from the last day of month production. (CDRL A001 – E001).

The contractor shall input the data IAW the CAVAF Statement of Work. In addition, the contractor shall submit an SDR when required IAW the contract’s, “CAVAF Statement of Work, End Item and Government Furnished Equipment Management,” Section 7. Contractor shall process DRs when required IAW Section 3.0 of this SOW. This data should match the CAVAF reporting requirement. (CDRL A002-E002).

A001: AFMC Form 413

A002: Commercial Asset Visibility Air Force (CAVAF) Reporting formerly CAVII

7.0 Shipping and Transportation: The contractor shall not destroy reusable shipping containers, and will reuse them for return shipment. At any time the contractor has an overage of shipping containers due to condemned parts, the shipping container will be recycled under contractor discretion.

8.0. Safety: 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 Contracting Officer (CO), as soon as possible however notification shall not exceed; eight (8) hours for any damage to government property where the dollar value

FD2030-16-00015 Page 6 exceeds $500,000.00 and within two workdays, for any damage to government property less than

$500,000.00 during the execution of the contract.

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

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

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

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

d. Cause of accident/incident, if known

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

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

g. Corrective actions (taken or proposed)

h. Other pertinent information

If requested by the designated CO, the contractor shall immediately secure the mishap scene/damaged property and impound pertinent maintenance and training records, until released by the Procuring Safety Office. Contractors will not dispose of contract data related to a mishap until notified to do so by the CO.

SECTION II

GOVERNMENT PROPERTY

Government Furnished Material (GFM): None, contractor shall furnish all material, support equipment, tools and test equipment. Government Furnished Material is not provided.

Government Furnished Property (GFP): All parts to be remanufactured will be shipped to the contractor.

FD2030-16-00015 Page 7

APPENDIX A

ACRONYMS

ACSS Air Combat Sustainment Squadron

AF Air Force

AFMC Air Force Materiel Command

CAVAF Commercial Asset Visibility Air Force

CDRL Contract Data Requirements List

CFMI CFM International

CIT Compress Inlet Temperature

CMM Commercial Maintenance Manual

DD Department of Defense

DER Designated Engineering Representative

DCMA Defense Contract Management Agency

DR Deficiency Report

FAA Federal Aviation Administration

FAR Federal Acquisition Regulation

IAW In Accordance With

ISO International Standards Organization

NSN National Stock Number

OC-ALC Oklahoma City Air Logistics Center

PCO Procurement Contracting Officer

P/N Part Number

PMS Production Management Specialist

PP Performance Plan

SB Service Bulletin

SDR Supply Discrepancy Report

S/N Serial Number

SOW Statement of Work

SRAN Stock Record Account Number

SS Service Summary

TAFB Tinker Air Force Base

USAF United States Air Force

FD2030-16-00015 Page 8

ATTACHMENT 1

TO

TF33 VANE & SHROUD STATEMENT OF WORK

INSPECTION AND REPAIR CRITERIA FOR TF33 VANE AND SHROUDS THAT

REQUIRE ALUMINUM COATING AND AIR SEALING RING REPLACEMENT.

1. Rework and re-identify N1 vane and shrouds IAW T.O. 2J-TF33-53-2, SWP

003 04. Identify the N1 Vane and Shrouds. 5 th through 8 th stages, per the following:

th stage - P3, 5, 7, 9, 11, 100, 102, 103

Condemn: n/a P/N 541975 n/a P/N 555875 n/a P/N 701375

Input: 2840-00-765-8932RV P/N 389385

2840-00-966-8028RV P/N 484095/704385/730695

2840-00-981-1804RV P/N 478935/704175/730665

2840-01-003-0718RV P/N 748675

2840-01-004-1796RV P/N 748685

2840-01-161-1132RV P/N 748885

Output: 2840-01-004-1796RV P/N 748685

7th stage - P3, 5, 7, 9, 11, 100, 102, 103

Input: 2840-00-765-8169RV P/N 389387

2840-00-918-1624RV P/N 516197/704377/730687

2840-00-966-8030RV P/N 484097

2840-00-991-9209RV P/N 480677/704177/730667

2840-01-003-2843RV P/N 748677

2840-01-004-1797RV P/N 749777

2840-01-161-1133RV P/N 749377

Output: 2840-01-004-1797RV P/N 749777

8th stage - P3, 5, 7, 9, 11, 100, 102, 103 Input: 2840-00-765-8179RV P/N 389388

2840-00-867-5872RV P/N 478578/704178/730668

2840-00-918-1625RV P/N 516198/704188/730778

2840-00-966-8031RV P/N 484098

2840-00-991-1048RV P/N 480678

2840-01-003-1000RV P/N 748678

2840-01-004-1794RV P/N 748688

2840-01-161-1131RV P/N 748878

Output: 2840-01-004-1794RV P/N 748688

FD2030-16-00015 Page 9

2. Rework and re-identify N2 vane and shrouds IAW T.O. 2J- TF33-53-2, SWP 005 02.

Identify the N2 vane and shrouds per the following:

10P3, 5, 9, 11, 103 BRAZE

Input: 2840-00-757-8260RV P/N 730770/523190/704180 GOLD NICKEL

2840-00-765-9891RV P/N 389467 SILVER

2840-00-907-1484RV P/N 523390 SILVER

2840-01-004-1798RV P/N 748690/765180 GOLD NICKEL/NICKEL

Output: 2840-01-004-1798RV P/N 748690/765180 GOLD NICKEL/NICKEL

10P7, 100

Input: 2840-00-908-6065RV P/N 512270/704170/730670 GOLD NICKEL

2840-00-981-9217RV P/N 454380 SILVER

2840-01-004-1802RV P/N 748680/765190 GOLD NICKEL/NICKEL

Output: 2840-01-004-1802RV P/N 748680/765190 GOLD NICKEL/NICKEL

11P3, 5, 9, 11, 103

Input: 2840-00-717-2716RV P/N 389468 SILVER

2840-00-757-8261RV P/N 523191/704281/730791 GOLD NICKEL

2840-00-907-1483RV P/N 523391 SILVER

2840-01-004-1799RV P/N 748681/765181 GOLD NICKEL/NICKEL

Output: 2840-01-004-1799RV P/N 748681/765181 GOLD NICKEL/NICKEL

11P7, 100

Input: 2840-00-908-6059RV P/N 512271/704271/730781 GOLD NICKEL

2840-01-004-5771RV P/N 748691/765191 GOLD NICKEL/NICKEL

2840-00-981-9215RV P/N 454381 SILVER

Output: 2840-01-004-5771RV P/N 748691/765191 GOLD NICKEL/NICKEL

FD2030-16-00015 Page 10

12P3, 5, 9, 11, 103

Input: 2840-00-759-6322RV P/N 511472/704272/730782 GOLD NICKEL

2840-00-765-9894RV P/N 389469 SILVER

2840-01-004-1800RV P/N 748692/765182 GOLD NICKEL/NICKEL

Output: 2840-01-004-1800RV P/N 748692/765182 GOLD NICKEL/NICKEL

12P7, 100

Input: 2840-00-999-3295RV P/N 512272/704282/730792 GOLD NICKEL

2840-01-004-5774RV P/N 748884/765192 GOLD NICKEL/NICKEL

Output: 2840-01-004-5774RV P/N 748884/765192 GOLD NICKEL/NICKEL

13 P7, 100

Input: 2840-00-999-3295RV P/N 512272/704282/730792 GOLD NICKEL

2840-01-004-5774RV P/N 748884/765192 GOLD NICKEL/NICKEL

Output: 2840-01-004-5774RV P/N 748884/765192 GOLD NICKEL/NICKEL

15P7, l00

Input: 2840-00-966-8060RV P/N 476675/704285/730675 GOLD NICKEL

2840-00-966-8060RV P/N 673985 SILVER

2840-01-004-5772RV P/N 749395/766595 GOLD NICKEL/NICKEL

Output: 2840-01-004-5772RV P/N 749395/766595 GOLD NICKEL/NICKEL

FD2030-16-00015 Page 11

3. Rework and re-identify N2 vane and shrouds that require 100% EVR Vane and

Shroud replacement IAW T.O. 2J- TF33-53-2, SWP 005 02. Identify the N2 vane and shrouds per the following:

Note: A repair is considered to be “100% EVR Vane & Shroud Replacement” when a stator is de-brazed, any vanes are removed and replaced and the stator assembly is re-brazed, due to the level of work required. It does not necessarily require replacing every vane with brand new; vanes that have been inspected and meet the requirements listed in Section 1.4.6 and 1.4.7 may be used.

100% EVR Vane & Shroud Replacement 10 th

P3, 5, 9, 103

Input: 2840-00-757-8260RV P/N 730770/523190/704180 GOLD NICKEL

2840-00-765-9891RV P/N 389467 SILVER

2840-00-907-1484RV P/N 523390 SILVER

2840-01-004-1798RV P/N 748690/765180 GOLD NICKEL/NICKEL

Output: 2840-01-004-1798RV P/N 748690/765180 GOLD NICKEL/NICKEL

100% EVR Vane & Shroud Replacement 10

P7, 100

Input: 2840-00-908-6065RV P/N 512270/704170/730670 GOLD NICKEL

2840-00-981-9217RV P/N 454380 SILVER

2840-01-004-1802RV P/N 748680/765190 GOLD NICKEL/NICKEL

Output: 2840-01-004-1802RV P/N 748680/765190 GOLD NICKEL/NICKEL

100% EVR Vane & Shroud Replacement 11

P3, 5, 9, 11, 103

Input: 2840-00-717-2716RV P/N 389468 SILVER

2840-00-757-8261RV P/N 523191/704281/730791 GOLD NICKEL

2840-00-907-1483RV P/N 523391 SILVER

2840-01-004-1799RV P/N 748681/765181 GOLD NICKEL/NICKEL

Output: 2840-01-004-1799RV P/N 748681/765181 GOLD NICKEL/NICKEL

FD2030-16-00015 Page 12

100% EVR Vane & Shroud Replacement 11

P7, 100

Input: 2840-00-908-6059RV P/N 512271/704271/730781 GOLD NICKEL

2840-01-004-5771RV P/N 748691/765191 GOLD NICKEL/NICKEL

2840-00-981-9215RV P/N 454381 SILVER

Output: 2840-01-004-5771RV P/N 748691/765191 GOLD NICKEL/NICKEL

100% EVR Vane & Shroud Replacement 12

P3, 5, 9, 11, 103

Input: 2840-00-759-6322RV P/N 511472/704272/730782 GOLD NICKEL

2840-00-765-9894RV P/N 389469 SILVER

2840-01-004-1800RV P/N 748692/765182 GOLD NICKEL/NICKEL

Output: 2840-01-004-1800RV P/N 748692/765182 GOLD NICKEL/NICKEL

100% EVR Vane & Shroud Replacement 12

P7, 100

Input: 2840-00-999-3295RV P/N 512272/704282/730792 GOLD NICKEL

2840-01-004-5774RV P/N 748884/765192 GOLD NICKEL/NICKEL

Output: 2840-01-004-5774RV P/N 748884/765192 GOLD NICKEL/NICKEL

100% EVR Vane & Shroud Replacement 13

P7, 100

Input: 2840-00-966-8058RV P/N 476673/704283/730793 GOLD NICKEL

2840-01-005-1882RV P/N 748893/766593 GOLD NICKEL/NICKEL

Output: 2840-01-005-1882RV P/N 748893/766593 GOLD NICKEL/NICKEL

FD2030-16-00015 Page 13

100% EVR Vane & Shroud Replacement 15

P7, 100

Input: 2840-00-966-8060RV P/N 476675/704285/730675 GOLD NICKEL

2840-00-966-8060RV P/N 673985 SILVER

2840-01-004-5772RV P/N 749395/766595 GOLD NICKEL/NICKEL

Output: 2840-01-004-5772RV P/N 749395/766595 GOLD NICKEL/NICKEL

FD2030-16-00015 Page 14

CONTRACTOR FURNISHED VANES

(LPSAAD APPROVED SOURCES)

P/N NSN APPROVED MANUFACTURING SOURCE

479055 2840-00-963-1495 PRATT AND WHITNEY 77445

360156 2840-00-768-2111 ELECTRO METHODS INC 33617

HAWKER SIDDELEY CANADA INC 35013

J T SLOCOMB CO 55282

PRATT AND WHITNEY 77445

360157 2840-00-768-2112 ELECTRO METHODS INC 33617

HAWKER SIDDLEY CANADA INC 35013

360158 2840-00-768-2113 ELECTRO METHODS 33617

UNITED TECHNOLOGIES CORP 52661

511660 2840-00-759-6323 J T SLOCOMB CO 55282

511661 2840-00-759-6324 PRATT AND WHITNEY 77445

511662 2840-00-759-6325 PRATT AND WHITNEY 77445

534463 2840-01-160-3183 ELECTRO METHODS INC 33617

PRATT AND WHITNET 77445

446064 2840-00-819-6133 PRATT AND WHITNEY 77445

534464 2840-01-160-3184 CHROMALLOY COMP TECH 01681

446065 2840-00-819-6134 PRATT AND WHITNEY 77445

534465 2840-01-159-6820 ELECTRO METHODS INC 33617

512360 2840-00-962-6746 ELECTRO METHODS INC 33617

512361 2840-00-962-6747 COMPONENT ENG INC 1DP23

ELECTRO METHODS INC 33617

HAWKER SIDDELEY CANADA INC 35013

FD2030-16-00015 Page 15

512362 2840-00-962-6744 COMPONENT ENG INC 1DP23

ELECTRO METHODS INC 33617

477053 2840-00-966-8062 AIRFOIL TEXTRON INC 33755

477054 2840-00-966-8063 HOWMET TURBINE COMP CORP 3V257

AIRFOIL TEXTRON INC 33755

UNITED TECHNOLOGIES 52661

477055 2840-00-966-8064 AIRFOIL TEXTRON INC 33755

UNITED TECHNOLOGIES 52661

534460 2840-01-160-3181 UNITED TECHNOLOGIES 52661

534461 2840-01-160-3180 ELECTRO METHODS INC 33617

534462 2840-01-160-3182 ELECTRO METHODS INC 33617