Performance Work Statement.pdf

PERFORMANCE WORK STATEMENT (PWS)

for the

TF33 2nd, 3rdAND 4th STAGE TURBINE NOZZLE VANES

PURCHASE REQUEST NUMBER:

FD2030-19-03037

REV. 1

PREPARATION DATE: 30 March 2020

PREPARING ORGANIZATION:

421st Supply Chain Management Squadron (SCMS)/GUME

Oklahoma Air Logistics Center And

Air Force Life Cycle Management Center (AFLCMC) TF33 Technical Services Flight (LPSEA)

TINKER AFB, OK 73145-3031

File Number: FD2030-19-03037 1

TABLE OF CONTENTS Page

TABLE OF CONTENTS 1

1.0

DESCRIPTION OF SERVICES

SECTION I

1.1 Introduction 2

1.2 Receiving 2

1.3 Disassembly 2

1.4 Repair Procedures 2

1.5 Quality System and Quality Assurance 5

1.6 Deficiency Report (DR) Investigation 6

1.7 Condemned Assets 6

1.8 Counterfeit Prevention Plan (CPP) 6

1.9 Reporting CDRLs 8

1.10 Item Unique Identification (IUID) 9

1.11 Packaging and Handling 9

1.12 Shipping and Transportation 9

1.13 Preservation 10

1.14 Document Storage 10

1.15 Safety 10

1.16 Mission Essential Services (N/A) 10

SECTION II

2.0 SERVICE SUMMARY (SS) 10

2.1 Service Summary Requirements 10

2.2 TF33 2nd-4th Stage Turbine Nozzle Vanes Summary 11

2.3 Contractor Performance Evaluation 11

SECTION III

3.0 GOVERNMENT PROPERTY 12

3.1 Government Furnished Material (GFM) 12

3.2 Government Furnished Property (GFP) 12

APPENDIX “A”

ACRONYMS 13

File Number: FD2030-19-03037 2

File Number: FD2030-19-03037 3

SECTION I

1.0 DESCRIPTION OF SERVICES

1.1 Introduction: The Contractor shall provide repairs for the TF33 2nd-4th Stage Turbine Nozzle Vanes that applies to the following National Stock Numbers (21 NSNs) and Part Numbers (P/Ns) Attachment 1 below. During the contractual Period of Performance (PoP), all 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. Contractor shall perform cleaning, inspection, repair, and if applicable, rework and re-identification of the TF33 2nd-4th Stage Turbine Nozzle Vanes. The Contractor shall be a rated repair facility to repair TF33 engine components; Contractor must have the repair capabilities to include appropriate technical data, repair documents, and license agreements, required to accomplish repair of TF33 2nd-4th Stage Turbine Nozzle Vanes. The Contractor is responsible for the production, repair and scheduled delivery of a quality product.

1.2 Receiving: The Contractor shall perform a receiving visual inspection upon receipt of each TF33 2nd-4th Stage Turbine Nozzle Vane for serviceability or repairable condition for repair In Accordance With (IAW) Technical Order (T.O.) 2J-TF33-53-6, Work Package (WP) 065 00. Any 2nd-4th Stage Turbine Nozzle Vanes previously re-worked/repaired in a manner that would cause the finished part to exceed repair limits as received shall be reported to 421/GUME, Production Management Specialist (PMS), for review and disposition. Disposition will be provided by AFLCMC/LPSEA. The Contractor shall perform a receiving visual inspection for any shipping or packaging damage. The Contractor shall report to the Procurement Contracting Officer (PCO) and the Production Management Specialist to obtain disposition instructions for any received assets which are misidentified, misdirected, have a variation in quantity, non-requisitioned items, lost or damaged parcel post or incorrect shipments. The contractor will input the misdirected assets into CAVAF in condition J pending disposition instruction. The Contractor shall initiate a Report of Shipping (Item) and Packaging Discrepancy, Subtitle Supply Discrepancy Report (SDR) IAW Contractor Data Reporting List (CDRL) A003 – Data Item Description (DID): DI-MGMT-80503, for such shipments or any assets as described 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 the Contractor cannot initiate an SDR electronically, a manual form will be required to be submitted. Assistance with this process can be obtained by calling the help desk number located on the web site of the web address shown above.

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) Reporting Requirements. The prime packaging specialist may authorize exceptions to these requirements.

If the contractor is unable to access WEBSDR, they shall submit the SDR form 364 via email to dlacontactcenter@dla.mil. Include as courtesy copy the following: lourdes.santiago@us.af.mil

1.3 Disassembly: Not required for TF33 2nd-4th Stage Turbine Nozzle Vanes.

1.4 Repair Procedures: Contractor shall induct for repair all TF33 2nd-4th Stage Turbine Nozzle Vanes IAW T.O. 2J-TF33-53-7, WP 065 00. Hold turbine vanes that exceed repair limits outlined in T.O. 2J-TF33-53-6, File Number: FD2030-19-03037 4

WP 065 00 for disposition instructions from 421 SCMS/GUME. All tooling provided by Source of Repair (SOR) shall be approved by AFLCMC/LPSEA unless certified to have been built to the Pratt & Whitney Aircraft (PWA) drawing. Any modified tooling used for inspection and test purposes will require approval prior to use. All detail parts and/or components required to accomplish repair of turbine vanes to a finished end item shall be contractor furnished material.

1.4.1 Inspection: Contractor shall visually and dimensionally inspect for serviceability or reparable condition using T.O. 2J-TF33-53-6 WP 065 00. Any turbine nozzle vanes previously reworked-repaired in a manner that would cause the finished part to exceed present inspection or repair limits and/or assets that exceed repair limits as received shall be held in a bond room for review/ disposition by AFLCMC/LPSEA. Parts will be cleaned prior to inspection and repair IAW T.O. 2-1-111 and 2J-

TF33-53-5 WP 004 00.

1.4.2 Additional Inspection and Repair Criteria for TF33 2nd-4th Stage Turbine Vanes:

a. Input part number (P/N) listed from Attachment 1 for repair as required and rework 2nd-4th Stage Turbine Vanes IAW T.O. 2J-TF33-53-7, WP 065 00 and detailed inspection/ repair criteria in the following paragraphs of this PWS.

b. Pre-cleaning of end items will be at the discretion of the SOR. The contractor shall assure the cleaning and preserving materials meet requirements specified in the required Service Process Operation Procedure (SPOP):

(1) Abrasive cleaning, utilizing 60 Pounds per Square inch (PSI) maximum line pressure and 80 mesh aluminum oxide grit or finer, may be used to remove oxidation and stains from uncoated vanes, SOR shall use caution not to damage vanes during cleaning.

(2) Vibratory finishing method of cleaning vanes may be used in conjunction with required SPOPs.

c. Contractor’s work control documents/inspection requirements shall contain data/criteria from pertinent drawings and dimensional specifications required by T.O.s or this PWS. Appropriate blue prints may be used as reference; blueprints shall be to the latest revision change letter.

d. Any turbine vane that exhibits non-reparable conditions such as obvious scrap, missing pieces, Foreign Object Debris (FOD)/impact damage, etc., that would make vane non-reparable shall be condemned and will not require mutilation.

e. No data.

f. Condemn Vanes exhibiting these conditions. They will not require mutilation:

(1) Any turbine vane that has a previous rework that would cause the finished part to exceed present rework or inspection limits.

(2) Cracks exceeding ¼ inch across width of vane (vane body cracks).

(3) Vanes exhibiting material deterioration in excess of 0.500 inch; length and width and 0.15 inch depth.

(4) Evidence of being bent or otherwise deformed other than acceptable bow.

(5) Trailing edge must be 0.025-inch minimum thickness.

(6) Vanes that have been conditionally condemned shall be identified by letter “S” using blue dykem ink on convex side of airfoil, prior to turning vanes into disposal officer.

g. Inspection/repairable limits of 2nd-4th Stage Turbine Vanes:

(1) Visually inspect each vane using 10X magnification for evidence of cracks or metal deterioration.

(2) Surface deterioration caused by oxidation that does not exceed 0.025-inch in depth may be removed from airfoil by belt sanding or blending. Only minimum airfoil material should be removed during belt sanding or blending, and trailing edge thickness must be maintained. Leading and trailing edge oxidation may be notched and weld repaired if crack limits are not exceeded. Power tools such

File Number: FD2030-19-03037 5 as stones, burrs, cloth wheels and belt sanders may be used as an alternate procedure for removal of excess weld material.

(3) Second, Third and Fourth Stage Vanes exhibiting cracks may be welded provided the following crack limits are not exceeded. Welding processes and procedures to be used are listed in T.O. 2J-TF33-53-7, WP 065 00 or T.O. 2-1-111, Standard Maintenance procedures.

(a) Trailing edge cracks 0.500-inch maximum length, 4 per vane

(b) Leading edge cracks 0.250-inch maximum length, 3 per vane

(c) Buttress cracks 0.125 maximum length, 4 per vane.

(d) Airfoil cracks 0.250-inch maximum length, 2 per vane.

h. Classify all vanes IAW T.O. 2J-TF33-53-7, WP 065 00, to determine vane actual class. Hot form/strike vanes as required to remove body bow and excessive twist. Vanes shall be hot formed/ re-classified using heated ovens and press dies. Refer to the PWA turbine vane straightening press manual.

(1) Vanes that meet classification requirements within +/- two classes of original legible class marked on vane are acceptable to process vanes through repair process without being hot formed/re-classed

(2) When original class number cannot be determined, mark vanes with Hot Form (as “HF”) and gaged class number. Vanes that require reclassification HF shall be marked with letters HF followed by the class number (Example HF9). Vanes that do not require classification HF shall be marked with letters CL followed by the class number (Example CL9). Identification of straightened vanes and vane class after straightening per T.O. 2J-TF33-53-7, WP 065 00 is not required.

i. Final vane classification will be performed by using specified class gage outlined in T.O. 2J-TF33- 53-7, WP 065 00. All repair processes shall be completed prior to final vane classification.

j. The SOR shall identify all repaired end items with SOR’s symbol (reference T.O. 2-1-111) and date of the repair. Temporary marking will be applied to convex airfoil surface with a rubber stamp.

k. All vanes shall be marked with PWA part number in original or “new” location designated in T.O.

2J-TF33-53-7, WP 065 00 and permanent class number if necessary. Refer to appropriate part drawing for vane part number marking in prescribed area. Roller die is the preferred method of marking. Alternate marking such as vibropeen or dot peen may be used if roller die method is not available.

l. Rework 3rd Stage Turbine Vanes P/N 565753/446953/495253 classes 1 thru 7, IAW T.O. 2J-TF33- 53-2, Subordinate Work Package (SWP) 010 01. After rework, re-identify all 3rd Stage Turbine Vanes to P/N 565753 classes 1 thru 5. Repair 3rd Stage Turbine Vanes P/N 781253 classes 1 thru 7 IAW T.O. 2J-TF33-53-7, WP 065 00. Process reworked vanes as required through normal repair process.

m. Rework 4th Stage Turbine Vanes P/N 565754/446954/495254 classes 5 thru 9, IAW T.O. 2J- TF33-53-2 SWP 010 01. After rework, re-identify all 4th Stage Turbine Vanes to P/N 565754. This paragraph (m) provides SOR authorization to re-identify P/N 495254 to P/N 565854. No stress relief is required for 4th Stage Turbine Vanes. Process reworked vanes as required through normal process.

n. Rework all 3rd and 4th Stage Turbine Vanes that will require to be re-indexed in accordance with T.O. 2J-TF33-53-2, SWP 010 01, excluding the following paragraphs. Paragraphs 5 (5) (a), 5 (5) (b) and 5 (6) (b) for 3rd Stage and paragraphs 5 (8) (b) and 5 (8) (c) for 4th Stage. Third Stage Vanes shall be re-identified to P/N 565753 and/or 781253. Fourth Stage Vanes shall be re-identified to P/N/ 565854

o. Third and Fourth Stage Turbine Vanes that have been previously repaired by welding existing slot as an alternate method instead of using shoulder pin P/N 490750 are acceptable without any additional modification required.

1.4.3 Repair Documentation: Contractor shall document all inspections and repair required for each part. This documentation shall have the correct part number and/or assembly part number, serial

File Number: FD2030-19-03037 6 number and work accomplished annotated. Source of Repair (SOR) shall provide complete documentation with each part that has been repaired with the intent of returning part to serviceable condition.

1.4.4 Repair Deviations: Prior to Contractor’s use in repairing of TF33 2nd-4th Stage Turbine Nozzle Vanes, the Contractor shall obtain written approval from the PCO for any deviations from the processes, materials, material processes or procedures on DD form 1694, per MIL-STD-481B.

1.4.4 Designated Engineering Representative (DER) Processes and Procedures: Contractor shall obtain written approval from the PCO for all DER processes and procedures.

1.4.6 Initial Product Evaluation: Initial Product Evaluation (IPE) shall be required for contractors who have not successfully passed an IPE within the last three years or if repair processes and dimensions in the procedures specified throughout this PWS are updated. The IPE will consist of three (3) assets. The Contractor shall demonstrate the repairs required in T.O 2J-TF33-53-7, WP 065

00. All repairs listed in this technical data will be performed. The Contractor shall provide written documentation as to which asset received which repairs. These assets will be delivered to the United States Air Force/Department of Defense (USAF/DOD) for material and process testing. The Contractor shall not repair any additional assets until the IPE assets have been inspected and deemed successful. The Contractor shall be provided the results of the testing and any corrective actions required to begin the repair of the remainder of the contract quantity.

1.5 Quality System and Quality Assurance: Each TF33 2nd-4th Stage Turbine Nozzle Vane identified as serviceable shall be delivered to the government free of defects. A defect is defined as a rejected asset which is returned to the contractor for rework due to non-compliance with contract requirements. The Contractor shall develop and maintain a system that adheres to the requirements of Special Areas of Emphasis (SAE) AS9100, ISO 9001, North Atlantic Treaty Organization (NATO), Allied Quality Assurance Provision (AQAP) 2070 or equivalent and product or process specific quality standards such as North American Aerospace and Defense Contractors Accreditation Program (NADCAP) certified or Original Equipment Manufacturer (OEM) certification for significant industrial processes and supplemental requirements imposed by this contract. Develop and implement procedures to properly maintain measuring and test equipment in accordance with American National Standards Institute (ANSI) 2340-1. The quality system will include a clear and complete set of work documents for all maintenance required by this contract. The quality program shall be designed to promptly detect and correct conditions adverse to quality.

1.5.1 First Time Defect Detection Ratio: This is the identification element of a Quality Measurement System (QMS) to determine who typically finds and documents a contractual non-conformity. To receive a score of 0 or meets standard, the contractor must identify the same number of contractual non-conformities (defects) as the COR/QAR or miss no more than 4 defects. To receive a score of -1 or unacceptable, will be assessed if the contractor misses more than 4 defects than the COR/QAR detects.

1.5.2 Defense Contract Management Agency (DCMA) Quality/Surveillance: The Contractor shall allow quality assurance reviews to be conducted at the site of repair at the request of the Defense Contract Management Agency (DCMA) throughout the contract period.

The Contractor shall allow a quality acceptance review by the DCMA representative at the site of repair for each End Item generated under the terms of this contract. The Contractor shall support quality acceptance inspections of each End Item and shall be performed prior to packaging and transportation. Quality acceptance will be performed by DCMA at the repair

File Number: FD2030-19-03037 7 site. Quality acceptance documentation for each end-item shall be maintained by the Contractor as part of the item document package.

1.6 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 items repaired by this contract, which are reported to be defective. The Contractor shall investigate returned exhibit within 30 days from time of exhibit receipt and processed in accordance with Deficiency Report DID: DI-PSSS-81535A CDRL A005.

1.7 Condemned Assets: The Contractor shall condemn, at the Contractor’s facility, any TF33 2nd-4th Stage Turbine Vanes component parts that do not meet inspection limits. The Contractor shall process all condemned assets through Plant Clearance Automated Reutilization Screening System (PCARSS).

Condemnations shall be reported to 421 SCMS/GUME, Air Force Sustainment Center (AFSC) to establish usage rates and cost planning by reporting quantities by P/N and NSN of reparable components condemned and annotate on Contract Depot Maintenance (CDM) Production Report IAW CDRL A002 (DID) DI-PSSS- 81995 and Commercial Asset Visibility Air Force (CAVAF) Reporting Requirements IAW CDRL A001

(DID) DI-MGMT-81634C.

1.8 Counterfeit Prevention Plan (CPP): Contractors that supply electronic parts or systems that contain electronic parts will establish policies, procedures to avoid, detect, mitigate, and disposition counterfeit electronic parts to prevent such parts from entering the USAF/DoD supply chain. These policies and procedures will be documented in a CPP for submission and approval in accordance with (DID) DI-MISC- 81832 IAW CDRL A004 and accomplished for all specified contract items. DI-MISC-81832 is applicable to Parts, Material and Processes Selection (PMPS) associated with delivery of systems and assemblies to the USAF and DoD. The requirements established by DI-MISC-81832 also apply to electronics components procured in sustainment of such systems and assemblies. The requirements of the recently DoD-adopted SAE 5553, Aerospace Standard, Counterfeit Electronics Parts; Avoidance, Detection, Mitigation and Disposition will also apply.

1.8.1 At a minimum, the CPP will address:

1.8.1.1 Applicability. The Contractor shall identify all Business locations and programs to which the CPP applies. The CPP will address materials, hardware, electronic parts, and procured assemblies.

1.8.1.2 Definitions. The Contractor shall utilize definitions per AS 5553 to ensure consistency. Any Contractor-derived definitions must be included in an appropriate CPP Appendix or annex. (Ref. AS5553, paragraph 3, 3.1, 3.2, 3.3, Appendix H)

1.8.1.3 Parts Availability and Use of Parts Brokers. The Contractor shall not procure materials, systems, assemblies, subassemblies or parts from parts Brokers when available from Original Manufacturers (OM) or their Authorized Distributors. In cases where materials, systems, assemblies, sub-assemblies or parts are no longer available from the OM or their Authorized Distributors, procurement from Brokers may be authorized as defined by the Contractor's policy and their CPP. (Ref. AS5553, paragraph 4.1.1, 4.1.2.e., Appendix A)

1.8.1.4 Procurement Policies. The Contractor shall provide and implement policy directing development and implementation of business practices and procedures, and processes to prevent procurement of Counterfeit materials and parts. The Contractor shall identify the

File Number: FD2030-19-03037 8 appropriate office(s), business units, functional organizations, and programs, which shall have responsibility for development, maintenance and implementation of the CPP. The CPP will identify the specific roles and responsibility for each. (Ref. AS5553, paragraph 4.1.2, 4.1.3, Appendix B, C, D)

1.8.1.5 Risk Assessment. The contract shall address the risk of using unknown sources and or unauthorized suppliers in the CPP. Application or technical risk assessments will establish the effect that counterfeit parts may have on performance. Vendor or source of supply risk assessments shall establish the potential for obtaining counterfeit parts. Using any risk analysis tool acceptable to the Government, the Contractor shall conduct a risk assessment based upon item characteristics and how likely it is that a counterfeit part will be received.

The Contractor shall identify and describe in the CPP how parts are selected for assessment and what risk is acceptable based upon the parts design, construction, material and functional requirements. As a minimum, analysis will be completed for flagging high risk items, such as items that are obsolete, is discontinued, rare, etc. The Contractor shall require completion of a trade study, documented within the CPP that will facilitate determining whether 100% testing of parts procured from after-market sources is more cost effective than qualification or requalification of a manufacturer. (Ref. AS5553, paragraph 4.1.2, 4.1.3, Appendix B, C, D)

1.8.1.6 Detection and Avoidance Responsibilities. The Contractor shall establish processes for the review and approval of Contractor and applicable sub-Contractor systems for the detection and avoidance of counterfeit electronic parts and suspect counterfeit electronic parts, which processes will be comparable to the processes established for Contractor business systems under section 893 of the Ike Skelton National Defense Authorization Act for Fiscal Year 2011 (Public

Law 111-383; 124 Stat. 4311; 10 U.S.C. 2302 note). The Contractor shall flow down such requirements and processes to their sub-Contractors per ODASD Memo titled "Overarching DoD Counterfeit Prevention Guidance", dated 16 March 2012. (Ref. AS5553, paragraph 4.1.4, 4.1.5, Appendix E)

1.8.1.7 Testing and Verification. The Contractor shall establish and accomplish testing and verification processes for items not received from an original equipment manufacturer, original component manufacturer, or authorized distributor that are identified as having high risk for counterfeit potential. These processes apply to prime contracts, and to subcontracts or suppliers below the prime contracts. The Contractor shall provide a list of acceptable test facilities if the sub-Contractor or supplier does not have the capability to perform required testing. Submittal of Certificates of Compliance indicating the parts are not counterfeit will be acceptable for verification of testing. (Ref. AS5553, paragraph 4.1.4, Appendix E)

1.8.1.8 Configuration Identification and Traceability. The Contractor shall identify and control the configurations of all systems, assemblies, subassemblies and parts, and enable mechanisms to provide traceability of parts. The Contractor shall report to the Government when control of the configurations of all systems, assemblies, subassemblies and parts, and mechanisms to provide traceability of parts are not possible. The Contractor shall identify the specific systems, assemblies, subassemblies and parts beyond the Contractors' control. The Contractor shall be responsible for detecting and avoiding the use or inclusion of counterfeit materials and parts, to include procured assemblies and subassemblies, in such products and will be responsible for the rework or corrective action that may be required to resolve the use or inclusion of counterfeit materials and parts. The cost of counterfeit electronic parts and

File Number: FD2030-19-03037 9 suspect counterfeit electronic parts and the cost of rework or corrective action that may be required to remedy the use or inclusion of such parts are not allowable costs under Department contracts , unless: a) the Contractor has established a counterfeit avoidance/detection system approved by the DoD, b) the counterfeit parts were procured from a DoD-accredited trusted supplier or provided as Government property, and c) the Contractor has provide timely notification to the Government. (Ref. AS5553, paragraph 4.1.6, Appendix F)

1.8.1.9 Counterfeit Notification and Reporting. The Contractor shall report in writing to the Procuring Activity within 30 calendar days of determining any end item, component, part, or material contained in supplies purchased by the Department of Defense, or purchased by a Contractor or sub-Contractor for delivery to, or on behalf of, the Department, contains counterfeit electronic parts or suspect counterfeit electronic parts for the purpose of investigation and notification of the Air Force Office of Special Investigations (AFOSI). The Procuring Contracting Officer (PCO) will coordinate reporting to the appropriate Program Management/Item Management, System Engineering Management, the AFMC Discrepant Materiel Reporting Program (DMRP) Office in 406 SCMS/GULAB, and the AFOSI.

Additionally, the Contractor shall within the same 30 day period ensure all suspected or confirmed counterfeit items are entered into the Government-Industry Data Exchange Program (GIDEP) system, which will serve as the DoD central reporting repository. (Ref.

AS5553, paragraph 4.1.7, Appendix G)

1.8.1.10 Counterfeit Prevention Training. The Contractor shall provide appropriate training and shall require all personnel working procurement within their company, to include at a minimum their supply chain management specialists, receiving inspectors, and engineers, to complete said training. The Contractor shall determine the appropriate training required.

Training may be developed in-house or may be other Industry accepted training. The CPP will describe and list the training provided by the Contractor to their personnel.

1.9 Reporting CDRLs: The Contractor shall provide completed Certificate of Conformance documentation with each asset and its component parts that have been repaired with the intent of returning these assemblies or component parts to service. This documentation will have part number, serial number, work accomplished, Service Bulletins complied with on serviceable tag DD Form 1574.

The Contractor shall ensure that all reporting as specified under the following CDRL’s is accomplished:

A001: Commercial Asset Visibility Air Force (CAVAF) Reporting Requirements – DID: DI-

MGMT- 81634C

A002: Contract Depot Maintenance (CDM) Production Report – DID: DI-PSSS-81995 A003: Report of Shipping (Item) and Packaging Discrepancy (Subtitle SDR) – DID: DI-MGMT- 80503 A004: Counterfeit Prevention Plan (CPP) Report – DID: DI-MISC-81832

A005: Deficiency Report (DR) – DID: DI-PSSS-81535A A006: Annual Inventory Report – DID: DI-MGMT-80441C

A001: CAVAF Reporting Requirements CDRL – Contractor shall input the data IAW CAVAF Reporting Requirements guide and will not be waived. For CAVAF reporting, the Contractor shall submit (SDRs) when required and IAW CDRL DD Form 1423-1 IAW Para 1.2 & 1.7 of this PWS.

A002: CDM Production Report CDRL – Data IAW the CDM report will not be waived. The

File Number: FD2030-19-03037 10 report format Source: https://assist.dla.mil – Downloaded: 2015-09-24T17:50Z (sample form attached to CDRL). Data totals will be as of the end of each month and submitted to the PMS by the first week of next month. Contractor’s format with the same data elements as found on the CDM report may be accepted if approved through the PCO and IAW CDRL DD Form 1423-1 IAW Para 1.7 of this PWS.

A003: Report of Shipping (Item) and Packaging Discrepancy (SDR) CDRL – This report enables the Contractor to notify the Government when freight contents do not agree with shipping documents and IAW CDRL DD Form 1423-1. In addition, the Contractor shall submit Supply Discrepancy Reports (SDRs) when required IAW the contract’s CAVAF Reporting Requirements. Contractor shall process SDRs when required IAW Para 1.2 of this PWS.

A004: Counterfeit Prevention Plan (CPP) CDRL – The plan shall be delivered in electronic PDF format through the Wide Area Workflow (WAWF) system no later than 90 calendar days after contract award and IAW Para 1.8 of this PWS.

A005: Deficiency Reporting (DR) CDRL – The Deficiency Reporting (DR) is initiated on the occurrence when deficient Government assets are received by the Contractor. Contractor shall refer to T.O. 00-35D-54. Contractor shall process Deficiency Reports when required IAW Section 1.6 of this PWS.

A006: Annual Inventory Report CDRL – This report enables the contractor to periodically provide to the DoD Service/Agency an inventory listing of Government Property (i.e., both Government Furnished Property (GFP) and Contractor Acquired Property (CAP) in the contractor’s possession (to include sub-contractors) by contract.

A007: Government Furnished Material (GFM) by National Stock Number (NSN) CDRL – This Government Furnished Material report enables the contractor to provide special reporting in accordance (GFM). The first report should be submitted within five (5) business days after the close of the first reporting period (previous month's last calendar date). Format shall be IAW DI-PSSS- 80727A.

1.10 Item Unique Identification (IUID): The contractor shall follow the latest DoD instructions to install IUID compliant marks. TOs and drawings will be complied with for any component where direction is currently called out in the TO or drawings. Unless otherwise directed, the following Number Structure will be used as the IUID, in the order specified, in accordance with UII Construct #2 specified in MIL-STD-130N Table IV “UII construct business rules and supplemental data”. This number shall be incorporated into the box label, affixed or attached to the exterior of the item packaging, and shall not be affixed or attached to the part itself. Issuing Agency Code (IAC), Enterprise Identifier (CAGE Code, DUNs number or DODAAC), Original Part Number and Serial number.

1.11 Packaging and Handling: The contractor shall be responsible for the preservation and packaging of the TF33 2nd-4th Stage Turbine Nozzle Vanes IAW the Special Packaging Instructions specified on AFMC Form 158. 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- 129R, Department of Defense Standard Practice, Military Marking for Shipment and Storage. Use additional guidance for preparation and shipment IAW T.O.s 00-20-1, 00-20-3, MIL-STD-2073-1, MIL-STD-129, AFPAM24-237, and AFMAN 24-206. This contract does not allow for Commercial Packaging.

1.12 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 assets as appropriate in order to have the assets available to support the customer’s operational requirements and IAW the contract.

File Number: FD2030-19-03037 11

The Contractor shall not destroy reusable shipping containers, and will reuse them for return shipment.

In addition, the contractor shall submit Supply Discrepancy Reports (SDRs) related to shipment of misidentified items, variations in quantity, non-requisitioned items, lost or damaged parcel post, and items in dubious condition. These discrepancies shall be reported and resolved using the DoD web-based application WebSDR (Supply Discrepancy Report), 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.

1.13 Preservation: The contractor shall not destroy reusable shipping containers, and will reuse them for return shipment.

1.14 Document Storage: All records and reports outlined in this PWS shall be prepared for each part and a copy kept on file by the contractor for five (5) years.

1.15 Safety: The Contractor shall maintain and execute a safety program using MIL-STD-882E, AFI 91-301 and AFI 91-204 as guides.

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, in writing by email, of any damage to Government property where the dollar value 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.

1.16 Mission Essential Services:

1.16.1 Contractor Manpower Reporting: The contractor shall report ALL contractor labor hours (including subcontractor labor hours) required for performance of services provided under this contract for the USAF via a secure data collection site. The contractor is required to completely fill in all required data fields at https://www.ecmra.mil/Default.aspx . Reporting inputs will be for the labor executed during the period of performance for each Government fiscal year (FY), which runs 1 October through 30 September. While inputs may be reported any time during the FY, all data shall be reported no later than 31 October* of each calendar year. Contractors may direct questions to the CMRA help desk.

*Reporting Period: Contractors are required to input data by 31 October of each year.

SECTION II

2.0 SERVICE SUMMARY (SS)

Contractor performance shall be measured and assessed using the Performance Objectives listed in the TF33 2nd-4th Stage Turbine Nozzle Vanes Service Summary, Table 2-1.

File Number: FD2030-19-03037 12

2.1 Service Summary Requirements: The Contractor shall ensure the performance objectives and thresholds are achieved as follows:

2.1.1 Performance Objectives and Thresholds: The Contractor shall achieve performance thresholds identified in Table 2-1 of this PWS. The Contractor service requirements are summarized into performance objectives that relate directly to the mission essential items.

The performance threshold describes the minimum acceptable levels of service for each requirement. The government will use the surveillance methods contained in the performance plan to evaluate the Contractor’s performance for the performance objectives listed below. In the event the performance objective is not met, the Contractor will be given a reasonable time after notification to correct the unacceptable performance, if such correction is possible.

The Contractor shall immediately take corrective action in accordance with the performance threshold(s). In cases where the Contractor fails to implement corrective action, the PCO will take appropriate measures.

NOTE: The TF33 2nd-4th Stage Turbine Nozzle Vanes government PMS and PCO will exercise surveillance over the performance thresholds. The absence of any contract requirement from the SS shall not detract from this enforceability nor limit the rights or remedies of the government under any other provision of the contract.

2.1.2 Surveillance Methods: The Contractor shall support the Quality Assurance Representative (QAR)/ Defense Contract Management Agency (DCMA) surveillance methods as identified below:

a. Periodic Inspection of Process or Output

b. Random Sampling of Recurring Service Output

c. One Hundred (100) Percent Inspection of Output

d. Customer Observation or Complaint.

NOTE 1: The method of surveillance may include one or more of the methods specified above.

NOTE 2: The government will use the methods contained in the Contractor’s performance for the listed performance objectives. The TF33 2nd-4th Stage Turbine Nozzle Vanes government PMS and/or PCO will monitor Contractor performance to determine if it meets the contract thresholds as set forth in the performance measures and this PWS.

2.2 TF33 2nd-4th Stage Turbine Nozzle Vanes Service Summary:

Table 2-1

Performance Objective Reference / Paragraph (Para)

Performance Threshold

File Number: FD2030-19-03037 13

Quality Product:

Each TF33 2nd-4th Stage Turbine Nozzle Vane identified as serviceable shall be delivered to the government free of defects.

PWS

Para.1.5

100% of TF33 2nd-4th Stage Turbine Nozzle Vanes delivered shall be defect free.

Delivery Performance:

The Contractor shall meet the delivery schedule.

PWS

Para1.12 IAW

Contractual Delivery Schedule.

100% of TF33 2nd-4th Stage Turbine Nozzle Vanes shall be delivered IAW the contractual delivery schedule.

Quality Management System (QMS) for SS, Performance Objective: First Time Defect Detection Ratio: This is the identification element of a QMS to determine who typically finds and documents a contractual non-conformity, the CORs or the contractor’s quality system

Para 1.5.1 To receive a score of “0” or meets standard, the contractor must identify the same number of defects as the COR or miss no more than 4 defects.

(Example - COR detects 25 defects and the contractor QA detects 21)

2.3 Contractor Performance Evaluation: Evaluation will occur when the QAR or DCMA evaluates the service of the Contractor to determine whether or not it meets the SS objectives of the contract. In the event the performance measure is not met, the QAR or DCMA will issue written notification to the Contractor. In cases where the Contractor fails to implement corrective action, the QAR or DCMA will take appropriate measures.

SS -1: The Contractor's failure to meet this requirement shall result in a negative Contractor Performance Assessment Reporting (CPAR) rating and remedies as allowed under FAR 52.212-4 Inspection/Acceptance.

SS - 2: The Contractor's failure to meet this requirement shall result in a negative CPAR rating and remedies as allowed under FAR 52.212-4 Inspection/Acceptance.

SS -3: The Contractor's failure to meet this requirement shall result in a negative Contractor Performance Assessment Reporting (CPAR) rating and remedies as allowed under FAR 52.212-4 Inspection/Acceptance.

SECTION III

File Number: FD2030-19-03037 14

3.0 GOVERNMENT PROPERTY

3.1 Government Furnished Material (GFM): NONE. All parts and components required to accomplish the intent of the CMM, PWS or Service Bulletin’s (SB) shall be Contractor furnished material. Contractor furnished material and parts used for replacement shall be parts specified in CMM 75-21-30 Illustrated Parts Catalog (IPC), SB’s or has written approval from the AFMC AFLCMC/LPSAD and/or in writing through the PCO.

3.2 Government Furnished Property (GFP): All parts to be repaired will be shipped to the Contractor.

File Number: FD2030-19-03037 15

ACRONYMS

AFLCMC Air Force Life Cycle Management Center AFSC Air Force Sustainment Center AQAP Allied Quality Assurance Provision CAVAF Commercial Asset Visibility Air Force CDM Contract Depot Maintenance CDRL Contract Data Requirements List CPAR Contractor Performance Assessment Rating DID Data Item Description DER Designated Engineering Representative DR Deficiency Report DCMA Defense Contract Management Agency DLMS Defense Logistics Management System ES Equipment Specialist GFM Government Furnished Material GFP Government Furnished Property IAW In Accordance With IPE Initial Product Evaluation ISO International Standards Organization NADCAP North American Aerospace and Defense Contractors Accreditation Program NATO North Atlantic Treaty Organization ANSI American National Standards Institute NSN National Stock Number OEM Original Equipment Manufacturer PWS Performance Work Statement PCO Procurement Contracting Officer PCARSS Plant Clearance Automated Reutilization Screening System PMPS Parts, Material and Processes Selection PMS Production Management Specialist P/N Part Number QAR Quality Assurance Representative QMS Quality Management System ROD Report of Discrepancy SAE Special Areas of Emphasis SB Service Bulletin SCMS Supply Chain Management Report SDR Supply Discrepancy Report T.O. Technical Order USAF/DoD United States Air Force/Department of Defense WP Work Package

File Number: FD2030-19-03037 16

ATTACHMENT 1 (NSNs and P/Ns)

TF33 2nd-4th STAGE TURBINE NOZZLE VANES - NSNs AND P/Ns

NOUN: TF33 2-4th Stage Turbine Nozzle Vanes, CLIN 0001

INPUT/OUTPUT NSN: 2840-00-803-6721RV

INPUT/OUTPUT P/Ns: 446952CL9; 422552CL9; 565752CL9; 781252CL9; 798452CL9

NOUN: TF33 2-4th Stage Turbine Nozzle Vanes, CLIN 0002 INPUT NSNs: 2840-00-962-1256RV; 2840-00-768-3009RV

OUTPUT NSN: 2840-00-962-1256RV

INPUT P/Ns: 565854CL5; 495254CL5; 799554CL5; 565754CL5; 446954CL5; 387254CL5; 798454CL5

OUTPUT P/N: 565854CL5

NOUN: TF33 2-4th Stage Turbine Nozzle Vanes, CLIN 0003 INPUT NSNs: 2840-00-962-1260RV; 2840-00-898-7575RV

OUTPUT NSN: 2840-00-962-1260RV

INPUT P/Ns: 495253CL3; 565753CL3; 781253CL3; 799353CL3; 565853CL3; 446953CL3; 413853CL3 OUTPUT P/Ns: 565753CL3; 781253CL3

NOUN: TF33 2-4th Stage Turbine Nozzle Vanes, CLIN 0004 INPUT NSNs: 2840-00-962-1255RV; 2840-00-086-5103RV

OUTPUT NSN: 2840-00-962-1255RV

INPUT P/Ns: 781253CL1; 495253CL1; 565753CL1; 799353CL1; 565853CL1; 446953CL1; 413853CL1 OUTPUT P/Ns: 565753CL1; 781253CL1

NOUN: TF33 2-4th Stage Turbine Nozzle Vanes, CLIN 0005

INPUT/OUTPUT NSN: 2840-00-673-2210RV

INPUT/OUTPUT P/Ns: 446952CL10; 422552CL10; 565752CL10; 781252CL10; 798452CL10

NOUN: TF33 2-4th Stage Turbine Nozzle Vanes, CLIN 0006

OUTPUT/OUTPUT NSN: 2840-00-757-0307RV

INPUT/OUTPUT P/Ns: 446952CL11; 422552CL11; 565752CL11; 781252CL11; 798452CL11

NOUN: TF33 2-4th Stage Turbine Nozzle Vanes, CLIN 0007

INPUT/OUTPUT NSN: 2840-00-757-0303RV

INPUT/OUTPUT P/Ns: 446952CL12; 422552CL12; 565752CL12; 781252CL12; 798452CL12

NOUN: TF33 2-4th Stage Turbine Nozzle Vanes, CLIN 0008

File Number: FD2030-19-03037 17

INPUT/OUTPUT NSN: 2840-00-757-0305RV

INPUT/OUTPUT P/Ns: 446952CL14; 422552CL14; 565752CL14; 781252CL14; 798452CL14

NOUN: TF33 2-4th Stage Turbine Nozzle Vanes, CLIN 0009 INPUT NSNs: 2840-00-962-1259RV; 2840-00-086-5111RV

OUTPUT NSN: 2840-00-962-1259RV

INPUT P/Ns: 495253CL2; 565753CL2; 781253CL2; 565853CL2; 446953CL2; 413853CL2 OUTPUT P/Ns: 565753CL2; 781253CL2

NOUN: TF33 2-4th Stage Turbine Nozzle Vanes, CLIN 0010 INPUT NSNs: 2840-00-962-1261RV; 2840-00-898-7574RV

OUTPUT NSN: 2840-00-962-1261RV

INPUT P/Ns: 495253CL4; 565753CL4; 781253CL4; 799353CL4; 565853CL4; 446953CL4; 413853CL4 OUTPUT P/Ns: 565753CL4; 781253CL4

NOUN: TF33 2-4th Stage Turbine Nozzle Vanes, CLIN 0011

INPUT/OUTPUT NSN: 2840-00-757-0304RV

INPUT/OUTPUT P/Ns: 446952CL13; 42255CL13; 565752CL13; 781252CL13; 798452CL13; 403352CL13

NOUN: TF33 2-4th Stage Turbine Nozzle Vanes, CLIN 0012

INPUT/OUTPUT NSN: 2840-00-966-3028RV

INPUT/OUTPUT P/Ns: 489152CL11; 565852CL11

NOUN: TF33 2-4th Stage Turbine Nozzle Vanes, CLIN 0013

INPUT/OUTPUT NSN: 2840-00-966-3027RV

INPUT/OUTPUT P/Ns: 489152CL10; 565852CL10

NOUN: TF33 2-4th Stage Turbine Nozzle Vanes, CLIN 0014 INPUT NSNs: 2840-00-962-1262RV; 2840-00-898-7573RV; 2840-00-836-4162RV; 2840-00-836-4166RV;

2840-00-898-7572RV; 2840-00-898-7571RV

OUTPUT NSN: 2840-00-962-1262RV

INPUT P/Ns: 781253CL5; 495253CL5; 565753CL5; 799353CL5; 565853CL5; 413853CL5; 781253CL5 446953CL5; 495253CL6; 565753CL6; 781253CL6; 799353CL6; 495253CL7; 565753CL7; 781253CL7;

446953CL6; 413853CL6; 446953CL7; 413853CL7

OUTPUT P/Ns: 565753CL5; 781253CL5; 495253CL5

NOUN: TF33 2-4th Stage Turbine Nozzle Vanes, CLIN 0015 INPUT NSNs: 2840-00-962-1264RV; 2840-00-768-3007RV

OUTPUT NSN: 2840-00-962-1264RV

INPUT P/Ns: 565854CL7; 495254CL7; 799554CL7; 565754CL7; 446954CL7; 387254CL7; 798454CL7

File Number: FD2030-19-03037 18

OUTPUT P/N: 565854CL7

NOUN: TF33 2-4th Stage Turbine Nozzle Vanes, CLIN 0016 INPUT NSNs: 2840-00-962-1263RV; 2840-00-768-3008RV

OUTPUT NSN: 2840-00-962-1263RV

INPUT P/Ns: 565854CL6; 495254CL6; 799554CL6; 565754CL6; 446954CL6; 387254CL6; 798454CL6

OUTPUT P/N: 565854CL6

NOUN: TF33 2-4th Stage Turbine Nozzle Vanes, CLIN 0017

INPUT/OUTPUT NSN: 2840-00-966-3030RV

INPUT/OUTPUT P/Ns: 489152CL13; 565852CL13

NOUN: TF33 2-4th Stage Turbine Nozzle Vanes, CLIN 0018

INPUT/OUTPUT NSN: 2840-00-966-3029RV

INPUT/OUTPUT P/Ns: 489152CL12; 565852CL12

NOUN: TF33 2-4th Stage Turbine Nozzle Vanes, CLIN 0019 INPUT NSNs: 2840-00-962-1265RV; 2840-00-962-1266RV; 2840-00-768-3005RV

OUTPUT NSN: 2840-00-962-1265RV

INPUT P/Ns: 565854CL8; 495254CL8; 799554CL8; 565854CL9; 495254CL9; 799554CL9; 565754CL9;

446954CL9; 798454CL9; 387254CL9

OUTPUT P/N: 565854CL8

NOUN: TF33 2-4th Stage Turbine Nozzle Vanes, CLIN 0018

INPUT NSN: 2840-00-966-8081RV

INPUT P/Ns: 489152CL9; 565852CL9

NOUN: TF33 2-4th Stage Turbine Nozzle Vanes, CLIN 0019 INPUT NSNs: 2840-00-803-6721

INPUT P/N: 446952CL9; 422552CL9; 565752CL9; 781252CL9; 798452CL9

File Number: FD2030-19-03037 19