MEC_-_SOWFINALFINAL.docx

STATEMENT OF WORK (SOW)

F108-100/201 MAIN ENGINE CONTROL (MEC)

PURCHASE REQUEST NUMBER: FD2030-13-02142

PREPARATION DATE: 09 May 2014

TABLE OF CONTENTS Page

Section I

Section II

Section III

Appendix

Acronyms 7

1.0 Work Scope: This Statement of Work (SOW) defines the requirements necessary to ensure that delivered remanufactured F108 Main Engine Control (MEC) are remanufactured as nearly as possible to original life expectancy consistent with Air Force (AF) requirements set forth herein. This SOW applies to the following National Stock Numbers (NSN) and Part Numbers (P/N):

The instructions stipulated are brief, concise statements providing general requirements for delivered remanufactured F108 Main Engine Control. All performance, with respect to the delivered remanufactured F108 Main Engine Control and component parts shall be performed at a contractor owned or operated that performs remanufacture using manufacturing processes similar to those used in the manufacture of F108 Main Engine Control. Contractor shall have remanufacture capabilities to include required technical data, repair documents, and license agreements to accomplish remanufacture of F108 Main Engine Control 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 Federal Acquisition Regulation (FAR) 22.1003-6(a)(1) prior to approval and performance.

1.2 Quality System and 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 In Accordance With (IAW) AFPD 63-5, Quality Assurance and AFI63-501, Air Force Acquisition Quality Program, or an ISO 9001:2000/ANSI ASQC Q92 or equivalent requirements 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 Safety:

The Contractor shall maintain and execute a safety program usingMIL-STD-882D, Air Force Instruction (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 Commercial 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 Government Furnished Property (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.

1.4 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 F108 Main Engine Control ordered, the Government will provide, on a one to one basis, degraded or inoperable F108 Main Engine Control consistent with aircraft engine usage.

1.5 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 Main Engine Control 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 CFMI Overhaul Instructions Manual, Technical Order (T.O.) 6J3-4-113-3, for Main Engine Control. 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, lost or damaged parcel post, and meaningful damage to GFP inconsistent with aircraft engine usage. These discrepancies shall be reported and resolved using the Department of Defense (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.

1.6 Remanufacture

Remanufactured F108 Main Engine Control shall be restored to original life expectancy or nearly so, in compliance with CFMI Overhaul Instructions Manual, T.O. 6J3-4-113-3, for Main Engine Control; CFMI Illustrated Parts Breakdown, T.O. 6J3-4-113-4 for Main Engine Control; and all applicable CFM56-2B Service Bulletin authorized modifications. Contractor shall identify all Military Main Engine Controls processed through contractor’s remanufacture facility as Military Parts prior to processing.

1.6.1 Remanufacture Procedures:

F108 Main Engine Control and component parts shall be remanufactured IAW the procedures outlined in the CFMI Overhaul Instructions Manual, T.O. 6J3-4-113-3, for Main Engine Control; CFMI Illustrated Parts Breakdown, T.O. 6J3-4-113-4 for Main Engine Control; and all applicable CFM56-2B Service Bulletin authorized modifications.

Delivered remanufactured F108 Main Engine Control shall contain remanufactured hardware or new parts meeting the requirements of this SOW. The Contractor shall inspect remanufactured and new components to ensure that they meet United States Air Force (USAF) build requirements.

Contractor shall acquire component parts from Air Force approved vendors, Government inventory; Original Equipment Manufacturer (OEM) approved vendors, or commercial inventories approved by the USAF and/or OEM. All remanufactured MECs delivered will meet the inspection criteria. All remanufactured components shall comply with the latest revision of all CFMI Overhaul Instructions Manual, T.O. 6J3-4-113-3, for Main Engine Control; CFMI Illustrated Parts Breakdown, T.O. 6J3-4-113-4 for Main Engine Control; and all applicable CFM56-2B Service Bulletin authorized modifications, along with any outstanding FAA Airworthiness Directives.

Testing & Evaluation: The Contractor shall conduct all testing IAW CFMI Overhaul Instructions Manual, T.O. 6J3-4-113-3, for Main Engine Control; CFMI Illustrated Parts Breakdown, T.O. 6J3-4-113-4 for Main Engine Control; and all applicable CFM56-2B Service Bulletin authorized modifications. The Government reserves the right to witness any and/or all tests conducted by the Contractor and/or subcontractors on a noninterference basis.

1.6.2 Remanufacture Deviations:

Prior to effecting deviations in manufacturing or inspection processes for Main Engine Controls the contractor shall obtain written approval for deviations from the PCO.

1.6.3 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.

1.7 Packaging and Handling:

The Contractor shall be responsible for the preservation and packaging of the delivered F108 Main Engine Control IAW the Special Packaging Instructions specified on Air Force Material Command (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.

1.8 Shipping and Transportation:

Contractor shall meet the delivery schedule. Contractor shall ship or transport applicable deliverables as appropriate in order to have the deliverables available to support the customer’s operational requirements and in accordance with the contract’s delivery schedule. Contractor shall not destroy reusable shipping containers, and will reuse them for return shipment.

1.9 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.

SECTION II

2.0 Applicable Documents

2.1 Reporting:

The Contractor shall meet the delivery schedule. Contractor shall provide completed Federal Aviation Administration (FAA) Form 8130-3 with each remanufactured F108 Main Engine Control 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 Contract Data Requirements List (CDRL) is accomplished:

A001: Commercial Asset Availability Air Force (CAV AF) A002: Depot Maintenance Production Report (DMPR)-AFMC Form 413 A003: Comprehensive Engine Management System (CEMS)-AF Form 1534 A004: Test Inspection Report A005: Quality Deficiency Report (QDR)-SF Form 368 A006: Supply Discrepancy Report (SDR)

A001- CAV AF Reporting: CAV AF Reporting: The contractor shall input the data IAW CAV AF SOW guide. For CAV AF reporting, the Contractor shall submit SDRs when required.

A002- DMPR: The data totals shall be as of the end of each month. This data requirement shall not be waived. However, the Contractor’s format for reporting production data may be accepted if it includes all the same data elements as the Air Force Materiel Command (AFMC) Form 413 Report.

A003 - Comprehensive Engine Management System: The contractor shall provide the following information for each remanufactured MEC on the Air Force (AF) Form 1534: Configured Item Identifier (CII) Designation, Serial Number (S/N), Date work was accomplished, Stock Record Account Number (SRAN), P/N, Type of Transaction and Time on MEC. The AF Form 1534 is required to be submitted by close of business of the business day following the occurrence of the reportable event. (An example of the AF Form 1534 may be provided to use as a guide.) If contractor doesn’t have CEMS access yet they can e-mail the AF Form 1534 to the following email address, cems.pmo.helpdesk@us.af.mil , until they gain access.

A004- Test Inspection Report: The Test Inspection Reporting is used when an occurrence of a Mishap Investigation is conducted. The report documents test results, findings and analyses that will enable the Government or contracting agency to evaluate compliance with system requirements and performance objectives.

A005- QDR: The QDR is initiated on the occurrence when deficient Government assets are received by the Contractor. Contractor shall refer to T.O. 00-35D-54 and create a report in Joint Deficiency Reporting System (JDRS).

A006-SDR: 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.

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 CFMI Overhaul Instructions Manual, T.O. 6J3-4-113-3, for Main Engine Control; CFMI Illustrated Parts Breakdown, T.O. 6J3-4-113-4 for Main Engine Control; and all applicable Service Bulletin authorized modifications. All remanufactured nozzles must meet the inspection criteria.

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 CFMI Overhaul Instructions Manual, T.O. 6J3-4-113-3, for Main Engine Control; CFMI Illustrated Parts Breakdown, T.O. 6J3-4-113-4 for Main Engine Control; and/or all applicable Service Bulletin authorized modifications. 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 Number: FD20301302142 Page 2