Oc-Alc/Dir Of Contracting/Propulsion, 3001 Staff Dr Ste 1ag81, Tinker Air Force Base Ok 73145-3032

J -- ENGINE MONITORING SYSTEM PROCESSOR SOL F34601-97-R-54806 DUE 070396 POC For copy, OC-ALC/PKXDA TINKER AFB OK 73145-3015, For additional information contact Lois Frederick/Lpdpa/(405)739-4401 Services, Non-Personal: The contractor shall provide all labor, facilities, equipment and all material to accomplish and packaging of the Engine SMonitoring System Processor (EMSP). A Firm Fixed Price Requirements type contract is contemplated for One Year, plus one One-Year Options. The Items and Best Estimated Quantities (BEQ) are as follows: CLIN 0001: NSN 6620-01-379-1235JU and/or 6620-01-378-5214JU and/or6620-01- 378-5512JU (INPUT) 6620-01-137-5214JU and/or 6620-01-378-5512JU;(OUTPUT) P/N 1529M60P13 and/or 1529M60P14 and/or 1529M60P15 (INPUT) 1529M60P14 AND/OR 1529M60P15 (OUTPUT); NOUN: Engine Monitoring System Processor (EMSP); APPL: F118-GE-100 Engine; Basic Year Qty: 24 Ea; Option I Qty: 26 Ea; Material: Aluminum. Description and Function: The EMSP is comprised of nine plug-in circuit card assemblies (CCA), a power supply, two pressure transducers, a wiring harness, and cooling fuel inlet and outlet ports. The wiring harness consists of 2 motherboards hard-wired to a potentiometer assemble, 12 external connectors, 3 terminal boards, and a cold junction All components are housed in a dip-brazed aluminum housing. a. Fuel tubing is brazed to the housing. A fuel flow of 60-916 pph through the tubing is used to cool the kkEMSP. b. The CCA contain electronic components mounted on multilayer printed wiring boards. Each CCA coonnector is keyed to its respective motherboard connector, this prevents insertion into a wiring location. Each CCA is secured to the housing by two locking card extractors which lock the CCA tight to the housing heat-sink locking bars. Removal of the cover allows access to the nine CCA. c. The EMSP housing incorporates four mounts with vibration isolation hardware for use when mounting the EMSP to an engine. CLIN 0002: DATA IAW DD Form 1423. Basic year: Exhibit ''A''; Option I: Exhibit ''B''; Item 0002 data, 1 lot Item 0003 data, 1 lot The approximate issue/response date will be 03 Jun 96. To: LOCKHEED-MARTIN CONTROL SYSTEM, BINGHAMPTON NY. To: General Electric Co Aircraft Engine, Cincinnati Oh 45215-6301. No telephone requests. Only written or faxed requests received directly from the requestor are acceptable. All responsible sources solicited may submit a bid, proposal, or quotation which shall be considered. It is suggested that small business firms or others interested in subcontracting opportunities in connection with the described procurement make contact with the firm(s) listed. Specifications, plans, or drawings relating to the procurement described are incomplete or not available and cannot be furnished by the Government. Note: An Ombudsman has been appointed to hear concerns from offerors or potential Offerors during the proposal development phase of this acquisition. The purpose of the Ombudsman is not to diminish the authority of the program director or contracting officer, but to communicate contractor concerns, issues, disagreements, and recommendations to the appropriate government personnel. When requested, the Ombudsman will maintain strict confidentiality as to source of the concern. The Ombudsman does not participate in the evaluation of proposals or in the source selection process. Interested parties are invited to call the Ombudsman at (405) 736-3273. DO NOT CALL THIS NUMBER FOR SOLICITATION REQUESTS. Note: Faxed solicitation requests can be submitted to OC-ALC/PKXDA, Tinker AFB OK 73145-3015, FAX NUMBER (405)739-5411. (0136)

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