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

J -- REPAIR OF F101 DIVERGENT FLAPS SOL F34601-98-R-XXXX1 DUE 042098 POC For copy, OC-ALC/PKXDA TINKER AFB OK 73145-3015, For additional information contact Tommy Nicholson/Lpdpa/[405]739-4400 THIS IS A REPAIR SOURCE SEEKING SYNOPSIS. A REQUIREMENT EXISTS FOR THE REPAIR OF THE F101 DIVERGENT FLAP, P/N 9989M80G06. GENERAL REQUIREMENTS ARE TO: (1) INSPECT AND REPAIR IN ACCORDANCE WITH APPLICABLE DRAWING AND TECHNICAL ORDERS. REFERENCED DATA IS AS FOLLOWS: A. DRAWING 9980M83, B. T.O. 2J-F101-3-5, WP 163 00, C. T.O. 2J-F101-3-6, WP 163 00, D. T.O. 2J-F101-3-8, SWP 003 08, E. 2J-F101-3- 4, SWP 005 01, F. T.O. 2J-F101-3-4, SWP 005 19. AN ADDITIONAL REPAIR PROCEDURE FOR MID STIFFENER WILL HAVE TO BE DEVELOPED AND DEMONSTRATED ON A SAMPLE PART. ALL OTHER REPAIRS MUST BE DEMONSTRATED ON SIMILAR TYPE WORK. DIVERGENT FLAPS TO BE UPGRADED TO THE G08 CONFIGURATION. THE DIVERGENT FLAP IS A WELDED SHEET METAL ASSEMBLY THAT INCLUDES SOME CAST COMPONENTS. NUMEROUS WELDING OPERATIONS ARE ALSO REQUIRED. THE MATERIAL IS RENE 41 WITH DIMENSIONS AS FOLLOWS: 24 INCHES LONG BY 7 INCHES WIDE AND 4 INCHES AT THE HIGHEST POINT. SOME SURFACES REQUIRE APPLICATION OF A WEAR COATING. HEAT TREAT IS ALSO REQUIRED DURING THEREPAIR. THE AIR FORCE WILL HOLD A SEMINAR AT 1300 HOURS ON 20 APR 98 AT TINKER AFB OK TO ALLOW PROSPECTIVE VENDORS TO VIEW A SAMPLE PART. IN ADDITION, TECHNICAL ENGINEERING AND REQUIREMENTS PERSONNEL FROM THE AIR FORCE WILL BE ON HAND TO ANSWER QUESTIONS AND DISCUSS REQUIREMENTS. ALL INTERESTED PARTIES MUST CONTACT TOMMY NICHOLSON, OC-ALC/LPDPA, A/C 405-739-4400, FAX 405-739-4237 FOR ADDITIONAL INFORMATION. The approximate issue/response date will be 06 APR 98. 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. (0097)

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