Sa-Alc/Propulsion Directorate, 485 Quentin Roosevelt Rd, Kelly Afb, Texas 78241-6427

28 -- HIGH PRESSURE TURBINE SOL F41608-98-R-43161 DUE 040998 POC For copy, Fax request to LPKAF at (210)925-8496, For additional information contact Johnson, B./lpkaf/[210]925-6566 Item 0001 NSN 2840-01-341-6211PT P/N: 4067247, Government Furnished Drawings And Specifications Are Not Available. Size: 7" high X 30" diameter; Predominate Material: nickel based alloy (inconel 718, IN100, waspaloy); Function: Design. Rear compressor turbine section includes 1st and 2nd stage disk and blades, (turbine rotors), 1st and 2nd stage turbine stator vanes, and front turbine case; Turbine Rotor. Two rotor stages are contained in front turbine case; Stator and supports. First stage turbine stator vamen assembly consists of paired stator vanes contained by two supports; Front Case. Front turbine case encloses two turbine rotor stages. It contains 2nd stage turbine stator vanes and turbine blade tip seal land segments. It also provides passage for 13th stage cooling air to 1st stage turbine stator vanes. Borescope inspection port for turbine inlet is located at approximately 5 o'clock position; The high pressure turbine extracts the power required to rotate the high pressure compressor. 3EA. Applicable to: F100-220. Destn: FMS. Delivery: 31 Jul 98 3 ea The approximate issue/response date will be 10 Mar 98. To: United Technologies Corp/Pratt And, West Palm Beach Fl 33410-9600. 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. Authority: 10 U.S.C. 2304(C)(1), Justification: Supplies (or Services) required are available from only one or a limited number of responsible source(s) and no other type of supplies or services will satisfy agency requirements. See Note (s) 22, 26. (0049)

Loren Data Corp. http://www.ld.com (SYN# 0191 19980220\28-0002.SOL)