SOLICITATION NOTICE
28 -- DISK,TURBINE,AIRCRA
- Notice Date
- 4/22/2010
- Notice Type
- Presolicitation
- NAICS
- 336412
— Aircraft Engine and Engine Parts Manufacturing
- Contracting Office
- DEFENSE LOGISTICS AGENCY; DLR PROCUREMENT OPS DSCR-ZBA;3001STAFF DRIVE; TINKER AFB; OK; 73145
- ZIP Code
- 73145
- Solicitation Number
- SPRTA1-10-Q-0391
- Response Due
- 5/24/2010
- Point of Contact
- James Menefee, Phone 405-734-8111, Fax 000-000-0000, Emailjames.menefee@tinker.af.mil
- E-Mail Address
-
James Menefee
(james.menefee@tinker.af.mil)
- Small Business Set-Aside
- N/A
- Description
- DUMMY SYNOPSIS: SYNPOSIS NOT REQUIRED PR Number(s): FD20301071361Item: 0001NSN: 2840011594265RVRV DISK,TURBINE,AIRCRAP/N: 496801, P/N: 812001, Description: The first stage turbine disk is round and flat and isapprox 2 inches thick. This disk has a center bore approximately 5.6inches in diameter and 130 fir tree slots around the periphery of thedisk, with an offset front flange 12.7 inches in diameter. The functionof the first stage turbine disk is to provide support and attachment ofthe first stage turbine blades to the N2 roto. The dimensions areapprox 23.5 inches dia by approx 2 inches thick at the bore and approx1.25 inches thick at the fir tree slots. The material consists of AMS5660 and PWA 1003 nickel alloy. Acft: Joint Stars; Engine: TF33P102.From Quantity: 1.0000 EA Destn: FB2039,Tinker AFB,OK.,73145-9013. Delivery: 29 OCT 2010, 2.00 PR Number(s): FD20301071361Item: 0002CEMS TRACKING DATA Description: Quantity: 1.0000 LO Destn: DD1423,,., -. Delivery: TBC, 1.00 LO PR Number(s): FD20301071361Item: 0003NSN: 2840011594265RVRV DISK,TURBINE,AIRCRAP/N: 496801, P/N: 812001, Description: The first stage turbine disk is round and flat and isapprox 2 inches thick. This disk has a center bore approximately 5.6inches in diameter and 130 fir tree slots around the periphery of thedisk, with an offset front flange 12.7 inches in diameter. The functionof the first stage turbine disk is to provide support and attachment ofthe first stage turbine blades to the N2 roto. The dimensions areapprox 23.5 inches dia by approx 2 inches thick at the bore and approx1.25 inches thick at the fir tree slots. The material consists of AMS5660 and PWA 1003 nickel alloy. Acft: Joint Stars; Engine: TF33P102.From Quantity: 1.0000 EA Destn: FB2039,Tinker AFB,OK.,73145-9013. Delivery: 29 OCT 2010, 2.00 The anticipated award date will be:30NOV2009 Duration of Contract Period: DUMMY SYNOPSIS -- SYNOPSIS NOT REQUIRED Electronic procedure will be used for this solicitation. To: UNITED TECHNOLOGIES CORPORATION, EAST HARTFORD, CT.,06108-0968. To:UNITED TECHNOLOGIES CORPORATION, EAST HARTFORD, CT.,06108-0968. To:UNITED TECHNOLOGIES CORPORATION, EAST HARTFORD, CT.,06108-0968. To:UNITED TECHNOLOGIES CORPORATION, EAST HARTFORD, CT.,06108-0968. IAW FAR 5.207(c)(15)(ii), All responsible sources may submit acapability statement, proposal, or quotation, which shall be consideredby the agency
- Web Link
-
FBO.gov Permalink
(https://www.fbo.gov/spg/USAF/AFMC/OCALCCC/SPRTA1-10-Q-0391/listing.html)
- Record
- SN02129780-W 20100424/100422235137-e18a70e58bcc72bc0a1a09f2aa0078dc (fbodaily.com)
- Source
-
FedBizOpps Link to This Notice
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