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30 -- SHOULDERED SHAFT

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Reference-Number-FD2030-05-54704Federal

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The contract pertains to the procurement of a single shouldered shaft, part number 4060568-01, measuring 72 inches in length, specifically designed to drive the inlet fan of the F100-229 engine. Manufactured primarily from a nickel alloy, this component is critical to engine functionality and has been designated a reliability control part due to the unacceptable safety risks associated with its potential failure. Consequently, strict reliability requirements are in place, though the data to define and control these parameters are not provided or available from the Government. The contract foregoes the use of a written procedure for the solicitation and emphasizes the importance of adherence to established reliability standards. The solicitation, identified by reference number FD2030-05-54704 and posted on June 8, 2005, is categorized under NAICS code 336412, which relates to aerospace product and parts manufacturing. The contract is directed to Pratt and Whitney, a key manufacturer in the aerospace sector. Contact for further information is Kelli D. Jones, reachable by phone or email at the Tinker Air Force base. The contract documentation underscores the critical nature of the shaft in maintaining safe engine operation, and any deviation in performance could compromise the safety of personnel and equipment.

General Info

Procurement of a critical nickel alloy shaft for F100-229 engine inlet fan, emphasizing reliability control.

Agency

N/A

NAICS

336412 - Aircraft Engine and Engine Parts Manufacturing

Place of Performance

Not specified

Set-Aside

NONE

Documents

0

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Timeline

PhasePresolicitation
Posted

Presolicitation

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Organization & Contact Information

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AgencyN/A
Contacts1 person available
OfficeN/A
Organization / Agency
N/A
Office AddressN/A

Full Description

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3040-01-310-0756NZ- SHOULDERED SHAFT. Item No. 0001, P/N: 4060568-01, QTY 1 EA. Size/Dimensions: 72 inches long. Form/Fit/Function: Shaft is used to drive inlet fan. Predominant Material: Nickel Alloy. Applicable to: F100-229 Engine. Written procedure will not be used for this solicitation. To: Pratt and Whitney. This part has been designated a reliability control part under a formal reliability program. The probability of failure would be unacceptable from the standpoint of safety of personnel and/or equipment. Data to control the reliability limits and/or define the performance parameters that control these limits is not defined nor can they be adequately drafted by the Government. See Note (s) 22, 26.

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DLA WEAPONS SUPPORT LAND SUPPLIER OPNS VEHICLE SPT

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in 11 days
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