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This Award Notice opportunity was posted on September 28, 2012. The submission period has ended. Browse the details below for market research, or find similar active opportunities.

29--Engine Accessories

Awarded
SPRTA1-12-R-0013Federal

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This contract, awarded to Hamilton Sundstrand Corporation, involves the procurement of 22 Super VP Control Units and associated CEMS tracking data. The control units are complex aluminum assemblies consisting of a control cover and housing that integrate pressure transducers, printed circuit board assemblies, and various interface modules. These units are designed for engine management, utilizing engine fuel and nacelle air for cooling to maintain the functionality of the internal processor, memory, and converter modules. The deliverables are scheduled for delivery to Tinker Air Force Base in Oklahoma, with a final delivery date of January 31, 2014. The contract period for the tracking data is one year. This acquisition falls under the category of engine accessories and was processed via an electronic solicitation under NAICS code 336412.

General Info

Agency

N/A

Contract Value

$3,687,003

NAICS

336412 - Aircraft Engine and Engine Parts Manufacturing

Place of Performance

IL, USA

Set-Aside

NONE

Award Issued Date

Documents

0

No documents available

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Timeline

1 update
PhaseAwarded
Posted

Presolicitation

Type Changed

Presolicitation → Solicitation

Justification (J&A)

Justification & Approval published

Awarded

Contract was awarded

Submission Closed

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Organization & Contact Information

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AgencyN/A
ContactsNo contacts available
OfficeN/A
Organization / Agency
N/A
Office AddressN/A
ContactsNo contact information available

Full Description

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PR Number(s): FD20301270006Item: 0001NSN: 2995015203563NZ CONTROL UNIT,SUPERVP/N: 1002300H02D03, P/N: 4088029D01, Description: Aluminum. The DEEC consists of a control cover and acontrol housing, that contain pressure transducers, input/output (I/O)connectors, and printed circuit board assemblies. Circuit boardassemblies are interconnected by flexible cables and connectors. Acenter connector provides a signal cross link between circuit boardassemblies housed within the control cover and control housing. I/Oconnectors provide electrical connection between and DEEC and enginesensors, interfaces and actuators. Unit cooling is provided by enginefuel via cooling passages in the control cover and control housing, withadditional outer wall heat dissipation provided by nacelle air.Control Cover: Control cover is an aluminum casting, which includes afuel outlet port connected to internal 1/4-inch diameter cooling cores,brackets for vibration isolators, a handle to simplify transport andcutouts for five I/O connectors. Control cover houses the AircraftInterface Module and Engine Interface Module.Control Housing: Control housing is an aluminum casting, which includesa fuel inlet port connected to internal 1/4 inch diameter cooling cores,brackets for vibration isolators, cutouts for three pressure transducersand an I/O connectors. Control housing contains two printed circuitboard assemblies: Converter Module, and processor and memory boardassembliesFrom Quantity: 22.0000 EA Destn: SW3211,TINKER AFB,OK ,73145-8000. Delivery: 31 JAN 2014 Monthly Beginning On or Before, 10.00 PR Number(s): FD20301270006Item: 0002CEMS TRACKING DATA Description: Quantity: 1.0000 LO Duration of Contract Period: One Year Electronic procedure will be used for this solicitation. To: HAMILTON SUNDSTRAND CORPORATION, WINDSOR LOCKS, CT.,06096-1000.

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