SOLICITATION NOTICE
49 -- Flight Control Test Set
- Notice Date
- 6/12/2002
- Notice Type
- Solicitation Notice
- Contracting Office
- Department of the Air Force, Air Force Materiel Command, WR-ALC, WR-ALC/PK Acquisition Opportunities 235 Byron Street, Warner Robins ALC, GA, 31098-1611
- ZIP Code
- 31098-1611
- Solicitation Number
- F09603-02-R-71973
- Response Due
- 8/5/2002
- Archive Date
- 8/20/2002
- Point of Contact
- William Hecker, Contract Specialist, Phone (478)926-7851, ext 132, Fax (478) 926-7801, - Michelle Wood, Contracting Officer, Phone (478) 926-7851, ext 135, Fax (478) 926-7801,
- E-Mail Address
-
William.Hecker@robins.af.mil, Michelle.Wood@robins.af.mil
- Description
- ITEM: Flight Control Test Set*** PART NUMBER: AS111694*** NSN: 4920-01-126-1759RN*** QUANTITY: 32 Each*** DELIVERY REQUIRED By 29 Nov 2002*** REQUEST FOR Proposal Will Be Posted To This Notice On Or About 3 July 2002*** DRAWINGS ARE NOT AVAILABLE*** EXPORT CONTROLLED: NO*** GENERAL ITEM CHARACTERISTICS: Test Set for Emergency Power Unit System. Electrical Requirements: 28 vdc at 1 amp. Pneumatic Requirements: Gaseous nitrogen at 400 psi (nominal) and 55 psi (minimum). Dimensions (approximate): L = 22.44 inches, W = 14.06 inches, H = 16.38 inches, Weight = 60 lbs. Consists of a panel assembly, two cable assemblies, two hose assemblies, a contents plate, a schematic diagram, and spare lamps contained within a carrying case. The panel assembly is fastened to the bottom hald of the carrying case; the cableassemblies and hose assemblies are stowed in a storage compartment in the upper half of the carrying case; the contents plate and schematic diagram are cemented to the storage compartment lid; and the spare lamps are contained in a padded box on the storage compartment lid. The panel assembly consists of electrical and pneumatic components mounted on a panel and on a chassis assembly. The test set is used to functionally test components of the EPU system with the system installed in the aircraft. The test set contains circuits for testing the airborne emergency power unit system (EPU) with the EPU system installed in the aircraft. Components of the test set include: Power supply circuit, Lamp test circuit, Sensor continuity circuit, Augment circuit, Simulated turbine speed circuit, Controller response circuit, and Gaseous nitrogen circuit. Application is for the F-16 A/B aircraft. APPLICABLE NUMBERED NOTES: 22 (One Known Source), 26 (Non-Commercial Item) APPLICABLE WR-ALC LOCAL NOTES: "B" Ombudsman, ""B" - All potential offerors should contact the buyer/PCO identified below for additional information and/or to communicate concerns, if any, concerning this acquisition. If your concerns are not satisfied by the contacting officer an Ombudsman has been appointed to hear serious concerns that are not resolved through established channels. The purpose of the Ombudsman is not to diminish the authority of the program director or contracting officer, but to communicate serious contractor concerns, issues, disagreements, and recommendations to the appropriate government personnel. When requested, the Ombudsman will maintain strict confidentiality as to the source of the concern. The Ombudsman does not participate in the evaluation of proposals or in the source selection process. When appropriate, potential offerors may contact Ombudsman Ms Kathy Cames, PKP, at 478-926-2604. Please be prepared to identify previous contacts made by you in an attempt to resolve your concerns.
- Record
- SN00092337-W 20020614/020613084519 (fbodaily.com)
- Source
-
FedBizOpps.gov Link to This Notice
(may not be valid after Archive Date)
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