SOLICITATION NOTICE
49 -- TEST SET, AIRCRAFT
- Notice Date
- 5/18/2010
- Notice Type
- Presolicitation
- NAICS
- 336413
— Other Aircraft Parts and Auxiliary Equipment Manufacturing
- Contracting Office
- Department of the Air Force, Air Force Materiel Command, WR-ALC, WR-ALC/PK Acquisition Opportunities, 235 Byron St,, Warner Robins, Georgia, 31098-1611, United States
- ZIP Code
- 31098-1611
- Solicitation Number
- FA8532-10-R-22615
- Archive Date
- 7/17/2010
- Point of Contact
- Kathryn G Canady, Phone: 478-222-1905
- E-Mail Address
-
Kathy.Canady@robins.af.mil
(Kathy.Canady@robins.af.mil)
- Small Business Set-Aside
- N/A
- Description
- NSN 4920007786091RN, TEST SET, AIRCRAFT ENGINE, PART NUMBER 281069-1UTILIZED ON F-15 AND C-130 AIRCRAFT AND A/M 32A-60A. DIMENSIONS: 22 1/2 x 19 1/2 X 10 1/2 INCHES. APPROXIMATE WEIGHT 50 LBS. FUNCTION: The analyzer is a lightweight, portable testing unit which incorporates an electrical system with associated meters and indicators, and a hydraulic and pneumatic syThe analyzer is a lightweight, portable testing unit which incorporates an electrical system with associated meters and indicators, and a hydraulic and pneumatic system with associated gages and controls for checking and controlling performance of gas turbine engines and their components. The analyzer may be used for measurement of turbine unit speeds, temperatures, pressures, output frequencies, and electrical circuit parameters. The analyzer may also be used for monitoring the turbine unit during operation, for functional check of turbine unit performance, for static check of turbine unit components, and for control of turbine unit during motoring.stem with associated gages and controls for checking and controlling performance of gas turbine engines and their components. The analyzer may be used for measurement of turbine unit speeds, temperatures, pressures, output frequencies, and electrical circuit parameters. The analyzer may also be used for monitoring the turbine unit during operation, for functional check of turbine unit performance, for static check of turbine unit components, and for control of turbine unit during motoring. QUANTITY: 5 EACH IN BASIC YEAR. FOUR ADDITIONAL OPTIONS FOR QUANTITY RANGE OF 1-5 EACH. DELIVERY OF BASIC YEAR IS 220 DAYS ARO; OPTION DELIVERY IS 220 DAYS AFTER EXERCISE OF OPTION. DELIVERY POINT FOR BASIC QUANTITY IS FE6122, FE6231, FE6421, FE6525. DESTINATION UNKNOWN FOR OPTION REQUIREMENTS - COULD BE USAF OR FMS LOCATIONS. DUE TO A LACK OF TECHNICAL DATA FOR THIS ITEM, THIS REQUIREMENT IS BEING SOLICITED ON A LIMITED BASIS TO HONEYWELL INTERNATIONAL AND SERVICE AND SALES, A HONEYWELL LICENSEE. ALL RESPONSIBLE SOURCES MAY SUBMIT A CAPABILITY STATEMENT, PROPOSAL OR QUOTATION WHICH SHALL BE CONSIDERED BY THE AGENCY. THE RFP WILL NOT BE POSTED AT FBO. HOWEVER, SHOULD YOU DESIRE TO RECEIVE A COPY, NOTICE THE POC LISTED BELOW AND ONE WILL BE PROVIDED UPON RELEASE. NOTES 22, 26 APPLY.
- Web Link
-
FBO.gov Permalink
(https://www.fbo.gov/spg/USAF/AFMC/WRALC/FA8532-10-R-22615/listing.html)
- Record
- SN02152236-W 20100520/100518234558-27d9b22c608bd2560f60498c5973525e (fbodaily.com)
- Source
-
FedBizOpps Link to This Notice
(may not be valid after Archive Date)
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