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FBO DAILY ISSUE OF MAY 20, 2010 FBO #3099
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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