SOLICITATION NOTICE
29 -- MDEC P/N2123M24P04 End Item F110
- Notice Date
- 1/14/2010
- Notice Type
- Presolicitation
- NAICS
- 336412
— Aircraft Engine and Engine Parts Manufacturing
- Contracting Office
- DEFENSE LOGISTICS AGENCY; DLR PROCUREMENT OPS DSCR-ZBA;3001 STAFF DRIVE; TINKER AFB; OK; 73145
- ZIP Code
- 73145
- Solicitation Number
- SPRTA1-10-R-0269
- Response Due
- 3/1/2010
- Point of Contact
- Thomas Kanaly, Phone 405-734-8112, Fax 405-734-8106, Email thomas.kanaly@tinker.af.mil - Donna M Lovell, Phone 405-734-8105, Fax 405-734-8106, Email donna.lovell@dla.mil
- E-Mail Address
-
Thomas Kanaly
(thomas.kanaly@tinker.af.mil)
- Small Business Set-Aside
- N/A
- Description
- PR Number(s): FD20301070039, FD20301070106Item: 0001NSN: 2995015404818PRPR MDECP/N: 2123M24P04, Description: DIM: 16"L; 13"W; 6.5"H; 35LB WT; MATERIAL: HOUSING IS DIP-BRAZED ALUMINUM; FUNCTION: CONTROLS ALL VARIABLE ENGINE PARAMETERS Item description is a Turbine Engine Supervisory Control Unit; (MDEC). Item function is as follows:The DEC directs engine manipulated variables; acquires and monitors engine parameters, executes system fault detection and isolation. It also communicates with the airframe and ground support equipment, and executes other functions as provided by the resident application software. The DEC interfaces with components of main engine control subsystem, augmenter control subsystem, engine monitoring system (EMS), and aircraft. The following functions are performed by the DEC: 1 Limits maximum fan speed (NF) in primary and secondary mode. 2 Provides maximum core speed limit, accel and decel schedules, full fan speed control, HPT blade temperature (T4B) limit, and minimum and maximum CDP (PS3C) limit control. 3 Includes logic necessary to automatically switch to a hybrid or secondary control mode by sensing a failure in the primary control system. 4 Limits minimum core speed. 5 Controls fan IGV position. 6 Controls core VSV position. 7 Controls augmenter fuel ratio units (WFR/PS3). 8 Provides a self check and logic to indicate a failure of the electrical control. 9 Schedules nozzle area roof and floor. 10 Controls fan discharge pressure ratio (Delta P/P). 11 Coordinates exhaust nozzle and augmenter fuel flow transients. 12 Provides the logic necessary to automatically control high energy main and augmenter ignition. Provides logic which develops and sequences signals to provide transition between nonaugmented and augmented operation regimes. 13 Provides signals to the EMSC that are required for engine and control system fault isolation. 14 Provides electrical excitation for linear and rotary variable differential transducers (LVDT and RVDT) and also the T2 sensor, flame sensor, and T4B pyrometer. Quantity: 285.0000 EA Destn: FB2039,Tinker AFB,OK.,73145-9013. Delivery: 31 JAN 2012, 20.00 Per month PR Number(s): FD20301070039, FD20301070106Item: 0002CEMS TRACKING DATA Description: Quantity: 1.0000 LO Destn: DD1423,,., -. Delivery: TBC, 1.00 LO Duration of Contract Period: Unk Electronic procedure will be used for this solicitation. IAW FAR 5.207(c)(12)(ii) - Trade Agreements - One or more of the items under this acquisition is subject to the World Trade Organization Government Procurement Agreement and Free Trade Agreement. IAW FAR 5.207(c)(15)(ii), All responsible sources may submit a capability statement, proposal, or quotation, which shall be considered by the agency
- Web Link
-
FBO.gov Permalink
(https://www.fbo.gov/spg/USAF/AFMC/OCALCCC/SPRTA1-10-R-0269/listing.html)
- Record
- SN02042126-W 20100116/100114234144-356740c7bc8abff970261ab0fc267239 (fbodaily.com)
- Source
-
FedBizOpps Link to This Notice
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