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Quality Commitment
Serving our customers with quality and safety first.
- AS9120 Certified
- Audited supply chain
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- Customer service objectives
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Datasheet. 1087-1000-FA specification
Those unusual or unique characteristics or qualities of an item not covered in the other requirements and which are determined to be essential for identification.
melb test set: 1087 basic kit assembly
Answers.
Schedule B number: 8411997050
Parts of gas turbine aircraft engines, other than for use in civil aircraft
FSC 2995 ⁓ Miscellaneous engine accessories, aircraft
Note-items classified in this class must be specifically designed for use with aircraft or quided missile primemovers only.
Excluding exhaust system; (fsc 1560); jet engine hydraulic reservoirs (fsc 2840); jet engine oil tanks (fsc 2840); electrical starters (fsc 2925); cockpit mounted control quadrants (fsc 1680); aircraft engine covers (fsc 1730).
NSN 2995-01-577-9222 CONTROL UNIT,SUPERVISORY,TURBINE
melb test set: 1087 basic kit assembly
- NIIN
- 015779222
- NIIN Date
- 09/22/09
- Schedule B
- 8411997050
- Name Code
- 47093
- FIIG
- A23900
- QUP
- Historical Price
- $53,912.08 EA
- DEMIL / ITAR
- USML/ITAR controlled item (Code: B)
- Hazmat
- No hazard information available from HMIRS.
- MSDS
- N/A
- Precious Metals
- No precious metals
- Enviromental
- N/A
- Electrostatic ESD & EMI
- No ESD or EMI sensitivity
Other Part Numbers Parts with same form, fit, and function by other manufacturers
Major End Users Countries and entities
- - Department of The Army DSOR Contract contiguous united states (conus)
- - Department of The Air Force DSOR Contract contiguous united states (conus)
- - U.s. Marine Corps DSOR Contract contiguous united states (conus)
- - Department of The Navy DSOR Contract contiguous united states (conus)
- - Hq United States Special Operations Command (ussocom) DSOR Contract contiguous united states (conus)
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1087-1000-FA / Control unit,supervisory,turbineWhat is the formal definition of this item?
An electronic unit that continously monitors engine speed, temperature, and air flow and adjusts the fuel control, main, turbine engine to compensate for changes. features may include load sharing capabilities, rotor speed governing, loss-of-load protection and analog or manual backup modes. it may contain automatic start capability or self-diagnostic circuitry.
