824998-7-207

8249987207 Supervisory Turbine Control Unit

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Datasheet. 824998-7-207 specification

End Item Identification
The national stock number or the identification information of the end equipment for which the item is a part.

F117-PW-100 C-17A

Answers.

What quantity is this sold in?

1EA

What is the NSN for 824998-7-207?

2995-01-572-4816

How is this classified for shipping?

Schedule B number: 8411997050
Parts of gas turbine aircraft engines, other than for use in civil aircraft

What's the federal classification of 824998-7-207?

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 2995-01-572-4816 CONTROL UNIT,SUPERVISORY,TURBINE

Used on f117-pw-100 c-17a.

NIIN
015724816
NIIN Date
03/11/09
Schedule B
8411997050 
Name Code
47093
FIIG
A23900
QUP
Historical Price
$797,185.73 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

1. 824998-5-207 Cage 73030
2. 1B8507 Cage 77445
3. 1B8510 Cage 77445

Major End Users Countries and entities

  • - Department of The Air Force  DSOR Contract contiguous united states (conus)

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Similar by Design Other control units with similar characteristics

Nothing similar to this part number was found in our inventory

824998-7-207 / 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.