2118780-8

21187808 Supervisory Turbine Control Unit
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Datasheet. 2118780-8 specification

Overall Length
The dimension measured along the longitudinal axis with terminated points at the extreme ends of the item.

12.210in. ⁓12-7/32"

Overall Width
An overall measurement taken at right angles to the length of an item,in distinction from thickness.

11.890in.

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

pacer dawn

Answers.

What is the overall width?

11.890 inches

What is the NSN for 2118780-8?

2995-01-414-6257

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 2118780-8?

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 2995-01-414-6257 CONTROL UNIT,SUPERVISORY,TURBINE

Used on pacer dawn. 11.890" overall width 12.210" overall length

NIIN
014146257
NIIN Date
06/09/95
Schedule B
8411997050 
Name Code
47093
FIIG
A23900
DEMIL / ITAR
Uncontrolled item (Code A)
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

Major End Users Countries and entities

  • - Taiwan, Province of China 

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Similar by Design Other control units with similar characteristics

Nothing similar to this part number was found in our inventory

2118780-8 / 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.