4110T55P38

4110T55P38 Supervisory Turbine Control Unit
Home » Catalog » Engine Components (p. 26) » Supervisory Turbine Control Units (p. 1) » Part Number 4110T55P38

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Datasheet. 4110T55P38 specification

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

ct 7 turboshaft engine

Part Name Assigned By Controlling Agency
The name assigned to the item by the government agency or commercial organization controlling the design of the item.

electronic engine control

Answers.

What is the NSN for 4110T55P38?

2995-01-584-8420

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 4110T55P38?

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 2995-01-584-8420 CONTROL UNIT,SUPERVISORY,TURBINE

Used on ct 7 turboshaft engine. electronic engine control

NIIN
015848420
NIIN Date
05/07/10
Schedule B
8411997050 
Name Code
47093
FIIG
A23900
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

Major End Users Countries and entities

  • - Republic of Korea 

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Similar by Design Other control units with similar characteristics

Nothing similar to this part number was found in our inventory

4110T55P38 / 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.