ESC103-04E4

ESC10304E4 Supervisory Turbine Control Unit

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Datasheet. ESC103-04E4 specification

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

B757 aircraft

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.

CONTROL-Engine

Supplementary Features
Characteristics or qualities of an item,not covered in any other requirement,which are considered essential information for one or more functions excluding nsn assignment.

parts catalog, maintenance 73-21-10-03

Answers.

What is the NSN for ESC103-04E4?

2995-01-516-0594

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 ESC103-04E4?

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 2995-01-516-0594 CONTROL UNIT,SUPERVISORY,TURBINE

Used on b757 aircraft. control-engine

NIIN
015160594
NIIN Date
12/17/03
Schedule B
8411997050 
Name Code
47093
FIIG
A23900
DEMIL / ITAR
USML/ITAR controlled item (Code: Q)
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

  • - New Zealand 

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Similar by Design Other control units with similar characteristics

Nothing similar to this part number was found in our inventory

ESC103-04E4 / 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.