5923385-102

5923385102 Engine Gas Turbine Starter

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Datasheet. 5923385-102 specification

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

f/A-22 raptor

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.

starter

Special Features
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.

F119

Answers.

What quantity is this sold in?

1EA

What is the NSN for 5923385-102?

2995-01-490-6993

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 5923385-102?

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 2995-01-490-6993 STARTER,ENGINE,GAS TURBINE

Used on f/a-22 raptor. F119 starter

NIIN
014906993
NIIN Date
10/04/01
Schedule B
8411997050 
Name Code
21907
FIIG
A23900
QUP
Historical Price
$2,207.48 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

Major End Users Countries and entities

  • - Department of The Air Force 

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Similar by Design Other starters with similar characteristics

Nothing similar to this part number was found in our inventory

5923385-102 / Starter,engine,gas turbineWhat is the formal definition of this item?

An item designed to accelerate a gas turbine engine from rest to starter cutoff speed by means of a combustion gas driven turbine and reduction gear assembly constructed to be mounted on the engine starter drive. the combustion gas is generated from ignited liquid fuel and air in the combustion chamber or from a solid propellant cartridge attached to the combustion chamber of the starter. may have provision for energizing the turbine by low pressure air from engine bleed or ground equipment air supply.