3505468-6

35054686 Engine Gas Turbine Starter

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Datasheet. 3505468-6 specification

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

Answers.

What is the NSN for 3505468-6?

2995-01-578-5464

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 3505468-6?

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 2995-01-578-5464 STARTER,ENGINE,GAS TURBINE

starter

NIIN
015785464
NIIN Date
10/09/09
Schedule B
8411997050 
Name Code
21907
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

Other Part Numbers Parts with same form, fit, and function by other manufacturers

1. 3505468-5 Cage 59364
2. 3505468-5 Cage 59364

Major End Users Countries and entities

  • - Australia 

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Similar by Design Other starters with similar characteristics

Nothing similar to this part number was found in our inventory

3505468-6 / 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.