2995-14-412-2408
Gas Turbine Engine Starter
2995144122408 144122408 002-02-07 613-989-281-0
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. View more Gas Turbine Engine Starter
Managed by France
NSN Created on 8 Oct 1986
Data Last Changed
January 2023
January 2023
NATO Update Count
1
1
NATO Data Quality

Marketplace 2995-14-412-2408
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Related Documents 2995-14-412-2408 1+ Documents (More...)
002-02-07 613-989-281-0 An item designed to accelerate a gas turbine engine from rest to starter cutoff
RQST NE Updated Every Day 2995-14-412-2408 RQST Updated Every Day 2995-14-412-2408 RQST NE Related Documents
2995-14-412-2408 1+ Documents ( More... ) https//www.nsnlookup.com /fsg-29/fsc-2995/fr 2995-14-412-2408
RQST NE Updated Every Day 2995-14-412-2408 RQST Updated Every Day 2995-14-412-2408 RQST NE Related Documents
2995-14-412-2408 1+ Documents ( More... ) https//www.nsnlookup.com /fsg-29/fsc-2995/fr 2995-14-412-2408
Restrictions 2995-14-412-2408
End Users 2995-14-412-2408
- Brazil (YA)
- France (ZF)
Approved Sources 2995-14-412-2408
- Part Number
- Manufacturer
- Status
- 002-02-07
- Manufacturer
- F1989 - Safran Power Units (Active)
- Primary Buy
- Primary Buy
- 613-989-281-0
- F0301 - Safran Aircraft Engines (Active)
- Secondary Buy
- Secondary Buy
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