2995-14-351-3373
Gas Turbine Engine Starter
2995143513373 143513373 002-02-01 002-02-1A
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
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Managed by France
NSN Created on 10 Aug 1978
Data Last Changed
January 2023
January 2023
NATO Update Count
1
1
NATO Data Quality

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002-02-01 002-02-1A An item designed to accelerate a gas turbine engine from rest to starter cutoff
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2995009513467 380-2232 2995-00 -065-2932 2915-99-984-7288 Engine Starter 2995997335570 2995/fr 2995-14-351-3373
929-8734 2995-01-380-2232 2995-00-065-2932 2915-99-984-7288 2995-33-210-2395 2995-14-573-6306 2995-14-351-3373
Restrictions 2995-14-351-3373
End Users 2995-14-351-3373
- France (ZF)
Approved Sources 2995-14-351-3373
- Part Number
- Manufacturer
- Status
- 002-02-01
- Manufacturer
- F1989 - Safran Power Units (Active)
- Primary Buy
- Primary Buy
- 002-02-1A
- F1989 - Safran Power Units (Active)
- Secondary Buy
- Secondary Buy
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