2995-14-443-4215

Gas Turbine Engine Starter

2995144434215 144434215 002-02-09

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

2995-14-443-4215 STARTER,ENGINE,GAS TURBINE 2995144434215 144434215

Managed by France
NSN Created on 22 Nov 1990
Data Last Changed
January 2023
NATO Update Count
1
NATO Data Quality
2995-14-443-4215 STARTER,ENGINE,GAS TURBINE 2995144434215 144434215 1/1
NSN 2995-14-443-4215 (Generic Image) 1/1

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2995-14-443-4215 Related Documents Related Documents 2995-14-443-4215 5+ Documents (More...)

https//www.nsnlookup.com /nato/nato-stock-numbers/inc Gas Turbine Engine Starter (INC 21907) 2995-14-443-4215
2995-14-415-2519 Gas Turbine Engine Starter 007-02-12RNCC: 3 | RNVC: 2 | DAC: 4 22 Apr 1987 2995-14-443-4215
2995-14-510-4243 2995145104243 145104243 is 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.
2995-14-443-0147 2995144430147 144430147 is 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.
2995-14-375-4521 2995143754521 143754521 is a rigid item usually in the form of an arm of various shapes and cross sections, containing two or more holes so spaced that one serves as a pivot with or without hubs and must have a definite means for securing to a shaft (such as threaded hole for set-screw, keyway(s), splines, serrations or some clamping device). the other hole(s) connect(s) to connecting link, rigid; wire rope assembly, single leg; or clevis, rod end; to provide transmission of movement to other parts of the mechanism. see also bell crank. for manually operated items see lever, manual control.

2995-14-443-4215 Demil Restrictions 2995-14-443-4215

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2995-14-443-4215 is a Gas Turbine Engine Starter

2995-14-443-4215 End Users End Users 2995-14-443-4215

Brazil (YA)
France (ZF)

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