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
Managed by France
NSN Created on 22 Nov 1990
Data Last Changed
January 2023
January 2023
NATO Update Count
1
1
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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.
Restrictions 2995-14-443-4215
End Users 2995-14-443-4215
- Brazil (YA)
- France (ZF)
Approved Sources 2995-14-443-4215
- Part Number
- Manufacturer
- Status
- 002-02-09
- Manufacturer
- F1989 - Safran Power Units (Active)
- Primary Buy
- Primary Buy
NATO Stock Numbers Related to 2995-14-443-4215
2995-14-445-8667 2995-12-390-4108 2990-99-438-0013 2995-21-896-1656 2990-99-524-2408 2995-14-314-6101 2995-01-578-5464 2990-00-929-8734 2995-01-380-2232 2995-00-065-2932 2915-99-984-7288 2995-33-210-2395 2995-14-573-6306 2995-14-351-3373 2995-99-733-5570 2995-14-510-4243 2995-00-113-4562 2990-01-469-7282