2995-12-390-4108

Gas Turbine Engine Starter

2995123904108 123904108 MSU 200

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

2995-12-390-4108 STARTER,ENGINE,GAS TURBINE 2995123904108 123904108

Managed by Germany
NSN Created on 9 Nov 2012
Data Last Changed
January 2023
NATO Update Count
1
NATO Data Quality
2995-12-390-4108 STARTER,ENGINE,GAS TURBINE 2995123904108 123904108 1/1
NSN 2995-12-390-4108 (Generic Image) 1/1

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2995-12-390-4108 Related Documents Related Documents 2995-12-390-4108 5+ Documents (More...)

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Gas Turbine Engine Starter 2995123904108 4108 DEMIL: | DEMILI : | CRITICALITY : | HMIC : https/
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2990994380013 NE Related Documents 2990-99-438-0013 Gas Turbine Engine Starter 2990994380013 2995-12-390-4108
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Starter 2995123904108 item designed to accelerate a gas turbine engine Day 2995-12-390-4108 RQST NE

2995-12-390-4108 Demil Restrictions 2995-12-390-4108

DEMIL: | DEMILI: | CRITICALITY: | HMIC: | PMIC: | EDC: | ADPEC:

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