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.
Classification: Parts of gas turbine aircraft engines, other than for use in civil aircraft
NSN 5999-00-338-9365
NSN 6105-00-822-5165
NSN 5895-01-442-9314
NSN 5996-01-619-4966
NSN 6130-00-439-6344
NSN 5990-01-170-6081
NSN 5999-01-498-4543
NSN 5895-00-385-9003
NSN 5985-01-415-7999
NSN 6220-01-484-0365
NSN 5855-01-288-6341
NSN 6650-01-350-0067