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 6685-00-445-7725
NSN 7035-01-459-8268
NSN 5998-01-229-1350
NSN 5965-01-534-9961
NSN 5910-01-363-6124
NSN 5965-00-246-5612
NSN 6650-01-455-1805
NSN 5835-01-416-6455
NSN 6685-00-437-5229
NSN 5915-01-212-9590
NSN 6610-00-003-3958
NSN 5835-01-041-6879