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 5930-01-583-3275
NSN 6620-01-111-3335
NSN 6685-01-481-5725
NSN 5910-00-596-3179
NSN 5975-01-323-6361
NSN 6145-00-945-4220
NSN 5895-01-324-0864
NSN 5935-01-023-0789
NSN 6320-01-243-2276
NSN 6240-01-649-4420
NSN 5935-00-903-4955
NSN 5945-01-344-3320