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 6150-01-607-8245
NSN 5965-01-386-2988
NSN 5920-01-472-6199
NSN 5930-01-039-0496
NSN 6610-01-498-0524
NSN 4140-01-146-8274
NSN 5945-01-660-0718
NSN 6645-01-612-6885
NSN 5930-01-428-9614
NSN 6240-01-633-9357
NSN 5998-00-352-7114
NSN 5905-00-226-2123