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 7035-01-348-5153
NSN 5895-01-462-2038
NSN 6130-01-510-2934
NSN 5975-01-360-0688
NSN 5975-00-882-9780
NSN 5835-01-455-3380
NSN 5895-01-170-8310
NSN 5996-00-556-7708
NSN 6150-01-463-9083
NSN 5998-01-538-0032
NSN 5910-01-401-5279
NSN 5999-00-518-4503