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 5925-00-826-6901
NSN 5965-01-406-6320
NSN 5915-01-133-3683
NSN 6145-00-526-2878
NSN 6240-01-504-2675
NSN 5910-01-442-5697
NSN 6110-01-227-0432
NSN 6150-01-427-3764
NSN 6110-01-541-2639
NSN 5996-01-530-0823
NSN 5999-01-118-6871
NSN 6620-00-708-1417