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 6150-01-400-4211
NSN 5998-01-200-7207
NSN 5910-01-438-6748
NSN 5855-01-271-6617
NSN 5905-01-413-8074
NSN 6650-01-333-7546
NSN 6150-01-463-2577
NSN 6110-01-386-1536
NSN 5925-01-607-3296
NSN 6105-00-384-1693
NSN 5835-01-081-9345
NSN 5925-01-160-9069