An item designed to accelerate a gas turbine engine from rest to starting speed by means of gas generated by combustion of fuel and air in a combustion chamber, and thrust directly on the engine turbine through an impingement nozzle mounted in the turbine section. Consists of a combustion chamber, air and fuel system components and igniter. May include the starter tube and/or impingement nozzle.
NSN 6130-00-403-8232
NSN 5996-01-183-1695
NSN 5998-01-605-1712
NSN 6610-01-284-6968
NSN 5996-00-877-3278
NSN 6620-00-153-0982
NSN 6110-00-805-6320
NSN 6620-01-034-4539
NSN 5990-00-879-5000
NSN 5999-01-650-1850
NSN 5835-01-495-0595
NSN 2925-01-554-5246