Original name compressor, axial, turbine engine
A single or multistage item designed to receive, compress, and deliver air to the combustion area at a required pressure and velocity. it consists of a case (3) and vane assembly, compressor, aircraft gas turbine engine and a rotor, compressor, aircraft gas turbine engine.
Classification: Parts of gas turbine aircraft engines, other than for use in civil aircraft
NSN 6620-00-516-3204
NSN 6240-01-463-3132
NSN 5998-01-203-5288
NSN 5905-00-885-5850
NSN 6650-00-016-9426
NSN 5835-00-683-4612
NSN 6620-00-193-0518
NSN 5925-01-502-3074
NSN 6110-00-713-3693
NSN 5950-00-174-5467
NSN 5855-01-436-7621
NSN 6145-01-430-2784