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 5945-00-983-4374
NSN 5945-01-077-5736
NSN 6645-00-960-6594
NSN 6685-01-019-4493
NSN 5998-01-433-2308
NSN 6650-01-576-6512
NSN 6685-01-175-5844
NSN 5999-01-338-5491
NSN 6150-01-233-0966
NSN 7035-01-530-6707
NSN 6650-00-339-5458
NSN 6150-01-234-6749