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 5930-00-274-7167
NSN 6145-01-339-5112
NSN 4140-01-231-8578
NSN 5920-01-521-9550
NSN 5950-00-244-8332
NSN 6240-01-040-1321
NSN 5905-01-147-5126
NSN 5965-00-137-9291
NSN 5998-01-445-6345
NSN 6645-01-314-6716
NSN 6240-00-607-4303
NSN 6610-01-255-4544