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 5990-01-514-8708
NSN 6135-01-600-8345
NSN 5999-01-542-1837
NSN 5996-00-965-5261
NSN 5945-01-068-9973
NSN 5950-01-592-3145
NSN 5960-00-888-7218
NSN 4140-01-607-2975
NSN 5975-00-016-9774
NSN 6130-01-567-6485
NSN 6685-01-475-8409
NSN 7035-00-300-3208