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 5920-01-297-5895
NSN 6150-01-232-6380
NSN 5855-01-010-4921
NSN 5965-01-375-5238
NSN 5996-01-285-0002
NSN 6240-00-170-5302
NSN 5996-01-303-6882
NSN 6240-00-573-7514
NSN 5895-01-103-1982
NSN 5855-01-006-1827
NSN 5895-01-184-9515
NSN 6320-00-779-5923