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 5895-01-141-9544
NSN 7035-01-386-3004
NSN 5985-01-567-1066
NSN 7035-01-492-6799
NSN 5835-01-059-1550
NSN 5999-00-013-5116
NSN 5965-00-246-5612
NSN 5950-01-431-7311
NSN 6685-01-357-3825
NSN 5985-00-361-8863
NSN 7035-01-629-4362
NSN 5998-00-814-5272