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 6645-01-391-9477
NSN 5910-01-134-4251
NSN 5998-01-226-0766
NSN 6130-00-407-8109
NSN 6110-00-945-8944
NSN 6645-00-155-2398
NSN 6685-01-117-5846
NSN 6320-01-616-0843
NSN 5960-01-521-6865
NSN 6145-00-565-6828
NSN 6145-01-368-7358
NSN 5930-01-440-6647