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 6620-01-376-3744
NSN 2925-01-136-2551
NSN 5920-01-244-1669
NSN 5965-00-620-7154
NSN 7035-01-361-8821
NSN 6130-00-804-6031
NSN 7035-01-297-5877
NSN 5910-01-566-3296
NSN 2925-01-599-1901
NSN 6145-00-625-0714
NSN 6240-01-576-0884
NSN 6145-00-286-9588