Surface treat, ams2416 chromate, modified per pwa-s-2416; 15.199-15.201 in. Id., 4th stage
A rigid item designed to maintain a predetermined space between two rotor, compressor, aircraft gas turbine engine. It may be a complete 360 degrees or a section thereof.
Classification: Parts of gas turbine aircraft engines, other than for use in civil aircraft
NSN 5999-00-735-9865
NSN 5925-01-139-0882
NSN 6130-01-027-2839
NSN 5915-01-163-9253
NSN 5925-00-364-7969
NSN 5920-01-092-9252
NSN 6620-01-228-1571
NSN 6650-00-769-3003
NSN 6320-01-246-4390
NSN 6650-00-587-6917
NSN 6650-01-434-6434
NSN 6240-01-353-7760