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 5960-00-151-7576
NSN 5905-00-219-2969
NSN 5945-00-735-0827
NSN 5996-01-600-0348
NSN 6220-01-382-7997
NSN 5999-01-569-1651
NSN 2925-01-510-9378
NSN 5915-01-609-2686
NSN 5910-01-406-3880
NSN 6645-01-626-0411
NSN 5935-00-229-5656
NSN 6110-01-440-5000