Surface treat, ams 2416 chromate, modified per pwa-s-2416, 15.199-15.201in. Id., 5th 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 6620-00-793-7733
NSN 6110-00-963-4035
NSN 6320-01-612-7035
NSN 2925-01-651-8683
NSN 5920-01-167-0810
NSN 5990-00-902-5268
NSN 5855-00-337-3679
NSN 5930-01-599-1258
NSN 5990-01-191-1772
NSN 6150-01-634-0575
NSN 5975-01-031-1303
NSN 5990-01-432-4249