Surface treatment, ams2416 chromate modified per pwa-s-2416; 15.199-15.201 in. Id., 3rd 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 4140-00-442-6373
NSN 6135-01-459-0089
NSN 5915-00-597-2369
NSN 4140-01-299-6713
NSN 5945-00-481-8837
NSN 6130-00-811-3799
NSN 6650-01-593-5993
NSN 5920-00-103-7642
NSN 5930-01-254-3475
NSN 6240-01-082-3387
NSN 6650-00-405-0702
NSN 5925-01-401-5314