Surface treat, ams 2416, chromate, modified per pwa-s-2416; 15.199-15.201 in. Id., 6th 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 6650-01-412-1040
NSN 5930-01-469-0263
NSN 6320-01-592-6248
NSN 5985-00-161-2723
NSN 6110-01-411-1403
NSN 6650-01-242-4857
NSN 5915-00-154-3984
NSN 6220-01-008-7401
NSN 5990-01-647-8574
NSN 5950-00-836-2343
NSN 5915-01-209-8891
NSN 5915-01-279-6813