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 6650-01-467-2355
NSN 5945-01-262-0885
NSN 6620-01-577-6285
NSN 5835-00-770-2843
NSN 7035-00-104-7613
NSN 6145-00-244-8152
NSN 6320-01-339-9974
NSN 6135-01-280-2883
NSN 6220-01-068-4066
NSN 6685-01-158-5454
NSN 6685-01-551-1293
NSN 6620-00-873-9825