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 5835-01-399-5820
NSN 6650-01-192-9075
NSN 6685-01-145-7850
NSN 6105-01-536-4066
NSN 6145-01-043-1530
NSN 5855-01-328-3570
NSN 5975-01-536-5093
NSN 5935-01-633-6794
NSN 5975-01-278-2206
NSN 5999-01-583-9348
NSN 5835-00-711-3371
NSN 5925-01-611-5036