Surface treatment ams 2416, chromate, modified per pwa-s-2416; 15.199-15.201 in. Id., 8th 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 5905-00-660-9962
NSN 5895-01-628-8747
NSN 5920-01-224-7028
NSN 6130-00-504-0133
NSN 5998-01-188-8751
NSN 5835-01-629-2044
NSN 5935-01-487-3783
NSN 5998-00-163-6190
NSN 6610-01-107-2658
NSN 5910-01-560-6939
NSN 5965-01-293-0121
NSN 5996-01-127-5431