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 5996-01-581-0018
NSN 6240-00-204-9355
NSN 5945-01-608-5558
NSN 6150-01-414-4948
NSN 6135-01-599-4006
NSN 5910-01-391-5009
NSN 5999-01-328-7350
NSN 5996-01-145-4900
NSN 6610-01-269-5437
NSN 5930-00-076-2629
NSN 5998-01-415-8990
NSN 5835-01-495-0595