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 5905-01-441-2322
NSN 6110-00-902-1702
NSN 5855-01-295-2313
NSN 5915-01-605-3326
NSN 5999-00-850-7607
NSN 5930-00-060-2147
NSN 5905-00-968-8046
NSN 6110-01-211-4714
NSN 6650-01-106-8601
NSN 6650-01-305-8881
NSN 7035-01-263-5463
NSN 5910-01-399-0255