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 5905-01-419-5798
NSN 6130-01-579-4861
NSN 5895-01-562-2965
NSN 5985-01-521-3617
NSN 5999-01-093-6209
NSN 5999-00-303-4624
NSN 5945-01-190-1295
NSN 6645-00-269-2764
NSN 6645-00-137-5682
NSN 5930-01-398-9576
NSN 5945-00-161-5109
NSN 5996-01-338-2998