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 5990-01-341-5735
NSN 5905-01-139-3261
NSN 6645-01-063-0714
NSN 5835-01-323-2581
NSN 5975-01-461-7852
NSN 5925-01-449-4509
NSN 5975-00-827-1107
NSN 6145-01-053-2969
NSN 6110-01-382-9698
NSN 5999-01-575-9055
NSN 5945-01-442-8081
NSN 5990-00-085-4299