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 5950-00-133-8953
NSN 6150-01-372-6824
NSN 5990-01-615-7823
NSN 7035-00-320-5644
NSN 5965-00-858-5398
NSN 5935-01-218-5653
NSN 5910-00-241-2754
NSN 5935-01-270-5188
NSN 5910-00-811-3477
NSN 5965-01-573-6387
NSN 6130-00-081-2186
NSN 6610-01-365-0971