Surface treat, ams2416 chromate, modified per pwa-s-2416; 15.199-15.201 in. Id., 4th 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 5996-01-513-9511
NSN 6610-00-841-8221
NSN 6150-01-344-7635
NSN 6150-00-027-9279
NSN 6110-01-101-6722
NSN 6105-01-445-5247
NSN 2925-00-373-8837
NSN 5998-00-258-4992
NSN 5999-00-212-7853
NSN 5920-00-261-9848
NSN 6685-00-800-6456
NSN 6645-01-653-2848