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 5895-01-440-1308
NSN 5895-00-030-9778
NSN 5920-00-427-7267
NSN 5835-01-519-3834
NSN 6130-00-174-4652
NSN 5975-00-619-8159
NSN 5905-01-250-1484
NSN 6110-01-344-5852
NSN 6110-00-926-0781
NSN 6220-01-603-7605
NSN 5950-01-215-1177
NSN 5905-01-238-9039