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 5985-01-332-2950
NSN 5945-01-207-6564
NSN 6105-01-435-2751
NSN 5975-00-203-1265
NSN 6610-00-156-5699
NSN 5965-01-432-1943
NSN 6240-01-078-0352
NSN 5990-00-240-6454
NSN 5996-01-060-9882
NSN 6220-01-250-5190
NSN 6105-01-111-8319
NSN 5975-01-213-2866