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 5935-01-560-4598
NSN 5930-01-353-5603
NSN 5950-01-433-0313
NSN 6145-01-199-9554
NSN 5996-01-074-8161
NSN 5895-01-192-3138
NSN 5910-00-409-4384
NSN 6150-01-097-3126
NSN 4140-01-193-1814
NSN 6130-00-275-5929
NSN 5910-00-479-8315
NSN 6645-01-292-5215