Surface treat, ams 2416, chromate, modified per pwa-s-2416; 15.199-15.201 in. Id., 6th 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 6620-01-168-8450
NSN 5975-01-386-2281
NSN 5950-01-305-4612
NSN 6645-01-643-2558
NSN 5920-00-314-6870
NSN 5985-01-585-6857
NSN 7035-01-146-7096
NSN 5998-01-044-5816
NSN 5835-01-495-0595
NSN 6620-01-253-0374
NSN 6135-00-284-1406
NSN 6130-00-155-2490