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 5960-01-458-0774
NSN 5925-01-256-5147
NSN 7035-01-268-8042
NSN 5905-00-100-3054
NSN 6150-01-457-8970
NSN 5950-00-468-1007
NSN 4140-01-378-8390
NSN 5835-01-559-3824
NSN 6645-00-394-8924
NSN 5835-01-240-5022
NSN 6610-01-287-9814
NSN 5930-01-287-0706