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 5920-00-584-4592
NSN 5975-00-094-5959
NSN 5985-01-511-1236
NSN 6320-01-102-0799
NSN 5925-01-170-4132
NSN 5998-01-514-7145
NSN 5950-00-406-0510
NSN 5975-01-381-2763
NSN 6130-01-073-8860
NSN 6645-01-623-4199
NSN 7035-01-314-7559
NSN 6685-01-447-3859