Surface treatment, ams2416 chromate modified per pwa-s-2416; 15.199-15.201 in. Id., 3rd 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 5975-00-907-7487
NSN 6240-00-419-3196
NSN 5960-00-761-3833
NSN 4140-01-561-2766
NSN 5835-01-116-2369
NSN 5925-01-364-0771
NSN 5935-00-007-9747
NSN 6145-00-952-9290
NSN 6610-01-236-8359
NSN 5960-01-254-3541
NSN 6650-00-059-6268
NSN 6130-01-425-0235