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 5975-00-854-6519
NSN 5999-01-347-5875
NSN 5998-00-022-2146
NSN 5895-01-080-1657
NSN 5998-01-359-9680
NSN 6105-01-106-2558
NSN 2925-01-125-9169
NSN 6645-01-172-6838
NSN 5990-00-932-3070
NSN 5895-01-530-4998
NSN 5925-00-417-3256
NSN 7035-01-385-3628