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 5905-01-648-2685
NSN 5960-01-323-6432
NSN 6685-01-076-4703
NSN 5835-00-911-6330
NSN 5910-01-036-3976
NSN 5960-00-266-6741
NSN 5930-00-215-4851
NSN 6685-01-634-0611
NSN 5915-01-186-2401
NSN 5895-01-123-8694
NSN 6620-01-451-3742
NSN 6685-00-141-4300