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 5920-01-127-0252
NSN 5999-00-293-1718
NSN 5895-01-069-1345
NSN 6685-01-199-9943
NSN 5945-00-540-8178
NSN 7035-01-346-8800
NSN 5905-00-823-9533
NSN 5910-01-382-4889
NSN 6145-00-528-6467
NSN 6110-00-371-2458
NSN 5925-00-290-4451
NSN 6110-00-438-6686