Surface treatment ams 2416, chromate, modified per pwa-s-2416; 15.199-15.201 in. Id., 8th 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 5999-01-533-3938
NSN 5895-01-296-9922
NSN 6620-01-234-1799
NSN 6685-01-145-3938
NSN 5935-01-417-2074
NSN 6220-01-460-0180
NSN 5915-01-152-5394
NSN 4140-00-306-0886
NSN 5855-01-007-9541
NSN 5935-00-789-6179
NSN 6645-00-879-9941
NSN 6150-01-426-8986