Surface treat, ams 2416 chromate, modified per pwa-s-2416, 15.199-15.201in. Id., 5th 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 6105-00-190-0224
NSN 5895-01-398-9088
NSN 6150-01-044-3909
NSN 5835-00-642-8148
NSN 5935-01-441-8225
NSN 6610-01-341-4014
NSN 6130-01-588-7145
NSN 5915-01-480-5787
NSN 5835-01-572-6900
NSN 6320-01-522-0318
NSN 6130-00-917-1364
NSN 5998-01-005-3655