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 5895-01-246-3665
NSN 5965-01-538-8795
NSN 6145-00-351-4539
NSN 5935-01-228-5248
NSN 5950-01-467-9998
NSN 5835-01-261-2978
NSN 5835-01-307-8954
NSN 2925-00-497-7808
NSN 2925-00-824-2186
NSN 5965-01-598-6114
NSN 6150-00-114-2785
NSN 5835-01-424-0054