For stage 5
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 5855-01-660-5088
NSN 4140-01-097-6691
NSN 6135-01-581-8163
NSN 5960-00-678-9851
NSN 5925-01-238-8563
NSN 5895-01-571-1014
NSN 5990-00-860-9207
NSN 5965-00-289-6280
NSN 6105-01-571-4867
NSN 5910-01-103-6697
NSN 5935-01-481-1957
NSN 5920-00-655-4251