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 5965-00-244-4324
NSN 5965-01-650-1764
NSN 5998-01-218-5733
NSN 6610-01-238-8712
NSN 5960-00-003-7982
NSN 7035-01-362-4924
NSN 5915-01-496-2314
NSN 5855-01-363-1143
NSN 4140-00-928-9097
NSN 2925-01-548-6674
NSN 5930-01-585-3615
NSN 5905-01-373-8268