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 5920-00-021-3697
NSN 6320-00-546-9249
NSN 6150-01-364-1537
NSN 5998-01-633-7525
NSN 5965-01-424-0542
NSN 5996-01-391-7489
NSN 5930-00-258-9997
NSN 5855-01-253-6076
NSN 6610-00-477-4349
NSN 6220-01-055-7423
NSN 5930-00-778-2145
NSN 6150-00-484-1112