T.O. 2j-tf39-4
A stationary arched metal segment used to establish clearance and a seal for the tip of a blade, turbine rotor, aircraft gas turbine engine. The inner dimension may have open honeycomb or composition filled surface or may be formed by the knife edge metal protrusions of a seal ring, labyrinth, aircraft gas turbine engine.
Classification: Parts of gas turbine aircraft engines, other than for use in civil aircraft
NSN 5920-00-127-9992
NSN 6685-01-032-5591
NSN 5935-01-300-8248
NSN 5910-01-433-0142
NSN 5915-01-363-9524
NSN 5998-01-392-0880
NSN 6610-00-511-3328
NSN 5910-01-633-9963
NSN 2925-00-373-8837
NSN 7035-01-549-6765
NSN 6135-01-627-3786
NSN 5935-00-101-5866