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 6650-01-364-1313
NSN 6320-00-228-5678
NSN 6105-01-526-4660
NSN 7035-00-870-0290
NSN 6320-00-701-0437
NSN 6105-01-023-4108
NSN 5998-01-647-0669
NSN 6610-01-568-7611
NSN 6220-01-553-0368
NSN 5935-00-285-2767
NSN 7035-01-633-9537
NSN 6650-01-040-6971