T.O. 2j-tf39-4; goes on the fan stator assembly
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 5975-01-066-6171
NSN 5960-00-457-5560
NSN 6145-01-546-1100
NSN 5998-00-395-2692
NSN 6320-01-285-1922
NSN 6650-00-479-2089
NSN 6220-00-885-8197
NSN 5998-00-296-3570
NSN 6610-01-338-0628
NSN 5996-00-406-4951
NSN 5920-00-120-9347
NSN 5990-01-411-5930