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 5998-01-236-5498
NSN 5960-00-726-0580
NSN 6240-01-530-7241
NSN 6220-01-510-3927
NSN 6150-00-503-9234
NSN 6105-00-904-5289
NSN 5915-01-012-2964
NSN 6135-01-348-8264
NSN 6110-00-494-3056
NSN 5999-00-456-4819
NSN 5990-00-883-6364
NSN 5990-01-303-6110