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 2925-01-065-0060
NSN 5960-01-066-4771
NSN 5835-00-936-8753
NSN 5920-01-142-3984
NSN 7035-00-436-1229
NSN 2925-01-307-2637
NSN 5960-00-584-4553
NSN 5945-01-118-2681
NSN 5975-01-069-2196
NSN 6610-01-409-1781
NSN 4140-01-370-1309
NSN 5945-00-186-5069