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 6135-00-900-2139
NSN 5920-01-303-6841
NSN 5930-00-830-4431
NSN 5990-01-143-2518
NSN 5895-01-451-0743
NSN 5945-01-659-4448
NSN 6145-00-177-4731
NSN 6650-01-005-8570
NSN 6610-01-107-2658
NSN 6145-00-905-6797
NSN 6105-01-476-5374
NSN 5925-01-190-9102