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 5905-00-033-3573
NSN 5950-01-559-0264
NSN 5999-01-423-7426
NSN 5990-01-492-6575
NSN 5990-01-514-8708
NSN 5910-01-579-8118
NSN 6105-01-448-7843
NSN 5945-00-189-0763
NSN 5925-01-634-0664
NSN 6620-01-576-7723
NSN 5855-01-627-7577
NSN 5905-01-120-9046