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 5935-00-087-4289
NSN 5925-01-351-5541
NSN 2925-00-305-8030
NSN 6320-00-116-3658
NSN 4140-00-189-0235
NSN 5925-00-758-6227
NSN 6650-01-344-1965
NSN 5910-00-232-5028
NSN 5935-01-571-4486
NSN 6150-01-204-2237
NSN 5910-00-126-3838
NSN 6645-01-413-0515