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 5925-00-251-3283
NSN 5998-01-233-0719
NSN 5930-01-246-5112
NSN 6320-01-512-2031
NSN 5905-00-361-9539
NSN 2925-01-580-8072
NSN 5950-01-075-7275
NSN 6105-01-336-9316
NSN 5930-01-496-4127
NSN 5990-01-582-5238
NSN 6130-01-519-7875
NSN 6320-00-809-5744