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 5990-01-449-7090
NSN 5996-01-274-3980
NSN 5975-01-389-6324
NSN 5895-01-203-2782
NSN 5990-01-239-1474
NSN 5965-00-110-3330
NSN 6320-01-570-8814
NSN 6620-01-391-9829
NSN 6240-01-593-2170
NSN 5935-01-445-5917
NSN 5915-01-523-6727
NSN 6650-01-308-9394