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 5930-01-339-7836
NSN 5920-01-243-4377
NSN 5910-01-574-9765
NSN 5910-00-879-6088
NSN 5975-00-357-6136
NSN 4140-00-111-3247
NSN 6110-01-496-5254
NSN 6145-00-170-6467
NSN 6145-01-137-4473
NSN 6320-00-360-1744
NSN 6145-00-627-9010
NSN 6620-01-456-0529