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 6145-01-449-3611
NSN 6320-01-511-1526
NSN 6110-01-319-5570
NSN 5975-01-409-2948
NSN 6610-01-172-4041
NSN 5996-01-006-2324
NSN 5835-00-918-8169
NSN 5945-01-244-9355
NSN 5990-01-341-5735
NSN 6620-01-037-4631
NSN 5835-01-462-5983
NSN 5945-01-502-6921