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 5960-00-101-5461
NSN 6145-01-435-6458
NSN 5975-00-278-7437
NSN 5930-01-119-4205
NSN 6220-01-017-2734
NSN 6145-01-181-6198
NSN 5998-00-661-0380
NSN 6110-01-599-7300
NSN 4140-00-477-1863
NSN 5960-01-308-6421
NSN 5910-00-475-2402
NSN 5960-00-686-0559