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 6220-01-423-2814
NSN 5996-01-281-7336
NSN 6135-01-579-3534
NSN 5985-01-420-6536
NSN 5920-01-439-2118
NSN 5975-01-219-4496
NSN 5945-01-153-7280
NSN 5975-01-495-0991
NSN 6130-00-454-8342
NSN 6150-01-565-2114
NSN 5945-00-659-1658
NSN 5930-01-449-1915