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 6145-01-068-4668
NSN 5999-01-593-8130
NSN 6220-00-379-4044
NSN 5950-01-113-4903
NSN 5990-01-310-0738
NSN 6220-01-265-2705
NSN 6645-01-367-2581
NSN 5965-01-378-7335
NSN 5895-00-865-7634
NSN 6645-01-074-4063
NSN 2925-01-196-6187
NSN 5975-00-189-0857