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 6135-01-449-2144
NSN 5996-01-457-2001
NSN 5999-01-504-8201
NSN 5999-01-256-3468
NSN 6650-01-118-3222
NSN 6130-01-225-3166
NSN 5999-00-513-7763
NSN 6685-01-223-3940
NSN 6220-01-168-7773
NSN 6220-01-454-0815
NSN 5999-01-123-7941
NSN 7035-00-252-7467