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 2925-01-250-2731
NSN 6130-00-387-2051
NSN 5920-01-513-9340
NSN 5999-00-210-4205
NSN 5985-00-923-5192
NSN 5855-00-631-4565
NSN 6130-00-528-7838
NSN 5835-00-876-4544
NSN 6620-00-816-9755
NSN 4140-00-898-7045
NSN 6110-01-632-9628
NSN 5975-00-203-1265