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 5999-01-090-0664
NSN 5960-00-914-9277
NSN 5905-00-996-3092
NSN 6105-01-525-4822
NSN 4140-01-381-7043
NSN 5855-01-020-7982
NSN 5905-01-069-4666
NSN 6610-00-969-9815
NSN 6650-01-200-7657
NSN 5965-01-046-9619
NSN 5965-01-060-2558
NSN 5985-01-552-1553