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 6105-01-348-1799
NSN 5855-00-118-8762
NSN 5945-01-495-7676
NSN 6645-00-915-9397
NSN 5920-01-100-8939
NSN 5960-00-099-8591
NSN 5920-00-064-3523
NSN 6610-00-023-0076
NSN 5925-00-491-2363
NSN 2925-01-359-4027
NSN 6650-01-314-3577
NSN 5915-01-116-2932