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 5960-01-601-5565
NSN 5985-01-539-9402
NSN 6645-00-930-1487
NSN 6110-00-954-8248
NSN 5999-01-426-8740
NSN 5910-00-711-0367
NSN 6130-00-797-6187
NSN 5915-01-342-2773
NSN 6240-00-134-9094
NSN 6105-01-334-8128
NSN 6150-01-419-3558
NSN 6320-01-181-9474