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 6320-00-004-9158
NSN 5915-00-291-3736
NSN 2925-01-309-5007
NSN 6240-01-028-2592
NSN 5895-00-137-0439
NSN 7035-00-763-6180
NSN 5930-00-186-9934
NSN 5950-01-409-2785
NSN 6645-01-391-9477
NSN 5945-01-127-5489
NSN 6610-01-189-3001
NSN 5930-00-064-7684