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 7035-01-525-8263
NSN 6150-00-800-3652
NSN 6110-01-452-5654
NSN 5905-01-254-8241
NSN 5996-01-280-6461
NSN 6150-00-223-2596
NSN 6685-01-534-7944
NSN 5915-00-218-6513
NSN 5985-00-794-1358
NSN 6650-01-589-3585
NSN 6320-01-098-2503
NSN 6220-01-415-5698