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 6150-01-271-5408
NSN 6610-01-092-9846
NSN 5935-01-054-0866
NSN 5920-01-412-4742
NSN 5996-00-059-7061
NSN 6110-00-835-7563
NSN 6110-00-754-7926
NSN 5996-01-128-1504
NSN 6150-00-890-7631
NSN 6130-00-551-8316
NSN 6320-00-270-8222
NSN 5905-01-025-6949