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 6150-01-429-2924
NSN 5895-01-330-9179
NSN 5975-00-278-7437
NSN 5925-01-018-1375
NSN 2925-00-724-9252
NSN 6150-00-507-7870
NSN 6130-00-540-5305
NSN 5910-01-119-8899
NSN 6220-01-134-5329
NSN 5999-01-250-1666
NSN 6105-01-447-2984
NSN 6135-01-036-0432