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 5905-01-517-1245
NSN 6110-01-412-9334
NSN 5965-00-170-5254
NSN 5965-00-518-0958
NSN 5999-00-161-3421
NSN 5998-01-650-8146
NSN 5920-00-189-0858
NSN 5990-00-716-7796
NSN 6150-01-500-6255
NSN 5998-01-581-3149
NSN 6610-01-500-5046
NSN 5905-00-528-9975