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 6650-01-565-6977
NSN 6220-01-411-6919
NSN 6135-01-359-5798
NSN 6105-01-092-2362
NSN 5990-01-032-0710
NSN 5910-01-319-1876
NSN 4140-01-518-5516
NSN 6685-01-012-3657
NSN 5925-00-971-2126
NSN 6130-00-518-4305
NSN 7035-01-223-4097
NSN 6650-01-528-0538