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 5835-01-112-9008
NSN 5915-00-525-5753
NSN 5895-01-559-1997
NSN 5855-00-337-3679
NSN 6610-01-160-0417
NSN 5905-01-552-5038
NSN 6685-01-096-9252
NSN 6240-01-502-7883
NSN 6105-01-006-3282
NSN 6650-01-279-8736
NSN 6645-01-399-1626
NSN 5998-01-242-1066