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 5990-01-652-7373
NSN 5910-01-444-1429
NSN 4140-01-058-3818
NSN 5905-01-014-0697
NSN 6650-00-175-7520
NSN 5990-01-386-5561
NSN 6685-00-107-6043
NSN 2925-01-444-2061
NSN 6320-00-242-3300
NSN 6610-01-322-7677
NSN 5996-01-170-9659
NSN 6650-01-285-4546