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 5985-01-579-5006
NSN 5930-01-215-1476
NSN 4140-01-334-9043
NSN 5835-01-089-1076
NSN 5930-00-570-9888
NSN 5920-01-417-1928
NSN 5945-01-472-8713
NSN 6110-01-615-5758
NSN 5915-01-605-3326
NSN 5950-00-099-9612
NSN 5905-01-326-1028
NSN 2925-01-426-3410