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 5996-01-358-6528
NSN 6110-00-578-7243
NSN 6145-00-828-9024
NSN 5895-01-518-2789
NSN 5915-01-551-8160
NSN 5950-01-310-9669
NSN 5965-01-241-0553
NSN 6650-01-062-1926
NSN 6645-01-369-4371
NSN 6320-01-240-4637
NSN 2925-01-471-4912
NSN 5950-01-608-5667