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 5999-00-048-7541
NSN 5996-01-265-5150
NSN 6645-01-197-9090
NSN 6130-01-576-6002
NSN 6220-01-101-4158
NSN 5925-01-457-0289
NSN 5915-00-332-8963
NSN 6150-01-443-9431
NSN 6645-01-350-3138
NSN 5930-00-900-5758
NSN 5930-00-081-7956
NSN 5985-01-294-7148