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 6145-01-449-1885
NSN 2925-01-363-1805
NSN 5935-00-977-7877
NSN 5950-01-089-9860
NSN 5990-00-301-0144
NSN 5915-00-398-0677
NSN 6105-01-060-3539
NSN 6105-01-040-5665
NSN 6610-01-431-8575
NSN 5835-00-393-1996
NSN 5835-00-233-6327
NSN 2925-01-336-2820