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 6685-01-467-2493
NSN 5910-01-521-1467
NSN 6240-01-346-3904
NSN 5920-01-513-5847
NSN 6110-00-509-9704
NSN 5990-01-116-2181
NSN 6110-00-143-9931
NSN 5965-01-371-8031
NSN 5835-01-589-4735
NSN 5920-00-115-0001
NSN 5950-01-608-3142
NSN 5915-01-243-9192