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 5910-01-490-3268
NSN 6610-00-632-9502
NSN 5975-00-004-9431
NSN 4140-01-124-8070
NSN 6685-01-421-4403
NSN 5996-01-399-2319
NSN 6150-00-403-7332
NSN 5835-01-123-8305
NSN 5985-00-068-3782
NSN 6240-01-190-3541
NSN 5998-00-423-7121
NSN 5855-01-136-1916