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 6150-01-593-9382
NSN 6650-00-287-5868
NSN 6150-00-824-8626
NSN 6620-01-364-0195
NSN 5930-00-040-1306
NSN 5996-00-594-8587
NSN 5998-01-653-1509
NSN 6685-00-422-9900
NSN 7035-01-069-3537
NSN 6105-01-492-5723
NSN 5996-00-833-2521
NSN 6240-01-046-9424