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 2925-01-329-3665
NSN 5945-00-101-8629
NSN 6685-01-295-6339
NSN 5945-01-275-1493
NSN 5925-01-421-4276
NSN 2925-01-004-5627
NSN 6240-01-480-5897
NSN 5905-01-140-2861
NSN 5930-00-043-0018
NSN 5945-01-445-9498
NSN 6110-00-705-1368
NSN 6240-01-338-6045