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 6610-00-834-0713
NSN 5925-01-658-3233
NSN 5855-01-317-5354
NSN 6110-01-506-0041
NSN 6105-01-245-8932
NSN 7035-00-275-5604
NSN 5985-01-472-2357
NSN 5855-01-493-9486
NSN 6650-01-144-2509
NSN 5998-01-661-1335
NSN 5999-01-502-7827
NSN 5960-01-252-8821