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 5855-01-103-1474
NSN 5895-01-586-7892
NSN 5950-01-425-5820
NSN 5990-01-492-6575
NSN 6610-01-166-4860
NSN 6645-01-326-0747
NSN 5930-01-191-5338
NSN 5835-01-373-9506
NSN 6645-01-382-0292
NSN 5965-00-563-1882
NSN 5975-00-535-9720
NSN 5905-01-039-3758