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 5960-01-495-0859
NSN 4140-01-474-7950
NSN 5895-01-188-2150
NSN 5965-00-630-7872
NSN 5835-01-536-5739
NSN 6135-01-650-9371
NSN 5965-01-384-7670
NSN 6685-00-296-0392
NSN 5950-01-463-2796
NSN 4140-01-349-8491
NSN 6620-01-233-7466
NSN 6145-01-501-0996