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 5945-01-429-9824
NSN 5835-00-143-4153
NSN 6135-01-508-6083
NSN 6620-01-012-2852
NSN 5960-01-284-1642
NSN 5935-01-407-3324
NSN 6150-01-262-1883
NSN 5998-01-465-0662
NSN 2925-00-441-8252
NSN 6610-00-005-4409
NSN 5998-01-432-4003
NSN 5996-00-392-7626