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 2925-01-347-4208
NSN 5920-01-351-2193
NSN 5990-00-391-4945
NSN 5920-01-406-5195
NSN 5950-01-259-7028
NSN 5998-01-306-5603
NSN 5950-00-471-4586
NSN 5935-00-682-6249
NSN 5950-01-403-2852
NSN 5950-01-091-9436
NSN 6135-00-107-6662
NSN 6135-00-179-0538