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 6645-00-295-8535
NSN 5915-00-081-3929
NSN 5965-01-552-4272
NSN 6650-00-590-9073
NSN 7035-01-112-1054
NSN 6135-01-187-4382
NSN 5895-01-106-4161
NSN 5990-01-378-5443
NSN 5985-01-372-8108
NSN 5915-00-432-6333
NSN 6650-01-510-9488
NSN 6135-01-317-6021