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 6135-01-127-0173
NSN 5855-00-285-8172
NSN 5960-01-042-3337
NSN 5965-01-088-5414
NSN 5999-01-145-4274
NSN 6110-00-105-0428
NSN 5975-01-499-1055
NSN 6105-01-008-9223
NSN 5960-01-305-1874
NSN 5990-01-507-7495
NSN 5999-00-148-9072
NSN 5998-00-912-0569