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 6610-01-115-0391
NSN 5965-00-866-3371
NSN 5855-00-494-9581
NSN 5998-00-248-2791
NSN 6650-01-467-2355
NSN 6685-00-912-6803
NSN 5945-01-495-3673
NSN 5855-01-338-1424
NSN 5996-01-548-6975
NSN 5985-01-400-0882
NSN 5905-01-410-8694
NSN 5945-00-528-1920