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 6135-01-442-4581
NSN 5950-00-389-7139
NSN 2925-00-305-8030
NSN 2925-00-456-7627
NSN 5925-01-194-9600
NSN 7035-01-595-5270
NSN 5915-01-204-1406
NSN 5999-01-113-8120
NSN 6110-01-375-2025
NSN 6320-01-652-3806
NSN 5835-01-378-6804
NSN 6685-00-333-8192