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 5945-01-025-4256
NSN 5930-00-185-5142
NSN 6135-01-056-4609
NSN 5960-01-326-8986
NSN 5910-01-487-8330
NSN 6130-01-575-9505
NSN 6105-01-509-7399
NSN 5835-00-729-9305
NSN 5965-00-199-4456
NSN 5996-01-473-8814
NSN 5895-00-286-3788
NSN 5990-01-311-3710