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 6610-01-524-0636
NSN 5985-00-399-1174
NSN 5945-01-361-7687
NSN 5895-01-199-0147
NSN 5975-01-303-8289
NSN 6320-00-908-6841
NSN 5996-01-406-6647
NSN 5895-01-094-0634
NSN 5910-01-015-8222
NSN 6110-01-246-8202
NSN 6645-01-213-1739
NSN 6220-01-391-6084