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 5996-00-901-0519
NSN 6320-00-336-9123
NSN 5930-01-602-0646
NSN 6620-01-204-5650
NSN 5965-01-215-0993
NSN 6645-01-300-9280
NSN 5895-01-507-0596
NSN 5998-00-754-0663
NSN 5930-01-006-8808
NSN 5950-01-644-4709
NSN 5935-01-593-8378
NSN 5996-00-905-6610