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 5895-01-051-2024
NSN 4140-00-170-5152
NSN 5905-01-592-2405
NSN 5999-00-688-4454
NSN 5855-01-050-4944
NSN 5835-00-155-1379
NSN 5930-00-769-5947
NSN 6150-00-101-8895
NSN 7035-01-191-2822
NSN 6620-00-338-2515
NSN 6645-00-862-2904
NSN 5996-00-248-7061