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 5985-01-565-1516
NSN 5950-00-922-8489
NSN 5945-00-708-2363
NSN 5925-00-830-8148
NSN 4140-01-412-4568
NSN 6220-00-915-9871
NSN 5915-01-380-3107
NSN 7035-00-225-6499
NSN 6685-01-445-0243
NSN 5990-01-411-5930
NSN 6620-01-552-2889
NSN 5920-01-202-4977