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 5935-00-250-5724
NSN 5915-01-159-2404
NSN 5998-00-961-0773
NSN 5935-01-400-1127
NSN 6130-01-604-1383
NSN 5930-00-915-1408
NSN 5905-00-354-9408
NSN 6135-01-613-1464
NSN 5998-01-238-5815
NSN 5935-00-221-0925
NSN 5999-01-202-8282
NSN 5965-01-315-5764