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 6220-01-360-4530
NSN 6145-01-634-0388
NSN 5985-01-441-2285
NSN 5895-01-485-6660
NSN 6135-00-112-8637
NSN 6610-00-774-5656
NSN 5935-00-241-4446
NSN 5990-01-534-8609
NSN 5996-00-976-3356
NSN 6645-01-111-8218
NSN 7035-00-008-4173
NSN 6685-01-607-4526