T.O. 2j-j85-94; 125.0 microinch finish all surfaces
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 5905-01-036-7883
NSN 5935-00-014-3287
NSN 5998-00-107-5370
NSN 7035-00-442-1869
NSN 6685-01-457-5046
NSN 5895-00-789-4033
NSN 5930-00-109-0952
NSN 6320-01-106-4414
NSN 5915-01-068-6409
NSN 7035-01-487-6481
NSN 5905-01-025-1889
NSN 6650-01-459-8703