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 5996-00-083-3163
NSN 5895-01-476-2326
NSN 5999-00-805-2150
NSN 6130-00-783-8272
NSN 5910-01-225-0649
NSN 5895-01-412-4729
NSN 2925-01-455-2558
NSN 5965-01-151-0903
NSN 5915-00-324-4874
NSN 5930-01-049-3213
NSN 6685-01-074-4345
NSN 6150-01-606-8268