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 6110-00-421-3549
NSN 6130-01-547-6652
NSN 5895-00-516-9357
NSN 6685-01-531-5061
NSN 4140-00-061-3110
NSN 6240-01-411-6714
NSN 5996-01-618-8986
NSN 5945-00-203-5575
NSN 5950-01-307-0801
NSN 5965-01-560-0056
NSN 6240-00-201-9011
NSN 6685-00-484-8137