180 deg. 7.998-8.002 in. Id based on 360 deg; 21 slots 0.352-0.354 in. Wide by 0.477-0.481 in deep; 21 holes 0.186-0.187
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 6620-00-538-8746
NSN 6320-01-173-7950
NSN 5925-01-411-3466
NSN 5965-01-591-3958
NSN 6650-01-649-6849
NSN 6620-01-212-8089
NSN 5930-01-213-0744
NSN 5950-01-599-8476
NSN 6240-00-646-6931
NSN 6220-00-959-1195
NSN 6645-01-578-6815
NSN 5935-01-178-4017