Outer radius 2nd end 11.908 in.; inner radius 1st end 11.393 in.; inner radius 2nd end 11.14 in.; formed shape 45 deg. 57 min. 27 sec.; 11 holes 0.3535 in. Dia. Counterbore 0.520 in. Dia. W/2 cutter run outs per ea hole
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 5950-00-619-0800
NSN 5905-01-004-9961
NSN 5999-01-123-0558
NSN 6610-01-341-6041
NSN 5945-01-403-2800
NSN 6105-01-070-3911
NSN 5905-01-056-5434
NSN 5960-01-575-7818
NSN 6150-01-322-6835
NSN 6650-01-656-5649
NSN 5990-00-767-0893
NSN 5895-01-046-4382