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 5835-01-565-3411
NSN 6620-01-275-2781
NSN 6220-01-009-5967
NSN 6110-00-177-3105
NSN 6110-01-080-9621
NSN 6320-01-426-8947
NSN 6220-00-115-5842
NSN 5998-00-997-5320
NSN 5905-01-192-7963
NSN 5930-00-915-3464
NSN 6135-00-235-1938
NSN 6130-01-365-1021