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 5945-01-525-2918
NSN 6130-01-513-9970
NSN 5925-01-130-1802
NSN 5960-01-425-1454
NSN 6150-01-391-7118
NSN 6685-01-633-7905
NSN 5975-00-953-4568
NSN 6240-01-519-8781
NSN 6685-01-407-8675
NSN 6240-01-633-9357
NSN 5965-01-429-9777
NSN 5945-01-190-7327