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 4140-00-501-7833
NSN 7035-01-590-5755
NSN 6650-00-826-7396
NSN 6135-00-027-3914
NSN 5930-00-947-8335
NSN 6645-01-190-4297
NSN 5960-01-017-0989
NSN 5950-00-900-5773
NSN 5895-01-167-6236
NSN 6685-00-928-7639
NSN 5998-00-495-4505
NSN 5985-01-294-3712