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 6610-00-571-4846
NSN 4140-01-566-6614
NSN 6240-00-304-7015
NSN 5965-01-056-7225
NSN 5910-01-131-1689
NSN 6320-01-652-3806
NSN 6240-01-331-5246
NSN 6220-01-253-0380
NSN 5835-00-707-6266
NSN 5998-01-150-8286
NSN 5998-01-408-4676
NSN 5996-00-976-1429