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 6130-01-212-9912
NSN 5895-00-929-6885
NSN 5960-00-190-5817
NSN 6130-01-229-6801
NSN 6150-00-445-5438
NSN 6150-01-052-6239
NSN 5990-00-852-0432
NSN 4140-00-916-2771
NSN 6220-01-432-7498
NSN 5920-00-937-2131
NSN 7035-01-363-4540
NSN 6105-01-258-5688