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 6240-01-103-9884
NSN 5935-00-419-2530
NSN 6685-00-763-9059
NSN 6320-01-345-5818
NSN 6150-00-240-8024
NSN 6240-01-587-6623
NSN 6220-01-271-2678
NSN 5945-00-826-7068
NSN 6105-01-606-4265
NSN 6150-00-176-9112
NSN 5920-00-042-9165
NSN 6110-00-960-7341