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 5925-01-351-5542
NSN 5920-01-197-8397
NSN 6685-01-331-5678
NSN 6685-01-123-3248
NSN 6220-01-011-0865
NSN 5950-01-144-9969
NSN 6105-00-250-0279
NSN 6610-00-716-1117
NSN 6145-01-441-2630
NSN 6220-01-374-2235
NSN 6610-01-070-0230
NSN 5960-00-099-9790