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 6130-01-003-7543
NSN 6145-01-201-4347
NSN 6145-01-414-9681
NSN 6685-01-536-3531
NSN 5915-01-551-0745
NSN 5945-01-248-6161
NSN 5835-00-811-4554
NSN 6320-00-403-6003
NSN 6110-00-684-6844
NSN 6650-01-532-2078
NSN 5996-01-250-3912
NSN 5950-01-034-5435