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 6645-01-166-1841
NSN 2925-01-622-8568
NSN 5910-01-040-6075
NSN 6685-01-487-3988
NSN 5950-01-337-1404
NSN 6135-00-073-8939
NSN 5895-01-217-8726
NSN 2925-00-779-3410
NSN 5930-00-555-3007
NSN 6320-01-072-2073
NSN 5905-01-050-4194
NSN 5965-01-439-6650