3.250-4.922 in. Id.; 0.263-0.270 in. Dia. Of 8 holes eq sp; 0.188 in. Diameter of 2 holes; external spline data: 4.680 in. Od; 4.571 in. Pitch dia.; 32 teeth; 2nd external spline data: 4.781in. Od; 4.750 in. Pitch dia.; 76 teeth; 0.125 in. Dia. Of 5 holes
An item designed to transfer rotary motion from a rotary, turbine, aircraft gas turbine engine to a rotor, compressor, aircraft gas turbine engine and/or a rotor, fan, aircraft gas turbine engine. It may include the hub, turbine, aircraft gas turbine engine. It may include provisions for mounting bearings and/or seals.
Classification: Parts of gas turbine aircraft engines, other than for use in civil aircraft
NSN 5960-00-153-7115
NSN 6320-01-125-3361
NSN 5985-01-044-6027
NSN 6645-01-625-1192
NSN 5975-00-428-1683
NSN 6145-01-139-4859
NSN 5945-01-099-1534
NSN 6650-00-170-5095
NSN 5935-00-786-3510
NSN 5999-00-100-5761
NSN 6145-01-604-0245
NSN 6320-01-549-7201