Special Features:

First end od thd; 2.5625 in.-16ns 3a thd; 0.286 in. Nom thd lg; second end od thd; 3.2812 in.-16ns 3a thd; 0.39 in. Nom thd lg; 3.0937 in.-12ns 3a thd on od 2.123 min 2.127 max in. From first end; external splines on od; 65 splines; 30 degrees pressure angle; 2.7083 in. Nom pitch dia; 0.576 min 0.588 max in. Lg splines; 0.762 min 0.774 max in. From first end to splines; 79 splines; 30 degrees pressure angle; 3.2917 in. Nom pitch dia; 0.58 min 0.66 max in. Lg splines; 2.846 min 2.89 max in. From second end to splines; 106 splines; 30 degrees pressure angle; 3.3125 in. Nom pitch dia; 0.081 min 0.085 max in. Lg splines; 0.36 min 0.37 max in. From second end to splines

Properties:

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.