Model: 1-100-620-01

Special Features:

Tapered od; 3.67 min 3.675 max in. Largest od; first end; ext splines; 19 teeth; 30 degrees pressure angle; 1.248 min 1.25 max in. Od; 1.1675 in. Nom pitch dia; 1.88 min 2.44 max in. Lg splines; 0.267 min 0.272 max in. Distance from first end to splines; sceond end; ext splines; 13 teeth; 30 degrees pressure abgle; 1/162 min 1.167 max in. Od; 1.0833 in. Nom pitch dia; 2.12 min 2.26 max in. Lg splines; 0.96 in. Nom distance from second end to splines; first end; int thd; 0.625 in.-18 unf 2b thd; 0.88 min 0.92 max in. Dp thd; 0.267 min 0.272 max in. Distance from first end to thd; second end; int thd; 0.625 in.-18 unf 2b thd; 0.65 min 0.69 max in. Dp thd countersunk 60 degrees to 0.72 in. Nom dia

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.