10.9 in. Lg; 0.75 in. Od; 0.45 min 0.48 max in. Id; 11 teeth; 0.458 in. Pd; 30 degrees pressure angle; teeth act as splines; finish all over; rockwell hardness
No other part numbers with same form, fit, and function found.
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 6650-01-237-4689
NSN 6650-01-246-4262
NSN 6105-00-941-6493
NSN 4140-01-241-5759
NSN 5975-01-188-8873
NSN 5855-01-602-3437
NSN 5960-01-254-3541
NSN 6650-00-479-7888
NSN 5965-01-053-7168
NSN 4140-00-740-2153
NSN 5930-00-359-6532
NSN 6620-01-633-8443