According to the DC-3 AOM the minimum control speed in the air VMC is 76 kt DIAS, which corresponds with 82 kt CAS. VMC is the lowest airspeed at which the aircraft can be flown on one engine, on a constant heading and with a bank angle of 5?? towards the live engine, with the propeller of the shut down engine feathered in clean configuration and with maximum except take-off power on the running e