Methods and apparatus of notification of a flight asymmetry influencing an aircraft

Methods and apparatus of notification of a flight asymmetry influencing an aircraft (100) are disclosed herein. An example method includes monitoring a roll characteristic of an aircraft (100) and determining an output of an autopilot system of the aircraft (100) to control the roll characteristic. The example method further includes generating an alert based on the output and an authority of the autopilot system to control the roll characteristic.