Abstract: Aircraft, fly-by-wire systems, and controllers are provided. An aircraft includes a trim control system and a fly-by-wire system. The trim control system is configured for controlling surfaces of the aircraft. The fly-by-wire system is communicatively coupled with the trim control system and includes an input device and a controller. The input device is configured to receive a re-trim input from a user. The controller is communicatively coupled with the input device and is configured to control the trim control system, to obtain the re-trim input from the user, and to set a pitch trim of the aircraft based on a stable flight condition at a present airspeed of the aircraft in response to the re-trim input from the input device.

Abstract: Aircraft, fly-by-wire systems, and controllers are provided. An aircraft includes a trim control system and a fly-by-wire system. The trim control system is configured for controlling surfaces of the aircraft. The fly-by-wire system is communicatively coupled with the trim control system and includes an input device and a controller. The input device is configured to receive a re-trim input from a user. The controller is communicatively coupled with the input device and is configured to control the trim control system, to obtain the re-trim input from the user, and to set a pitch trim of the aircraft based on a stable flight condition at a present airspeed of the aircraft in response to the re-trim input from the input device.

Abstract: Aircraft, fly-by-wire systems, and controllers are provided. An aircraft includes a trim control system and a fly-by-wire system. The trim control system is configured for controlling surfaces of the aircraft. The fly-by-wire system is communicatively coupled with the trim control system and includes an input device and a controller. The input device is configured to receive a re-trim input from a user. The controller is communicatively coupled with the input device and is configured to control the trim control system, to obtain the re-trim input from the user, and to set a pitch trim of the aircraft based on a stable flight condition at a present airspeed of the aircraft in response to the re-trim input from the input device.

Abstract: Systems, methods, and computers for aircraft are provided. A system includes a portable device and an on-board computer for an aircraft. The on-board computer is configured to record preliminary squawk events that occur while the aircraft is in flight for potential corrective action. The portable device is configured to communicate with the on-board-computer and is configured for: receiving—from the on-board computer—preliminary squawk events that occur while the aircraft is in flight; presenting the preliminary squawk events; receiving approval inputs that indicate approved squawk events of the preliminary squawk events; and generating a squawk list that includes each of the approved squawk events to be investigated for corrective action after the flight.

Abstract: The disclosed embodiments relate to methods, systems and apparatus for automated generation a flight log and a squawk list file. A computer records a preliminary flight log data file (PFLDF), and automatically generates a preliminary squawk list file (PSLF) that includes a plurality of squawk events recorded while an aircraft is in flight. A wireless communication device includes a processor configured to execute a software application, a display that displays a graphical user interface that presents each squawk event from the PSLF for review, and an input system configured to receive inputs including an input for each particular squawk event. These inputs for each particular squawk event can be an edit input, an approval input, or a removal input.

Abstract: The disclosed embodiments relate to automated generation a flight log and a squawk list file. A computer records a preliminary flight log data file (PFLDF), and automatically generates a preliminary squawk list file (PSLF) that includes a plurality of squawk events recorded while an aircraft is in flight. A portable wireless communication device executes a software application, which can cause a display to display each squawk event from the PSLF for review. An input system receives an input for each particular squawk event. These inputs for each particular squawk event can be an edit input, an approval input, or a removal input. When all squawk events in the PSLF have been reviewed, the processor can generate a final flight log and a final squawk list file (FSLF) that includes each of the squawk events from the PSLF that have been reviewed and approved for inclusion in the final squawk list.

Abstract: The disclosed embodiments relate to methods, systems and apparatus for automated generation a flight log and a squawk list file. A computer records a preliminary flight log data file (PFLDF), and automatically generates a preliminary squawk list file (PSLF) that includes a plurality of squawk events recorded while an aircraft is in flight. A wireless communication device includes a processor configured to execute a software application, a display that displays a graphical user interface that presents each squawk event from the PSLF for review, and an input system configured to receive inputs including an input for each particular squawk event. These inputs for each particular squawk event can be an edit input, an approval input, or a removal input.

Abstract: Aircraft, fly-by-wire systems, and controllers are provided. An aircraft includes a trim control system and a fly-by-wire system. The trim control system is configured for controlling surfaces of the aircraft. The fly-by-wire system is communicatively coupled with the trim control system and includes an input device and a controller. The input device is configured to receive a re-trim input from a user. The controller is communicatively coupled with the input device and is configured to control the trim control system, to obtain the re-trim input from the user, and to set a pitch trim of the aircraft based on a stable flight condition at a present airspeed of the aircraft in response to the re-trim input from the input device.