Abstract: An aircraft operational state monitoring system is provided that includes a module for acquiring a logic state of a plurality of components of the aircraft, the components belonging to airplane systems. The aircraft operational state monitoring system includes a module for determining the operability status of a plurality of macroscopic functions of the aircraft, each macroscopic function being defined independently of the components and airplane systems necessary for the performance of the macroscopic function, the operability status being determined based on logic states of the plurality of components between an operational status and at least one nonoperational status. The aircraft operational state monitoring system includes a display and at least one graphic display management assembly on the display, configured for displaying, on the display, summary indicators of the operability status of the macroscopic functions of the aircraft.

Abstract: An aircraft operational state monitoring system is provided that includes a module for acquiring a logic state of a plurality of components of the aircraft, the components belonging to airplane systems. The aircraft operational state monitoring system includes a module for determining the operability status of a plurality of macroscopic functions of the aircraft, each macroscopic function being defined independently of the components and airplane systems necessary for the performance of the macroscopic function, the operability status being determined based on logic states of the plurality of components between an operational status and at least one nonoperational status. The aircraft operational state monitoring system includes a display and at least one graphic display management assembly on the display, configured for displaying, on the display, summary indicators of the operability status of the macroscopic functions of the aircraft.

Abstract: A system for controlling and monitoring pieces of equipment of an aircraft, each piece of equipment being able to be switched between two logic activation state values, comprising a man-machine interface, a module for configuration of a functional activation state of a function able to be performed on at least pieces of equipment of a system of the aircraft, the functional activation state being configurable between an active state and an inactive state, the configuration module being adapted for detecting an action of selection of a functional activation state of the function by an operator, and a control and monitoring module configured for determining a logic activation state of each of the pieces of equipment of the system, so that, when each of the pieces of equipment is in the determined logic activation state, the function is in the selected functional activation state.