Abstract: A system for monitoring the operational status of an aircraft between successive missions of the aircraft includes a computer able to determine at least one operational impact measurement on at least one future mission of the aircraft related to the aircraft and/or to an aircraft equipment and/or to a consumable and/or to the aircraft crew, the operational impact measurement being determined as a function of the flight logbook and/or technical logbook data of at least one already completed mission of the aircraft and/or a context of the future mission. The system includes a display and a display manager on the display, able to display on the display at least one operational impact indicator related to the aircraft and/or to the equipment and/or to the consumable and/or to the crew, as a function of the operational impact measurement determined by the computer.

Abstract: A system for assisting in a dispatch decision of an aircraft and related process are provided. The system includes a synthesis module, configured to generate at least one dispatch status for the aircraft, based on at least one defect and/or fault datum of the aircraft received from the acquisition module and at least data contained in a first database and in a second minimum equipment list database; and a display, configured to display at least one synthesis window containing at least one defect and/or fault identification indicator of the aircraft developed from the or each defect and/or fault datum, and at least one dispatch status indicator based on the dispatch status determined by the synthesis module.

Abstract: A system for assisting in a dispatch decision of an aircraft and related process are provided. The system includes a synthesis module, configured to generate at least one dispatch status for the aircraft, based on at least one defect and/or fault datum of the aircraft received from the acquisition module and at least data contained in a first database and in a second minimum equipment list database; and a display, configured to display at least one synthesis window containing at least one defect and/or fault identification indicator of the aircraft developed from the or each defect and/or fault datum, and at least one dispatch status indicator based on the dispatch status determined by the synthesis module.

Abstract: The method of generating an image in the form of a disc portion on a display, the disc portion comprising a center and a maximum radius defining a limit of the image generated, the disc portion comprising a plurality of angular sectors, each angular sector comprising a plurality of disjoint areas, each disjoint area of an angular sector being delimited by two circular arcs defined between two radii, and each disjoint area being called a “ring”, is characterized in that it comprises: a first step of selecting a ring, a second step of comparing the area of the ring with at least one predefined value, dubbed the grain, a third step of generating the image of the ring as a function of the result of the comparison, a fourth step of incrementing the next ring to be selected.

Abstract: The method of generating an image in the form of a disc portion on a display, the disc portion comprising a centre and a maximum radius defining a limit of the image generated, the disc portion comprising a plurality of angular sectors, each angular sector comprising a plurality of disjoint areas, each disjoint area of an angular sector being delimited by two circular arcs defined between two radii, and each disjoint area being called a “ring”, is characterized in that it comprises: a first step of selecting a ring, a second step of comparing the area of the ring with at least one predefined value, dubbed the grain, a third step of generating the image of the ring as a function of the result of the comparison, a fourth step of incrementing the next ring to be selected.