Abstract: The disclosure herein updates distant equipment while avoiding protocols and connections and concerns a deported downloading system of data on distant equipment, and includes a gateway adapted to receive a set of data comprising operational data addressed to the distant equipment as well as a temporary downloading engine, the gateway being also adapted to download the operational data into the distant equipment by starting the execution of the downloading engine.

Abstract: The disclosure herein updates distant equipment while avoiding protocols and connections and concerns a deported downloading system of data on distant equipment, and includes a gateway adapted to receive a set of data comprising operational data addressed to the distant equipment as well as a temporary downloading engine, the gateway being also adapted to download the operational data into the distant equipment by starting the execution of the downloading engine.

Abstract: Input/output interfaces of avionic modules of IMA type in a device including several modules is tested. A system includes at least one application employed by a set of computer modules. This set includes the computer module (a first module), and at least one other computer module (at least one second module). A system test is associated with the at least one system for functionally testing the set of computer modules according to the system. The system test includes at least one elementary system test for functionally testing at least one input/output interface of the first module. The execution of the at least one elementary system test is independent of the at least one second module. At least one result of execution of the at least one elementary system test is transmitted to a maintenance computer distinct from the computer modules of the plurality of computer modules.

Abstract: Assistance in the maintenance of an aircraft system comprising a set of elements, means for detecting faults of elements or of functions implemented by elements and means for establishing a first level of diagnostic. After having detected a fault, a plurality of elements are identified, each element of that plurality of elements being liable to be at the origin of the detected fault, alone or in combination with at least one other element of that plurality of elements. A probability that the element considered is at the origin of said detected fault is then determined for each element of that plurality of elements.

Abstract: Input/output interfaces of avionic modules of IMA type in a device including several modules is tested. A system includes at least one application employed by a set of computer modules. This set includes the computer module (a first module), and at least one other computer modul (at least one second module). A system test is associated with the at least one system for functionally testing the set of computer modules according to the system. The system test includes at least one elementary system test for functionally testing at least one input/output interface of the first module. The execution of the at least one elementary system test is independent of the at least one second module. At least one result of execution of the at least one elementary system test is transmitted to a maintenance computer distinct from the computer modules of the plurality of computer modules.