FIELD: physics.
SUBSTANCE: method comprises the following steps: connecting a test device (1) to a plurality of separate test points in an aircraft control system simultaneously; selecting each of the plurality of test points individually, such that the test device can be electrically connected to the selected one of the plurality of test points; conducting a test on the control system at each of the plurality of test points selected by means of a selector unit (20, 22) using the test device, including detecting a signal or voltage at the test point selected by means of the selector unit; and displaying the result of the test at the selected test point to an operator. Disclosed also is a device for realising said method.
EFFECT: easier testing of aircraft control systems.
6 cl, 4 dwg
