FIELD: transport.
SUBSTANCE: proposed device comprises aircraft pedal actuator, transducer to measure force applied to aircraft pedal to actuate it and to generate signal corresponding to force applied, device to measure deviation of component in response to actuation of aircraft pedal, and control unit to process signals from force transducer and deviation meters to generate output signals indicating aforesaid deviation depending on force applied to aircraft pedal.
EFFECT: reliable and comprehensive test results.
15 cl, 1 dwg
