FIELD: transport.
SUBSTANCE: set of invention relates to aircraft trailing and maneuvering. Warning system 4 comprises turning angle transducer unit 11 arranged at aircraft and alarm signaling unit 19. Said system 4 outputs generated first signal subject to turning angle between aircraft under carriage leg and aircraft fuselage lengthwise axis. Alarm signaling unit outputs alarm signal subject to said excess turning angle in case the latter exceeds preset value, said 60 degrees. Said turning angle transducer unit 11 can perform the function related with aircraft steering system, say, function of turning angle indication for pilot in maneuvering on ground.
EFFECT: efficient and simple means.
22 cl, 6 dwg
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