FIELD: physics.
SUBSTANCE: apparatus for determining aircraft mass has series-connected piezoelectric pressure sensors fitted at points where the landing gear unit is mounted, a processor and a display device in the crew cabin. The apparatus also includes a transmitting device, an AND element, two signal selectors, an altitude sensor and a dispatcher receiving channel, which consists of a receiving device, an OR element, a display and a memory unit.
EFFECT: higher flight safety.
2 cl, 3 dwg
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