FIELD: aviation.
SUBSTANCE: invention relates to aircraft engineering, particularly to aircraft control devices. Post of manual doubled aircraft comprises wheels, steering column, base with tips, which is pivotally fixed in arms on cabin floor. Steering column of double crew cabin are synchronised by angular deviations with via general thrust and common shaft. Structure of each steering column includes another degree of freedom, specifically steering column is rotatable about its own longitudinal axis.
EFFECT: reduced weight of control system, avoiding need to harmonise positions of chair on height and distance from pedals.
1 cl, 5 dwg
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