FIELD: aviation.
SUBSTANCE: device for refueling a light aircraft of the upper plane type or biplane, the filling necks (2, 3) of which are installed at the upper area of the rotary manifold (1). The collector (1) is located in the plane of symmetry of the aircraft and is hingedly fixed in the lower part. The position of the filling necks (2, 3) with the vertical position of the manifold (1) exceeds the upper level of the fuel tanks (7).
EFFECT: invention provides guaranteed filling of the right and left tanks of the V-shaped wing at all allowable angles of the aircraft's roll in the parking lot.
4 dwg
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