A floatplane (100) comprising a fuselage (102), at least one primary wing (104) attached to the fuselage (102), a float arrangement comprising a number of floats (106), and propulsion means (500) for driving the floatplane (100), characterised in that the floats (106) of the float arrangement are attached to the fuselage (102) by a number of second wing structures (108), said second wing structures (108) producing additional lift.
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