| 摘要 |
An aircraft has a fuselage, one or more propellers and a main wing. The wing has a central portion located beneath the fuselage and distal portions which exten d outwardly from opposite sides of the fuselage. The wing floats on water when the aircraft i s stationary and maintains the fuselage above and out of the water. The aircraft optionally h as a tail having a horizontal stabilizer which provides additional support to the fuselage to maintain it out of water. The structure of the aircraft can be adapted for use as a water-craft by reducing the length of the wing.
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