| 摘要 |
<p>An aircraft (1) of the type having retractable landing gear (10) and a pusher propeller (8) is provided with a twin tail boom (4). The tail boom (4) has a configuration to prevent the lowermost point of the pusher propeller (8) from contacting a landing surface when landing the aircraft (1), even with the landing gear (10) retracted, so that the engine of the aircraft (1) is not damaged as a result of the pusher propeller (8) being unable to rotate during the landing.</p> |
