| CPC B64C 3/56 (2013.01) | 20 Claims |

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1. An apparatus for shortening a wingspan of an aircraft, the apparatus comprising:
a first link extending from a wingtip of the aircraft and moveably coupled to a fixed wing of the aircraft;
a second link extending from the wingtip and moveably coupled to the fixed wing; and
an actuator coupled to the fixed wing and to the second link, the actuator comprising a piston;
wherein the actuator is configured to extend the piston to move the second link and cause the wingtip to move between an extended position in which the wingtip is substantially coplanar with the fixed wing and a stowed position in which the wingtip is substantially coplanar with the fixed wing.
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