Weight-shift-control aircraft

Weight-shift-control aircraft means a powered aircraft with a framed pivoting wing and a fuselage controllable only in pitch and roll by the pilot's ability to change the aircraft's center of gravity with respect to the wing. Flight control of the aircraft depends on the wing's ability to flexibly deform rather than the use of control surfaces.

Source

14 CFR § 1.1

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Scoping language

As used in Subchapters A through K of this chapter, unless the context requires otherwise:

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