§ 25.333. Flight maneuvering envelope.
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/us/cfr/t14/s§ 25.333·A research copy — for the controlling text, always check the official state or federal source. Not legal advice.
(a)General. The strength requirements must be met at each combination of airspeed and load factor on and within the boundaries of the representative maneuvering envelope (V-n diagram) of paragraph
(b)of this section. This envelope must also be used in determining the airplane structural operating limitations as specified in § 25.1501.
(b)Maneuvering envelope. [Doc. No. 5066, 29 FR 18291, Dec. 24, 1964, as amended by Amdt. 25-86, 61 FR 5220, Feb. 9, 1996]