Sec. 25.333 — Flight maneuvering envelope.
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. View or download PDF
[Doc. No. 5066, 29 FR 18291, Dec. 24, 1964, as amended by Amdt. 25–86, 61 FR 5220, Feb. 9, 1996]
NEXT: Sec. 25.335 - Design airspeeds.
PREVIOUS: Sec. 25.331 - Symmetric maneuvering conditions.