25.333—Flight maneuvering envelope.
(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.
Code of Federal Regulations
Code of Federal Regulations
399