StacksVerified U.S. regulatory reference

14 CFR §25.333

Verified against eCFR.gov as of June 20, 2026View official text on eCFR.gov ↗
  1. (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.
  2. (b)Maneuvering envelope.