Text in force at 25-153: from 25-86, effective 11 Mar 1996.
(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 Sec. 25.1501.]
(b) Maneuvering envelope.
(c) [Removed.]
61 FR 5220 · Source