CS 25.333 Flight manoeuvring envelope
ED Decision 2016/010/R
(See AMC 25.333)
(a) General. The strength requirements must be met at each combination of airspeed and load factor on and within the boundaries of the representative manoeuvring envelope (V-n diagram) of sub-paragraph (b) of this paragraph. This envelope must also be used in determining the aeroplane structural operating limitations as specified in CS 25.1501.
(b) Manoeuvring envelope (See AMC 25.333(b))
[Amdt 25/11]
[Amdt 25/13]
[Amdt 25/18]