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
                        
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