[Code of Federal Regulations]

[Title 14, Volume 1]

[Revised as of January 1, 2006]

From the U.S. Government Printing Office via GPO Access

[CITE: 14CFR25.333]



[Page 371-372]

 

                     TITLE 14--AERONAUTICS AND SPACE

 

CHAPTER I--FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION

 

PART 25_AIRWORTHINESS STANDARDS: TRANSPORT CATEGORY AIRPLANES--Table 

of Contents

 

                           Subpart C_Structure

 

Sec. 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 Sec. 25.1501.

    (b) Maneuvering envelope.



[[Page 372]]



[GRAPHIC] [TIFF OMITTED] TC28SE91.035





[Doc. No. 5066, 29 FR 18291, Dec. 24, 1964, as amended by Amdt. 25-86, 

61 FR 5220, Feb. 9, 1996]