[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: 14CFR25.119]



[Page 355]

 

                     TITLE 14--AERONAUTICS AND SPACE

 

CHAPTER I--FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION

 

PART 25_AIRWORTHINESS STANDARDS: TRANSPORT CATEGORY AIRPLANES--Table 

of Contents

 

                            Subpart B_Flight

 

Sec. 25.119  Landing climb: All-engines-operating.



    In the landing configuration, the steady gradient of climb may not 

be less than 3.2 percent, with--

    (a) The engines at the power or thrust that is available eight 

seconds after initiation of movement of the power or thrust controls 

from the minimum flight idle to the go-around power or thrust setting; 

and

    (b) A climb speed of not more than VREF.



[Doc. No. 5066, 29 FR 18291, Dec. 24, 1964, as amended by Amdt. 25-84, 

60 FR 30749, June 9, 1995; Amdt. 25-108, 67 FR 70826, Nov. 26, 2002]