FAA Federal Aviation Regulations (FARS, 14 CFR)
FARs > Part 25 > Section 119 - Landing climb: All-engines-operating
section 25.117 |
section 25.121
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. 1-49, 67 FR 70826, Nov. 26, 2002]
   
Current page: FARs > Part 25 > Section 119 - Landing climb: All-engines-operating
section 25.117 |
section 25.121
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