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 the engines at the power or thrust that is available 8 seconds after initiation of movement of the power or thrust controls from the minimum flight idle to the go-around power or thrust setting—
(a) In non-icing conditions, with a climb speed of VREFdetermined in accordance with §25.125(b)(2)(i); and
(b) In icing conditions with the landing ice accretion defined in appendix C, and with a climb speed of VREFdetermined in accordance with §25.125(b)(2)(ii).
[Amdt. 25–121, 72 FR 44666; Aug. 8, 2007]
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