§ 25.119. Landing climb: All-engines-operating.
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/us/cfr/t14/s§ 25.119·A research copy — for the controlling text, always check the official state or federal source. Not legal advice.
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 VREF determined in accordance with § 25.125(b)(2)(i); and
(b)In icing conditions with the most critical of the landing ice accretion(s) defined in Appendices C and O of this part, as applicable, in accordance with § 25.21(g), and with a climb speed of VREF determined in accordance with § 25.125(b)(2)(ii). [Amdt. 25-121, 72 FR 44666; Aug. 8, 2007, as amended by Amdt. 25-,140, 79 FR 65525, Nov. 4, 2014]