14 CFR 25.119
§ 25.119 Landing climb: All-engines-operating.
United States · 14 CFR — Aeronautics and Space · Status: effective
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- Citation
- 14 CFR 25.119, § 25.119 Landing climb: All-engines-operating, United States, version 1 as recorded 2026-07-09, yourstate.us, https://yourstate.us/provision/53983
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Full text
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).
Legislative history
This is a federal regulation, adopted through agency rulemaking under the Administrative Procedure Act — not enacted by a recorded vote of Congress.