---
kind: "section"
citation: "14 C.F.R. § 25.119"
title: "14"
number: "25.119"
heading: "Landing climb: All-engines-operating."
url: "https://uscodex.org/cfr/14/25.119"
---

# §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 VREF determined in accordance with [§ 25.125(b)(2)(i)](/cfr/14/25.125.md?p=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)](/cfr/14/25.21.md?p=g), and with a climb speed of VREF determined in accordance with [§ 25.125(b)(2)(ii)](/cfr/14/25.125.md?p=b-2-ii).

## Notes

### Amendments

[Amdt. 25-121, 72 FR 44666; Aug. 8, 2007, as amended by Amdt. 25-,140, 79 FR 65525, Nov. 4, 2014]

### Authority

Authority: 49 U.S.C. 106(f), 106(g), 40113, 44701, 44702 and 44704; Pub. L. 115-254, 132 Stat 3281 (49 U.S.C. 44903 note).

### Source

Source: Docket No. 5066, 29 FR 18291, Dec. 24, 1964, unless otherwise noted.

### Amendments

[Amdt. 25-121, 72 FR 44666; Aug. 8, 2007, as amended by Amdt. 25-,140, 79 FR 65525, Nov. 4, 2014]