CS 25.119 Landing climb: all engines operating
ED
Decision 2016/010/R
(See AMC 25.119)
In the
landing configuration, the steady gradient of climb may not be less than 3·2%,
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; and
(a) In non-icing conditions, with a climb
speed of VREF determined in accordance with CS 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, as applicable, in accordance with CS 25.21(g),
and with a climb speed of VREF determined in accordance with CS
25.125(b)(2)(i).
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