AMC to
Appendix Q, (SAL) 25.5 Safe operational and flight characteristics
ED Decision 2016/010/R
(a) For the
approach demonstrations required by (SAL)
25.5(a), due account should be taken of:
(1) The
systems’ aspects of the power/thrust levers being at idle (e.g. arming of
ground lift dump);
(2) The most
adverse flight idle power/thrust (e.g. effects of engine bleeds or FADEC idle
power/thrust control); and
(3) The
effects on controllability from the use of auxiliary drag devices such as
flight spoilers (e.g. increased stall warning and stall speeds, loss of
manoeuvrability).
(b) For the
flare, touchdown and landing demonstrations required by (SAL) 25.5(a), there should not
be any occurrence of:
(1) Stall
warning;
(2) Tail
strike; or
(3) Any
other characteristic that would interfere with the completion of the landing
(e.g. automatic thrust increase).
(c) For the go-around demonstrations required by (SAL) 25.5(e) and (i), due account should be taken of time delays associated with automatic or manual retraction of auxiliary drag devices.
[Amdt No: 25/13]
[Amdt No: 25/18]
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