Pilatus PC-12 NGX, Руководство пилота

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5-4-6 Flight in Icing Conditions - Accelerate-Stop Performance
The flaps must be set to 15° for takeoff. The use of flaps 30° for takeoff is prohibited.
The maximum speed for power chop is assumed to be 10 kt higher than that for non-icing
conditions.
The total accelerate-stop distance is calculated by first computing the total accelerate-stop
distance in non-icing conditions from
Fig. 5-3-2-13 (standard units), Fig. 5-3-2-14 (metric units)
and then correcting that distance for takeoff in or into known icing conditions by using the
corrections in
Table 5-4-6-1 , Table 5-4-6-2 and Table 5-4-6-3 .
Icing correction (%) = A + B + C
Section 5 - Performance (EASA Approved)
Flight in Icing Conditions - Accelerate-Stop Performance
Pilot's Operating Handbook Report No: 02406
Issue date: Mar 06, 2020
Page 5-4-6-1
12-C-A15-60-0504-06A-030A-A
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