Pilatus PC-12 NGX, Pilot'S Information Manual

Page: 493 / 625

Example:
− Pressure Altitude = 6000 ft
− Outside Air Temperature = -10 °C
− Weight = 3500 kg
− Headwind Component = 8 kt
− Uphill Component = 1%
− Takeoff Ground Roll = 300 m (from Fig. 5-3-2-16 )
− Icing Correction (A + B + C) = 28.5% + 1.6% + 0.5% = 30.6%
− Takeoff Ground Roll in Icing Conditions = 300 m * 1.306 = 392 m.
Section 5 - Performance (EASA Approved)
Flight in Icing Conditions - Takeoff Performance
Pilot's Operating Handbook Report No: 02406
Issue date: Dec 18, 2020
Page 5-4-5-5
12-C-A15-60-0504-05A-030A-A
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