Table 5-4-5-4: Icing Corrections to Takeoff Ground Roll - Altitude Correction (Table A)
Table A
Takeoff Weight (kg (lb))
Altitude
Correction
(%)
2900
(6393)
3300
(7275)
3700
(8157)
4100
(9039)
4500
(9921)
4740
(10450)
V
R
/ V
50ft
(KIAS)
72 / 88
77 / 94
81 / 100
86 / 105
90 / 110
92 / 113
0 ft
+28
+28
+29
+29
+30
+30
2000 ft
+28
+28
+29
+29
+30
+30
4000 ft
+28
+28
+29
+29
+30
+30
6000 ft
+28
+28
+29
+29
+30
+30
8000 ft
+28
+28
+29
+29
+30
+30
10000 ft
+28
+28
+29
+29
+30
+30
12000 ft
+28
+28
+29
+29
+30
+30
14000 ft
+28
+29
+30
+30
+31
+32
Table 5-4-5-5: Icing Corrections to Takeoff Ground Roll - Wind Correction (Table B)
Table B
Takeoff Weight (kg (lb))
Wind Correction (%)
2900 - 4740
(6393 - 10450)
10 kt Tailwind
-4
No Wind
0
10 kt Headwind
+2
20 kt Headwind
+5
30 kt Headwind
+8
Table 5-4-5-6: Icing Corrections to Takeoff Ground Roll - Slope Correction (Table C)
Table C
Takeoff Weight (kg (lb))
Slope
Correction
(%)
2900
(6393)
3300
(7275)
3700
(8157)
4100
(9039)
4500
(9921)
4740
(10450)
4% down
0
0
-1
-1
-1
-1
2% down
0
0
0
0
0
-1
No Slope
0
0
0
0
0
0
2% up
+1
+1
+1
+2
+2
+3
4% up
+1
+2
+3
+4
+6
+6
Section 5 - Performance (EASA Approved)
Flight in Icing Conditions - Takeoff Performance
Pilot's Operating Handbook
Report No: 02406
Issue date: Dec 18, 2020
Page 5-4-5-4
12-C-A15-60-0504-05A-030A-A
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GENERAL
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