Table 5-4-10-11: Icing Corrections to Landing Ground Roll - Flaps 0° - No Reverse Thrust - Al-
titude Correction (Table A)
Table A
Landing Weight (kg (lb))
Altitude
Correction
(%)
2900
(6393)
3300
(7275)
3700
(8157)
4100
(9039)
4500
(9921)
V
APP
(KIAS)
104
111
118
124
130
0 ft
+117
+112
+111
+113
+115
2000 ft
+114
+110
+112
+115
+117
4000 ft
+111
+112
+115
+1118
+121
6000 ft
+110
+114
+117
+121
+124
8000 ft
+113
+117
+121
+125
+129
10000 ft
+115
+120
+124
+129
+133
12000 ft
+118
+122
+127
+132
+138
14000 ft
+122
+127
+134
+137
+137
Table 5-4-10-12: Icing Corrections to Landing Ground Roll - Flaps 0° - No Reverse Thrust -
Wind Correction (Table B)
Table B
Landing Weight (kg (lb))
Wind Correction (%)
2900
(6393)
3300
(7275)
3700
(8157)
4100
(9039)
4500
(9921)
10 kt Tailwind
-13
-12
-11
-10
-10
No Wind
0
0
0
0
0
10 kt Headwind
+12
+10
+9
+8
+8
20 kt Headwind
+26
+22
+19
+18
+17
30 kt Headwind
+46
+38
+33
+30
+28
Table 5-4-10-13: Icing Corrections to Landing Ground Roll - Flaps 0° - No Reverse Thrust -
Slope Correction (Table C)
Table C
Landing Weight (kg (lb))
Slope
Correction
(%)
2900
(6393)
3300
(7275)
3700
(8157)
4100
(9039)
4500
(9921)
4% down
-7
-7
-6
-7
-6
2% down
-3
-3
-3
-2
-2
No Slope
0
0
0
0
0
2% up
+6
+6
+6
+6
+6
4% up
+12
+11
+11
+11
+10
Section 5 - Performance (EASA Approved)
Flight in Icing Conditions - Landing Performance
Pilot's Operating Handbook
Report No: 02406
Issue date: Mar 06, 2020
Page 5-4-10-6
12-C-A15-60-0504-10A-030A-A
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GENERAL
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