Table 5-4-10-23: Icing Corrections to Landing Ground Roll - Flaps 0° - With Reverse Thrust -
Altitude 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
+103
+99
+96
+97
+98
2000 ft
+101
+97
+97
+98
+98
4000 ft
+99
+97
+98
+99
+99
6000 ft
+97
+98
+99
+99
+100
8000 ft
+98
+99
+100
+101
+102
10000 ft
+98
+100
+101
+102
+104
12000 ft
+99
+100
+102
+103
+105
14000 ft
+100
+102
+104
+106
+105
Table 5-4-10-24: Icing Corrections to Landing Ground Roll - Flaps 0° - With 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
-14
-13
-13
-13
-12
No Wind
0
0
0
0
0
10 kt Headwind
+11
+9
+8
+8
+7
20 kt Headwind
+24
+21
+18
+17
+16
30 kt Headwind
+42
+36
+31
+29
+27
Table 5-4-10-25: Icing Corrections to Landing Ground Roll - Flaps 0° - With Reverse Thrust -
Slope Correction (Table C)
Table C
Landing Weight (kg (lb))
Slope Correction (%)
2900 - 4500
(6393 - 9921)
4% down
-6
2% down
-3
No Slope
0
2% up
+4
4% up
+8
Section 5 - Performance (EASA Approved)
Flight in Icing Conditions - Landing Performance
Pilot's Operating Handbook
Report No: 02406
Issue date: Mar 06, 2020
Page 5-4-10-10
12-C-A15-60-0504-10A-030A-A
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