Table 5-4-10-8: Icing Corrections to Landing Total Distance - Flaps 0° - No 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
+86
+92
+97
+101
+104
2000 ft
+89
+94
+99
+103
+106
4000 ft
+93
+98
+103
+107
+110
6000 ft
+95
+100
+105
+109
+113
8000 ft
+99
+104
+109
+113
+118
10000 ft
+101
+107
+112
+116
+121
12000 ft
+104
+109
+115
+120
+120
14000 ft
+108
+114
+120
+119
+117
Table 5-4-10-9: Icing Corrections to Landing Total Distance - 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
-12
-11
-11
-11
-11
No Wind
0
0
0
0
0
10 kt Headwind
+7
+6
+6
+6
+6
20 kt Headwind
+15
+14
+14
+13
+13
30 kt Headwind
+25
+24
+23
+22
+21
Table 5-4-10-10: Icing Corrections to Landing Total Distance - 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
-2
-3
-4
-4
-3
2% down
-1
-1
-1
-1
-1
No Slope
0
0
0
0
0
2% up
+2
+2
+2
+2
+2
4% up
+3
+3
+3
+3
+3
Section 5 - Performance (EASA Approved)
Flight in Icing Conditions - Landing Performance
Pilot's Operating Handbook
Report No: 02406
Issue date: Mar 06, 2020
Page 5-4-10-5
12-C-A15-60-0504-10A-030A-A
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GENERAL
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