Table 5-4-10-20: Icing Corrections to Landing Total Distance - 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
+77
+84
+88
+91
+94
2000 ft
+80
+86
+89
+93
+95
4000 ft
+84
+89
+92
+95
+98
6000 ft
+86
+90
+94
+97
+99
8000 ft
+89
+93
+96
+99
+99
10000 ft
+91
+95
+98
+98
+103
12000 ft
+93
+96
+97
+102
+105
14000 ft
+95
+95
+102
+105
+107
Table 5-4-10-21: Icing Corrections to Landing Total Distance - 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
-13
-13
-14
-14
-9
No Wind
0
0
0
0
0
10 kt Headwind
+6
+6
+6
+6
+6
20 kt Headwind
+14
+14
+14
+13
+13
30 kt Headwind
+24
+23
+23
+22
+21
Table 5-4-10-22: Icing Corrections to Landing Total Distance - Flaps 0° - With Reverse Thrust -
Slope Correction (Table C)
Table C
Landing Weight (kg (lb))
Slope Correction (%)
2900 - 4500
(6393 - 9921)
4% down
-3
2% down
-1
No Slope
0
2% up
+2
4% up
+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 5-4-10-9
12-C-A15-60-0504-10A-030A-A
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