Table 5-4-10-5: Icing Corrections to Landing Ground Roll - Flaps 15° - 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)
84
90
95
100
105
0 ft
+64
+59
+56
+57
+58
2000 ft
+61
+57
+57
+58
+59
4000 ft
+59
+56
+58
+59
+60
6000 ft
+56
+57
+58
+59
+60
8000 ft
+57
+58
+59
+61
+62
10000 ft
+57
+59
+60
+61
+63
12000 ft
+58
+59
+61
+62
+64
14000 ft
+59
+61
+62
+64
+65
Table 5-4-10-6: Icing Corrections to Landing Ground Roll - Flaps 15° - 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
-7
-7
-6
-5
-5
No Wind
0
0
0
0
0
10 kt Headwind
+6
+5
+4
+4
+4
20 kt Headwind
+14
+11
+9
+9
+8
30 kt Headwind
+23
+19
+16
+15
+14
Table 5-4-10-7: Icing Corrections to Landing Ground Roll - Flaps 15° - No 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
+4
Section 5 - Performance (EASA Approved)
Flight in Icing Conditions - Landing Performance
Pilot's Operating Handbook
Report No: 02406
Issue date: Mar 06, 2020
Page 5-4-10-4
12-C-A15-60-0504-10A-030A-A
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