Table 5-4-10-17: Icing Corrections to Landing Ground Roll - Flaps 15° - 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)
84
90
95
100
105
0 ft
+55
+52
+49
+50
+50
2000 ft
+53
+50
+50
+50
+50
4000 ft
+52
+50
+50
+50
+51
6000 ft
+50
+50
+50
+50
+51
8000 ft
+50
+50
+51
+51
+51
10000 ft
+50
+50
+51
+51
+51
12000 ft
+50
+51
+51
+51
+52
14000 ft
+50
+51
+51
+52
+52
Table 5-4-10-18: Icing Corrections to Landing Ground Roll - Flaps 15° - 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
-7
-7
-7
-6
-6
No Wind
0
0
0
0
0
10 kt Headwind
+5
+5
+4
+4
+4
20 kt Headwind
+12
+10
+9
+8
+8
30 kt Headwind
+21
+18
+15
+14
+13
Table 5-4-10-19: Icing Corrections to Landing Ground Roll - Flaps 15° - With Reverse Thrust -
Slope Correction (Table C)
Table C
Landing Weight (kg (lb))
Slope Correction (%)
2900 - 4500
(6393 - 9921)
4% down
-2
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 5-4-10-8
12-C-A15-60-0504-10A-030A-A
FOR
GENERAL
AND
FAMILIARIZATION
PURPOSES
ONLY
