Table 5-4-10-2: Icing Corrections to Landing Total Distance - Flaps 15° - 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)
84
90
95
100
105
0 ft
+38
+41
+43
+45
+47
2000 ft
+39
+42
+44
+46
+48
4000 ft
+41
+44
+46
+48
+49
6000 ft
+42
+45
+47
+49
+50
8000 ft
+44
+46
+48
+50
+52
10000 ft
+45
+47
+50
+51
+53
12000 ft
+46
+49
+51
+52
+53
14000 ft
+48
+50
+52
+52
+52
Table 5-4-10-3: Icing Corrections to Landing Total Distance - 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
-5
-5
-5
-5
-5
No Wind
0
0
0
0
0
10 kt Headwind
+3
+3
+3
+3
+3
20 kt Headwind
+6
+6
+6
+6
+6
30 kt Headwind
+11
+10
+10
+10
+9
Table 5-4-10-4: Icing Corrections to Landing Total Distance - Flaps 15° - No Reverse Thrust -
Slope Correction (Table C)
Table C
Landing Weight (kg (lb))
Slope Correction (%)
2900 - 4500
(6393 - 9921)
4% down
+1
2% down
0
No Slope
0
2% up
0
4% up
0
Section 5 - Performance (EASA Approved)
Flight in Icing Conditions - Landing Performance
Pilot's Operating Handbook
Report No: 02406
Issue date: Mar 06, 2020
Page 5-4-10-3
12-C-A15-60-0504-10A-030A-A
FOR
GENERAL
AND
FAMILIARIZATION
PURPOSES
ONLY
