Table 5-4-10-14: Icing Corrections to Landing Total Distance - 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
+32
+36
+38
+40
+41
2000 ft
+34
+37
+39
+40
+42
4000 ft
+36
+38
+40
+42
+43
6000 ft
+37
+39
+41
+42
+44
8000 ft
+39
+41
+42
+44
+43
10000 ft
+40
+41
+43
+43
+45
12000 ft
+40
+42
+43
+45
+46
14000 ft
+42
+42
+45
+46
+47
Table 5-4-10-15: Icing Corrections to Landing Total Distance - Flaps 15° - With Reverse Thrust
- Wind Correction (Table B)
Table B
Landing Weight (kg (lb))
Wind Correction (%)
2900 - 4500
(6393 - 9921)
10 kt Tailwind
-5
No Wind
0
10 kt Headwind
+3
20 kt Headwind
+6
30 kt Headwind
+11
Table 5-4-10-16: Icing Corrections to Landing Total Distance - Flaps 15° - With Reverse Thrust
- Slope Correction (Table C)
Table C
Landing Weight (kg (lb))
Slope Correction (%)
2900 - 4500
(6393 - 9921)
4% down
0
2% down
0
No Slope
0
2% up
0
4% up
+1
Section 5 - Performance (EASA Approved)
Flight in Icing Conditions - Landing Performance
Pilot's Operating Handbook
Report No: 02406
Issue date: Mar 06, 2020
Page 5-4-10-7
12-C-A15-60-0504-10A-030A-A
FOR
GENERAL
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