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OPERATING SPEEDS (KT)
CG ≥ 25 %
W (1000 KG) F S Green dot
FL < 200(1) VLS CONF 3 VREF
40 117 152 160 109 106
44 122 159 168 114 111
48 128 166 176 119 116
52 133 173 184 124 121
56 138 179 192 128 125
60 143 185 200 133 129
64 148 192 208 137 134
68 152 197 216 142 138
72 157 203 224 146 142
76 161 209 232 150 146
78 163 211 236 152 147
(1) Above FL 200 add 1 kt per additional 1 000 ft.
For CG < 25 % add 2 kt to VLS and VREF
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A318/A319/A320/A321 FLEET , , MSN 4473
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SPEEDS
SPEEDS
OPERATING SPEEDS (KT)
W (1000 KG) F S Green dot FL < 200(1) VLS CONF 3 VREF
52 130 168 188 121 116
54 133 171 191 123 119
56 135 174 194 125 121
58 137 177 197 128 123
60 140 180 200 130 125
62 142 183 203 132 127
64 144 186 206 134 129
66 147 189 209 136 131
68 149 192 212 138 133
70 151 195 215 140 135
72 153 197 218 142 137
74 155 200 221 144 139
76 157 203 224 146 141
78 159 205 227 148 143
80 161 208 230 150 144
82 163 211 233 152 146
84 165 213 236 154 148
86 167 216 239 156 150
(1) Above FL 200 add 1 kt per additional 1 000 ft.
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VAPP DETERMINATION
The FMGS performs the following VAPP computation for landing in normal
configuration (CONF 3 or CONF
FULL).
Note: FOR CG < 25 %, add 2 kt to VLS CONF FULL and VLS CONF 3.
1. The 5 kt increment is required when the A/THR is used, or when an autoland is
performed.
2. In case of ice accretion, Vapp must not be lower than:
‐ VLS + 5 kt in CONF FULL
‐ VLS + 10 kt in CONF 3
In case of strong or gusty crosswind greater than 20 kt, Vapp should be at least VLS +
5 kt. The 5 kt
increment above VLS may be increased up to 15 kt at the flight crew’s discretion.
LANDING DISTANCE WITHOUT AUTOBRAKE - CONF 3
The actual landing distance is the distance to come to a complete stop from a point 50
ft above the landing
surface. No margin is included in this distance.
CONFIGURATION 3
ACTUAL LANDING DISTANCE (METERS)
WEIGHT (1000 KG) 46 50 54 58 62 66 70 74 78
DRY 750 780 820 860 910 1000 1100 1200 1290
WET 1020 1090 1160 1240 1320 1400 1480 1570 1650
STANDING
WATER 1340 1430 1540 1660 1790 1930 2060 2200 2310
SLUSH 1300 1390 1470 1560 1650 1760 1890 2010 2110
COMPACTED
SNOW 1300 1380 1460 1540 1620 1700 1780 1850 1910
RUNWAY
CONDITION COVERED
WITH
ICE 2970 3110 3260 3410 3560 3720 3880 4040 4170
CORRECTIONS
CORRECTION ON ACTUAL LANDING DISTANCE
runway covered with
dry runway wet
runway standing water slush compacted
snow ice
per 1 000 ft above SL +3 % +4 % +4 % +5 % +3 % +4 %
per 10 kt headwind No correction for headwind due to wind correction on approach
speed
per 10 kt tailwind +18 % +21 % +24 % +22 % +17 % +29 %
To be continued on next page
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Continued from previous page
CORRECTION ON ACTUAL LANDING DISTANCE
runway covered with
dry runway wet
runway standing water slush compacted
snow
ice
forward C.G. +2 % +3 % +3 % +3 % +3 % +3 %
2 reversers operative -3 % -9 % -12 % -11 % -9 % -26 %
Per 5 kt speed increment (and no failure) add 8 % (all runways)
Note: THE ABOVE DISTANCES ARE ‐ GIVEN FOR USE IN FLIGHT
‐ BEFORE DEPARTURE Refer to FCOM/PER-LND-ILD-ALD
CONFIGURATION 3.
EXAMPLE: Actual Landing Distance (ALD) calculation with multiple corrections
Data: LW = 62 000 kg
Pressure altitude = 2 000 ft
Approach speed = VLS +5 kt
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空客320快速检查单QRH QUICK REFERENCE HAND BOOK10(100)
