Landing Runway Limit Charts
FLAPS 28.
ELEV 6,001’ - 7,500’ DRY RUNWAY
Max Landing Weight in 1000 Lbs. (-217 & -217A)
Runway Length Feet Anti-Skid On Anti-Skid Off
Auto Spoilers Manual Spoilers Auto Spoilers Manual Spoilers
0 Wind -10 Wind
5,001 -6,000 102.3 82.5 88.8 NA NA
6,001 -7,000 130.0 109.7 117.6 NA NA
7,001 -8,000 130.0 130.0 130.0 94.7 87.1
8,001 -9,000 130.0 130.0 130.0 110.9 103.3
9,001 - 10,000 130.0 130.0 130.0 127.1 119.5
10,001 - 11,000 130.0 130.0 130.0 130.0 130.0
11,001 - 12,000 130.0 130.0 130.0 130.0 130.0
600 lbs. may be added per knot of headwind
Note: Structural weight limitations must be observed.
FLAPS 28.
ELEV 6,001’ - 7,500’ WET RUNWAY
Max Landing Weight in 1000 lbs. (-217 & -217A)
Runway Length Feet Anti-Skid On Anti-Skid Off
Auto Spoilers Manual Spoilers Auto Spoilers Manual Spoilers
0 Wind -10 Wind
5,001 -6,000 83.5 NA NA NA NA
6,001 -7,000 108.6 88.4 96.8 NA NA
7,001 -8,000 130.0 112.1 121.9 NA NA
8,001 -9,000 130.0 130.0 130.0 94.0 87.4
9,001 - 10,000 130.0 130.0 130.0 108.1 101.5
10,001 - 11,000 130.0 130.0 130.0 122.2 115.6
11,001 - 12,000 130.0 130.0 130.0 130.0 129.7
600 lbs. may be added per knot of headwind
ABNORMAL
V-Speeds for Abnormal Landings
ABNORMAL CONFIGURATION ARRIVAL AND V/REF SPEEDS
WT. 1000 LB. Maneuver V/REF
15./RET 0./RET 0./TO 11./TO 15./TO 28./RET 40./RET
90 163 162 137 122 120 141 131
92 165 164 139 124 122 142 133
94 166 166 140 125 123 144 134
96 168 168 142 126 124 145 136
98 170 170 143 128 126 147 137
100 172 171 145 129 127 148 138
102 173 173 146 130 128 150 140
104 175 175 148 131 129 151 141
106 177 176 149 133 131 153 142
108 178 178 150 134 132 154 144
110 180 180 152 135 133 156 145
112 182 181 153 136 134 157 147
114 184 183 155 138 136 158 148
116 185 185 156 139 137 160 149
118 187 186 157 140 138 161 150
120 188 188 159 141 139 163 152
122 190 189 160 142 140 164 153
124 191 191 161 143 141 165 154
126 193 192 163 145 142 167 155
128 194 194 164 146 144 168 157
130 196 195 165 147 145 169 158
132 197 197 166 148 146 171 159
134 199 198 168 149 147 172 160
Estimated Landing Distance Required (In Feet) For Various Flap/Slat Configurations
Flaps/ Slats Aircraft Gross Weight in 1,000 Pounds
90 100 110 120 130 140 150
40./Ext 2240 2400 2560 2720 2880 3040 3200
28./Ext 2340 2520 2680 2860 3040 3200 3380
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本文鏈接地址：MD-80 Flight Manual 麥道80飛行手冊 2(103)
