曝光台 注意防骗
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knots (225 MPH). Tire fuseplug release limits occur when Brake
Kinetic Energy (BKE) for a maximum effort landing (full brake
application at touchdown) exceeds 57 MFP, making fuseplug release
possible. If brake application is delayed following touchdown, the
resulting lower level of BKEs can be determined from GIV Airplane
Flight Manual Appendix C, GIV-SP Brake Kinetic Energy and Carbon
Brake Cooling.
Limits shown in the charts that follow are conservative in nature and
represent a combination of worst-case conditions, i.e., maximum
temperature at a given altitude plus a 2% downhill runway slope.
These limits apply to a nil or headwind condition only.
NOTE: All speeds shown are KCAS.
Weight = 45000 LB Normal
Flaps 39°
Abnormal
Flaps 20°
Abnormal
Flaps 10°
Abnormal
Flaps UP
Altitude F39°
Shake
F39°
Push VAPP VREF VAPP VREF VAPP VREF VAPP VREF
0 101 95 133 123 136 126 141 131 149 139
2000 101 95 133 123 136 126 142 132 149 139
4000 101 95 133 123 137 127 143 133 151 141
6000 102 95 134 124 138 128 144 134 152 142
8000 103 96 135 125 139 129 146 136 154 144
10000 104 97 136 126 141 131 147 137 156 146
12000 105 98 137 127 142 132 149 139 158 148
14000 106 99 139 129 143 133 150 140 160 150
15000 107 100 139 129 144 134 151 141 161 151
CAUTION: Fuseplug Release Possible
With Max. Braking
CAUTION: Tire Speed Limit
Quick Reference Handbook
REVISION 7 GIV-SP PERFORMANCE
May 30/02 (GIV-SP AIRPLANES ONLY) Page PC - 3
GIV-SP Landing Speed Schedule, ctd… AFM 5.11
NOTES:
1. See the explanatory text presented on page PC-2 of this section.
2. All speeds shown are KCAS.
Weight = 50000 LB Normal
Flaps 39°
Abnormal
Flaps 20°
Abnormal
Flaps 10°
Abnormal
Flaps UP
Altitude F39°
Shake
F39°
Push VAPP VREF VAPP VREF VAPP VREF VAPP VREF
0 107 100 140 130 143 133 149 139 157 147
2000 107 100 140 130 143 133 149 139 157 147
4000 107 100 140 130 144 134 150 140 158 148
6000 107 100 140 130 145 135 151 141 160 150
8000 108 101 142 132 147 137 153 143 162 152
10000 109 102 143 133 148 138 155 145 164 154
12000 111 103 144 134 149 139 156 146 166 156
14000 112 104 146 136 151 141 158 148 168 158
15000 112 105 146 136 152 142 159 149 170 160
CAUTION: Fuseplug Release Possible
With Max. Braking
CAUTION: Tire Speed Limit
Weight = 55000 LB Normal
Flaps 39°
Abnormal
Flaps 20°
Abnormal
Flaps 10°
Abnormal
Flaps UP
Altitude F39°
Shake
F39°
Push VAPP VREF VAPP VREF VAPP VREF VAPP VREF
0 112 105 146 136 149 139 155 145 164 154
2000 112 105 146 136 149 139 155 145 164 154
4000 112 105 146 136 150 140 157 147 166 156
6000 113 105 147 137 152 142 158 148 168 158
8000 114 106 148 138 153 143 160 150 170 160
10000 115 107 149 139 154 144 162 152 172 162
12000 116 108 151 141 156 146 163 153 174 164
14000 117 110 152 142 158 148 165 155 176 166
15000 118 110 153 143 158 148 166 156 177 167
CAUTION: Fuseplug Release Possible
With Max. Braking
CAUTION: Tire Speed Limit
Quick Reference Handbook
GIV-SP PERFORMANCE REVISION 7
Page PC - 4 (GIV-SP AIRPLANES ONLY) May 30/02
GIV-SP Landing Speed Schedule, ctd… AFM 5.11
NOTES:
1. See the explanatory text presented on page PC-2 of this section.
2. All speeds shown are KCAS.
Weight = 60000 LB Normal
Flaps 39°
Abnormal
Flaps 20°
Abnormal
Flaps 10°
Abnormal
Flaps UP
Altitude F39°
Shake
F39°
Push VAPP VREF VAPP VREF VAPP VREF VAPP VREF
0 117 109 152 142 156 146 162 152 171 161
2000 117 109 152 142 156 146 162 152 171 161
4000 117 109 152 142 157 147 163 153 173 163
6000 118 110 153 143 158 148 165 155 175 165
8000 119 111 154 144 160 150 167 157 177 167
10000 120 112 156 146 161 151 168 158 179 169
12000 121 113 157 147 163 153 170 160 181 171
14000 123 114 159 149 164 154 172 162 184 174
15000 123 115 160 150 165 155 173 163 185 175
CAUTION: Fuseplug Release Possible
With Max. Braking
CAUTION: Tire Speed Limit
Weight = 65000 LB Normal
Flaps 39°
Abnormal
Flaps 20°
Abnormal
Flaps 10°
Abnormal
Flaps UP
Altitude F39°
Shake
F39°
Push VAPP VREF VAPP VREF VAPP VREF VAPP VREF
0 122 114 158 148 162 152 168 158 178 168
2000 122 114 158 148 162 152 168 158 178 168
4000 122 114 158 148 163 153 169 159 179 169
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湾流4快速检查单QRH GULFSTREAM IV QUICK REFERENCE HANDBOOK 2(5)
