曝光臺(tái) 注意防騙 網(wǎng)曝天貓店富美金盛家居專營(yíng)店坑蒙拐騙欺詐消費(fèi)者

�� If the aircraft weight is above the maximum weight for circling in CONF 3 (given in the
table below):
The aircraft cannot maintain flight level with CONF 3 and landing gear down.
Delay gear extension.
Note: If the approach is flown at ‐ less than 750 ft RA, the warning “L/G NOT DOWN” will
be triggered. The pilot can cancel aural warning by pressing the EMER CANC pb
on the ECAM control panel.
‐ ”TOO LOW GEAR” warning is to be expected, if the landing gear is not downlocked
at 500 ft RA.
OAT AIRPORT ELEVATION (ft)
(°C) 0 2 000 4 000 6 000 8 000 10 000 12 000 14 000
0 230 220 212 204 198 188 178 158
5 230 220 212 204 198 188 176 158
10 230 220 212 204 198 184 170 158
15 230 220 212 204 192 178 158 154
20 230 220 212 200 186 172 158 148
25 230 220 206 192 178 158 154 142
30 230 214 198 186 172 158 148
35 220 206 192 178 158 154
40 212 198 184 172
45 204 190 176
50 196 182
55 186
MAXIMUM WEIGHT FOR CIRCLING IN CONF 3 (1000 kg)
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
OPERATING TECHNIQUES
A330/A340 FLEET PRO-ABN-10 P 12/18
FCOM 19 AUG 10
CIRCLING APPROACH WITH ONE ENGINE INOPERATIVE
Applicable to: ,
LANDING WEIGHT..................................................................................................................CHECK
�� If the aircraft weight is above the maximum weight for circling in CONF 3 (given in the
table below):
The aircraft cannot maintain flight level with CONF 3 and landing gear down.
Delay gear extension.
Note: If the approach ‐ is flown at less than 750 ft RA, the warning “L/G NOT DOWN” will
be triggered. The pilot can cancel aural warning by pressing the EMER CANC pb
on the ECAM control panel.
‐ ”TOO LOW GEAR” warning is to be expected, if the landing gear is not downlocked
at 500 ft RA.
OAT AIRPORT ELEVATION (ft)
(°C) 0 2 000 4 000 6 000 8 000 10 000 12 000 14 000
0 232 224 214 208 200 192 182 170
5 232 224 214 208 200 192 178 158
10 232 224 214 208 200 186 172 158
15 232 224 214 208 194 180 168 156
20 232 224 214 202 188 174 158 150
25 232 224 210 196 182 168 156 146
30 232 218 202 188 174 158 150
35 224 208 194 180 168 156
40 216 200 186 174
45 206 192 178
50 198 184
55 190
MAXIMUM WEIGHT FOR CIRCLING IN CONF 3 (1000 kg)
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
OPERATING TECHNIQUES
A330/A340 FLEET PRO-ABN-10 P 13/18
FCOM 19 AUG 10
LANDING WITH SLATS OR FLAPS JAMMED
Applicable to:
Determine landing configuration, according to the table Refer to 99 Duref Cible FCOM.
�� Repeat the following, until landing configuration is reached:
SPEED SEL ......................................................................................................VFE NEXT -5 KT
Decelerate towards VFE NEXT -5 kt, but not below VLS. In case of turbulence, to avoid VFE
exceedance, the pilot may decide to decelerate to a lower speed, but not below VLS.
Note: The autopilot may be used down to 500 ft AGL. As it ‐ is not tuned for abnormal
configurations, its behavior can be less than optimum and must be monitored.
‐ Approach with A/THR and selected speed is recommended.
‐ OVERSPEED warning and VLS, displayed on the PFD, are computed according to
the actual flap/slats position.
‐ VFE and VFE NEXT are displayed on PFD, according to the FLAPS lever position.
If not displayed, use the placard speeds.
‐ If VLS is greater than VFE NEXT (overweight landing case), the FLAPS lever
can be set in the required next position, while the speed is reduced to follow VLS
reduction as surfaces extend. The VFE warning threshold should not be triggered.
In this case, disconnect the A/THR. A/THR can be reengaged when the landing
configuration is established.
As speed reduces through VFE NEXT:
FLAPS LEVER................................................................................................ONE STEP DOWN
�� When landing configuration is established:
DECELERATE TO CALCULATED APPROACH SPEED IN FINAL APPROACH
FOR GO AROUND
The table (See below) provides the MAX SPEEDS for abnormal configurations.
�� IF SLATS FAULT:
�� FOR CIRCUIT:
MAINTAIN SLATS/FLAPS CONFIGURATION
Recommended speed: MAX SPEED -10 KT.
�� FOR DIVERSION:
SELECT CLEAN CONFIGURATION
�� If SLATS jammed at 0:
Normal operating speeds.
To be continued on next page
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
　
中國(guó)航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A330/A340機(jī)組操作手冊(cè) FLIGHT CREW OPERATING MANUAL FCOM 6(118)