曝光台 注意防骗
网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者
Do not maneuver based on a TA alone.
Attempt to see the reported traffic.
Resolution advisory : All “CLIMB” and “DESCEND” or “MAINTAIN
VERTICAL SPEED
MAINTAIN” or “ADJUST VERTICAL SPEED ADJUST” or “MONITOR
VERTICAL SPEED” type
messages
AP (if
engaged)..........................................................................................................................
...... OFF
BOTH
FDs..................................................................................................................................
...... OFF
Respond promptly and smoothly to an RA by adjusting or maintaining the vertical
speed, as required,
to reach the green area and/or avoid the red area of the vertical speed scale.
Note: Avoid excessive maneuvers while aiming to keep the vertical speed just outside
the red area
of the VSI, and within the green area. If necessary, use the full speed range between
Vαmax
and VMAX.
Respect stall, GPWS, or windshear warning.
Notify ATC.
When “CLEAR OF CONFLICT” is announced:
Resume normal navigation in accordance ‐ with ATC clearance.
‐ AP/FD can be re-engaged as desired.
GO AROUND procedure must be performed when an RA “CLIMB” or
“INCREASE CLIMB” is
triggered on final approach:
Note: Resolution Advisories (RA) are inhibited below 900 ft.
UNRELIABLE SPEED INDICATION/ADR CHECK PROC - MEMORY
ITEMS
If the safe conduct of the flight is impacted:
MEMORY ITEMS
AP/FD..............................................................................................................................
................ OFF
A/THR.............................................................................................................................
.................OFF
PITCH/THRUST:
Below THRUST RED
ALT................................................................................................ 15°/TOGA
Above THRUST RED ALT and Below FL
100.....................................................................10°/CLB
Above THRUST RED ALT and Above FL
100...................................................................... 5°/CLB
FLAPS............................................................................................................. Maintain
current CONFIG
SPEEDBRAKES..............................................................................................................
Check retracted
L/G..................................................................................................................................
................... UP
GPS
ALTITUDE..................................................................................................................
Display on MCDU
PROBE WINDOW
HEAT...........................................................................................................................O
NT
o be continued on next page
ABN-34
6/6
AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1
ABNORMAL AND
EMERGENCY PROCEDURES 30 AUG 10
A318/A319/A320/A321 FLEET , , , , , MSN,,
UNRELIABLE SPEED INDICATION/ADR CHECK PROC - MEMORY
ITEMS (Cont'd)
AFFECTED ADR(S) IDENTIFICATION
Crosscheck all speeds and altitudes indications.
Alternates sources may be used to evaluate the air data:
‐ GPS altitude
‐ GPS and IRS Group Speeds, taking into account altitude and wind effect.
If affected ADR(s) identified:
Affected ADR(s)
P/B.......................................................................................................................OFF
REMAINING AIR
DATA........................................................................................................ CONFIRM
If affected ADR(s) cannot be identified or all ADRs are affected:
ALL ADRs
P/B..............................................................................................................................OF
F
All ADRs must be switched off to replace the PFD's normal speed scale and altitude
indication by
the backup speed scale and GPS altitude indication.
NAV ADR 1+2+3 FAULT
ABN-34
1/6
AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1
ABNORMAL AND
EMERGENCY PROCEDURES 30 AUG 10
A318/A319/A320/A321 FLEET MSN
ADR 1 + 2 + 3 FAULT
The ECAM does not display this procedure. In the case of a triple ADR failure, the
ECAM only displays
dual ADR warnings.
ADR
(all)..................................................................................................................................
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：
空客320快速检查单QRH QUICK REFERENCE HAND BOOK4(9)
