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...... ENTER
The flight crew must enter the heading in the SET HDG field (5R KEY).
ABN-34
8/12
AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1
ABNORMAL AND
EMERGENCY PROCEDURES 30 AUG 10
A318/A319/A320/A321 FLEET
TCAS WARNINGS
�� Traffic advisory: “TRAFFIC” messages:
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
�� When at, or above MSA or Circuit Altitude:
‐ Level off for troubleshooting
GPS
ALTITUDE..................................................................................................................
Display on MCDU
To be continued on next page
ABN-34
9/12
AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1
ABNORMAL AND
EMERGENCY PROCEDURES 30 AUG 10
A318/A319/A320/A321 FLEET
UNRELIABLE SPEED INDICATION/ADR CHECK PROC - MEMORY
ITEMS (Cont'd)
WHEN FLIGHT PATH IS STABILIZED
PROBE/WINDOW
HEAT........................................................................................................................ ON
TECHNICAL RECOMMENDATIONS:
‐ Respect Stall Warning
‐ To monitor speed, refer to IRS Ground Speed, or GPS Ground Speed variations
�� If remaining altitude indication is unreliable:
‐ Do not use FPV and/or V/S, which are affected.
‐ ATC altitude is affected. Notify the ATC.
‐ Refer to GPS altitude: altitude variations may be used to control level flight, and is
an altitude
cue.R ‐ efer to Radio Altimeter.
CAUTION If the failure is due to radome destruction, the drag will increase and
therefore N1
must be increased by 5 %. Fuel flow will increase by about 27 %.
AFFECTED ADR IDENTIFICATION:
Crosscheck all speed indications and Refer to FPE-SPD Speeds
�� If at least one ADR is reliable:
Faulty
ADR(s).............................................................................................................................
OFF
REMAINING AIR
DATA.................................................................................................... CONFIRM
　
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