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MODE
SELECTOR......................................................................................................................
.............ATT
ALIGN light on for 30 s.
ATT MODE displayed on CDU.
LEVEL A/C
ATTITUDE......................................................................................................................
... HOLD
CONSTANT A/C
SPEED................................................................................................................
MAINTAIN
DISPLAY SYS
switch...........................................................................................................
AFFECTED SYS
DISPLAY DATA
switch..........................................................................................................................
HDG
�� MCDU INITIALIZATION:
DATA (MCDU
KEY).......................................................................................................................PRES
ST
he DATA INDEX page is displayed.
IRS MONITOR (2L
KEY)...............................................................................................................PRESS
The IRS MONITOR page is displayed.
A/C
HEADING........................................................................................................................
...... ENTER
The flight crew must enter the heading in the SET HDG field (5R KEY).
�� CDU INITIALIZATION:
Depending on the CDU keyboard installed, an “H” may be written on the “5” key:
�� If “H” is written on the “5” key:
H KEY.................................................................................................................................
.. PRESS
Degree marker, 0 decimal point, ENT and CLR lights come on.
A/C
HEADING........................................................................................................................
ENTER
�� If “H” is not written on the “5” key:
A/C
HEADING........................................................................................................................
ENTER
Enter aircraft's magnetic heading on the CDU keyboard. Then, press the ENT key to
enter data.
Example : To enter heading 320 °, dial 3, 2, 0, 0 then press ENT.
Heading will be displayed on the associated ND.
“HDG–ATT MODE” will be displayed on CDU.
Due to IR drift, magnetic heading has to be periodically crosschecked with standby
compass if
required.
ABN-34
5/10
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.............................................................................................................................
　
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