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...... ENTER
Enter aircraft magnetic heading on CDU keyboard. Then press 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 and
updated if required.
IR ALIGNMENT IN ATT MODE
If IR alignment is lost, the navigation mode is inoperative (red ATT flag on PFD and
red HDG flag on ND).
Aircraft attitude and heading may be recovered by applying the following procedure.
Aircraft must stay level with constant speed during 30 s.
MODE
SELECTOR......................................................................................................................
.............ATT
LEVEL A/C
ATTITUDE......................................................................................................................
... HOLD
CONSTANT A/C
SPEED................................................................................................................
MAINTAIN
�� 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).
ABN-34
6/10
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.............................................................................................................................
.................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..................................................................................................................................
　
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