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THRUST
LEVERS.........................................................................................................................
TOGA
SPEED BRAKES lever..........................................................................................
CHECK RETRACTED
BANK.............................................................................................................WINGS
LEVEL or ADJUST
�� When flight path is safe and the warning stops:
Decrease pitch attitude and accelerate.
�� When speed is above VLS, and vertical speed is positive:
Clean up aircraft as required.
�� “TERRAIN TERRAIN” “TOO LOW TERRAIN”:
Adjust the flight path or initiate a go-around.
�� "CAUTION TERRAIN" - "CAUTION OBSTACLE":
Adjust the flight path. Stop descent. Climb and/or turn, as necessary, based on
analysis of all available
instruments and information.
�� “SINK RATE” “DON’T SINK”:
Adjust pitch attitude and thrust to silence the alert.
�� “TOO LOW GEAR” - “TOO LOW FLAPS”:
Perform a go-around.
�� “GLIDE SLOPE”:
Establish the aircraft on the glideslope, or switch OFF the G/S mode pb-sw, if flight
below the
glideslope is intentional (non precision approach (NPA)).
ABN-34
5/10
AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1
ABNORMAL AND
EMERGENCY PROCEDURES 30 AUG 10
A318/A319/A320/A321 FLEET
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
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.
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......................................................................................................................
　
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