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F
BRAKES ON ACCU ONLY
AFTER LANDING
�� When aircraft has stopped:
PARKING
BRK...............................................................................................................................
ON
ATC
(VHF1)............................................................................................................................
NOTIFY
FIRE pushbutton (ENG and
APU)...............................................................................................PUSH
AGENTS (ENG and
APU)..........................................................................................................DISCH
�� If Evacuation required:
EVACUATION................................................................................................................
...INITIATE
�� If Evacuation not required:
CABIN CREW and PASSENGERS
(PA)...........................................................................NOTIFY
ABN-80
8/32
AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1
ABNORMAL AND
EMERGENCY PROCEDURES 30 AUG 10
A318/A319/A320/A321 FLEET
EMER DESCENT
IMMEDIATE ACTION
CREW OXY
MASKS...........................................................................................................................
..ON
SIGNS.............................................................................................................................
...................... ON
The recommendation is to descend with the AP engaged :
‐ Turn the ALT selector knob and pull
‐ Turn the HDG selector knob and pull
‐ Adjust the target SPD/MACH.
THR LEVERS(if A/THR not
engaged)................................................................................................. IDLE
‐ If autothrust is engaged, check that THR IDLE is displayed on the FMA.
‐ If not engaged, retard the thrust levers.
SPD
BRK.................................................................................................................................
..........FULL
Extension of the speedbrakes will significantly increase Vls.
To avoid AP disconnection and automatic retraction of the speedbrakes, due to
possible activation of
Angle-of-Attack protection, allow the speed to increase before starting to use the
speedbrakes.
WHEN DESCENT ESTABLISHED
EMER DESCENT FL100, or minimum allowable altitude.
SPEED.......................................................................................................................
MAX/APPROPRIATE
CAUTION Descend at the maximum appropriate speed. If structural damage is
suspected, use the
flight controls with care and reduce speed as appropriate.
Landing gear may be extended below 2 500 ft. In such a case, speed must be reduced
to VLO/VLE.
Note: The recommendation is to descend with the autopilot engaged.
Use of the autopilot is also permitted in EXPEDITE mode ��
ENG MODE
SEL.................................................................................................................................
IGN
ATC.................................................................................................................................
...............NOTIFY
To save oxygen, set the oxygen diluter selector to the N position. If the oxygen diluter
selector remains
at 100 %, the quantity of oxygen may not be sufficient for the entire emergency
descent profile.
MAX
FL....................................................................................................................................
....100/MEA
�� IF CAB ALT > 14 000 ft:
PAX OXY
MASKS...................................................................................................................MAN
ON
Contact the cabin crew to confirm that the passenger oxygen masks are released.
ABN-80
9/32
AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1
ABNORMAL AND
EMERGENCY PROCEDURES 30 AUG 10
A318/A319/A320/A321 FLEET
OVERWEIGHT LANDING
Automatic landing is certified up to the Maximum Landing Weight (MLW). Autoland
flight tests have,
however, been successful up to 69 t .
Depending on the situation (e.g. emergency or other) and provided that the runway is
approved for
automatic landing, the flight crew can decide to perform an autoland up to 69 t .
LDG
CONF............................................................................................................................
AS REQUIRED
Use the ECAM flap setting, if required for abnormal operations. In all other cases :
FULL is preferred for ‐ optimized landing performance.
‐ If the aircraft weight is above the maximum weight for go-around (given in the
　
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