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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
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
table below), use FLAP 3
for landing.
In all cases, if landing configuration is different from FLAP FULL, use 1+F for
go-around.
Note: At very high weights, VFE CONF1 is close to VLS clean. To select CONF1,
deselect A/THR,
decelerate to (or slightly below) VLS and select CONF1 when below VFE. When
established at
CONF1, the crew can re-engage the A/THR and use managed speed again
LDG
DIST................................................................................................................................
.......... CHECK
PACK 1 and 2..........................................................................................................OFF
or supplied by APU
Selecting packs OFF (or supplied from APU) will increase the maximum thrust
available from the engines
in the event of a go-around.
�� In the final approach stages
TARGET
SPEED..............................................................................................................................
VLS
Reduce the selected speed on the FCU to reach VLS at runway threshold.
Touch down as smoothly as possible (Maximum V/S at touchdown 360 ft/min ).
�� At main landing gear touchdown
REVERSE THRUST............................................................................................. USE
MAX AVAILABLE
�� After nosewheel touchdown
BRAKES............................................................................................................APPLY
AS NECESSARY
Maximum braking may be used after nose wheel touchdown. But, if landing distance
permits, delay or
reduce braking to fully benefit from the available runway length.
�� Landing complete
BRAKE FANS
�� ...............................................................................................................................ON
Be prepared for tire deflation, if temperatures exceed 800 °C.
MAXIMUM WEIGHT FOR GO AROUND IN CONF 3 (1000 kg)
　
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