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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
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: For weights greater than 68 000 kg (or 150 000 lb ) S speed is greater than VFE
CONF 2
(200 kt ). Consequently the crew must select on FCU a speed below 200 kt before
setting
FLAPS 2. When in FLAPS 2, the crew can 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)
OAT °C AIRPORT ELEVATION (FT)
0 2 000 4 000 6 000 8 000 10 000 12 000 14 000
<10 75 73 71 69 66 63 60 57
15 75 73 71 69 66 63 60 57
20 75 73 71 69 66 63 60 56
25 75 73 71 69 66 63 58
30 75 72 71 68 65 60 55
35 74 72 70 67 62 57
40 74 72 69 64
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空客320快速检查单QRH QUICK REFERENCE HAND BOOK7(14)