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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)
OAT °C AIRPORT ELEVATION (FT)
0 2 000 4 000 6 000 8 000 10 000 12 000 14 000
<10 89 85 81 77 72 67 61 56
15 89 85 81 77 71 65 59 54
20 88 84 81 75 69 63 57 52
25 88 84 79 73 67 61 56 50
30 87 81 76 70 64 59 54
35 84 78 73 67 62
40 81 75 69 64
45 76 70 65
50 72 67
55
ABN-80
10/32
AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1
ABNORMAL AND
EMERGENCY PROCEDURES 30 AUG 10
A318/A319/A320/A321 FLEET
TAILSTRIKE
In the event of a tailstrike, apply the following procedure:
LAND ASAP
MAX
FL....................................................................................................................................
...100 or MSA
500 ft/min should be targeted for the climb, to minimize pressure changes, and for
passenger and crew
comfort. Similarly, the rate of descent must be limited to about 1 000 ft/min , except
for the final approach
that must be performed normally.
Notify the ATC of the aircraft’s rate of climb.
RAM
AIR..................................................................................................................................
................. ON
PACK 1 and
2.......................................................................................................................................
..OFF
VOLCANIC ASH ENCOUNTER
Accomplish the following, while making a 180 ° turn.
ATC.................................................................................................................................
...................NOTIFY
A/THR.............................................................................................................................
.........................OFF
THRUST (conditions
permitting)...................................................................................................DECREASE
CREW OXYGEN
MASKS...............................................................................................................
ON/100 %
CABIN
CREW.............................................................................................................................
...... NOTIFY
ENG ANTI
ICE..................................................................................................................................
........ON
WING ANTI
ICE..................................................................................................................................
......ON
ECON
FLOW..............................................................................................................................
.............OFF
APU.................................................................................................................................
....................START
ENGINE
PARAMETERS...............................................................................................................
..MONITOR
AIRSPEED
INDICATIONS..............................................................................................................
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空客320快速检查单QRH QUICK REFERENCE HAND BOOK9(14)
