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.......... 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 83 81 78 74 71 66 62 58
15 83 81 78 74 71 66 62 58
20 83 81 78 74 71 66 61 56
25 83 81 78 74 70 64 59
30 83 81 78 73 67
35 83 81 76 70 65
40 83 80 73 67
45 82 76 70
50 79 73
55
ABN-80
9/32
AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1
ABNORMAL AND
EMERGENCY PROCEDURES 30 AUG 10
A318/A319/A320/A321 FLEET MSN 4566
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
PACK
FLOW..............................................................................................................................
.................HI
APU.................................................................................................................................
....................START
ENGINE
PARAMETERS...............................................................................................................
..MONITOR
AIRSPEED
INDICATIONS..............................................................................................................
MONITOR
If airspeed is unreliable or lost, Refer to ABN-34-C UNRELIABLE SPEED
INDICATION/ADR CHECK
PROC - Memory Items If both engines flame out and speed indications are lost, Refer
　
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