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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 87 83 79 74 70 65 60 55
15 87 83 79 74 69 64 59 54
20 87 83 79 73 67 62 57 53
25 87 83 76 70 65 60 55
30 87 80 74 68 63
35 84 77 71 65 60
40 80 74 68 63
45 77 71 65
50 74 68
55
ABN-80
10/32
AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1
ABNORMAL AND
EMERGENCY PROCEDURES 30 AUG 10
A318/A319/A320/A321 FLEET MSN 4617
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..............................................................................................................
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
to ABN-70-A ENG
ALL ENG FLAME OUT - FUEL REMAINING - ENGINE RELIGHT ATTEMPT to
get the required pitch
altitude for optimum relight speed.
In case of engine failure, switch off the wiring anti-ice before engine start.
Note: If sufficient visibility is not granted for approach due to windshield/window
damage, consider
AUTOLAND. If AUTOLAND is not available, consider opening the sliding window
on the PF's
side, after cabin depressurization.
�� To manually depressurize the cabin:
CAB PRESS MODE
SEL................................................................................................... MAN
MAN V/S
CTL..............................................................................................................FULL UP
Due to the increased noise level, pay particular attention to visual warnings.
ABN-80
11/32
AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1
ABNORMAL AND
EMERGENCY PROCEDURES 30 AUG 10
A318/A319/A320/A321 FLEET MSN 4617
WINDSHEAR
A red flag “WINDSHEAR” is displayed on each PFD associated with an aural
synthetic voice
“WINDSHEAR” repeated three times.
If windshear is detected by pilot observation, apply the following recovery technique:
　
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