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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 71 69 68 65 63 61 59 56
15 71 69 68 65 63 61 59 56
20 71 69 68 65 63 61 59 55
25 71 69 68 65 63 61 58 54
30 71 69 68 65 63 61 57
35 71 69 68 65 63
40 71 69 68 65
45 71 69 68
50 71 69
55
ABN-80
11/32
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
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
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
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空客320快速检查单QRH QUICK REFERENCE HAND BOOK5(92)
