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CABIN OVERPRESSURE
Apply the following procedure (not displayed on ECAM) in case of total loss of the
cabin pressure control
leading to overpressure
PACK 1 or
2.......................................................................................................................................
.....OFF
BLOWER +
EXTRACT.......................................................................................................................
.. OVRD
Cabin air is extracted overboard.
ΔP...........................................................................................................................FREQ
UENTLY MONITOR
�� If ΔP >9 PSI
PACK
1+2...................................................................................................................................
......OFF
LAND ASAP
Before 10 min minutes from landing:
PACK
1+2...................................................................................................................................
............ OFF
BLOWER +
EXTRACT.......................................................................................................................
...AUTO
CAUTION Check that ΔP is zero before opening the doors.
ABN-21
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AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1
ABNORMAL AND
EMERGENCY PROCEDURES 30 AUG 10
Intentionally left blank
A318/A319/A320/A321 FLEET , , , , , , , ,
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ABN-22
1/2
AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1
ABNORMAL AND
EMERGENCY PROCEDURES 30 AUG 10
A318/A319/A320/A321 FLEET , , , , , , , ,
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LOSS OF FMS DATA IN DESCENT/APPROACH (SEVERE RESET)
AP/FD lateral and vertical selected modes, and A/THR, are available immediately
after the reset. If
necessary, the pilot may perform the FCU selections for short-term navigation.
When the FMS has automatically recovered:
The database ‐ cycle may have changed
‐ The FMGS does not autotune the ILS and ADF
‐ The FMS position bias is lost
‐ Lateral and vertical managed modes cannot re-engage
‐ The “CAB PR LDG ELEV FAULT ” message is displayed on the ECAM
‐ A “MAP NOT AVAIL” message may be displayed on one ND.
With respect to the Auto Flight System, and depending on when the flight plan is lost,
the following two
procedures list the actions to be performed, in their order of priority:
�� INITIAL APPROACH OR CLOSE TO ILS INTERCEPTION:
�� When the system has recovered:
Access the RAD NAV Page, and manually tune the ILS (preferably using IDENT).
Enter the ILS
course, if a frequency has been entered.
Fly in selected speed.
Note: ‐ LOC and G/S guidance modes are available
‐ VLS speed is still available and displayed on the PFD
‐ Missed approach trajectory is not available.
�� DESCENT or TERMINAL AREA:
�� When the system has recovered:
Select the initial database
Perform DIR TO a downpath waypoint. Select heading, if required.
Perform a LAT REV at the downpath waypoint and redefine the DESTINATION in
the NEW DEST
field.
Redefine the arrival and/or the approach procedure.
Select the FUEL PRED Page, and enter the GW.
Activate the APPROACH phase.
Enter destination data on the PERF APPR Page, as required. Managed speed is
available.
LOW ENERGY WARNING
The “SPEED SPEED SPEED” synthetic voice sounds every 5 s whenever the aircraft
energy goes below a
threshold under which thrust must be increased.
“SPEED SPEED SPEED”
Increase the thrust until the warning stops and, depending on the circumstances,
adjust the pitch
accordingly.
ABN-22
2/2
AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1
ABNORMAL AND
EMERGENCY PROCEDURES 30 AUG 10
Intentionally left blank
A318/A319/A320/A321 FLEET , , , , , , , ,
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ABN-22
1/2
AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1
ABNORMAL AND
EMERGENCY PROCEDURES 30 AUG 10
A318/A319/A320/A321 FLEET , , , , , , , ,
, , , , , , , , , , , ,
, , , , ,
LOSS OF FMS DATA IN DESCENT/APPROACH (SEVERE RESET)
AP/FD lateral and vertical selected modes, and A/THR, are available immediately
after the reset. If
necessary, the pilot may perform the FCU selections for short-term navigation.
When the FMS has automatically recovered:
The database ‐ cycle may have changed
‐ The FMGS does not autotune the ILS and ADF
‐ The FMS position bias is lost
‐ Lateral and vertical managed modes cannot re-engage
　
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