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IMPORTANCE OF THE FLIGHT CREW BRIEFING
Among others, the aircraft status must be reviewed during the flight crew briefing. Any particularities (operational consequences, procedures, associated task sharing and callout) must be reviewed at that time. The flight crew must notably review:
? The status of the thrust reversers and if reverser thrust can be used
? Operational effect (aircraft handling during roll-out).
 

  ABNORMAL OPERATIONS
OPERATING TECHNIQUES
A318/A319/A320/A321
FLIGHT CREW TRAINING MANUAL 

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  ABNORMAL OPERATIONS
AUTOFLIGHT
A318/A319/A320/A321
FLIGHT CREW TRAINING MANUAL 

FMGC FAILURE
Applicable to: ALL
SINGLE FMGC FAILURE
Should a single FMGC failure occur, the AP, if engaged on affected side, will disconnect. The AP will be restored using the other FMGC. The A/THR remains operative. Furthermore, flight plan
information on the affected ND may be recovered by using same range as the opposite ND. The crew should consider a FMGC reset as detailed in QRH.
DUAL FMGC FAILURE
Should a dual FMGC failure occur, the AP/FD and A/THR will disconnect. The crew will try to recover both AP and A/THR by selecting them back ON (The AP and A/THR can be recovered if the FG parts of the FMGS are still available).
If both AP and A/THR cannot be recovered, the thrust levers will be moved to recover manual thrust. The pilot will switch off the FDs and select TRK / FPA to allow the blue track index and the bird to be displayed. The RMPs will be used to tune the NAVAIDs.
The crew will refer to the QRH for computer reset considerations and then will Refer to FCOM/PRO-SUP-22-A AUTOMATIC FMGS RESET AND RESYNCHRONIZATION - FM RESET to reload both FMGC as required.
 

  ABNORMAL OPERATIONS
AUTOFLIGHT
A318/A319/A320/A321
FLIGHT CREW TRAINING MANUAL 

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  ABNORMAL OPERATIONS
ELECTRICAL
A318/A319/A320/A321
FLIGHT CREW TRAINING MANUAL 

INTRODUCTION TO EMERGENCY ELECTRICAL CONFIGURATION
Applicable to: ALL
The procedure discussed in this section is the EMERGENCY ELECTRICAL CONFIGURATION. Whilst it is very unlikely that this failure will be encountered, it is useful:
? To refresh on the technical background
? To recall the general guidelines that must be followed in such a case
? To outline the main available systems according to the electrical power source.
TECHNICAL BACKGROUND
Criteria: SA
1 Applicable to: MSN 0045-0499
The emergency electrical configuration is due to the loss of AC BUS 1 and 2. The RAT extends automatically. This powers the blue hydraulic circuit which drives the emergency generator. The emergency generator supplies both AC and DC ESS BUS.
When landing gear is down, the emergency generator is no longer powered. The emergency generation network is automatically transferred to the batteries and AC SHED ESS and DC SHED ESS BUS are shed.
　
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