ABNORMAL OPERATIONS
FIRE PROTECTION
A318/A319/A320/A321
FLIGHT CREW TRAINING MANUAL
If the flight crew sets the electrical emergency configuration following a smoke detection in the avionic compartment ("AVIONICS SMOKE" ECAM caution triggered), the ECAM does not displays the same procedure as the one displayed following the loss of main generators. In fact in this
case, the ECAM displays a specific procedure that takes into account the smoke detection: As the flight crew has voluntarily set the electrical emergency configuration, the purpose of the ELEC EMER CONFIG ECAM procedure is not to try to restore the generators, but to remain in electrical
emergency configuration, and restore generators before landing to perform the landing in normal electrical configuration.
BOXED ITEMS
These items (applying SMOKE REMOVAL procedure, setting electrical emergency configuration, or considering immediate landing) may be applied at any time, in the procedure (but not before the immediate actions).
Once the first step of the smoke removal procedure have been applied, the flight crew will come back to the SMOKE/FUMES/AVNCS SMOKE procedure, to apply the appropriate steps, depending on the suspected smoke source while descending to FL 100. Reaching FL 100, the smoke removal procedure will be completed.
CARGO SMOKE
Applicable to: ALL
The crew should be aware that, even after successful operation of the cargo fire bottle, the CARGO SMOKE warning might persist due to the smoke detectors being sensitive to the extinguishing agent. On the ground, the crew should instruct the ground crew not to open the cargo door until the passengers have disembarked and fire services are present.
If SMOKE warning is displayed on ground with the cargo compartment door open, do not initiate an AGENT DISCHARGE. Request the ground crew to investigate and eliminate the smoke source. On ground, the warning may be triggered due to a high level of humidity.
ABNORMAL OPERATIONS
FIRE PROTECTION
A318/A319/A320/A321
FLIGHT CREW TRAINING MANUAL
Intentionally left blank
ABNORMAL OPERATIONS
FLIGHT CONTROLS
A318/A319/A320/A321
FLIGHT CREW TRAINING MANUAL
ABNORMAL FLAPS/SLATS CONFIGURATION
Applicable to: ALL
CAUSES
Abnormal operation of the flaps and/or slats may be due to one of the following problems:
? Double SFCC failure
? Double hydraulic failure (B+G or Y+G)
? Flaps/Slats jammed (operation of the WTB)
CONSEQUENCES
Abnormal operation of the flaps and slats has significant consequences since:
? The control laws may change
? The selected speed must be used
? A stabilized approach should be preferred
? The approach attitudes change
? Approach speeds and landing distances increase
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