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COCKPIT AT FIXED TEMP
SLATS/FLAPS SLOW
CAT 2 ONLY
INOP SYS
See below
INOP SYS
FCU 2 CAT 3 FAC 2
FUEL PUMPS ANTI SKID NORM BRK
AUTO BRK Y ELEC PUMP BRAKES SYS 1
BRAKES SYS 2 APU FIRE DET LAV DET
ENG 1 LOOP B L+R CAB FAN FCDC 2
GALLEY FAN CRG HEAT �� GND COOL ��
MAIN GALLEY ACP 3 CAPT STAT
F/O STAT STBY STAT WSHLD HEAT
WNDW HEAT PACK 1 PACK 2
COND CTL 1 SPLR 1+2+5 ELAC 2
SEC 2+3 VHF 2 N.W. STEER
LGCIU 2 REVERSER 2 CAB PRESS 2
AVNCS VENT VENT BLOWER ENG 2 LOOP A
AP 2 COND CTL 2
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
ELECTRICAL
A318/A319/A320/A321 FLEET PRO-ABN-24 P 251/252
FCOM 19 AUG 10
ELEC STAT INV FAULT
Applicable to: ALL
L2Crew awareness.
ELEC EMER GEN 1 LINE OFF
Applicable to: ALL
L2With the GEN 1 LINE pb-sw (on the EMER ELEC PWR panel) in the OFF position, the GEN 1 line
contactor is open and GEN 2 supplies the AC BUS 1 channel.
Crew awareness.
Set the GEN 1 LINE to ON pb-sw.
C/B TRIPPED
Applicable to: ALL
L2Crew awareness.
L1�� If one green circuit breaker (C/B) is tripped, one of the following messages appears after
one minute, depending on the location of the affected C/B:
C/B TRIPPED ON OVHD PNL
C/B TRIPPED ON L(R) ELEC BAY
C/B TRIPPED REAR PNL J-M OR N-R OR S-V OR W-Z
L12
Note: Do not reengage a C/B that has tripped by itself, unless the Captain judges it
necessary to do so for the safe continuation of the flight. This procedure should be
adopted only as a last resort, and only one reengagement should be attempted.
On ground, do not reengage the C/B of the fuel pump(s) of any tank. For all other
C/Bs, if the flight crew coordinates the action with maintenance, the flight crew may
reengage a tripped C/B, provided that the cause of the tripped C/B is identified.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
ELECTRICAL
A318/A319/A320/A321 FLEET PRO-ABN-24 P 252/252
FCOM 19 AUG 10
ELEC AC ESS BUS ALTN (ON GROUND)
Applicable to: , , MSN,,,,
L2 The AC ESS BUS is supplied from the AC BUS 2 although the AC ESS FEED pb-sw switch is set
to normal.
Crew awareness.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
COCKPIT DOOR
A318/A319/A320/A321 FLEET PRO-ABN-25 P 1/2
FCOM 19 AUG 10
COCKPIT DOOR FAULT
Applicable to: ALL
This procedure should be applied, if the Cockpit Door Locking System (CDLS) fails. This failure is
indicated when the FAULT light on the center pedestal’s COCKPIT DOOR panel comes on.
In the case of a DC BUS 2 fault, no FAULT indication appears on the center pedestal’s COCKPIT
DOOR panel. The CDLS is not electrically-supplied, and is inoperative.
CKPT DOOR CONT panel .....................................................................................................CHECK
This panel is located on the overhead panel. It is used to identify the faulty CDLS item, and to verify
the status of the pressure sensors and the three electrical latches (referred to as strikes).
�� If one or more electrical latches (strikes) are faulty:
The cockpit door is not intrusion-proof if two or more electrical latches are faulty.
The system may be recovered by performing the following steps:
Cockpit door.........................................................................................................................OPEN
COCKPIT DOOR sw.......................................................................................... SET to UNLOCK
After 10 s:
COCKPIT DOOR sw.............................................................................................. SET to NORM
�� If two pressure sensors are faulty:
Automatic latch release is not available, in case of cockpit decompression.
�� If no LED on the CKPT DOOR CONT panel is on:
The CDLS control unit is faulty, therefore, the cockpit door might unlock automatically. If it does
not, consider using the mechanical override system to unlock the door.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
COCKPIT DOOR
Intentionally left blank
A318/A319/A320/A321 FLEET PRO-ABN-25 P 2/2
FCOM 19 AUG 10
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
FIRE PROTECTION
A318/A319/A320/A321 FLEET PRO-ABN-26 P 1/176
FCOM 19 AUG 10
ENG 1(2)/APU FIRE LOOP A(B) FAULT
Applicable to:
L2No crew action required in flight.
　
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