DET FAULT
— Pull C/B C06 on 49VU, and C/B T18 on 122VU.
— Wait 10 seconds before pushing both
C/Bs.
27
F/CTL ELAC 1(2)
ELAC
— Refer to the FCOM 3.02.27, if applicable.
FAULT
F/CTL ALTN LAW
F/CTL ELAC 1(2)
PITCH FAULT
ELAC or SEC malfunction
ELAC or SEC
WARNING :
Do not reset more than one computer at a time.
. It is possible to reset the flight control
computers in flight, even if not requested by the ECAM, provided only one reset is performed at a time:
For the ELAC only, the reset is not
recommended in case of uncommanded maneuvers during the flight.A319/A320/A321
oviimm.,,
ABNORMAL PROCEDURES
REV 36
2.39
SEQ 001
ATA
System malfunction
or ECAM
Warning/Caution
Affected
system
Reset
30
ANTI ICE
WHC
Refer to the FCOM 3.02.30, if applicable.
L(R)/WINDSHIELD (WINDOW)
31
FWS FWC 1(2) FAULT
FWC
On ground, or in flight :
Pull, then push, the C/B of the affected FWC:
— FWC 1 E2 or F01 (<1) ON 49VU
— FWC 2 G7 ON 121 VU
32
Braking malfunction
BSCU
Refer to the 3.04.32 or OEB 50, if applicable.
L/G LGCIU 1(2) FAULT —
LGCIU 1(2)
On ground only :
LGCIU 1 : Pull C/B G34 on 121 VU, then C09 on 49VU. Then push C/B C09 and C/B G34. LGCIU 2 : Pull then push C/B G35 on 121 VU.
38
Failure messages on the CIDS FAP in the cabin
Vacuum System Controller
On ground, or in flight :
— Pull C/B 35 MG on 2001 VU, aft cabin,
— Wait 30 seconds, then push C/B 35 MG.
70
ENG IGN A+B FAULT
FADEC and EIU
Refer to the FCOM 3.02.70, if applicable.
ENG 1(2) FADEC
FADEC
Refer to the FCOM 3.02.70, if applicable.
A(B) FAULT
A319/A320/A321
oniatTril.,,
ABNORMAL PROCEDURES
REV 36
2.40
SEQ 001
ECAM ADVISORY CONDITIONS
SYSTEM
CONDITIONS
RECOMMENDED ACTION
CAB
PRESS
CAB VERTICAL SPEED V/S > 1800 ft/min
CPC changeover may be attempted : MODE SEL MAN
Wait 10 seconds, then :
MODE SEL AUTO
CAB ALTITUDE altitude 8800 ft
MODE SEL MAN
Manual pressure control
CAB DIFF PRESS
AP 1.5 psi in phase 7
LDG ELEV MAN ADJUST
If unsuccessful :
MODE SEL MAN
Manual pressure control
ELEC
IDG OIL TEMP 147°C
Reduce IDG load, if possible (GALLEY or GEN OFF).
If required, restore when the temperature has dropped.
Restrict generator use to a short time, if the temperature rises again excessively.
FUEL
Difference between wing fuel quantities greater than 1500 kg (3307 lb)
FUEL MANAGEMENT CHECK
If a fuel leak is suspected, refer to the FUEL LEAK procedure.
For limitations, see 3.01.28.
Fuel temp greater than 45°C in inner cell, or 55°C in outer cell
GALLEY OFF
Fuel temp lower than — 40°C in inner or outer cell
Consider descending to a lower altitude, and/or increasing Mach to increase TAT.
APU
EGT > EGT MAX — 33°C (inhibited during APU start)
OIL QTY
(message LOW OIL LEVEL pulsing)
If there is no oil leak, then the remaining oil quantity allows normal APU operation for about 10 hours.A319/A320/A321
oviimm.,,
ABNORMAL PROCEDURES
REV 36
2.39
SEQ 001
ATA
System malfunction
or ECAM
Warning/Caution
Affected
system
Reset
30
ANTI ICE
WHC
Refer to the FCOM 3.02.30, if applicable.
L(R)/WINDSHIELD (WINDOW)
31
FWS FWC 1(2) FAULT
FWC
On ground, or in flight :
Pull, then push, the C/B of the affected FWC:
— FWC 1 E2 or F01 (<1) ON 49VU
— FWC 2 G7 ON 121 VU
32
Braking malfunction
BSCU
Refer to the 3.04.32 or OEB 50, if applicable.
L/G LGCIU 1(2) FAULT —
LGCIU 1(2)
On ground only :
LGCIU 1 : Pull C/B G34 on 121 VU, then C09 on 49VU. Then push C/B C09 and C/B G34. LGCIU 2 : Pull then push C/B G35 on 121 VU.
38
Failure messages on the CIDS FAP in the cabin
Vacuum System Controller
On ground, or in flight :
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