ELEC DC ESS BUS FAULT
-VHF 2 OR 3..............USE
-AUDIO SWTG..............SELECT
(ACP 1 and 2 are lost. Therefore, set the AUDIO SWTG selector to CAPT 3 or F/O 3 to recover communications.
- BARO REF..............CHECK
NAV GPWS FAULT
-GPWS..............OFF
FUEL L TANK PUMP 1 LO PR
FUEL R TANK PUMP 1 LO PR
VENT BLOWER FAULT
NOTE: To shut down the engines on ground, use ENG FIRE pushbutton
AFFECTED SYSTEMS
* CAB PRESS
* HYD
* F/CTL
STATUS
LDG DIST PROC..............APLLY
ENG 1 APPR IDLE ONLY
ENG 2 APPR IDLE ONLY
BOTH PFD ON SAME FAC
SLATS/FLAPS SLOW
CAT2 ONLY
INOP SYS DISPLAYED ON ECAM
B HYD
SPLR 3
VHF1
ACP1+2
WING A. ICE
AP 1
A/THR
FCU1
FAC1
L TK PUMP 1
R TK PUMP 1
REV 2
ENG 2 START
CAB
PR 1
VENT EXTRACT
B ELEC PUMP
GPWS
ENG 1 LOOP A
ENG 2 LOOP B
FCDC 1
CAT 3
OTHER INOPERATIVE SYSTEMS
BRK PRESS INDICATOR
FLIGHT INTERPHONE
EIU 2
CPT REIN REPELLENT
AVIONICS AIR COND VALVE
STBY HORIZON
STBY COMPASS LIGHT
HP FUEL SHUT-OFF VALVES
SFCC 1
RMP 1
HYD FIRE VALVES ENG 1 AND 2
RAM AIR INLET
ECAM CONTROL PANEL
LEFT LOUDSPEAKER
DC SHED ESS BUS
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From Airbus FCOM training manual.
Best Regards
Rampi