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CIDS Norm Norm Norm
INTERPHONE Norm Norm Norm
CVR Norm Inop Inop
COM
LOUDSPEAKER 1 Norm Norm Norm
CREW OXY Norm Norm (1) Norm (1)
PAX OXY mask release (auto
EMER EQPT + man) Norm Inop Inop
SLIDES ARM/WARN Norm Norm Norm
(1) Crew oxygen valve inoperative.
ENG 1 LOOP A only A only A only
ENG 2 LOOP B only B only B only
APU LOOP Inop Inop Inop (1)
CARGO SMOKE DET Channel 1 Inop Inop
ENG FIRE EXT. Bottle 1 only Bottle 1 only Bottle 1 only
APU FIRE EXT. Squib A only Squib A only Squib A only
CARGO FIRE EXT. Inop Inop Inop (1)
FIRE
APU AUTO EXT. Inop Inop Inop (1)
(2) Restored, when speed is below 100 kt.
ELAC N° 1 only N° 1+ N° 2 N°1+ N°2 (2)
SEC N° 1 only N° 1 N° 1 (2)
FCDC N° 1 only Inop Inop
SFCC N° 1 only N° 1 only N° 1 only
FLT CTL
Flaps POS ind Norm Norm Norm (1)
(1) Lost 30 s after last engine shutdown.
(3) Lost, when speed is below 50 kt.
LP VALVE Norm Norm Norm
FQI channel 1 Norm Inop Inop
FUEL X FEED VALVE Norm Inop Inop
TRANSFER VALVE Norm Inop Inop
HYD FIRE VALVES Norm Norm Norm
WING A.ICE Norm Inop Inop
ENG A. ICE VALVE Open Open Open
CAPT PITOT Norm Norm Norm (1)
CAPT AOA Norm Inop Inop
ICE - RAIN
RAIN REPELLANT (CAPT) Norm Norm Norm
(4) Lost, when speed is below 50 kt
PFD 1 Norm Norm Norm(1)
EIS ND 1 Norm Inop Inop
ECAM upper disp. Norm Norm Norm (1)
To be continued on next page
ABN-24
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AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1
ABNORMAL AND
EMERGENCY PROCEDURES 30 AUG 10
A318/A319/A320/A321 FLEET
Continued from previous page
DMC 1 or 3 Norm Norm Norm (1)
SDAC 1, FWC 1 Norm Norm Norm (1)
ECAM CONT. panel Norm Norm Norm
FLT INS CLOCKS Norm Norm Norm
(5) Lost, when speed is below 50 kt.
LGCIU SYS 1 Norm Norm Norm
L/G BRK PRESS IND Norm Norm Norm
PARK BRK Norm Norm Norm
LIGHTS EEMMEERR CCAKBPT NNoorrmm NNoorrmm NNoorrmm
IR N° 1 only (2) N° 1 only (2) N° 1 only (2)
ADR N° 1 only N° 1 only N° 1 only
ADF N° 1 only Inop Inop
VOR-ILS N° 1 only N° 1 only N° 1 only (1)
DME N° 1 only Inop Inop
VOR/DDRMI Norm Norm Norm (1)
ATC N° 1 only Inop Inop
STBY HORIZON Norm Norm Norm
STBY COMP (LT) Norm Norm Norm
NAV
STBY ALTI (VIB) Norm Inop Inop
(1) IR2 and IR3 are lost 5 min after failure of the main generators. But, if IR3
replaces IR1 (ATT-HDG selector at CAPT3), IR3
remains supplied
(6) Lost, when speed is below 50 kt.
ENG 1 BLEED Norm BMC 1 inop BMC 1 inop
ENG 2 BLEED BMC 2 inop BMC 2 inop BMC 2 inop
APU BLEED Inop Inop Inop (1) PNEU
X BLEED (MAN CTL) Norm Inop Inop
(7) Restored, when speed is below 100 kt.
ECB - STARTER Norm (2) Inop Inop (1)
APU FUEL LP VALVE Norm Norm Norm
FUEL PUMP Norm Norm Norm
(1) Restored, when speed is below 100 kt.
(2) For APU start only.
FADEC A + B (1) A + B (1) A + B (1)
PWR PLT IGNITION A only A only A only
HP FUEL VALVE closure Norm Norm Norm
(1) Channels A and B are self-powered above 12 % N2. If N2 is below 12 % , only
Channel A is powered.
MISC MECH HORN Norm Norm Norm
FLT ON BAT ONLY
Flight time on batteries only may be increased to at least 30 min as follows:
ENG MODE
SEL.................................................................................................................................
NORM
ANTI ICE PITOT 1 C/B
(D02).................................................................................................................PULL
26 V ADIRU 1 C/B
(F07)........................................................................................................................PUL
L
CM 1 altitude, speed, and vertical speed indication on PFD are lost. Use standby
instruments
�� 7 min before landing:
ANTI ICE PITOT 1 C/B
(D02)....................................................................................................... RESET
�� After 1 min:
CAUTION This time delay is necessary to ensure reliable speed information even in
icing
conditions when the ADIRU is reset to ON.
26 V ADIRU 1 C/B
(F07)........................................................................................................ RESET
ABN-24
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AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1
ABNORMAL AND
EMERGENCY PROCEDURES 30 AUG 10
A318/A319/A320/A321 FLEET
ELEC EMER CONFIG SUMMARY
CRUISE
MAX
SPD..................................................................................................................................
　
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