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‐ Pull the C/Bs for DIR2 in the following order: G02
C/B on 49VU, M06 C/B on 121VU.
IF UNSCCESSFUL:
‐ Pull the C/Bs for DIR1 in the following order: G01
C/B on 49VU, M05 C/B on 121VU.
‐ Wait for 1 min, then:
‐ Push the C/Bs for DIR2 in the following order:
M06 C/B, G02 C/B.
‐ After CIDS reset, wait approximately 4 min,
before recovering normal operation.
Frozen RMP RMP Refer to PRO-SUP-23 FROZEN RMP
FAP freezing FAP On ground, or in flight:
‐ Pull FAP C/Bs in the following order: H01 C/B on
49VU, Q14 C/B on 121VU.
‐ Wait 10 s, then:
‐ Push the C/Bs in the following order: Q14 C/B,
H01.
24
GPU cannot be connected to the
aircraft
GAPCU On ground only:
The GPU cannot be connected to the electrical
network of the aircraft (AVAIL light is OFF)
‐ If at least one power source (IDG 1 or 2, APU
GEN or batteries) is connected to the electrical
network of the aircraft.
• Reset the EXT PWR pb switch on 35VU
(Press and release)
‐ If no power source is connected to the electrical
network of the aircraft.
• Set the BAT 1+2 pb switches to AUTO.
26
SMOKE LAV + CRG FAULT SIDCU On ground only:
‐ Pull C/B C06 C/B on 49VU, and C/B T18 C/B on
122VU.
‐ Wait 10 s before pushing the C/Bs.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
SUPPLEMENTARY PROCEDURES
ELECTRICAL
A318/A319/A320/A321 FLEET PRO-SUP-24 P 11/14
FCOM 19 AUG 10
F/CTL ELAC 1(2) FAULT
F/CTL ALTN LAW
F/CTL ELAC 1(2) PITCH FAULT
ELAC Refer to 99 Duref Cible FCOM, if applicable.
27
ELAC or SEC malfunction ELAC or SEC --- WARNING ----------------------
Do not reset more than one computer at a time.
It is possible to reset flight control computers in
flight, event if not requested by the ECAM, provided
only one reset is performed at a time: For the ELAC
only, in case of uncommanded maneuvers during
the flight, it is not recommended to reset the ELAC.
--------------------------------------------
Note: When an ELAC reset is performed on ground
the crew must check the pitch trim position. If a reset
is performed on ground, the flight crew must then
perform a flight control check, as per SOP.
28
Loss of fuel quantity indication or
Simultaneous triggering of FUEL L
XFR VALVE CLOSED and FUEL
R XFR VALVE CLOSED, although
FUEL SD indicates no anomaly.
FQIC On ground, or in flight:
‐ Pull the 3 C/B:
• Channel 1 (A13 C/B on 49VU)
• Channel 2 (M27 C/B on 121VU)
• Channel 1 and 2 (L26 C/B on 121VU)
‐ Wait 5 s, before pushing the 3 C/B.
Note: The fuel quantity indication will be
re-established within 1 min.
28
Loss of fuel quantity indication
or Simultaneous triggering of
FUEL L XFR VALVE CLOSED and
FUEL R XFR VALVE CLOSED ,
although FUEL SD indicates no
anomaly.
FQIC On ground, or in flight:
‐ Pull the 3 C/B:
• Channel 1 (A13 C/B on 49VU)
• Channel 2 (M27 C/B on 121VU)
• Channel 1 and 2 (L26 C/B on 121VU)
‐ Wait 5 s, before pushing the 3 C/B.
Note: The fuel quantity indication will be
re-established within 1 min.
--- CAUTION ----------------------
The FUEL AUTO FEED FAULT caution will be lost
for the remainder of the flight.
In flight:
‐ If center tank is not empty, while one inner tank
contains less than 5 000 kg (11 000 lb) of fuel:
• FUEL MODE SEL (MAN)
‐ When center tank is empty:
• CTR TK PUMP 1 and 2 (OFF)
• FUEL MODE SEL (MAN)
--------------------------------------------
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
SUPPLEMENTARY PROCEDURES
ELECTRICAL
A318/A319/A320/A321 FLEET PRO-SUP-24 P 12/14
FCOM 19 AUG 10
28
Loss of fuel quantity indication FQIC On ground, or in flight:
‐ Pull the 3 C/B:
• Channel 1 (A13 C/B on 49VU)
• Channel 2 (M27 C/B on 121VU)
Wait 5 s, ‐ before pushing the 3 C/B.
Note: The fuel quantity indication will be
re-established within 1 min.
28
Loss of fuel quantity indication or
Simultaneous triggering of FUEL L
XFR VALVE CLOSED and FUEL
R XFR VALVE CLOSED, although
FUEL SD indicates no anomaly.
FQIC On ground, or in flight:
‐ Pull the 3 C/B:
• Channel 1 (A13 on 49VU)
• Channel 2 (M27 on 121VU)
• Channel 1 and 2 (L26 on 121VU)
‐ Wait 5 s, before pushing the 3 C/B.
Note:
1. The fuel quantity indication will be re-established
within 1 min.
2. The fuel leak detection function will be lost for
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A320机组操作手册FLIGHT CREW OPERATING MANUAL 14(74)
