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DMC 3 EFIS/ECAM displays are lost for 40 s on ground after
reset or power-up.
FWC 2 NIL
31
SDAC 2 NIL
32 Braking malfunction BSCU Refer to PRO-SUP-32 BSCU Reset
LGCIU 2 An LGCIU reset must neither be made during landing
gear maneuvers, nor just prior to touchdown.
38 VSC Cabin aft
C/B panel
(VACUUM
TOILET
SYSTEM)
On ground or in flight
In case all toilets on one or both sides of the aircraft are
shut down (on the cabin aft C/B panel):
VACUUM TOILET ‐ SYSTEM (blue pb) RESET
The repeated use of the blue reset pb is not
recommended.
If the reset does not fix the problem, apply the
following procedure to both system sides, on the cabin
aft C/B panel (VACUUM TOILET SYSTEM).
Do not apply the following procedure in case of a
waste tank overfills.
On the cabin aft C/B panel:
‐ C/B SYSTEM (both) and VACUUM GEN (both) (4
C/Bs) PULL
‐ C/B LAVATORY POWER (LH and RH) (8 C/Bs) PULL
‐ C/B LAVATORY POWER (LH and RH) (8 C/Bs )PUSH
LH and RH SYSTEM and both VACUUM GEN C/Bs
remain pulled.
LH and RH SYSTEM and both VACUUM GEN C/Bs
remain pulled. In this configuration:
• The waste quantity indication is lost,
• The protection against waste tank overfill is lost,
• When the aircraft is below 16 000 ft do not use the
toilets.
• On ground, during servicing, do not use toilets.
To be continued on next page
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
SUPPLEMENTARY PROCEDURES
ELECTRICAL
A330/A340 FLEET PRO-SUP-24 P 22/36
FCOM 19 AUG 10
Continued from previous page
46 ATSU 1 When the ATSU is reset, ADS-C connections are no
longer active. The ATC center(s) assumes that the
connection is still active because a disconnection
message has not been sent to the ATC center(s).
Therefore, the ATC center(s) will not attempt to
re-establish ADS-C contracts with the aircraft, even after
re-notification.
ATSU reset, with the ATSU 1 reset sw on 261 VU
(overhead panel), should only be attempted, if:
″INVALID DATA″ is displayed ‐ on the DCDU.
‐ Key selection has no effect on the DCDU or any of the
MCDU ATSU DATALINK submenus.
49 ECB APU
MASTER sw
Reset must only be attempted when APU speed is below
7 %
52 PSCU 2 NIL
70 EIVMU 4 During the reset, and the subsequent 5 s, the following
occurs:
‐ On the corresponding engine:
• Loss of thrust reverser (T/R 1 and 4 are lost if
EIVMU 1 or 4 affected).
• Loss of vibration indication.
• If idle is selected, only high idle is available.
• Loss of man start and wet crank.
• Loss of bleed corrections on thrust limit.
‐ On all engines:
• Loss of autothrust
‐ Loss of Flex/Derated T.O.
70 EIVMU 4 During the reset, and the subsequent 5 s, the following
occurs:
On the ‐ corresponding engine:
• Loss of thrust reverser
• Loss of vibration indication
• If idle is selected, only high idle is available
• Loss of man start and wet crank
• Loss of bleed corrections on thrust limit
‐ On both engines:
• Loss of autothrust
‐ Loss of Flex/Derated T.O.
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
SUPPLEMENTARY PROCEDURES
ELECTRICAL
A330/A340 FLEET PRO-SUP-24 P 23/36
FCOM 19 AUG 10
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
SUPPLEMENTARY PROCEDURES
ELECTRICAL
A330/A340 FLEET PRO-SUP-24 P 24/36
FCOM 19 AUG 10
COMPUTER RESET TABLE
Applicable to:
ATA EQUIPMENT MANUAL RESET
OVHD
RESET Panel
System
Control Panel
REMARKS
PACK CONT 2 The pack flow indication may unduly be replaced
by amber XX on the ECAM BLEED SD page, in the
following conditions:
‐ Aircraft on ground
‐ APU ON
‐ APU BLEED OFF
‐ PACK 1 and/or PACK 2 selected ON
In these conditions, the flight crew may attempt to reset
the affected Pack Controller, with APU bleed valve open:
‐ APU BLEED (ON)
On the OVHD RESET:
‐ pack
1
flow
indication
is
affected
: pull then push PACK CONT 1 reset pb,
‐ pack
2
flow
indication
is
affected
: pull then push PACK CONT 2 reset pb,
‐ APU BLEED (AS RQRD)
If no new amber XX appear on the ECAM BLEED SD
page pack flow indication, resume normal operation.
Otherwise, apply Refer to 99 Duref Cible QRH
ZONE CONT 1
VENT CONT 2
21
AEVC 1
NIL
To be continued on next page
　
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