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• 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.
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
SUPPLEMENTARY PROCEDURES
ELECTRICAL
A330/A340 FLEET PRO-SUP-24 P 8/36
FCOM 19 AUG 10
COMPUTER RESET TABLE
Applicable to:
ATA EQUIPMENT MANUAL RESET
OVHD
RESET Panel
System
Control Panel
REMARKS
PACK CONT 2
ZONE CONT 1
VENT CONT 2
AEVC 1
21 NIL
CPC 2 To force a CPC changeover:
‐ MODE SEL (MAN)
AFTER 3 s:
‐ MODE SEL (AUTO)
The inactive CPC may then be reset (check the CAB
PRESS ECAM SD page).
FCU
2
Do not reset when PART FCU is displayed as an inop
system.
‐ On ground : The FCU has to be reconfigured after
reset.
‐ In flight : Check FCU targets after reset.
Following a total FCU loss, targets are selected
targets.
FMGEC and FM
4
• FMGEC or FM resets results in onside AP
disconnection (if engaged)
• Resynchronization of both FMs will occur after a reset
sequence, with associated messages on the MCDU
and ND :
‐ PLEASE WAIT
‐ MAP NOT AVAIL
• It is recommended to use FMGEC R/B, rather than FM
R/B.
22
MCDU BRT OFF CTL In case the MCDU is blank or locked, Refer to STLO-22
MCDU LOCKED OR BLANKED .
To be continued on next page
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
SUPPLEMENTARY PROCEDURES
ELECTRICAL
A330/A340 FLEET PRO-SUP-24 P 9/36
FCOM 19 AUG 10
Continued from previous page
CIDS 2 In the event of active CIDS reset (usually CIDS 1
when both are operative), a complete power-up test is
performed.
‐ In flight, test lasts about 20 s:
• The cabin light comes on at full intensity.
If selected, dimming is lost and must be reselected
after the test.
• PA, CALL and INTERPHONE functions are
interrupted and have to be reselected after the test.
• FAP cabin temperature corrections are lost, and
have to be reselected after the test.
‐ On ground, test lasts about 80 s, and includes
additionally:
• a sequencial cabin loudspeakers test (triggers a
tone for about 10 s).
• the cabin light might flash shortly. Dimming
selection is lost (as in flight)
ACP/AMU 2 NIL
23
RMP ON/OFF CTL In case of freezing of one RMP (impossibility to
interchange the ACTIVE and STBY radio navigation or
communication frequencies,...), all the RMP’s have to be
reset, one after the other, to recover a normal operation.
In order to be reset, RMP’s must be switched off at least
5 s by using the ON/OFF selector on the RMP control
panels.
24 GPCU 2 pb on
ELEC panel
GPCU reset may be attempted, if AVAIL and ON lights
do not light up.
1. Press once the affected EXT A(B) pb sw to reset the
functions of GPCU.
2. Switch ON the external power unit sw to reset the
GPU.
3. Check AVAIL light is ON and press the EXT A(B) pb
sw to connect the GPU.
If unsuccessful, check GPU voltage and frequency (bite
is available on batteries only
24 BCL 3 BAT pb on
ELEC panel
Use BAT pb to reset the BCL.
Do not reset the BCL when theBAT FAULT caution has
been triggered, and the BAT OFF selection has been
requested by the ECAM.
To be continued on next page
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
SUPPLEMENTARY PROCEDURES
ELECTRICAL
A330/A340 FLEET PRO-SUP-24 P 10/36
FCOM 19 AUG 10
Continued from previous page
25 Commercial
equipments and
galleys
2 pb on
ELEC panel On ground
When the commercial equipment and/or galley loads
have been shed by the ECMU, they can be recovered
when more electrical power is available.
If COMMERCIAL OFF ‐ is displayed on the ECAM
ELEC page : Switch the COMMERCIAL pb OFF then
ON.
‐ If GALLEY SHED or GALLEY PARTIALLY SHED
is displayed on the ECAM ELEC page : Switch the
GALLEY pbOFF then ON.
Do not reset more than one pushbutton at a time.
26 SDCU 2 Only a simultaneous reset of SDCU 1 and SDCU 2 is
authorized.
On ground:
‐ Simultaneously pull both SDCU 1 reset pb and SDCU 2
reset pb
‐ Wait 2 min
‐ Simultaneously push both SDCU 1 reset pb and SDCU
　
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