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A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
NAVIGATION
A330/A340 FLEET PRO-ABN-34 P 133/140
FCOM 19 AUG 10
NAV ADR 1+2+3 FAULT
Applicable to: MSN , ,
L2 This alert triggers if each of the 3 ADRs self-detects a failure or receives irrelevant data from the
probes. This procedure requires that the flight crew set the 3 ADRs to OFF to replace the PFD’s
normal speed scale and altitude indication by the backup speed scale and GPS altitude indication.
L1 AP+FD......................................................................................................................................... OFF
A/THR.......................................................................................................................................... OFF
�� If at least two AOA probe heating are failed:
PROBE WINDOW HEAT..........................................................................................................ON
ADR 1+2+3 P/B.............................................................................................................................OFF
L2Note: The STALL WARNING is not lost.
L1 SPD......................................................................................................................... FLY THE GREEN
L2 Fly the green area of the speed scale to ensure safe flight.
L1 STBY INST................................................................................................................MAY BE UNREL
L2 Depending on the source of the ADR 3 FAULT, the standby instruments’ indication may be
unreliable. Therefore, standby instrument must be used with care.
L1�� If at least one AOA probe heating is failed:
AVOID ICING CONDITIONS
ALL ADR OFF PROC...............................................................................................................APPLY
L2 Refer to PRO-ABN-34-S ALL ADR OFF
L1
ASSOCIATED PROCEDURES
F/CTL ALTN LAW
(PROT LOST)
USE RUDDER WITH CARE
L2Note: The rudder travel limit is frozen at the value it had at the moment when the failure
occurred, and may not be in correct position for the flight speed. At slats extension, full
rudder travel authority may be recovered.
L1 SPD BRK.......................................................................................................................DO NOT USE
To be continued on next page
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
NAVIGATION
A330/A340 FLEET PRO-ABN-34 P 134/140
FCOM 19 AUG 10
NAV ADR 1+2+3 FAULT (Cont'd)
L12
STATUS
STBY INST................................................MAY BE UNREL
SPD BRK.......................................................DO NOT USE
USE RUDDER WITH CARE
APPR PROC
FOR LDG...................................................................USE FLAP 3
This line is replaced by “FOR LDG: USE FLAP 3” when CONF 3
is selected, as a reminder.
LDG......................................................................... GRVTY EXTN
ALTN LAW: PROT LOST
WHEN L/G DN: DIRECT LAW
INOP SYS
ADR 1+2+3
F/CTL PROT
CAB PR 1+2
RUD TRV LIM
AP 1+2
A/THR
GPWS
GPWS TERR ��
TCAS
See (1)
REAC W/S DET
PRED W/S DET ��
(1)
NL2ote: Upon a triple ADR failure, the TCAS becomes inoperative. However, TCAS is displayed
in the INOP SYS list depending on the TCAS manufacturer.
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
NAVIGATION
A330/A340 FLEET PRO-ABN-34 P 135/140
FCOM 19 AUG 10
NAV ADR 1+2+3 FAULT
Applicable to:
L2 This alert triggers if each of the 3 ADRs self-detects a failure or receives irrelevant data from the
probes. This procedure requires that the flight crew set the 3 ADRs to OFF to replace the PFD’s
normal speed scale and altitude indication by the backup speed scale and GPS altitude indication.
L1 AP+FD......................................................................................................................................... OFF
A/THR.......................................................................................................................................... OFF
�� If at least two AOA probe heating are failed:
PROBE WINDOW HEAT..........................................................................................................ON
ADR 1+2+3..................................................................................................................................OFF
L2Note: The STALL WARNING is not lost.
L1 SPD......................................................................................................................... FLY THE GREEN
　
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