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A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
NAVIGATION
A330/A340 FLEET PRO-ABN-34 P 59/140
FCOM 19 AUG 10
NAV HDG DISCREPANCY
Applicable to: ALL
HDG....................................................................................................................................X CHECK
L2Compare the 3 IR headings on the MCDU page, or crosscheck with the standby compass.
L1 ATT HDG SWTG................................................................................................................. AS RQRD
L2 Select IR 3 to the faulty side.
NAV ATT DISCREPANCY
Applicable to: ALL
ATT.....................................................................................................................................X CHECK
L2Crosscheck with the standby horizon.
L1 ATT HDG SWTG................................................................................................................. AS RQRD
L2 Select IR 3 to the faulty side.
NAV ALTI DISCREPANCY
Applicable to: ALL
ALT..................................................................................................................................... X CHECK
L2Crosscheck with the standby altimeter.
L1 AIR DATA SWTG................................................................................................................ AS RQRD
L2 Select ADR 3 to the faulty side.
NAV BARO REF DISCREPANCY
Applicable to: ALL
L2 This caution is triggered, if there is a difference between the barometer reference selections on the
FCU control panels.
L1 BARO REF...........................................................................................................................X CHECK
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
NAVIGATION
A330/A340 FLEET PRO-ABN-34 P 60/140
FCOM 19 AUG 10
NAV IAS DISCREPANCY
Applicable to: ,
AIR SPD.............................................................................................................................X CHECK
AIR DATA SWTG................................................................................................................ AS RQRD
STATUS
CAT 3 SINGLE ONLY INOP SYS
CAT 3 DUAL
NAV IAS DISCREPANCY
Applicable to: MSN ,
,
AIR SPD.............................................................................................................................X CHECK
AIR DATA SWTG................................................................................................................ AS RQRD
STATUS
CAT 3 SINGLE ONLY INOP SYS
CAT 3 DUAL
NAV RA 1(2) FAULT
Applicable to: ,
GPWS (ONLY IN CASE OF AN RA 1 FAULT)............................................................................ OFF
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 61/140
FCOM 19 AUG 10
NAV RA 1(2) FAULT (Cont'd)
STATUS
CAT 2 ONLY INOP SYS
CAT 3
GPWS (if RA 1 fault)
RA 1(2)
NAV RA 1(2) FAULT
Applicable to:
GPWS SYS (ONLY IN CASE OF AN RA 1 FAULT)....................................................................OFF
STATUS
CAT 2 ONLY INOP SYS
CAT 3
GPWS (if RA 1 fault)
RA 1(2)
NAV RA 1+2 FAULT
Applicable to: ,
GPWS..........................................................................................................................................OFF
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 62/140
FCOM 19 AUG 10
NAV RA 1+2 FAULT (Cont'd)
L12
STATUS
On the ECAM, only one of the following two statements are
displayed, depending on the autopilot status.
Use manual pitch trim when flare law is active.
�� WHEN L/G DN:
MAN PITCH TRIM............................................................USE
Provided the autopilot is off, switching to flare law occurs at
landing gear extension.
�� WHEN L/G DN AND AP OFF:
MAN PITCH TRIM............................................................USE
When the autopilot is engaged, and the landing gear
is extended, switching to flare law occurs at autopilot
disengagement.
ILS APPR mode cannot be engaged, LOC mode is available via
the FCU LOC pb.
INOP SYS
RA 1+2
A/CALL OUT
CAT 2
GPWS
NAV RA 1+2 FAULT
　
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