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law, and to avoid autopilot/autothrust disconnection.
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 31/140
FCOM 19 AUG 10
NAV IR 1(2)(3) FAULT (Cont'd)
L2Note: In case of a simultaneous ADR and IR (same ADIRU) failure, apply the ADR FAULT
procedure before to the IR FAULT procedure.
L1 ATT HDG SWTG.............................................................................CAPT ON 3 (F/O ON 3) (NORM)
L2 Select IR 3 to the affected side.
L1�� If IR available in ATT mode:
IR (AFFECTED) MODE SEL.................................................................................................. ATT
L2 For IR alignment in ATT mode, Refer to 99 Duref Cible FCOM.
L1�� If IR totally faulty:
IR (AFFECTED) P/B...............................................................................................................OFF
L2 Set the IR pb to OFF.
Note: If desired, one attempt may be made to realign a faulty IRS (light steady) in ATT
mode by setting the IR MODE rotsel to OFF, then to ATT. However, in this case, the
ATT HDG SWTG rotsel must be in the same position as the AIR DATA SWTG rotsel
during the reset, to prevent the flight controls from temporarily reverting to alternate
law, and to avoid autopilot/autothrust disconnection.
L12
STATUS
CAT 3 SINGLE ONLY INOP SYS
IR 1 (2) (3)
CAT 3 DUAL
GPWS TERR (If IR1 fault)
TCAS
See (1)
(1)
NL2ote: In case of an IR 1 fault, the TCAS may be inoperative (depending on the TCAS
manufacturer). If the IR 1 is available in ATT mode, the TCAS can be recovered by
entering the aircraft magnetic heading into the CDU, as per IR ALIGNMENT IN ATT
MODE procedure (Refer to 00011424 **Not found**).
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
NAVIGATION
A330/A340 FLEET PRO-ABN-34 P 32/140
FCOM 19 AUG 10
NAV IR 1(2)(3) FAULT
Applicable to:
L2Note: In case of a simultaneous ADR and IR (same ADIRU) failure, apply the ADR FAULT
procedure before to the IR FAULT procedure.
L1 ATT HDG SWTG.............................................................................CAPT ON 3 (F/O ON 3) (NORM)
L2 Select IR 3 to the affected side.
L1�� If IR available in ATT mode:
IR MODE SEL.........................................................................................................................ATT
L2 For IR alignment in ATT mode, Refer to 99 Duref Cible FCOM.
L1�� If IR totally faulty:
IR...........................................................................................................................................OFF
L2 Set the IR pb to OFF.
Note: If desired, one attempt may be made to realign a faulty IRS (light steady) in ATT
mode by setting the IR MODE rotsel to OFF, then to ATT. However, in this case, the
ATT HDG SWTG rotsel must be in the same position as the AIR DATA SWTG rotsel
during the reset, to prevent the flight controls from temporarily reverting to alternate
law, and to avoid autopilot/autothrust disconnection.
L12
STATUS
CAT 3 SINGLE ONLY INOP SYS
IR 1 (2) (3)
CAT 3 DUAL
GPWS TERR (If IR1 fault)
TCAS
See (1)
(1)
NL2ote: In case of an IR 1 fault, the TCAS may be inoperative (depending on the TCAS
manufacturer). If the IR 1 is available in ATT mode, the TCAS can be recovered by
entering the aircraft magnetic heading into the CDU, as per IR ALIGNMENT IN ATT
MODE procedure (Refer to 00011424 **Not found**).
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
NAVIGATION
A330/A340 FLEET PRO-ABN-34 P 33/140
FCOM 19 AUG 10
IR ALIGNMENT IN ATT MODE
Applicable to:
If IR alignment is lost in flight, the navigation mode is inoperative (red ATT flag on the PFD, and red
HDG flag on the ND).
Aircraft attitude and heading may be recovered by applying the following procedure : The aircraft
must stay level, with a constant speed for 30 s.
MODE SELECTOR.......................................................................................................................ATT
LEVEL A/C ATTITUDE...............................................................................................................HOLD
CONSTANT A/C SPEED.................................................................................................... MAINTAIN
�� MCDU INITIALIZATION:
DATA (MCDU KEY)...........................................................................................................PRESS
The DATA INDEX page is displayed.
　
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