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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 DIST PROC................................................................APPLY
Refer to 99 Duref Cible QRH, or to the Refer to 99 Duref Cible
FCOM.
�� If the trim tank pump is operative:
�� IF CG AFT 32 %:
T TANK MODE..........................................................FWD
Fuel consumption is increased by approximately 1 %.
�� If the trim tank pump is inoperative, or not installed:
�� IF CG AFT 32 % AND WHEN SPD > 270 KT AND NOT
IN CLIMB:
T TANK MODE..........................................................FWD
Fuel consumption is increased by approximately 1 %.
ALTN LAW: PROT LOST
INOP SYS
F/CTL PROT
IR 1+2(1+3)(2+3)
AP 1+2
A/THR
GPWS TERR (If IR1 FAULT)
TCAS
See (1)
CAT 2
(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 the 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 40/140
FCOM 19 AUG 10
NAV IR 1+2 (1+3) (2+3) FAULT
Applicable to: MSN , ,
ATT HDG SWTG................................................................................. CAPT ON 3 (NORM) (NORM)
�� If IR (affected) available in ATT mode:
IR (AFFECTED) MODE SEL.................................................................................................. ATT
�� If IR (affected) totally faulty:
IR (AFFECTED) P/B...............................................................................................................OFF
L2Note: The crewmember on the affected side can recover IR information, by using the EFIS
DMC rotary selector (copy of the opposite side).
L1 SPD BRK.......................................................................................................................DO NOT USE
�� If the trim tank pumps are operative:
�� IF CG AFT 32 %:
T TANK MODE................................................................................................................FWD
L2 Fuel consumption is increased by approximately 1 %.
L1�� If the trim tank pumps are inoperative, or not installed:
�� IF CG AFT 32 % AND WHEN SPD > 270 KT AND NOT IN CLIMB:
T TANK MODE................................................................................................................FWD
L2 Fuel consumption is increased by approximately 1 %.
L1
ASSOCIATED PROCEDURES
F/CTL ALTN LAW
(PROT LOST)
MAX SPEED...........................................................................................................................330/.82
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 41/140
FCOM 19 AUG 10
NAV IR 1+2 (1+3) (2+3) FAULT (Cont'd)
L12
STATUS
SPD BRK.......................................................DO NOT USE
MAX SPEED............................................................ 305/.82
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 DIST PROC................................................................APPLY
Refer to 99 Duref Cible QRH, or to the Refer to 99 Duref Cible
FCOM.
�� If the trim tank pump is operative:
�� IF CG AFT 32 %:
T TANK MODE..........................................................FWD
Fuel consumption is increased by approximately 1 %.
�� If the trim tank pump is inoperative, or not installed:
�� IF CG AFT 32 % AND WHEN SPD > 270 KT AND NOT
IN CLIMB:
T TANK MODE..........................................................FWD
Fuel consumption is increased by approximately 1 %.
ALTN LAW: PROT LOST
INOP SYS
F/CTL PROT
IR 1+2(1+3)(2+3)
AP 1+2
A/THR
GPWS TERR (if IR 1 fault)
TCAS
See (1)
CAT 2
(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 the IR ALIGNMENT IN ATT
MODE procedure (Refer to 00011424 **Not found**).
　
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