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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 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**).
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 57/140
FCOM 19 AUG 10
NAV IR 1+2 (1+3) (2+3) FAULT (Cont'd)
L12
STATUS
SPD BRK.......................................................DO NOT USE
MAX SPEED............................................................ 330/.82
APPR PROC:
FOR LDG...................................................................USE FLAP 3
�� 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**).
NAV EXTREME LATITUDE
Applicable to: ,
NORTH REF SEL.......................................................................................................................TRUE
L2 The magnetic heading is replaced by the true heading on EFIS and DDRMI.
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
NAVIGATION
A330/A340 FLEET PRO-ABN-34 P 58/140
FCOM 19 AUG 10
NAV EXTREME LATITUDE
Applicable to:
NORTH REF SEL.......................................................................................................................TRUE
L2 The magnetic heading is replaced by the true heading on EFIS.
OVERSPEED
Applicable to:
VMO/MMO.............................................................................................................................. 330/.86
L2 255/.60 in case of dispatch with landing gear down.
L1 VLE......................................................................................................................................... 250/.55
VFE................................................................................................................................SEE BELOW
CONF VFE
FULL
32
1*
1 + F
1
180
186
196
205
215
255
OVERSPEED
Applicable to: ,
VMO/MMO.............................................................................................................................. 330/.86
L2 255/.60 in case of dispatch with landing gear down.
L1 VLE......................................................................................................................................... 250/.55
VFE................................................................................................................................SEE BELOW
CONF VFE
FULL
32
1*
　
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