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ADR 1+2+3 FAULT (Cont'd)
STATUS
MAX SPEED.......................................................... 320/0.82
RUD WITH CARE ABV 160 KT
See (1)
APPR PROC
FOR LDG...................................................................USE FLAP 3
Do not select CONF FULL, so as not to degrade handling
qualities.
GPWS LDG FLAP 3................................................................. ON
Displayed, when CONF 3 is selected.
APPR SPD...............................................................VREF +10 KT
LDG DIST PROC................................................................APPLY
Refer to 99 Duref Cible QRH, or to the Refer to 99 Duref Cible
FCOM.
Note: As the landing gear safety valve is closed, landing
gear extension must be performed by gravity(Refer to
STLO-ABN-32 L/G GRAVITY EXTENSION).
WHEN L/G DN : DIRECT LAW
At landing gear extension, control reverts to direct law in pitch, as
well as in roll.
DURING FINAL APPR
V/S CTL.................................................................... FULL UP
Note: In case of a go-around, respect the maximum
speed of 215 kt in CONF 1+F, due to loss of flap
auto retraction to CONF 1.
CAUTION Check that the outflow valve is fully open
and that cabin altitude is at airfield elevation
before opening the doors.
RAT automatic extension.
INOP SYS
F/CTL PROT
WINDSHEAR DET
GPWS
ADR 1+2+3
AP 1+2
A/THR
RUD TRV LIM 1+2
CAB PR 1+2
Other INOP SYS
CAT 2
ATC ALTI MODE
TCAS
L/G RETRACT
To be continued on next page
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
NAVIGATION
A318/A319/A320/A321 FLEET PRO-ABN-34 P 54/164
FCOM 19 AUG 10
ADR 1+2+3 FAULT (Cont'd)
(1) The rudder travel limit value is frozen at the moment when the failure occurs. Therefore, to
prevent damage to the aircraft structure, use the rudder with care, when the speed is above
160 kt . At slats’ extension, full rudder travel authority is recovered.
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 prior to the IR FAULT procedure.
L1 IR 1 FAULT:
ATT HDG SWTG..................................................................................................................CAPT
IR 2 FAULT:
ATT HDG SWTG..................................................................................................................... F/O
IR 3 FAULT:
ATT HDG SWTG (IF IR 3 IN USE)....................................................................................NORM
L2 This line is not displayed on the ECAM.
L12
STATUS
IR MAY BE AVAIL IN ATT
Refer to 99 Duref Cible FCOM
CAT 3 SINGLE ONLY
INOP SYS
IR 1(2)(3)
CAT 3 DUAL
GPWS TERR
TCAS
See (1)
(1)
L12
Note: 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.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
NAVIGATION
A318/A319/A320/A321 FLEET PRO-ABN-34 P 55/164
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 prior to the IR FAULT procedure.
L1 IR 1 FAULT:
ATT HDG SWTG.............................................................................................................. CAPT 3
IR 2 FAULT:
ATT HDG SWTG..................................................................................................................F/O 3
IR 3 FAULT:
ATT HDG SWTG (IF IR 3 IN USE)....................................................................................NORM
L2 This line is not displayed on the ECAM.
L12
STATUS
IR MAY BE AVAIL IN ATT
Refer to 99 Duref Cible FCOM
CAT 3 SINGLE ONLY
INOP SYS
IR 1(2)(3)
CAT 3 DUAL
GPWS TERR
TCAS
See (1)
(1)
L12
Note: 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.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
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A320机组操作手册FLIGHT CREW OPERATING MANUAL 10(67)
