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NAVIGATION
A318/A319/A320/A321 FLEET PRO-ABN-34 P 56/164
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
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.
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.
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 57/164
FCOM 19 AUG 10
NAV IR 1(2)(3) FAULT (Cont'd)
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.
NAV IR 1(2)(3) FAULT
Applicable to: ,
MSN,,,,
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.
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 58/164
FCOM 19 AUG 10
NAV IR 1(2)(3) FAULT (Cont'd)
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.
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.
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 59/164
FCOM 19 AUG 10
NAV IR 1(2)(3) FAULT (Cont'd)
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
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A320机组操作手册FLIGHT CREW OPERATING MANUAL 10(68)
