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FCOM 19 AUG 10
NAV ADR 1+2 (1+3) (2+3) FAULT (Cont'd)
L2 Flight control normal laws are lost. Pitch alternate law preserves the neutral static stability. All
protections, except maneuver protections are lost.
L1�� ADR 1+2 FAULT:
AIR DATA SWTG..............................................................................................................CAPT 3
L2 Set ADR 3 pb-sw (if available) to the captain's side.
L1 ADR (AFFECTED) P/B...........................................................................................................OFF
L2 The GPWS TERR FAULT light comes on, as the enhanced functions of the EGPWS are
inhibited. As such, the GPWS TERR pb-sw should be switched OFF.
L1
ASSOCIATED PROCEDURES
F/CTL ALTN LAW
(PROT LOST)
MAX SPEED...................................................................................................................... 320 KT
L2 Speed is limited, due to the loss of high-speed protections.
L1�� ADR 1+3 (or 2+3) FAULT:
L2 Air data information is lost on one PFD.
Note: In case of an ADR 1+3 pb-sw FAULT, the landing gear safety valve is controlled
closed:
Landing ‐ gear retraction is inoperative
‐ Landing gear extension must be performed by gravity.
L1 AIR DATA SWTG................................................................................................................NORM
ATC (IF ADR 1 FAILED).....................................................................................................SYS 2
ATC (IF ADR 2 FAILED).....................................................................................................SYS 1
ADR (AFFECTED) P/B...........................................................................................................OFF
L2 In case of an ADR 1+3 pb-sw FAULT, the GPWS TERR FAULT light comes on, as the
enhanced functions of the EGPWS are inhibited. As such, the GPWS TERR pb-sw should be
switched OFF.
L1
ASSOCIATED PROCEDURES
F/CTL ALTN LAW
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 41/164
FCOM 19 AUG 10
NAV ADR 1+2 (1+3) (2+3) FAULT (Cont'd)
(PROT LOST)
MAX SPEED...................................................................................................................... 320 KT
L2 Speed is limited, due to the loss of high-speed protections.
L12
STATUS
MAX SPEED............................................................ 320 KT
APPR PROC
FOR LDG...................................................................USE FLAP 3
Do not select CONF FULL to not degrade handling qualities.
GPWS LDG FLAP 3................................................................. ON
Appears when CONF 3 is selected.
�� If ADR 1+3 pb-sw FAULT
L/G.................................................................... GRVTY EXTN
Refer to PRO-ABN-32-B L/G GEAR NOT UPLOCKED -
FWSPAGE
APPR SPD............................................................. VREF + 10 KT
LDG DIST PROC................................................................APPLY
Refer to 99 Duref Cible QRH, or to the Refer to 99 Duref Cible
FCOM.
ALTN LAW : PROT LOST
WHEN L/G DN : DIRECT LAW
At L/G extension, control reverts to direct law in pitch and roll
(Refer to STLO-ABN-27-J F/CTL DIRECT LAW).
�� ADR 1 + 3 (or 2 + 3) pb-sw FAULT:
BOTH PFD ON THE SAME FAC
In the case of an ADR 1 + 3 pb-sw FAULT, the GPWS TERR
FAULT light comes on, because the enhanced EGPWS
functions are inhibited. So, the GPWS TERR pb-sw should
be switched OFF.
INOP SYS
F/CTL PROT
ADR 1 + 2 or (2 + 3) or (1 + 3)
AP 1 + 2
A/THR
RUD TRV LIM 1(2) (1)
GPWS (if ADR1 fault)
yaw damper 1(2) (1)
CAT 2
(1) (in the case of an ADR 1 + 3 FAULT or in the case of an ADR 2 + 3 FAULT)
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
NAVIGATION
A318/A319/A320/A321 FLEET PRO-ABN-34 P 42/164
FCOM 19 AUG 10
NAV ADR 1+2 (1+3) (2+3) FAULT
Applicable to: , , MSN,,,
L2 Flight control normal laws are lost. Pitch alternate law preserves the neutral static stability. All
protections, except maneuver protections are lost.
L1�� ADR 1+2 FAULT:
AIR DATA SWTG..............................................................................................................CAPT 3
L2 Set ADR 3 pb-sw (if available) to the captain's side.
L1 ADR (AFFECTED) P/B...........................................................................................................OFF
　
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