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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 46/164
FCOM 19 AUG 10
ADR 1+2+3 FAULT
Applicable to:
The ECAM does not display this procedure. In the case of a triple ADR failure, the ECAM only
displays dual ADR warnings.
ADR (all)......................................................................................................................................OFF
STBY INST (ALT + ASI)...............................................................................................................USE
Note: Disregard ECAM actions for AIR DATA SWTG and ATC, because these have no effect in
the case of a total loss of ADRs.
ASSOCIATED PROCEDURES
F/CTL ALTN LAW
(PROT LOST)
Note: The STALL WARNING is lost.
MAX SPEED..........................................................................................................................320/0.82
See the following table for the IAS/M relationship for 0.82
FL 390 370 350 330 310 290 280 and below
MAX SPD 252 265 278 290 305 315 320
WHEN L/G DN: DIRECT LAW
At landing gear extension, control reverts to direct law in pitch, as well as in roll Refer to
PRO-ABN-27-J F/CTL DIRECT LAW.
Note: Use manual control of cabin pressurization:
MODE SEL.................................................................................................................... MAN
MAN V/S CT......................................................................................................... AS RQRD
These lines are not displayed on the ECAM. (For details, Refer to PRO-ABN-21-D AIR
PACK 1 + 2 FAULT).
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 47/164
FCOM 19 AUG 10
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.
CAT 1 ONLY
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.
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
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 48/164
FCOM 19 AUG 10
ADR 1+2+3 FAULT (Cont'd)
RAT automatic extension.
(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
　
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