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Note: Disregard ECAM actions for AIR DATA SWTG and ATCsince these have no
effect in the case of
a total loss of ADRs.
ASSOCIATED PROCEDURES
F/CTL ALTN LAW
(PROT 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 .
Note: Use manual control of cabin pressurizationRefer to FCOM/99 Duref Cible
QRH
MODE
SEL..............................................................................................................................M
AN
MAN V/S
CTL...................................................................................................................AS RQRD
STATUS
MAX SPEED.................................................................. 320/0.82
RUD WITH CARE ABV 160 kt
See (1)
APPR PROC:
FOR LDG...........................................................................USE FLAP 3
GPWS LDG FLAP 3......................................................................... ON
APPR SPD..................................................................... VREF + 10 KT
LDG DIST PROC........................................................................APPLY
Refer to FCOM/99 Duref Cible QRH
�� FOR L/G GRVTY EXTN (not on the ECAM):
GRVTY GEAR EXTN handcrank.....................................................
............................................................................ PULL AND TURN
L/G LEVER........................................................................... DOWN
WHEN L/G DN : DIRECT LAW
�� DURING FINAL APPR
V/S CTL............................................................................ FULL UP
Note: In case of a go-around, respect maximum speed 215 kt
in CONF 1+F, due to the 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
ATT LIMIT
OVSP LIMIT
ALPHA LIMIT
ADR 1+2+3
WINDSHEAR DET
RUD TRV LIM 1+2
A/THR
AP 1+2
GPWS
Other INOP SYS
CAB PR1+2
RAT auto extension
ATC ALTI MODE
TCAS ��
L/G RETRACT
(1) At slats’ extension, full rudder travel authority is recovered.
ABN-34
2/10
AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1
ABNORMAL AND
EMERGENCY PROCEDURES 30 AUG 10
A318/A319/A320/A321 FLEET
ALL ADR OFF
SPD...................................................................................................................................
FLY THE GREEN
Fly within the green area of the speed scale to ensure safe flight. For slats/flaps
retraction, it is better to fly
at the top of the green area of the speed scale.
CAUTION The altitude displayed on the PFD is a GPS altitude.
BACK UP
NAV................................................................................................................................
........USE
When ADRs are OFF, both FMs are lost.
Revert to Back Up Nav via the NAV B/UP prompt on the MCDU MENU page.
NAVAID
TUNING..........................................................................................................................
.USE RMP
Set both RMPs to NAV.
MANUAL CABIN PRESSURE CONTROL
MODE
SEL..................................................................................................................................
.......MAN
MAN V/S
CTL............................................................................................................................AS
RQRD
MAN CAB PR CTL
TGT V/S : CLIMB 500 ft/min
DESC 300 ft/min
A/C GPS ALT CAB ALT TGT
410
350
300
250
<200
8000
6500
5000
2500
0
FOR APPROACH
SPD...............................................................................................................................
FLY THE GREEN
Before extending the slats/flaps, it is better to fly at the bottom of the speed scale
green area, and to be
in straight flight.
FOR
LDG..............................................................................................................................
USE FLAP 3
LDG DIST
PROC............................................................................................................................A
　
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