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3 F 4.0/74.8 4.0/70.6 4.0/65.0
(1) Due to the fact that the speed is unreliable, the SFCC may select the 1+F
configuration in approach, instead of 1.
FINAL APPROACH AT STANDARD -3 ° DESCENT FLIGHT PATH
LANDING GEAR DOWN
Above 78 t 78 t - 66 t Below 66 t
CONF Speed (kts) Pitch (°)/Thrust (% N1)
3 VLS +10 1.5/59.2 1.5/54.5 1.0/49.8
FLYING TECHNIQUE TO STABILIZE SPEED:
Adjust pitch in order to fly the required flight path.
When target pitch is reached, flying intended flight path, adjust thrust to target.
If the aircraft pitch tends to increase, aircraft is slow, then increase thrust.
If the aircraft pitch tends to decrease, aircraft is fast, then decrease thrust.
AFFECTED ADR(S) IDENTIFICATION
Crosscheck all speeds and altitudes indications.
Alternates sources may be used to evaluate the air data:
‐ GPS altitude
‐ GPS and IRS Group Speeds, taking into account altitude and wind effect.
�� If affected ADR(s) identified:
Affected ADR(s)
P/B.......................................................................................................................OFF
REMAINING AIR
DATA........................................................................................................ CONFIRM
�� If affected ADR(s) cannot be identified or all ADRs are affected:
ALL ADRs
P/B..............................................................................................................................OF
F
All ADRs must be switched off to replace the PFD's normal speed scale and altitude
indication by
the backup speed scale and GPS altitude indication.
NAV ADR 1+2+3 FAULT
ABN-34
10/10
AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1
ABNORMAL AND
EMERGENCY PROCEDURES 30 AUG 10
Intentionally left blank
A318/A319/A320/A321 FLEET
ABN-34
1/6
AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1
ABNORMAL AND
EMERGENCY PROCEDURES 30 AUG 10
A318/A319/A320/A321 FLEET , , , , , MSN,,
ADR 1 + 2 + 3 FAULT
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 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
　
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