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.. DIM
FLARE, TOUCH DOWN AND ROLL OUT
Engines should be shut down sufficiently early to ensure fuel is shut off before the
nacelles impact, but
sufficiently late to ensure adequate hydraulic supplies for the flight controls.
Engine pumps continue to supply adequate hydraulic pressure for 30 s after engine
shutdown.
REVERSE........................................................................................................................
.....DO NOT USE
�� If NOSE L/G abnormal:
NOSE............................................................................................................................
MAINTAIN UP
After touchdown, keep the nose off the runway by use of the elevator. Then, lower the
nose on to
the runway before elevator control is lost.
BRAKES (compatible with elevator
efficiency).......................................................................... APPLY
ENG
MASTERS.......................................................................................................................
......OFF
Shutdown the engines before nose impact.
To be continued on next page
ABN-32
4/4
AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1
ABNORMAL AND
EMERGENCY PROCEDURES 30 AUG 10
A318/A319/A320/A321 FLEET , , , , , , , ,
, , , , , , , MSN,,,
LDG WITH ABNORMAL L/G (Cont'd)
�� If one MAIN L/G abnormal:
ENG
MASTERS.......................................................................................................................
......OFF
At touchdown, shut down both engines.
FAILURE SIDE
WING....................................................................................................MAINTAIN UP
Use roll control, as necessary, to maintain the unsupported wing up as long as
possible.
DIRECTIONAL
CONTROL...................................................................................................
MAINTAIN
Use rudder and brakes (maximum 1 000 PSI) to maintain the runway axis as long as
possible.
�� If both MAIN L/G abnormal:
ENG
MASTERS.......................................................................................................................
......OFF
Shut down the engines in the flare, before touchdown.
PITCH ATTITUDE (at touchdown).......................................................................NOT
LESS THAN 6°
WHEN A/C STOPPED
ENG (all) and APU FIRE
pushbutton................................................................................................ PUSH
Pressing the ENG FIRE pb shuts off the related hydraulic pressure within a short
time.
ENG (all) and APU
AGENT..............................................................................................................DISCH
�� If Evacuation required:
EVACUATION................................................................................................................
........ INITIATE
All emergency and passenger doors may ‐ be used to evacuate the aircraft.
‐ Announce an appropriate command such as “PASSENGER
EVACUATION-EVACUATE
THROUGH LH or RH DOORS” using the Passenger Address (PA) system, and press
the EVAC
COMMAND pushbutton �� .
�� If Evacuation not required:
CABIN CREW and PASSENGERS
(PA)................................................................................. NOTIFY
Ensure that all the landing gears are secured before initiating the disembarkation
(before switching
OFF the seat belts signs).
ABN-34
1/8
AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1
ABNORMAL AND
EMERGENCY PROCEDURES 30 AUG 10
A318/A319/A320/A321 FLEET
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)
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
　
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