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TRAJECTORY...........................................................................................STABILISE
ASAP
LDG DIST
PROC............................................................................................................................A
PPLY
Refer to ABN-80-B LDG CONF/APPR SPD/LDG DIST On Dry Runways Following
Failures - 27 -
FLT/CTL.
ON GROUND
DIFFERENTIAL
BRAKING.........................................................................................................USE
ASAP
Do not use asymmetric reverse thrust.
Use nosewheel steering handle below 70 kt.
STABILIZER JAM
The ELACs may not detect a stabilizer jam when the pitch trim wheel is jammed.
The flight control normal law remains active in this case and there is no ECAM
warning.
AP....................................................................................................................................
........................OFF
MAN PITCH
TRIM.............................................................................................................................
CHECK
The pitch trim wheel may not be fully jammed, the force needed may be higher than
usual.
�� IF MAN TRIM AVAIL:
TRIM FOR NEUTRAL ELEV
If manual pitch trim is available, trim to maintain the elevator at the zero position
(indications on ECAM
F/CTL page).
APPR PROC
�� IF MAN TRIM NOT AVAIL:
FOR
LDG..........................................................................................................................USE
FLAP 3
Do not select configuration full so as not to degrade the handling qualities.
GPWS LDG FLAP
3.........................................................................................................................ON
CAT 2 INOP
ABN-27
4/4
AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1
ABNORMAL AND
EMERGENCY PROCEDURES 30 AUG 10
Intentionally left blank
A318/A319/A320/A321 FLEET MSN
ABN-28
1/4
AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1
ABNORMAL AND
EMERGENCY PROCEDURES 30 AUG 10
A318/A319/A320/A321 FLEET , , , , , , , ,
, , , , , , , , , ,
FUEL IMBALANCE
FOB.................................................................................................................................
...................CHECK
Compare the FOB + FU, with the FOB at departure.
If the difference is significant, or if the FOB + FU decreases, suspect a fuel leak.
CAUTION A fuel imbalance may indicate a fuel leak.
Do not apply this procedure, if a fuel leak is suspected.
Refer to ABN-28 FUEL LEAK.
FUEL X
FEED...............................................................................................................................
............ON
�� On the lighter side and in the center tank:
FUEL
PUMPS............................................................................................................................
.......OFF
�� When fuel is balanced:
FUEL PUMPS (WING +
CTR).............................................................................................................ON
FUEL X
FEED...............................................................................................................................
... OFF
ABN-28
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AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1
ABNORMAL AND
EMERGENCY PROCEDURES 30 AUG 10
A318/A319/A320/A321 FLEET , , , , , , , ,
, , , , , , , , , ,
FUEL LEAK
A fuel leak may be detected, if:
The sum of FOB and FU significantly less ‐ than FOB at engine start or is
decreasing, or
‐ A passenger observes fuel spray from engine/pylon or wing tip, or
‐ The total fuel quantity is decreasing at an abnormal rate, or
‐ A fuel imbalance is developing, or
‐ Fuel quantity in a tank is decreasing too fast (leak from engine/pylon, or hole in a
tank), or
‐ The Fuel flow is excessive (leak from engine), or
‐ Fuel is smelt in the cabin.
If visibility permits, leak source may be identified by a visual check from the cabin.
WHEN A LEAK IS CONFIRMED
LAND ASAP
�� LEAK FROM ENGINE/PYLON CONFIRMED:
Engine fuel leak can be confirmed by excessive fuel flow indication, or a visual
check.
THR LEVER (of affected
engine).................................................................................................. IDLE
ENG MASTER (of affected
engine)............................................................................................... OFF
FUEL X FEED..............................................................................................................
　
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