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�� WHEN SPD 200 KT
L/G..................................................................................................................................
.. GRVTY EXTN
�� WHEN L/G down: USE MAN PITCH TRIM
For Flaps extension: SPD
SEL.......................................................................................VFE NEXT- 5KT
When in landing CONF: DECELERATE TO CALCULATED VAPP
LANDING
FLARE: Only one ELEV and two spoilers per wing. No ailerons.
A/C slightly sluggish – Direct law
SPOILERS: Only 2 per wing
REVERSER: Only N°2
BRAKING: ALTERNATE
NO?NOSE?WHEEL?STEERING
LANDING
FLARE: Only one ELEV and two spoilers per wing. No ailerons.
A/C slightly sluggish – Direct law
SPOILERS: Only 2 per wing
REVERSER: Only N°2
BRAKING: ALTERNATE
GO-AROUND
NO GEAR RETRACTION. Increased fuel consumption
�� For circuit:
MAINTAIN SLATS/FLAPS CONFIGURATION
Recommended speed: MAX SPD - 10 kt
�� For diversion:
SELECT CLEAN CONFIGURATION
If Slats at zero: Normal operating speeds
If Slats not at zero: Recommended speed MAX SPD - 10 kt
ACTUAL LANDING DISTANCES (m) WITH FAILURE WITHOUT REV
(See )
WEIGHT (1 000 KG) 40 44 48 52 56 60 64 68 72 76
DRY runway 1 280 1 280 1 300 1 360 1 410 1 450 1 520 1 600 1 740 1 870
WET runway 1 890 1 890 1 960 2 080 2 210 2 310 2 420 2 570 2 710 2 800
CONTA runway Refer to FPE-IFL Landing Distance Without AUTOBRAKE
- CONF FULL and apply LDG DIST Factor = 1.95
ABN-29
3/4
AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1
ABNORMAL AND
EMERGENCY PROCEDURES 30 AUG 10
A318/A319/A320/A321 FLEET , , , , , , , ,
,
CORRECTIONS + 1 000 ft above SL + 10 kt tailwind
DRY runway + 3 % + 19 %
WET runway + 3 % + 23 %
(1) If the credit of the remaining reverser needs to be taken into account, Refer to
ABN-80 LDG CONF/APPR SPD/LDG DIST On
Dry Runways Following Failures - Introduction.
Refer to ABN-80 VAPP CALCULATION for approach speed computation method.
ABN-29
4/4
AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1
ABNORMAL AND
EMERGENCY PROCEDURES 30 AUG 10
A318/A319/A320/A321 FLEET , , , , , , , ,
,
HYD G + Y SYS LO PR SUMMARY
CRUISE
MAX
SPD..................................................................................................................................
....... 320/0.77
MANEUVER WITH CARE
ALTN LAW : PROT LOST
LANDING CONF APPROACH SPEED
Use FLAP 3 VAPP = VREF + 25 kt
W (1000 KG) 44 48 52 56 60 64 68 72 76
VREF = VLS CONF FULL 110 113 117 122 126 130 134 138 142
APPROACH
CAT 2 INOP SLATS SLOW / FLAPS JAMMED
GPWS FLAP
MODE.............................................................................................................................
.. OFF
�� For Flaps extension:
SPD SEL.......................................................................................................................
VFE NEXT - 5KT
When in landing
CONF
: DECELERATE TO CALCULATED VAPP
Stabilize at VAPP before L/G down, to be trimmed for approach.
L/G GRAVITY EXTENSION
LANDING
FLARE: PITCH AUTHORITY REDUCED (No stabilizer).
MAN TRIM Unusable
Only 1 spoiler per wing – Direct law
SPOILERS: Only 1 per wing
NO?REVERSER
BRAKING: BRK Y ACCU PR ONLY (7 applications)
MAX BRK PR 1 000 PSI
NO?NOSEWHEEL?STEERING
GO-AROUND
NO GEAR RETRACTION. Increased fuel consumption
�� For circuit:
MAINTAIN SLATS/FLAPS CONFIGURATION
Recommended?speed: MAX SPD – 10 kt
�� For diversion:
�� If Flaps at zero:
SELECT CLEAN CONFIGURATION
Normal operating speeds
�� If Flaps not at zero:
MAINTAIN SLATS/FLAPS CONFIG
Recommended?speed: MAX SPD – 10 kt
ACTUAL LANDING DISTANCES (m) WITH FAILURE WITHOUT REV
WEIGHT (1 000 KG) 40 44 48 52 56 60 64 68 72 76
DRY runway 1 900 1 900 1 930 2 010 2 090 2 150 2 260 2 370 2 590 2 780
WET runway Refer to FPE-IFL Landing Distance Without AUTOBRAKE
- CONF FULL and apply LDG DIST Factor = 2.10
CONTA runway Refer to FPE-IFL Landing Distance Without AUTOBRAKE
- CONF FULL and apply LDG DIST Factor = 2.05
CORRECTIONS + 1 000 ft above SL + 10 kt tailwind
DRY runway + 3 % + 19 %
Refer to ABN-80 VAPP CALCULATION for approach speed computation method.
ABN-29
1/4
AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1
ABNORMAL AND
EMERGENCY PROCEDURES 30 AUG 10
A318/A319/A320/A321 FLEET , , , , ,
HYD B + Y SYS LO PR SUMMARY
CRUISE
MAX
SPD..................................................................................................................................
　
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