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....... 320/0.77
MANEUVER WITH CARE
ALTN LAW : PROT LOST
LANDING CONF APPROACH SPEED
Use FLAP 3 VAPP = VREF + 25 kt
W (1 000 KG) 40 44 48 52 56 60 64 68 72 76 78
VREF = VLS CONF FULL 106 111 116 121 125 129 134 138 142 146 147
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
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
Intentionally left blank
A318/A319/A320/A321 FLEET , , MSN,
ABN-29
1/4
AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1
ABNORMAL AND
EMERGENCY PROCEDURES 30 AUG 10
A318/A319/A320/A321 FLEET MSN
HYD B + Y SYS LO PR SUMMARY
CRUISE
MAX
SPD..................................................................................................................................
......... 320/.77
MANEUVER WITH CARE
Flight controls remain in normal law.
LANDING CONF APPROACH SPEED
Use FLAP 3 VAPP = VREF + 10 kt + APPR COR
W (1 000 KG) 52 56 60 64 68 72 76 80 84 86
VREF = VLS CONF FULL 116 121 125 129 133 137 141 144 148 150
APPROACH
SLATS SLOW/FLAPS SLOW CAT 2 INOP
GPWS LDG FLAP
3.................................................................................................................................ON
L/G GRAVITY EXTENSION
LANDING
FLARE Only one ELEV and two spoilers per wing
SPOILERS Only 2 per wing
REVERSER Only N°1
BRAKING NORMAL
NO?NOSEWHEEL?STEERING
GO-AROUND
NO GEAR RETRACTION. Increased fuel consumption
ACTUAL LANDING DISTANCES (m) WITH FAILURE WITHOUT REV
(See )
WEIGHT (1000
KG) 58 62 66 70 74 78 82 86 90 94
DRY runway 1 400 1 450 1 520 1 590 1 650 1 740 1 840 2 200 2 350 2 500
WET runway 1 860 1 980 2 090 2 220 2 330 2 430 2 560 2 760 2 920 3 080
CONTA
runway Refer to FPE-IFL Landing Distance Without AUTOBRAKE - CONF FULL
and apply LDG DIST Factor = 1.75
CORRECTIONS + 1 000 ft above SL + 10 kt tailwind
DRY runway + 4 % + 17 %
WET runway + 4 % + 21 %
(1) If the credit of the remaining reverser needs to be taken into account, Refer to
ABN-80-B LDG CONF/APPR SPD/LDG DIST
On Dry Runways Following Failures - 29 - HYD.
Refer to ABN-80 VAPP CALCULATION for approach speed computation method.
ABN-29
2/4
AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1
ABNORMAL AND
EMERGENCY PROCEDURES 30 AUG 10
A318/A319/A320/A321 FLEET MSN
HYD G + B SYS LO PR SUMMARY
CRUISE
SPD
BRK.................................................................................................................................
DO NOT USE
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) 52 56 60 64 68 72 76 80 84 86
VREF = VLS CONF FULL 116 121 125 129 133 137 141 144 148 150
APPROACH
SLATS JAMMED/FLAPS SLOW CAT 2 INOP
ATHR..............................................................................................................................
.........................OFF
GPWS LDG FLAP
3.................................................................................................................................ON
�� WHEN SPD 200 KT
L/G..................................................................................................................................
　
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