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LANDING CONF APPROACH SPEED
3 VAPP = VREF +6 kt + APPR COR
FULL VAPP = VREF + APPR COR
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
SLATS SLOW/FLAPS SLOW CAT 2 INOP
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) 46 50 54 58 62 66 70 74 78
DRY runway
(CONF` full)
1 210 1 280 1 330 1 390 1 460 1 560 1 720 1 880 2 020
DRY runway
(CONF 3)
1 210 1 280 1 330 1 390 1 460 1 560 1 720 1 880 2 020
WET runway
(CONF full)
1 700 1 810 1 920 2 060 2 190 2 320 2 460 2 590 2 700
WET runway
(CONF 3)
1 740 1 860 1 970 2 110 2 250 2 380 2 520 2 660 2 770
CONTA
runway
(CONF full)
Refer to FPE-IFL Landing Distance Without AUTOBRAKE - CONF FULLand apply
LDG DIST Factor = 1.75
CONTA
runway
(CONF 3)
Refer to FPE-IFL Landing Distance Without AUTOBRAKE - CONF FULLand apply
LDG DIST Factor = 1.90
CORRECTIONS + 1 000 ft above SL + 10 kt tailwind
DRY runway + 3 % + 18 %
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) 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
SLATS JAMMED/FLAPS SLOW CAT 2 INOP
ATHR..............................................................................................................................
.........................OFF
GPWS LDG FLAP
3.................................................................................................................................ON
�� 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
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) 46 50 54 58 62 66 70 74 78
DRY runway 1 280 1 360 1 410 1 470 1 540 1 650 1 820 1 980 2 130
WET runway 1 830 1 950 2 080 2 220 2 360 2 510 2 650 2 790 2 920
CONTA runway Refer to FPE-IFL Landing Distance Without AUTOBRAKE
- CONF FULL and apply LDG DIST Factor = 1.95
CORRECTIONS + 1 000 ft above SL + 10 kt tailwind
DRY runway + 3 % + 18 %
WET runway + 4 % + 21 %
(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
3/4
AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1
ABNORMAL AND
EMERGENCY PROCEDURES 30 AUG 10
A318/A319/A320/A321 FLEET , , MSN,
HYD G + Y SYS LO PR SUMMARY
CRUISE
MAX
SPD..................................................................................................................................
　
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