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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 1 790 1 820 1 900 1 980 2 070 2 150 2 230 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 % + 18 %
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..................................................................................................................................
......... 320/.77
MANEUVER WITH CARE
Flight controls remain in normal law.
LANDING CONF APPROACH SPEED
3 VAPP = VREF +10 kt + APPR COR
FULL VAPP = VREF + APPR COR
W (1 000 KG) 40 44 48 52 56 60 64 68 72 76
VREF = VLS CONF FULL 106 107 112 117 121 125 129 133 137 141
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) 40 44 48 52 56 60 64 68 72 76
DRY runway
(CONF full)
1 210 1 230 1 280 1 340 1 390 1 450 1 500 1 600 1 740 1 870
DRY runway
(CONF 3)
1 170 1 190 1 250 1 300 1 350 1 410 1 460 1 550 1 700 1 820
WET runway
(CONF full)
1 620 1 660 1 780 1 900 1 990 2 090 2 210 2 340 2 460 2 540
WET runway
(CONF 3)
1 660 1 700 1 820 1 940 2 040 2 140 2 260 2 400 2 520 2 600
CONTA
runway
(CONF full)
Refer to FPE-IFL Landing Distance Without AUTOBRAKE - CONF FULLand apply
LDG DIST Factor = 1.80
CONTA
runway
(CONF 3)
Refer to FPE-IFL Landing Distance Without AUTOBRAKE - CONF FULLand apply
LDG DIST Factor = 1.95
CORRECTIONS + 1 000 ft above SL + 10 kt tailwind
DRY runway + 3 % + 18 %
WET runway + 4 % + 22 %
(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
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
VREF = VLS CONF FULL 106 107 112 117 121 125 129 133 137 141
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
NO?NOSE?WHEEL?STEERING
GO-AROUND
NO GEAR RETRACTION. Increased fuel consumption
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A318/A319/A320/A321QRH快速检查单QUICK REFERENCE HAND BOOK3(51)
