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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 78
VREF = VLS CONF FULL 106 111 116 121 125 130 134 138 142 146 148
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
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 1 300 1 360 1 430 1 480 1 560 1 690 1 840 2 000 2 170
WET runway 1 890 2 010 2 140 2 280 2 420 2 550 2 710 2 850 3 000
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 % + 18 %
WET runway + 3 % + 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
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) 40 44 48 52 56 60 64 68 72 76 78
VREF = VLS CONF FULL 106 111 116 121 125 130 134 138 142 146 148
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:
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
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A318/A319/A320/A321QRH快速检查单QUICK REFERENCE HAND BOOK3(47)
