曝光臺(tái) 注意防騙 網(wǎng)曝天貓店富美金盛家居專營(yíng)店坑蒙拐騙欺詐消費(fèi)者

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..................................................................................................................................
.. 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) 58 62 66 70 74 78 82 86 90 94
DRY runway 1 520 1 580 1 650 1 730 1 800 1 890 2 000 2 390 2 560 2 720
WET runway 2 010 2 150 2 270 2 400 2 520 2 640 2 770 2 990 3 160 3 340
CONTA runway Refer to FPE-IFL Landing Distance Without AUTOBRAKE
- CONF FULL and apply LDG DIST Factor = 1.80
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 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..................................................................................................................................
....... 320/0.77
MANEUVER WITH CARE
ALTN LAW : PROT LOST
LANDING CONF APPROACH SPEED
Use FLAP 3 VAPP = VREF + 30 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
CAT 2 INOP SLATS SLOW / FLAPS JAMMED
GPWS FLAP
MODE.............................................................................................................................
.. OFF
　
中國(guó)航空網(wǎng) m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A318/A319/A320/A321 QRH快速檢查單QUICK REFERENCE HAND BOOK3(62)