曝光臺 注意防騙 網曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

FPE-IFL
4/4
AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1
IN FLIGHT PERFORMANCE
30 AUG 10
Intentionally left blank
A318/A319/A320/A321 FLEET , , , , , , , ,
, , ,
FPE-IFL
1/4
AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1
IN FLIGHT PERFORMANCE
30 AUG 10
A318/A319/A320/A321 FLEET , , , , , , , ,
, , , , , , , , ,
VAPP DETERMINATION
The FMGS performs the following VAPP computation for landing in normal
configuration (CONF 3 or CONF
FULL).
1. The 5 kt increment is required when the A/THR is used, or when an autoland is
performed.
2. In case of ice accretion, Vapp must not be lower than:
‐ VLS + 5 kt in CONF FULL
‐ VLS + 10 kt in CONF 3
In case of strong or gusty crosswind greater than 20 kt, Vapp should be at least VLS +
5 kt. The 5 kt
increment above VLS may be increased up to 15 kt at the flight crew’s discretion.
LANDING DISTANCE WITHOUT AUTOBRAKE - CONF 3
The actual landing distance is the distance to come to a complete stop from a point 50
ft above the landing
surface. No margin is included in this distance.
CONFIGURATION 3
ACTUAL LANDING DISTANCE (METERS)
WEIGHT (1000 KG) 40 44 48 52 56 60 64 68 72 76
DRY 690 710 750 790 820 850 900 980 1070 1150
WET 930 980 1050 1120 1190 1250 1320 1400 1480 1530
STANDING
WATER 1280 1350 1460 1590 1700 1800 1910 2050 2170 2270
SLUSH 1250 1320 1420 1510 1600 1690 1800 1910 2050 2130
COMPACTED
SNOW 1220 1270 1350 1430 1490 1550 1620 1700 1770 1820
RUNWAY
CONDITION COVERED
WITH
ICE 2820 2900 3030 3170 3290 3400 3520 3670 3830 3910
CORRECTIONS
CORRECTION ON ACTUAL LANDING DISTANCE
runway covered with
dry runway wet
runway standing water slush compacted
snow ice
per 1 000 ft above SL +3 % +4 % +4 % +5 % +4 % +3 %
per 10 kt headwind No correction for headwind due to wind correction on approach
speed
per 10 kt tailwind +17 % +23 % +25 % +24 % +18 % +33 %
2 reversers operative -4 % -8 % -14 % -12 % -10 % -26 %
Per 5 kt speed increment (and no failure) add 8 % (all runways)
FPE-IFL
2/4
AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1
IN FLIGHT PERFORMANCE
30 AUG 10
A318/A319/A320/A321 FLEET , , , , , , , ,
, , , , , , , , ,
Note: ‐ THE ABOVE DISTANCES ARE GIVEN FOR USE IN FLIGHT
BEFORE DEPARTURE ‐ Refer to FCOM/PER-LND-ILD-ALD
CONFIGURATION 3.
EXAMPLE: Actual Landing Distance (ALD) calculation with multiple corrections
Data: LW = 60 000 kg
Pressure altitude = 2 000 ft
Approach speed = VLS + 5 kt
Dry runway
Read from ALD table,
ALD (0 ft, No wind, VLS, no reversers) = 850 m
Read from the Corrections table,
Pressure altitude correction: 3 × 2 = +6 %
Speed increment correction: +8 %
ALD (2 000 ft, No wind, VLS + 5 kt, no reversers) = 850 × 1.06 × 1.08 = 980 m.
LANDING DISTANCE WITHOUT AUTOBRAKE - CONF FULL
The actual landing distance is the distance to come to a complete stop from a point 50
ft above the landing
surface. No margin is included in this distance.
CONFIGURATION FULL
ACTUAL LANDING DISTANCE (METERS)
WEIGHT (1000 KG) 40 44 48 52 56 60 64 68 72 76
DRY 690 690 700 730 760 780 820 860 940 1010
WET 900 900 930 990 1050 1100 1150 1220 1290 1330
STANDING
WATER 1220 1230 1280 1370 1460 1550 1640 1750 1860 1930
SLUSH 1190 1210 1250 1340 1410 1480 1550 1650 1750 1820
COMPACTED
SNOW 1170 1180 1220 1290 1340 1400 1460 1520 1590 1630
RUNWAY
CONDITION COVERED
WITH
ICE 2480 2500 2570 2690 2790 2890 3000 3120 3250 3320
CORRECTIONS
CORRECTION ON ACTUAL LANDING DISTANCE
runway covered with
dry runway wet
runway
standing
water slush compacted
snow ice
per 1 000 ft above SL +3 % +3 % +4 % +5 % +3 % +3 %
per 10 kt headwind No correction for headwind due to wind correction on approach
speed
per 10 kt tailwind +19 % +23 % +25 % +24 % +19 % +35 %
2 reversers operative -3 % -6 % -12 % -11 % -9 % -24 %
Per 5 kt speed increment (and no failure) add 8 % (all runways)
Note: THE ABOVE DISTANCES ARE ‐ GIVEN FOR USE IN FLIGHT
‐ BEFORE DEPARTURE REFER TO FCOM.
EXAMPLE: Actual Landing Distance (ALD) calculation with multiple corrections
Data: LW = 60 000 kg
Pressure altitude = 2 000 ft
Approach speed = VLS + 5 kt
Dry runway
Read from ALD table,
ALD (0 ft, No wind, VLS, no reversers) = 780 m
Read from the Corrections table,
Pressure altitude correction: 3 × 2 = +6 %
Speed increment correction : +8 %
FPE-IFL
3/4
AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：空客320快速檢查單QRH QUICK REFERENCE HAND BOOK10(108)