曝光台 注意防骗
网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者
WEIGHT (1000 KG) 58 62 66 70 74 78 82 86 90 94
DRY 860 900 940 980 1020 1070 1150 1370 1470 1570
WET 1110 1180 1250 1320 1390 1460 1530 1650 1750 1850
STANDING
WATER 1550 1660 1780 1880 1990 2080 2190 2320 2430 2520
SLUSH 1490 1580 1670 1780 1880 1970 2070 2170 2280 2380
COMPACTED
SNOW 1390 1460 1530 1600 1670 1730 1790 1850 1920 1980
RUNWAY
CONDITION COVERED
WITH
ICE 2780 2910 3050 3190 3310 3440 3570 3700 3840 3960
CORRECTIONS
CORRECTION ON ACTUAL LANDING DISTANCE
dry runway wet runway standing water slurusnhway cocvoemrepda wctiethd snow ice
per 1 000 ft above SL +4 % +5 % +5 % +6 % +4 % +5 %
per 10 kt headwind No correction for headwind due to wind correction on approach
speed
per 10 kt tailwind +16 % +21 % +22 % +22 % +16 % +26 %
2 reversers operative -5 % -8 % -16 % -15 % -11 % -29 %
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 MSN 4617
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 = 70 000 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) = 980 m
Read from the Corrections table,
Pressure altitude correction: 4 × 2 = +8 %
Speed increment correction: +8 %
ALD (2 000 ft, No wind, VLS + 5 kt, no reversers) = 980 × 1.08 × 1.08 = 1 150 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) 58 62 66 70 74 78 82 86 90 94
DRY 820 850 890 930 970 1020 1080 1290 1380 1470
WET 1030 1100 1160 1230 1290 1350 1420 1530 1620 1710
STANDING
WATER 1430 1530 1640 1730 1830 1920 2020 2140 2240 2340
SLUSH 1390 1470 1560 1640 1730 1820 1910 2000 2120 2210
COMPACTED
SNOW 1310 1380 1440 1510 1570 1630 1680 1750 1810 1860
RUNWAY
CONDITION COVERED
WITH
ICE 2590 2720 2840 2970 3090 3210 3330 3450 3580 3690
CORRECTIONS
CORRECTION ON ACTUAL LANDING DISTANCE
dry runway covered with
runway
wet
runway standing water slush compacted
snow ice
per 1 000 ft above SL +4 % +4 % +5 % +6 % +4 % +5 %
per 10 kt headwind No correction for headwind due to wind correction on approach
speed
per 10 kt tailwind +17 % +21 % +24 % +22 % +17 % +28 %
2 reversers operative -4 % -8 % -15 % -14 % -10 % -28 %
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 = 70 000 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) = 930 m
Read from the Corrections table,
Pressure altitude correction: 4 × 2 = +8 %
Speed increment correction :+8 %
FPE-IFL
3/4
AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1
IN FLIGHT PERFORMANCE
30 AUG 10
A318/A319/A320/A321 FLEET MSN 4617
ALD (2 000 ft, No wind, VLS + 5 ft, no reversers) = 930 × 1.08 × 1.08 = 1 090 m.
AUTOLAND LANDING DISTANCE WITH AUTOBRAKE - CONF 3
ACTUAL LANDING DISTANCE
(METERS)
CORRECTIONS (%)
ON LANDING DISTANCE
WEIGHT (1000 KG)
RUNWAY CONDITION MODE 54 62 70 78 86 94
PER
1000
FT
ABOVE
SL
2
REV.
OP.
PER 10 KT
TAILWIND
PER 10 KT
HEADWIND
DRY MED
LOW
1340
1920
1440
2100
1550
2290
1650
2460
1810
2640
1970
2810
+6
+4
00
+14
+15
-1
-1W
ET MED
LOW
1400
1920
1530
2100
1680
2290
1810
2460
2000
2640
2190
2810
+6
+4
-2
0
+17
+15
-2
-1
STANDING
WATER
MED
LOW
1780
1910
1980
2100
2210
2300
2410
2510
2640
2720
2860
2940
+6
+5
-17
0
+21
+18
-3
-2
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空客320快速检查单QRH QUICK REFERENCE HAND BOOK10(114)
