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

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)
FPE-IFL
2/4
AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1
IN FLIGHT PERFORMANCE
30 AUG 10
A318/A319/A320/A321 FLEET MSN 4719
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 %
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
SLUSH MED
LOW
1700
1860
1890
2040
2100
2220
2290
2390
2510
2640
2690
2790
+7
+5
-16
0
+22
+18
-3
-2
COMPACTED
SNOW
MED
LOW
1580
1880
1700
2050
1830
2230
1940
2390
2060
2560
2170
2730
+6
+4
-11
0
+16
+15
-2
-1
COVERED
WITH
ICE MED
LOW
2980
3000
3240
3270
3520
3540
3780
3800
4040
4060
4300
4320
+6
+5
-28
-26
+26
+26
-4
-4
Note: MAX MODE IS NOT ‐ RECOMMENDED AT LANDING
‐ THE TABLES TAKE INTO ACCOUNT THE APPROACH SPEED
INCREMENT LINKED TO
HEADWIND AND AUTOLAND. FOR ANY EXTRA SPEED INCREMENT OF 5
kt (AND NO
FAILURE) INCREASE LANDING DISTANCE BY 7 % (ALL RUNWAYS).
AUTOLAND LANDING DISTANCE WITH AUTOBRAKE - CONF FULL
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
TAIL
WIND
PER
10 KT
HEAD
WIND
DRY MED
LOW
1280
1830
1370
1990
1460
2150
1530
2300
1660
2450
1800
2590
+4
+4
00
+13
+14
-1
-1W
ET MED
LOW
1320
1830
1430
1990
1550
2150
1650
2300
1800
2450
1960
2590
+4
+4
00
+17
+14
-1
-1
STANDING
WATER
MED
LOW
1660
1810
1840
1980
2030
2150
2210
2310
2390
2490
2580
2670
+5
+5
-16
0
+20
+18
-3
COVERED -1
WITH SLUSH MED
LOW
1590
1770
1760
1930
1930
2090
2100
2230
2270
2450
2440
2540
+6
+5
-15
0
+20
+17
-3
-2
To be continued on next page
FPE-IFL
3/4
AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1
　
中國航空網 m.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(116)