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

Dry runway
Read from ALD table,
ALD (0 ft, No wind, VLS, no reversers) = 910 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) = 910 × 1.06 × 1.08 = 1 050 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) 46 50 54 58 62 66 70 74 78
DRY 700 730 770 800 840 910 990 1080 1170
WET 920 980 1040 1110 1180 1240 1320 1390 1460
STANDING
WATER 1220 1300 1380 1480 1590 1700 1810 1930 2020
SLUSH 1180 1260 1340 1420 1500 1580 1670 1770 1860
COMPACTED
SNOW 1190 1270 1340 1410 1480 1550 1620 1700 1750
RUNWAY
CONDITION COVERED
WITH
ICE 2570 2690 2820 2950 3090 3230 3370 3510 3620
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 +3 % +3 % +4 % +5 % +3 % +4 %
per 10 kt headwind No correction for headwind due to wind correction on approach
speed
per 10 kt tailwind +18 % +21 % +23 % +22 % +18 % +31 %
forward C.G. +2 % +3 % +3 % +3 % +3 % +3 %
2 reversers operative -3 % -8 % -10 % -9 % -8 % -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
FPE-IFL
3/4
AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1
IN FLIGHT PERFORMANCE
30 AUG 10
A318/A319/A320/A321 FLEET , , ,
Data: LW = 62 000 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) = 840 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) = 840 × 1.06 × 1.08 = 970 m.
AUTOLAND LANDING DISTANCE WITH AUTOBRAKE - CONF 3
ACTUAL LANDING DISTANCE
(METERS)
CORRECTIONS (%)
ON LANDING DISTANCE
WEIGHT (1000 KG)
RUNWAY CONDITION MODE 40 50 60 70 80
PER
1000
FT
ABOVE
SL
2
REV.
OP.
PER 10 KT
TAILWIND
PER
10 KT
HEADWIND
FWD
CG
DRY MED
LOW
1360
1850
1450
2020
1570
2240
1670
2450
1770
2650
+3
+3
-3
0
+12
+15
-3
-3
+2
+2
WET MED
LOW
1400
1850
1520
2020
1680
2240
1840
2450
1990
2650
+4
+3
-3
0
+18
+15
-4
-3
+3
+2
STANDING
WATER
MED
LOW
1630
1820
1830
2000
2110
2250
2390
2530
2660
2790
+4
+4
-12
-2
+22
+18
-4
-3
+3
+2
SLUSH MED
LOW
1590
1770
1730
1940
1950
2150
2200
2370
2430
2600
+5
+4
-11
-1
+21
+17
-4
-3
+3
+2
COMPACTED
SNOW
MED
LOW
1600
1820
1720
1980
1870
2200
2000
2390
2120
2580
+3
+4
-9
-1
+16
+15
-3
-3
+3
+3
COVERED
WITH
ICE MED
LOW
3290
3320
3550
3580
3890
3930
4230
4270
4550
4590
+4
+4
-25
-25
+29
+28
-5
-5
+3
+3
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 5 % (ALL RUNWAYS).
AUTOLAND LANDING DISTANCE WITH AUTOBRAKE - CONF FULL
ACTUAL LANDING DISTANCE
(METERS)
CORRECTIONS (%)
ON LANDING DISTANCE
WEIGHT (1000 KG)
RUNWAY CONDITION MODE 40 50 60 70 80
PER
1000 FT
ABOVE
SL
2
REV.
OP.
PER
10 KT
TAIL
WIND
PER
10 KT
HEAD
　
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