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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) 46 50 54 58 62 66 70 74 78
DRY 730 760 800 840 890 970 1060 1160 1250
WET 970 1040 1110 1180 1260 1340 1420 1500 1580
STANDING
WATER 1270 1360 1440 1560 1690 1810 1940 2070 2180
SLUSH 1230 1310 1400 1480 1570 1660 1780 1900 2000
COMPACTED
SNOW 1230 1310 1380 1460 1540 1620 1690 1770 1830
RUNWAY
CONDITION COVERED
WITH
ICE 2320 2480 2650 2810 2970 3140 3300 3470 3600
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 % +5 %
per 10 kt headwind No correction for headwind due to wind correction on approach
speed
per 10 kt tailwind +17 % +21 % +24 % +22 % +16 % +24 %
To be continued on next page
FPE-IFL
2/4
AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1
IN FLIGHT PERFORMANCE
30 AUG 10
A318/A319/A320/A321 FLEET , , MSN 4566, 4473
Continued from previous page
CORRECTION ON ACTUAL LANDING DISTANCE
runway covered with
dry runway wet
runway standing water slush compacted
snow
ice
forward C.G. +2 % +3 % +3 % +3 % +3 % +3 %
2 reversers operative -5 % -12 % -15 % -14 % -12 % -27 %
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/PER-LND-ILD-ALD
CONFIGURATION 3.
EXAMPLE: Actual Landing Distance (ALD) calculation with multiple corrections
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) = 890 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) = 890 × 1.06 × 1.08 = 1 020 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 690 730 760 790 830 890 980 1070 1150
WET 890 950 1010 1080 1150 1220 1290 1360 1420
STANDING
WATER 1170 1250 1330 1420 1530 1630 1740 1850 1950
SLUSH 1130 1210 1290 1370 1450 1530 1620 1720 1800
COMPACTED
SNOW 1140 1220 1290 1360 1430 1500 1570 1650 1700
RUNWAY
CONDITION COVERED
WITH
ICE 2030 2170 2310 2450 2600 2740 2880 3030 3150
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 % +4 % +4 % +5 % +4 % +5 %
per 10 kt headwind No correction for headwind due to wind correction on approach
speed
per 10 kt tailwind +18 % +21 % +22 % +20 % +17 % +25 %
forward C.G. +2 % +3 % +3 % +3 % +3 % +2 %
2 reversers operative -5 % -11 % -14 % -13 % -11 % -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 , , MSN 4566, 4473
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) = 830 m
Read from the Corrections table,
Pressure altitude correction: 3 × 2 = +6 %
Speed increment correction : +8 %
ALD (2 000 ft, No wind, VLS, no reversers) = 830 × 1.06 × 1.08 = 960 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
1290
1760
1410
1990
1530
2220
1660
2450
1780
2680
+3
+3
0 -
2
+12
+16
-2
-3
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空客320快速检查单QRH QUICK REFERENCE HAND BOOK10(112)
