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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) - CONF 3
RUNWAY CONDITION 58 62 66 70 WEIG74HT (100708 KG) 82 86 90 94
DRY 870 910 950 990 1030 1090 1160 1390 1490 1590
WET 1140 1210 1280 1360 1430 1500 1570 1700 1800 1890
STANDING WATER 1620 1730 1850 1950 2070 2180 2280 2410 2520 2620
SLUSH 1550 1640 1740 1850 1950 2040 2150 2270 2370 2470
COMPACTED SNOW 1440 1510 1580 1650 1720 1780 1840 1910 1970 2020
COVERED
WITH
ICE 3050 3190 3330 3460 3590 3720 3840 3980 4110 4230
CORRECTIONS
CORRECTION ON ACTUAL LANDING DISTANCE (FEET) - CONF 3
RUNWAY COVERED WITH
RUNWAY CONDITION DRY WET STANDING
WATER SLUSH COMPACTED
SNOW ICE
per 1 000 ft above SL +4 % +4 % +4 % +5 % +4 % +4 %
per 10 kt headwind No correction for headwind due to wind correction on approach
speed
per 10 kt tailwind +17 % +22 % +24 % +23 % +16 % +27 %
2 reversers operative -5 % -7 % -12 % -11 % -7 % -21 %
Per 5 kt speed increment (and no failure) add 7 % (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 = 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) = 990 m
Read from the Corrections table,
Pressure altitude correction: 4 × 2 = +8 %
Speed increment correction: +7 %
ALD (2 000 ft, No wind, VLS + 5 kt, no reversers) = 990 × 1.08 × 1.07 = 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) - CONF FULL
RUNWAY CONDITION 68 62 66 70 WEIG74HT (107080 KG) 82 86 90 94
DRY 820 850 890 920 960 1010 1080 1280 1370 1460
WET 1040 1100 1160 1230 1290 1350 1420 1530 1610 1700
STANDING
WATER 1460 1560 1660 1770 1870 1970 2060 2170 2260 2360
SLUSH 1420 1500 1580 1660 1760 1850 1940 2020 2130 2210
COMPACTED
SNOW 1330 1400 1460 1530 1590 1640 1700 1760 1820 1870
COVERED WITH
ICE 2790 2910 3030 3160 3280 3390 3510 3630 3750 3860
CORRECTIONS
CORRECTION ON ACTUAL LANDING DISTANCE (METERS) - CONF FULL
COVERED WITH
RUNWAY CONDITION DRY WET STANDING
WATER SLUSH COMPACTED
SNOW ICE
PER 1000 FT ABOVE
SL +4 % +4 % +4 % +5 % +4 % +4 %
PER 10 KT HEADWIND NO CORRECTION FOR HEADWIND DUE TO WIND
CORRECTION ON APPROACH SPEED
PER 10 KT TAILWIND +18 % +23 % +25 % +23 % +17 % +28 %
2 REVERSERS
OPERATIVE -4 % -7 % -11 % -10 % -7 % -21 %
PER 5 kt SPEED INCREMENT (AND NO FAILURE) ADD 7 % (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) = 920 m
FPE-IFL
3/4
AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1
IN FLIGHT PERFORMANCE
30 AUG 10
A318/A319/A320/A321 FLEET , , , , , , , ,
, , , , , , , , , , , ,
, , , , , ,
Read from the Corrections table,
Pressure altitude correction: 4 × 2 = +8 %
Speed increment correction : +7 %
ALD (2 000 ft, No wind, VLS + 5 kt, no reversers) = 920 × 1.08 × 1.07 = 1 070 m
AUTOLAND LANDING DISTANCE WITH AUTOBRAKE - CONF 3
AUTOLAND LANDING WITH AUTOBRAKE ACTUAL LANDING DISTANCE
(METERS) - CONF FULL
WEIGHT (1000 KG) CORRECTIONS (%)
ON LANDING DISTANCE
RUNWAY CONDITION
MODE 50 60 70 80 90
PER
1000 FT
ABOVE
SL
2
REV.
　
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