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WIND
FWD
CG
DRY MED
LOW
1330
1800
1390
1910
1520
2130
1620
2340
1730
2530
+3
+3
00
+13
+16
-3
-3
+2
+2
WET MED
LOW
1340
1800
1420
1910
1570
2130
1720
2340
1860
2530
+3
+3
00
+17
+16
-4
-3
+3
+2
STANDING
WATER
MED
LOW
1540
1770
1670
1880
1910
2110
2150
2330
2390
2560
+4
+3
-10
-1
+21
+17
-4
-3
+3
+2
SLUSH MED
LOW
1500
1730
1610
1840
1790
2050
2000
2240
2210
2430
+5
+4
-9
-1
+21
+16
-5
-3
+3
+2
COMPACTED
SNOW
MED
LOW
1520
1770
1610
1880
1750
2090
1880
2280
2000
2460
+3
+4
-7
-1
+16
+16
-4
-3
+3
+2
COVERED
WITH
ICE MED
LOW
2920
2940
3110
3130
3420
3450
3730
3760
4010
4040
+4
+4
-23
-21
+30
+30
-5
-5
+3
+3
FPE-IFL
4/4
AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1
IN FLIGHT PERFORMANCE
30 AUG 10
A318/A319/A320/A321 FLEET , , ,
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).
FPE-IFL
1/4
AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1
IN FLIGHT PERFORMANCE
30 AUG 10
A318/A319/A320/A321 FLEET , , , , , ,
VAPP DETERMINATION
The FMGS performs the following VAPP computation for landing in normal
configuration (CONF 3 or CONF
FULL).
Note: FOR CG < 25 %, add 2 kt to VLS CONF FULL and VLS CONF 3.
1. The 5 kt increment is required when the A/THR is used, or when an autoland is
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)
WEIGHT (1000 KG) 46 50 54 58 62 66 70 74 78
DRY 750 780 820 860 910 1000 1100 1200 1290
WET 1020 1090 1160 1240 1320 1400 1480 1570 1650
STANDING
WATER 1340 1430 1540 1660 1790 1930 2060 2200 2310
SLUSH 1300 1390 1470 1560 1650 1760 1890 2010 2110
COMPACTED
SNOW 1300 1380 1460 1540 1620 1700 1780 1850 1910
RUNWAY
CONDITION COVERED
WITH
ICE 2970 3110 3260 3410 3560 3720 3880 4040 4170
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 % +3 % +4 %
per 10 kt headwind No correction for headwind due to wind correction on approach
speed
per 10 kt tailwind +18 % +21 % +24 % +22 % +17 % +29 %
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 , , , , , ,
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 -3 % -9 % -12 % -11 % -9 % -26 %
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) = 910 m
Read from the Corrections table,
Pressure altitude correction: 3 × 2 = +6 %
　
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