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IN FLIGHT PERFORMANCE
30 AUG 10
A318/A319/A320/A321 FLEET , , , , , , , ,
, , , , , , , , ,
ALD (2 000 ft, No wind, VLS + 5 kt, no reversers) = 780 × 1.06 × 1.08 = 900 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
DRY MED
LOW
1130
1770
1260
2000
1380
2220
1510
2460
1630
2670
+3
+3
0 -
4
+12
+15
-1
-2W
ET MED
LOW
1200
1770
1380
2000
1550
2220
1740
2460
1910
2670
+4
+3
-4
-3
+19
+15
-3
-2
STANDING
WATER
MED
LOW
1550
1710
1830
1960
2110
2230
2410
2540
2700
2850
+4
+4
-14
-7
+24
+21
-4
-3
SLUSH MED
LOW
1490
1680
1750
1910
1990
2140
2300
2410
2550
2690
+5
+5
-14
-6
+23
+20
-4
-3
COMPACTED
SNOW
MED
LOW
1420
1760
1590
1980
1730
2190
1890
2410
2020
2610
+4
+4
-9
-4
+17
+16
-3
-2
COVERED
WITH
ICE MED
LOW
3140
3230
3440
3550
3740
3850
4090
4210
4390
4520
+4
+4
-25
-25
+31
+31
-5
-5
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 8 % (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
WIND
DRY MED
LOW
1160
1730
1250
1880
1350
2060
1450
2250
1540
2420
+3
+3
0 -
4
+12
+15
-2
-2W
ET MED
LOW
1200
1730
1320
1880
1450
2060
1590
2250
1720
2420
+3
+3
-2
-3
+17
+15
-3
-2
STANDING
WATER
MED
LOW
1490
1670
1660
1820
1880
2020
2110
2240
2330
2460
+4
+4
-12
-5
+22
+20
-4
-3
SLUSH MED
LOW
1440
1640
1600
1790
1790
1960
2010
2160
2200
2350
+5
+4
-12
-4
+21
+18
-4
-3
COMPACTED
SNOW
MED
LOW
1400
1700
1520
1850
1640
2020
1760
2210
1860
2370
+4
+4
-8
-4
+17
+18
-3
-3
COVERED
WITH
ICE MED
LOW
2780
2840
2990
3080
3230
3330
3520
3620
3760
3860
+4
+4
-23
-22
+32
+32
-5
-5
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 8 % (ALL RUNWAYS).
FPE-IFL
4/4
AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1
IN FLIGHT PERFORMANCE
30 AUG 10
Intentionally left blank
A318/A319/A320/A321 FLEET , , , , , , , ,
, , , , , , , , ,
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).
1. The 5 kt increment is required when the A/THR is used, or when an autoland is
　
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