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

+18
-4
-3
COMPACTED
SNOW
MED
LOW
1380
1680
1520
1850
1640
2020
1760
2210
1860
2370
+4
+4
-8
-4
+17
+16
-3
-3
COVERED
WITH
ICE MED
LOW
2750
2820
2990
3080
3240
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 7 % (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
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) 40 44 48 52 56 60 64 68 72 76
DRY 670 710 740 780 820 850 900 990 1080 1160
WET 890 960 1030 1100 1170 1230 1300 1390 1470 1520
STANDING
WATER 1220 1310 1420 1550 1640 1750 1860 2000 2120 2210
SLUSH 1190 1280 1380 1470 1560 1660 1760 1880 2000 2090
COMPACTED
SNOW 1160 1240 1320 1400 1470 1530 1600 1670 1750 1800
RUNWAY
CONDITION COVERED
WITH
ICE 2380 2520 2660 2810 2940 3060 3190 3340 3500 3600
CORRECTIONS
CORRECTION ON ACTUAL LANDING DISTANCE
dry runway wet runway covered with
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 % +22 % +25 % +23 % +19 % +33 %
2 reversers operative -4 % -9 % -15 % -14 % -11 % -27 %
Per 5 kt speed increment (and no failure) add 8 % (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 = 60 000 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) = 850 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) = 850 × 1.06 × 1.08 = 980 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) 40 44 48 52 56 60 64 68 72 76
DRY 650 660 690 720 750 780 810 860 940 1010
WET 830 850 910 970 1020 1070 1130 1200 1260 1300
STANDING
WATER 1120 1150 1240 1320 1410 1500 1590 1690 1790 1860
SLUSH 1090 1120 1210 1290 1360 1430 1500 1600 1700 1760
COMPACTED
SNOW 1080 1110 1180 1250 1300 1360 1420 1480 1550 1590
RUNWAY
CONDITION COVERED
WITH
ICE 2110 2170 2290 2420 2520 2630 2740 2870 2990 3070
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 +18 % +22 % +25 % +23 % +19 % +35 %
　
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