曝光台 注意防骗
网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者
TAKEOFF DATA - QUICK REFERENCE TABLES
A330/A340 FLEET PER-TOF-TOD-40-30 P 3/26
FCOM 19 AUG 10
CORRECTIONS FOR WIND AND RUNWAY SLOPE
Applicable to:
Runway length (m) 2 000 2 250 2 500 2 750 3 000 3 250 3 500 3 750 4 000
Effect
of wind
per knot of head
wind add (meters) 9 10 11 11.5 12 12.5 13.5 14.5 15
per percent
uphill slope
subtract (meters)
Effect of 110 145 180 215 250 285 320 360 395
runway
slope per percent
downhill slope
add (meters)
75 90 105 120 130 145 160 175 190
CORRECTIONS FOR WIND AND RUNWAY SLOPE
Applicable to: ,
Runway length (m) 2 000 2 250 2 500 2 750 3 000 3 250 3 500 3 750 4 000
Effect
of wind
per knot of head
wind add (meters) 9 10 11 12 12 13 13 14 14
per percent
uphill slope
subtract (meters)
Effect of 130 160 200 250 300 350 420 480 520
runway
slope per percent
downhill slope
add (meters)
50 58 66 75 83 92 100 108 120
EXAMPLE
Applicable to:
Pressure altitude : 1 400 ft
Temperature : 30 °C
Runway length : 3 750 m
Wind : 10 kt head
Slope : 1 % up
Takeoff configuration : 1 + F
DETERMINATION OF CORRECTED RUNWAY LENGTH
(Refer to PER-TOF-TOD-40-30 CORRECTIONS FOR WIND AND RUNWAY SLOPE)
runway length........................................................................................................................3 750 m
correction for wind.............................................................................................10 x 14.5 = + 145 m
A330/A340 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
TAKEOFF
TAKEOFF DATA - QUICK REFERENCE TABLES
A330/A340 FLEET PER-TOF-TOD-40-30 P 4/26
FCOM 19 AUG 10
correction for slope................................................................................................................ - 360 m
corrected runway length........................................................................................................3 535 m
DETERMINATION OF A CONSERVATIVE MAXIMUM TAKEOFF WEIGHT :
(Refer to PER-TOF-TOD-40-30 CONF 1+F - PRESSURE ALTITUDE = 2 000 FT)
‐ Pressure altitude : 1 400 ft - Use the table for 2 000 ft.
‐ Enter the column corresponding to 3 500 m.
‐ Read the maximum takeoff weight on the line corresponding to the temperature of 30 °C :
254 300 kg
V1 = 138 kt, VR = 152 kt, V2 = 160 kt
DETERMINATION OF A PRECISE FLEXIBLE TEMPERATURE FOR THE ACTUAL TAKEOFF
WEIGHT OF 240 000 KG:
(Refer to PER-TOF-TOD-40-30 CONF 1+F - PRESSURE ALTITUDE = 1 000 FT)
(Refer to PER-TOF-TOD-40-30 CONF 1+F - PRESSURE ALTITUDE = 2 000 FT)
‐ Interpolate the temperature corresponding to 240 000 kg for the runway length of 3 535 m at
1 000 ft and 2 000 ft pressure altitude.
Results :
1 000 ft : 45 °C, V1 = 141 kt, VR = 148 kt, V2 = 155 kt
2 000 ft : 41 °C, V1 = 140 kt, VR = 148 kt, V2 = 155 kt
‐ Interpolate between these two values to get the flexible temperature.
1 400 ft : 43 °C, V1 = 141 kt, VR = 148 kt, V2 = 155 kt
EXAMPLE
Applicable to: ,
Pressure altitude : 1 400 ft
Temperature : 30 °C
Runway length : 3 750 m
Wind : 10 kt head
Slope : 1 % up
Takeoff configuration : 1 + F
DETERMINATION OF CORRECTED RUNWAY LENGTH
(Refer to PER-TOF-TOD-40-30 CORRECTIONS FOR WIND AND RUNWAY SLOPE)
runway length........................................................................................................................3 750 m
correction for wind................................................................................................10 x 14 = + 140 m
correction for slope................................................................................................................ - 480 m
A330/A340 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
TAKEOFF
TAKEOFF DATA - QUICK REFERENCE TABLES
A330/A340 FLEET PER-TOF-TOD-40-30 P 5/26
FCOM 19 AUG 10
corrected runway length........................................................................................................3 410 m
DETERMINATION OF A CONSERVATIVE MAXIMUM TAKEOFF WEIGHT :
(Refer to PER-TOF-TOD-40-30 CONF 1+F - PRESSURE ALTITUDE = 2 000 FT)
‐ Pressure altitude : 1 400 ft - Use the table for 2 000 ft.
‐ Enter the column corresponding to 3 250 m.
‐ Read the maximum takeoff weight on the line corresponding to the temperature of 30 °C :
231 700 kg
V1 = 143 kt, VR = 148 kt, V2 = 156 kt
DETERMINATION OF A PRECISE FLEXIBLE TEMPERATURE FOR THE ACTUAL TAKEOFF
WEIGHT OF 200 000 KG:
(Refer to PER-TOF-TOD-40-30 CONF 1+F - PRESSURE ALTITUDE = 1 000 FT)
(Refer to PER-TOF-TOD-40-30 CONF 1+F - PRESSURE ALTITUDE = 2 000 FT)
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：
A330/A340机组操作手册 FLIGHT CREW OPERATING MANUAL FCOM 6(48)
