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DETERMINATION OF A CONSERVATIVE MAXIMUM TAKEOFF WEIGHT :
(Refer to PER-TOF-TOD-40-40 CONFIGURATION 1+F / FT)
‐ Pressure altitude : 1 400 ft - Use the table for 2 000 ft.
‐ Enter the column corresponding to 2 250 m
‐ Read the maximum takeoff weight on the line corresponding to the temperature of 30 °C :
67 100 kg
V1 = 133 kt, VR = 134 kt, V2 = 139 kt
DETERMINATION OF A PRECISE FLEXIBLE TEMPERATURE FOR THE ACTUAL TAKEOFF
WEIGHT OF 64 000 KG :
(Refer to PER-TOF-TOD-40-40 CONFIGURATION 1+F / FT)
‐ Interpolate the temperature corresponding to 64 000 kg for the runway length of 2 415 m at
1 000 ft and 2 000 ft pressure altitude.
Results :
1 000 ft : 53 °C, V1 = 135 kt, VR = 136 kt, V2 = 140 kt
2 000 ft : 48 °C, V1 = 133 kt, VR = 135 kt, V2 = 140 kt
‐ Interpolate between these two values to get the flexible temperature
1 400 ft : 51 °C, V1 = 134 kt, VR = 136 kt, V2 = 140 kt
EXAMPLE
Applicable to: MSN,
Pressure altitude : 1 400 ft
Temperature : 30 °C
Runway length : 2 750 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 .......................................................................................................................2 750 m
correction for wind................................................................................................10 × 10 = + 100 kt
correction for slope................................................................................................................ - 435 m
corrected runway length........................................................................................................2 415 m
DETERMINATION OF A CONSERVATIVE MAXIMUM TAKEOFF WEIGHT :
(Refer to PER-TOF-TOD-40-40 CONFIGURATION 1+F / FT)
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
TAKEOFF
TAKEOFF DATA - QUICK REFERENCE TABLES
A318/A319/A320/A321 FLEET PER-TOF-TOD-40-30 P 7/10
FCOM 19 AUG 10
‐ Pressure altitude : 1 400 ft - Use the table for 2 000 ft.
‐ Enter the column corresponding to 2 250 m
‐ Read the maximum takeoff weight on the line corresponding to the temperature of 30 °C :
71 300 kg
V1 = 140 kt, VR = 146 kt, V2 = 148 kt
DETERMINATION OF A PRECISE FLEXIBLE TEMPERATURE FOR THE ACTUAL TAKEOFF
WEIGHT OF 64 000 KG :
(Refer to PER-TOF-TOD-40-40 CONFIGURATION 1+F / FT)
‐ Interpolate the temperature corresponding to 64 000 kg for the runway length of 2 415 m at
1 000 ft and 2 000 ft pressure altitude.
Results :
1 000 ft : 66 °C, V1 = 138 kt, VR = 139 kt, V2 = 140 kt
2 000 ft : 61 °C, V1 = 137 kt, VR = 139 kt, V2 = 140 kt
‐ Interpolate between these two values to get the flexible temperature
1 400 ft : 64 °C, V1 = 137 kt, VR = 139 kt, V2 = 140 kt
EXAMPLE
Applicable to:
Pressure altitude : 1 400 ft
Temperature : 30 °C
Runway length : 2 750 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 .......................................................................................................................2 750 m
correction for wind................................................................................................10 × 10 = + 100 kt
correction for slope................................................................................................................ - 435 m
corrected runway length........................................................................................................2 415 m
DETERMINATION OF A CONSERVATIVE MAXIMUM TAKEOFF WEIGHT :
(Refer to PER-TOF-TOD-40-40 CONFIGURATION 1+F / FT)
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
TAKEOFF
TAKEOFF DATA - QUICK REFERENCE TABLES
A318/A319/A320/A321 FLEET PER-TOF-TOD-40-30 P 8/10
FCOM 19 AUG 10
‐ Pressure altitude : 1 400 ft - Use the table for 2 000 ft.
‐ Enter the column corresponding to 2 250 m
‐ Read the maximum takeoff weight on the line corresponding to the temperature of 30 °C :
71 300 kg
V1 = 139 kt, VR = 146 kt, V2 = 148 kt
DETERMINATION OF A PRECISE FLEXIBLE TEMPERATURE FOR THE ACTUAL TAKEOFF
WEIGHT OF 64 000 KG :
(Refer to PER-TOF-TOD-40-40 CONFIGURATION 1+F / FT)
‐ Interpolate the temperature corresponding to 64 000 kg for the runway length of 2 415 m at
1 000 ft and 2 000 ft pressure altitude.
Results :
1 000 ft : 61 °C, V1 = 138 kt, VR = 139 kt, V2 = 140 kt
　
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