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FCOM 19 AUG 10
• Maximum takeoff weight correction :
MTOW = 70 100 - 1 300 = 68 800 kg, V1 = 151 - 15 = 136 kt, VR = 151 - 3 = 148 kt, V2 = 154 - 3 =
151 kt.
• Flex temperature correction :
Assuming an actual takeoff weight of 69 000 kg and an initial flex temperature of 45 °C
TOW = 69 000 kg ◂ Flex temperature = 45 - 3 = 42 °C
V1 = 149 - 15 = 134 kt, VR = 150 - 3 = 147 kt, V2 = 153 - 3 = 150 kt.
TAKEOFF PERFORMANCE ON WET RUNWAY
Applicable to:
With no thrust reversers operating and assuming that no clearway was used to compute the dry
RTOW chart, use the table Refer to PER-TOF-TOC-10-30 RTOW EXAMPLE.
• Maximum takeoff weight correction :
MTOW = 70 100 - 1 100 = 69 000 kg, V1 = 151 - 15 = 136 kt, VR = 151 - 4 = 147 kt, V2 = 154 - 4 =
150 kt.
• Flex temperature correction :
Assuming an actual takeoff weight of 69 000 kg and an initial flex temperature of 45 °C
TOW = 69 000 kg ◂ Flex temperature = 45 - 3 = 42 °C
V1 = 149 - 15 = 134 kt, VR = 150 - 4 = 146 kt, V2 = 153 - 4 = 149 kt.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
TAKEOFF
RUNWAY CONTAMINATION - EXAMPLES
A318/A319/A320/A321 FLEET PER-TOF-CTA-50 P 5/16
FCOM 19 AUG 10
Check the resulting speeds against the minimum speeds as per procedure Refer to
PER-TOF-CTA-40 TAKEOFF PERFORMANCE.
TAKEOFF PERFORMANCE ON WET RUNWAY
Applicable to:
With no thrust reversers operating and assuming that no clearway was used to compute the dry
RTOW chart, use the table Refer to PER-TOF-TOC-10-30 RTOW EXAMPLE.
• Maximum takeoff weight correction :
MTOW = 70 100 - 1 500 = 68 600 kg, V1 = 151 - 15 = 136 kt, VR = 151 - 4 = 147 kt, V2 = 154 - 4 =
150 kt.
• Flex temperature correction :
Assuming an actual takeoff weight of 69 000 kg and an initial flex temperature of 45 °C
TOW = 69 000 kg ◂ Flex temperature = 45 - 3 = 42 °C
V1 = 149 - 15 = 134 kt, VR = 150 - 4 = 146 kt, V2 = 153 - 4 = 149 kt.
Check the resulting speeds against the minimum speeds as per procedure Refer to
PER-TOF-CTA-40 TAKEOFF PERFORMANCE.
TAKEOFF PERFORMANCE ON WET RUNWAY
Applicable to: ,
, MSN
With no thrust reversers operating and assuming that no clearway was used to compute the dry
RTOW chart, use the table Refer to PER-TOF-TOC-10-30 RTOW EXAMPLE.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
TAKEOFF
RUNWAY CONTAMINATION - EXAMPLES
A318/A319/A320/A321 FLEET PER-TOF-CTA-50 P 6/16
FCOM 19 AUG 10
• Maximum takeoff weight correction :
MTOW = 82 800 - 100 = 82 700 kg, V1 = 151 - 9 = 142 kt, VR = 153 kt, V2 = 154 kt.
• Flex temperature correction :
Assuming an actual takeoff weight of 75 000 kg and an initial flex temperature of 47 °C
TOW = 75 000 kg ◂ Flex temperature = 47 - 1 = 46 °C
V1 = 149 - 9 = 140 kt, VR = 150 kt, V2 = 151 kt.
TAKEOFF PERFORMANCE ON WET RUNWAY
Applicable to:
With no thrust reversers operating and assuming that no clearway was used to compute the dry
RTOW chart, use the table Refer to PER-TOF-TOC-10-30 RTOW EXAMPLE.
• Maximum takeoff weight correction :
MTOW = 80 100 - 2 000 = 78 100 kg, V1 = 153 - 14 = 139 kt, VR = 156 - 1 = 155 kt, V2 = 158 - 1 =
157 kt.
• Flex temperature correction :
Assuming an actual takeoff weight of 78 400 kg and an initial flex temperature of 47 °C
TOW = 78 400 kg ◂ Flex temperature = 47 - 5 = 42 °C
V1 = 152 - 14 = 138 kt, VR = 154 - 1 = 153 kt, V2 = 156 - 1 = 155 kt.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
TAKEOFF
RUNWAY CONTAMINATION - EXAMPLES
A318/A319/A320/A321 FLEET PER-TOF-CTA-50 P 7/16
FCOM 19 AUG 10
Check the resulting speeds against the minimum speeds as per procedure Refer to
PER-TOF-CTA-40 TAKEOFF PERFORMANCE.
TAKEOFF PERFORMANCE ON WET RUNWAY
Applicable to: MSN
With no thrust reversers operating and assuming that no clearway was used to compute the dry
RTOW chart, use the table Refer to PER-TOF-TOC-10-30 RTOW EXAMPLE.
• Maximum takeoff weight correction :
MTOW = 82 800 - 1 600 = 81 200 kg, V1 = 151 - 15 = 136 kt, VR = 153 - 4 = 149 kt, V2 = 154 - 4 =
150 kt.
• Flex temperature correction :
Assuming an actual takeoff weight of 75 000 kg and an initial flex temperature of 47 °C
TOW = 75 000 kg ◂ Flex temperature = 47 - 4 = 43 °C
V1 = 149 - 15 = 134 kt, VR = 150 - 4 = 146 kt, V2 = 151 - 4 = 147 kt.
TAKEOFF PERFORMANCE ON WET RUNWAY
Applicable to: MSN,
With no thrust reversers operating and assuming that no clearway was used to compute the dry
RTOW chart, use the table Refer to PER-TOF-TOC-10-30 RTOW EXAMPLE.
　
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