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Enter the 10 kt head wind column and interpolate for 25 °C, CONF 2,
Maximum TO weight (1 000 kg) air conditioning OFF.............................................................70.9
Retain CONF 1+F as takeoff configuration.
Maximum TO weight (1 000 kg) air conditioning OFF.............................................................71.2
Air conditioning correction...................................................................................................... - 2.0
(Refer to PER-TOF-CTA-10 GENERAL)
Maximum permissible TO weight (1 000 kg) air conditioning ON........................................ = 69.2
Determine takeoff speeds for 69.2 (1 000 kg) in the 10 kt head wind column (CONF 1+F)
V1 = 151 kt, VR = 152 kt, V2 = 154 kt
CONSERVATIVE CORRECTIONS FOR QNH AND BLEEDS
Applicable to:
Refer to PER-TOF-TOD-24 EFFECT OF QNH AND BLEEDS
BnqqdbshnmrqdfhudmenqPMG≠0/02gO+hqbnmchshnmhmfNM+mshhbdNM
1. For the given wind and temperature conditions, read the maximum takeoff weight (choose the
configuration giving the highest weight).
2. Apply the published weight correction(s) to the maximum takeoff weight (for each correction) to
determine the maximum permissible takeoff weight.
3. Read the speeds associated with the maximum permissible takeoff weight by entering the chart
with the retained configuration and wind value.
EXAMPLE 1
DATA: OAT = 25 °C
Head Wind = 10 kt
Air conditioning ON
QNH = 1 013 hPa
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
TAKEOFF
TAKEOFF CHARTS - MTOW CALCULATION (TEMPERATURE ENTRY)
A318/A319/A320/A321 FLEET PER-TOF-TOC-12-10 P 5/22
FCOM 19 AUG 10
Use the chart (Refer to PER-TOF-TOC-10-30 RTOW EXAMPLE)
Enter the 10 kt head wind column and interpolate for 25 °C, CONF 1+F,
Maximum TO weight (1 000 kg) air conditioning OFF.............................................................71.2
Enter the 10 kt head wind column and interpolate for 25 °C, CONF 2,
Maximum TO weight (1 000 kg) air conditioning OFF.............................................................70.9
Retain CONF 1+F as takeoff configuration.
Maximum TO weight (1 000 kg) air conditioning OFF.............................................................71.2
Air conditioning correction...................................................................................................... - 2.2
(Refer to PER-TOF-CTA-10 GENERAL)
Maximum permissible TO weight (1 000 kg) air conditioning ON........................................ = 69.0
Determine takeoff speeds for 69.0 (1 000 kg) in the 10 kt head wind column (CONF 1+F)
V1 = 151 kt, VR = 151 kt, V2 = 153 kt
CONSERVATIVE CORRECTIONS FOR QNH AND BLEEDS
Applicable to:
Refer to PER-TOF-TOD-24 EFFECT OF QNH AND BLEEDS
BnqqdbshnmrqdfhudmenqPMG≠0/02gO+hqbnmchshnmhmfNM+mshhbdNM
1. For the given wind and temperature conditions, read the maximum takeoff weight (choose the
configuration giving the highest weight).
2. Apply the published weight correction(s) to the maximum takeoff weight (for each correction) to
determine the maximum permissible takeoff weight.
3. Read the speeds associated with the maximum permissible takeoff weight by entering the chart
with the retained configuration and wind value.
EXAMPLE 1
DATA: OAT = 25 °C
Head Wind = 10 kt
Air conditioning ON
QNH = 1 013 hPa
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
TAKEOFF
TAKEOFF CHARTS - MTOW CALCULATION (TEMPERATURE ENTRY)
A318/A319/A320/A321 FLEET PER-TOF-TOC-12-10 P 6/22
FCOM 19 AUG 10
Use the chart (Refer to PER-TOF-TOC-10-30 RTOW EXAMPLE)
Enter the 10 kt head wind column and interpolate for 25 °C, CONF 1+F,
Maximum TO weight (1 000 kg) air conditioning OFF.............................................................82.1
Enter the 10 kt head wind column and interpolate for 25 °C, CONF 2,
Maximum TO weight (1 000 kg) air conditioning OFF.............................................................82.1
Retain CONF 2 as takeoff configuration.
Maximum TO weight (1 000 kg) air conditioning OFF.............................................................82.1
Air conditioning correction...................................................................................................... - 2.1
(Refer to PER-TOF-CTA-10 GENERAL)
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A320機組操作手冊FLIGHT CREW OPERATING MANUAL 7(35)