A320机组操作手册FLIGHT CREW OPERATING MANUAL 7(70)

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between two consecutive rows and/or columns for weight and for wind values not displayed on the
chart.
• Repeat this process for the other configuration available. Select that configuration giving the
highest flexible temperature.
CORRECTIONS DUE TO DIFFERENT TAKEOFF CONDITIONS
Applicable to: MSN,
4473
When the takeoff conditions are different from those provided on the chart, apply the associated
corrections.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
TAKEOFF
TAKEOFF CHARTS - FLEXIBLE TAKEOFF (WEIGHT ENTRY)
A318/A319/A320/A321 FLEET PER-TOF-TOC-20-50 P 2/14
FCOM 19 AUG 10
Note: If the RTOW chart is based on the CG being at 25 %, the crew can determine the flexible
temperature at a more forward CG by decreasing the flexible temperature by 2 °C. V1, VR
and V2 must be increased by 1 kt.
CORRECTIONS DUE TO DIFFERENT TAKEOFF CONDITIONS
Applicable to:
, ,
MSN,,
When the takeoff conditions are different from those provided on the chart, apply the associated
corrections.
CONSERVATIVE CORRECTIONS FOR QNH AND BLEEDS
Applicable to:
Bnqqdbshnmr􀀃􀁄qd􀀃fhudm􀀃enq􀀃PMG􀀃≠􀀃0􀀃/02􀀃gO􀁄+􀀃􀁄hq􀀃bnmchshnmhmf􀀃NM+􀀃􀁄msh􀀃hbd􀀃NM􀀑
1. For a given takeoff weight and wind condition, read the flexible temperature. Retain the takeoff
speeds associated with the actual weight.
2. Apply the published temperature correction. To combine two or more corrections, add the different
corrections and apply to temperature value.
(No speed corrections required).
EXAMPLE D
DATA : Actual takeoff weight = 68 000 kg
Head wind = 10 kt
Air conditioning ON
QNH = 1 013 hPa
Use the chart from Refer to PER-TOF-TOC-16-30 RTOW EXAMPLE. Determine the maximum
permissible takeoff weight Refer to PER-TOF-TOC-18-10 CONSERVATIVE CORRECTIONS
FOR QNH AND BLEEDS. The actual weight being lower than the maximum one, flexible takeoff is
possible.
Enter the 10 kt head wind column and interpolate for 68 000 kg, CONF 1+F,
Flexible temperature.............................................................................................................. 53 °C
Enter the 10 kt head wind column and interpolate for 68 000 kg, CONF 2,
Flexible temperature.............................................................................................................. 51 °C
Retain CONF 1+F for takeoff configuration.
Takeoff speeds are V1 = 153 kt, VR = 153 kt, V2 = 155 kt
Flexible temperature with air conditioning OFF.........................................................................53 °C
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
TAKEOFF
TAKEOFF CHARTS - FLEXIBLE TAKEOFF (WEIGHT ENTRY)
A318/A319/A320/A321 FLEET PER-TOF-TOC-20-50 P 3/14
FCOM 19 AUG 10
Air conditioning correction..........................................................................................................-3 °C
(Refer to PER-TOF-TOD-24 EFFECT OF QNH AND BLEEDS)
Maximum flexible temperature.................................................................................................. 50 °C
CONSERVATIVE CORRECTIONS FOR QNH AND BLEEDS
Applicable to:
Bnqqdbshnmr􀀃􀁄qd􀀃fhudm􀀃enq􀀃PMG􀀃≠􀀃0􀀃/02􀀃gO􀁄+􀀃􀁄hq􀀃bnmchshoning ON, anti ice ON.
1. For a given takeoff weight and wind condition, read the flexible temperature. Retain the takeoff
speeds associated with the actual weight.
2. Apply the published temperature correction. To combine two or more corrections, add the different
corrections and apply to temperature value.
(No speed corrections required).
EXAMPLE D
DATA : Actual takeoff weight = 68 000 kg
Head wind = 10 kt
Air conditioning ON
QNH = 1 013 hPa
Use the chart from Refer to PER-TOF-TOC-16-30 RTOW EXAMPLE. Determine the maximum
permissible takeoff weight Refer to PER-TOF-TOC-18-10 CONSERVATIVE CORRECTIONS
FOR QNH AND BLEEDS. The actual weight being lower than the maximum one, flexible takeoff is
possible.
Enter the 10 kt head wind column and interpolate for 68 000 kg, CONF 1+F,
Flexible temperature.............................................................................................................. 53 °C
Enter the 10 kt head wind column and interpolate for 68 000 kg, CONF 2,
Flexible temperature.............................................................................................................. 51 °C
Retain CONF 1+F for takeoff configuration.
　
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