A320机组操作手册FLIGHT CREW OPERATING MANUAL 7(40)

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those provided on lines 3 and 4).
Since the speed check is fulfilled :
Maximum permissible takeoff weight = 85.2 (1 000 kg)
V1 = 155 kt, VR = 158 kt, V2 = 158 kt.
Takeoff Configuration : 2
TOW V1 VR V2
TOW (RTOW) 88.1
FCOM correction(s) - 3.3
Intermediate value 84.8 154 156 156
WET Correction 0.0 0 0 0
Intermediate value 84.8 154 156 156
QNH Correction + 0.4 +1 +2 +2
Final value 85.2 155 158 158
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 14/22
FCOM 19 AUG 10
COMBINING CORRECTIONS FROM FCOM AND CHART
Applicable to:
Proceed as follows :
1. Enter the chart with selected configuration, OAT and wind to read the maximum takeoff weight.
2. Apply corrections from FCOM to determine an intermediate weight. Interpolate associated speeds
for intermediate weight in the same column (same wind and configuration).
3. Apply corrections from RTOW chart as explained above.
EXAMPLE 3
DATA :: OAT = 25 °C
Head wind = 10 kt
Air conditioning ON
QNH = 1 028 hPa
WET runway
1. Use the chart (Refer to DSC-45-25 GENERAL).
Enter the 10 kt head wind column and interpolate for 25 °C, CONF 1+F,
Max TO weight (1 000 kg) air conditioning OFF..................................................................... 71.2
Enter the 10 kt head wind column and interpolate for 25 °C, CONF 2,
Max TO weight (1 000 kg) air conditioning OFF..................................................................... 70.8
Retain CONF 1+F for takeoff configuration.
2. First, apply the correction (Refer to DSC-52-30 WARNINGS AND CAUTIONS).
Max TO weight (1 000 kg) air conditioning OFF..................................................................... 71.2
Air conditioning correction.......................................................................................................- 2.0
Intermediate weight..................................................................................................................69.2
Interpolate takeoff speeds for 69.2 (1 000 kg) in the 10 kt head wind column,
V1 = 151 kt , VR = 152 kt , V2 = 154 kt
3. Apply WET correction
Enq􀀃N􀀤S􀀃􀀟􀀃SULB􀀃􀀋43􀀃°B(+􀀃ΔV􀀃<􀀑􀀑􀀑􀀑􀀑􀀑􀀑􀀑􀀑􀀑􀀑􀀑􀀑􀀑􀀑􀀑􀀑􀀑􀀑􀀑􀀑􀀑􀀑􀀑􀀑􀀑􀀑􀀑􀀑􀀑􀀑􀀑􀀑􀀑􀀑􀀑􀀑􀀑􀀑􀀑􀀑􀀑􀀑􀀑􀀑􀀑􀀑􀀑􀀑􀀑􀀑􀀑􀀑􀀑􀀑􀀑􀀑􀀑􀀑􀀑􀀑􀀑􀀑􀀑􀀑􀀑􀀑􀀑􀀑􀀑􀀑􀀑􀀑􀀑􀀑􀀑􀀑􀀑􀀑􀀑􀀑􀀑􀀑􀀑􀀑􀀑􀀑􀀑􀀑􀀑􀀑􀀑􀀑􀀑􀀃/􀀑/
Intermediate weight..................................................................................................................69.2
Associated speeds,
V1 = 151 kt - 4 = 147 kt
VR = 152 kt - 1 = 151 kt
V2 = 154 kt - 1 = 153 kt
Check that the speeds are higher than minimum speeds from the chart and from VMU table
Apply QNH correction
Enq􀀃N􀀤S􀀃􀀟􀀃SULB􀀃􀀋43􀀃°B(+􀀃ΔV􀀃<􀀃/􀀑0􀀃×􀀃04.0/􀀃<􀀑􀀑􀀑..................................................................+ 0.1
Maximum permissible takeoff weight.......................................................................................69.3
Associated speed,
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 15/22
FCOM 19 AUG 10
V1 = 147 kt + 0 × 15/10 = 147 kt
VR = 151 kt + 0 × 15/10 = 151 kt
V2 = 153 kt + 0 × 15/10 = 153 kt
Check that the speeds are higher than minimum speeds from the chart and from VMU table. (It
is reminded that if the speed checks are not fulfilled, the corrections must be recalculated using
those provided on lines 3 and 4).
Since the speed check is fulfilled :
　
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