曝光臺 注意防騙 網(wǎng)曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

with the retained configuration and weight value.
EXAMPLE A
DATA : OAT = 25 °C
Head Wind = 10 kt
Air conditioning ON
QNH = 1 013 hPa
Use the chart (Refer to PER-TOF-TOD-24 EFFECT OF QNH AND BLEEDS).
Enter the 10 kt head wind column CONF 1+F, to read for 25 °C.
The lowest temperature of the column is 38 °C, use Grad 1/Grad 2 to extrapolate the maximum
takeoff weight.
Max TO weight (1 000 kg) air conditioning OFF = 76.2 + 0.4 × 2 + 0.04 × 11 = 77.4
Enter the 10 kt head wind column CONF 2, to read for 25 °C.
The lowest temperature of the column is 37 °C, use Grad 1/Grad 2 to extrapolate the maximum
takeoff weight.
Max TO weight (1 000 kg) air conditioning OFF = 76.0 + 0.41 × 1 + 0.03 × 11 = 76.7
Retain CONF 1+F as takeoff configuration.
Maximum TO weight (1 000 kg) air conditioning OFF................................................................ 77.4
Air conditioning correction............................................................................................................ -2.1
(Refer to PER-TOF-TOD-24 EFFECT OF QNH AND BLEEDS)
Maximum permissible TO weight (1 000 kg) air conditioning ON............................................... 75.3
Determine takeoff speeds for 75.3 (1 000 kg) in the 10 kt head wind column (CONF 1+F)
V1 = 154 kt, VR = 157 kt, V2 = 160 kt
CONSERVATIVE CORRECTIONS FOR QNH AND BLEEDS
Applicable to:
Refer to PER-TOF-TOD-24 EFFECT OF QNH AND BLEEDS
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
TAKEOFF
TAKEOFF CHARTS - MTOW CALCULATION (WEIGHT ENTRY)
A318/A319/A320/A321 FLEET PER-TOF-TOC-18-10 P 7/26
FCOM 19 AUG 10
Corrections are given for QNH ≠􀀃0􀀃/02􀀃gO􀁄+􀀃􀁄hq􀀃bnmchshnmhmf􀀃NM+􀀃􀁄msh􀀃hbd􀀃NM􀀑
1. For the given wind and temperature conditions, determine 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 weight value.
EXAMPLE A
DATA : OAT = 25 °C
Head Wind = 10 kt
Air conditioning ON
QNH = 1 013 hPa
Use the chart (Refer to PER-TOF-TOD-24 EFFECT OF QNH AND BLEEDS).
Enter the 10 kt head wind column CONF 1+F, to read for 25 °C.
The lowest temperature of the column is 38 °C, use Grad 1/Grad 2 to extrapolate the maximum
takeoff weight.
Max TO weight (1 000 kg) air conditioning OFF = 76.2 + 0.4 × 2 + 0.04 × 11 = 77.4
Enter the 10 kt head wind column CONF 2, to read for 25 °C.
The lowest temperature of the column is 37 °C, use Grad 1/Grad 2 to extrapolate the maximum
takeoff weight.
Max TO weight (1 000 kg) air conditioning OFF = 76.0 + 0.41 × 1 + 0.03 × 11 = 76.7
Retain CONF 1+F as takeoff configuration.
Maximum TO weight (1 000 kg) air conditioning OFF................................................................ 77.4
Air conditioning correction............................................................................................................ -2.2
(Refer to PER-TOF-TOD-24 EFFECT OF QNH AND BLEEDS)
Maximum permissible TO weight (1 000 kg) air conditioning ON............................................... 75.2
Determine takeoff speeds for 75.2 (1 000 kg) in the 10 kt head wind column (CONF 1+F)
V1 = 154 kt, VR = 157 kt, V2 = 160 kt
CONSERVATIVE CORRECTIONS FOR QNH AND BLEEDS
Applicable to: MSN,
Refer to PER-TOF-TOD-24 EFFECT OF QNH AND BLEEDS
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
TAKEOFF
TAKEOFF CHARTS - MTOW CALCULATION (WEIGHT ENTRY)
A318/A319/A320/A321 FLEET PER-TOF-TOC-18-10 P 8/26
FCOM 19 AUG 10
Corrections are given for QNH ≠􀀃0􀀃/02􀀃gO􀁄+􀀃􀁄hq􀀃bnmchshnmhmf􀀃NM+􀀃􀁄msh􀀃hbd􀀃NM􀀑
1. For the given wind and temperature conditions, determine 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 weight value.
EXAMPLE A
DATA : OAT = 25 °C
Head Wind = 10 kt
Air conditioning ON
QNH = 1 013 hPa
　
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