曝光臺 注意防騙 網曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

330 0 0.1 0.1 0.1 0.2 0.2 0.2 10 min
310 0 0.1 0.1 0.1 0.1 0.2 0.2 10 min
290 0 0.1 0.1 0.1 0.1 0.2 0.2 10 min
270 0 0.1 0.1 0.1 0.1 0.2 0.2 10 min
250 0 0 0.1 0.1 0.1 0.1 0.2 10 min
200 0 0 0 0.1 0.1 0.1 0.1 9 min
150 0 0 0 0 0 0.1 0.1 8 min
100 0 0 0 0 0 0 0 8 min
DESCENT CORRECTION
Applicable to: MSN,
Correct the fuel and time values determined in the integrated cruise tables as follows to take into
account the descent down to 1 500 ft followed by a 6 min IFR approach and landing.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
FLIGHT PLANNING
FLIGHT PREPARATION - INTEGRATED CRUISE
A318/A319/A320/A321 FLEET PER-FPL-FLP-ICR-60 P 4/4
FCOM 19 AUG 10
CORRECTION ON FUEL CONSUMPTION (1 000 kg)
FL 46 50WEIGHT O5V4ERHEAD D5E8STINATION6 2(1 000 kg) 66 70 Time Correction
390 0.2 0.2 0.2 0.3 0.3 - - 10 min
370 0.2 0.2 0.2 0.2 0.3 0.3 0.4 10 min
350 0.2 0.2 0.2 0.2 0.3 0.3 0.3 11 min
330 0.2 0.2 0.2 0.2 0.3 0.3 0.3 11 min
310 0.2 0.2 0.2 0.2 0.3 0.3 0.3 11 min
290 0.2 0.2 0.2 0.2 0.3 0.3 0.3 11 min
270 0.2 0.2 0.2 0.2 0.3 0.3 0.3 11 min
250 0.2 0.2 0.2 0.2 0.3 0.3 0.3 11 min
200 0.2 0.2 0.2 0.2 0.3 0.3 0.3 10 min
150 0.1 0.2 0.2 0.2 0.2 0.2 0.2 10 min
100 0.1 0.1 0.1 0.1 0.1 0.2 0.2 9 min
DESCENT CORRECTION
Applicable to:
Correct the fuel and time values determined in the integrated cruise tables as follows to take into
account the descent down to 1 500 ft followed by a 6 min IFR approach and landing.
CORRECTION ON FUEL CONSUMPTION (1 000 kg)
FL 46 50WEIGHT O5V4ERHEAD D5E8STINATION6 2(1 000 kg) 66 70 Time Correction
390 0.2 0.2 0.2 0.3 0.3 - - 10 min
370 0.2 0.2 0.2 0.2 0.3 0.3 0.4 10 min
350 0.2 0.2 0.2 0.2 0.3 0.3 0.3 10 min
330 0.2 0.2 0.2 0.2 0.3 0.3 0.3 10 min
310 0.2 0.2 0.2 0.2 0.3 0.3 0.3 10 min
290 0.2 0.2 0.2 0.2 0.3 0.3 0.3 11 min
270 0.2 0.2 0.2 0.2 0.3 0.3 0.3 11 min
250 0.2 0.2 0.2 0.2 0.3 0.3 0.3 11 min
200 0.2 0.2 0.2 0.2 0.3 0.3 0.3 10 min
150 0.1 0.2 0.2 0.2 0.2 0.2 0.2 9 min
100 0.1 0.1 0.1 0.1 0.1 0.1 0.2 9 min
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
FLIGHT PLANNING
FLIGHT PREPARATION - QUICK DETERMINATION OF FLIGHT PLANNING
A318/A319/A320/A321 FLEET PER-FPL-FLP-QFP-10 P 1/4
FCOM 19 AUG 10
INTRODUCTION
INTRODUCTION
Applicable to: MSN,
The following flight planning tables allow the planner to determine trip fuel consumption and trip time
required to cover a given air distance.
These tables are established for :
‐ Takeoff
‐ Climb profile 250 kg/300 kt/M .78
‐ Cruise Mach number M .78/LR
‐ Descent profile M .78/300 kt/250 kt
‐ Approach and landing 120 kg - 6 min IFR
‐ ISA
‐ CG = 33 %
‐ Normal air conditioning
‐ Anti ice OFF
They are based upon a reference landing weight of 55 000 kg.
Note: 1. In the tables, the asterisk (*) means that a step climb of 4 000 ft must be flown to reach
the corresponding FL.
2. To obtain a flight plan at optimum cruise level, the highest flight level desired within the
flight has to be selected in the table.
3. For each degree Celcius above ISA temperature apply fuel correction 0.015 (kg/°C/NM)
× ◂ISA (°C) × Air Distance (NM).
INTRODUCTION
Applicable to: ,
, MSN,,
The following flight planning tables allow the planner to determine trip fuel consumption and trip time
required to cover a given air distance.
These tables are established for :
‐ Takeoff
‐ Climb profile 250 kg/300 kt/M .78
‐ Cruise Mach number M .78/LR
Descent ‐ profile M .78/300 kt/250 kt
‐ Approach and landing 140 kg - 6 min IFR
‐ ISA
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
FLIGHT PLANNING
FLIGHT PREPARATION - QUICK DETERMINATION OF FLIGHT PLANNING
A318/A319/A320/A321 FLEET PER-FPL-FLP-QFP-10 P 2/4
FCOM 19 AUG 10
‐ CG = 33 %
‐ Normal air conditioning
‐ Anti ice OFF
They are based upon a reference landing weight of 60 000 kg.
Note: 1. In the tables, the asterisk (*) means that a step climb of 4 000 ft must be flown to reach
the corresponding FL.
2. To obtain a flight plan at optimum cruise level, the highest flight level desired within the
flight has to be selected in the table.
3. For each degree Celcius above ISA temperature apply fuel correction 0.015 (kg/°C/NM)
× ◂ISA (°C) × Air Distance (NM).
INTRODUCTION
Applicable to:
The following flight planning tables allow the planner to determine trip fuel consumption and trip time
required to cover a given air distance.
　
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