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+ Contingency Fuel (holding, taxi, etc.) 005.500 LBS
= Planned Takeoff Weight (PTOW) XXX.XXX LBS (max 168.650 LBS)
+ Flight Plan Fuel (fuel for route) XXX.XXX LBS
Flight Plan Fuel + 14.500 LBS = Total Fuel
 Total fuel = Enough fuel for route, 1h contingency (holding & taxi), problematic winds, alternate
fuel for 200nm and a minimum landing fuel (1h). Modify alternate value as needed.
 Load all wing tanks with same amount of fuel; outer tanks full  inner tanks  center tanks.
A330-200 Attachments:
A330-200 Optimum & Maximum Flight Level Charts:
A330-200 Fuel Planing Charts:
Flightplan
Fuel at
CI = 50
MZFW
374800 lbs
Fuel
Consumed
(lbs)
Break
Release to
Landing
Climb:
250 / 300 kt
M 0.78
Cruise:
M 0.80
Descend:
M 0.82
300 / 250 kt
Distance
(nm)
Fuel (lbs) at
FL 310
Fuel (lbs) at
FL 330
Fuel (lbs) at
FL 350
Fuel (lbs) at
FL 370
Fuel (lbs) at
FL 390
Fuel (lbs) at
FL 410
100 5000
200 8200
300 11500
400 14800
500 18100
1000 34600
1500 51800
2000 67500
2500 84000 95% 92% 88% 86% 85%
3000 100500 of of of of of
3500 116900 FL310 FL310 FL310 FL310 FL310
4000 133400
4500 149800
5000 166300
5500 182800
6000 199300
6500 215700
7000 232200
7500 248700
8000 - - 243900 233376 228072 225420
8500 - - - 247900 242262 239445
Fuel planning notes A330-200:
Basic Operating Weight (OEW) 263.700 LBS
= Zero Fuel Weigh (ZFW) XXX.XXX LBS (max 374.800 LBS)
+ Payload (passengers & cargo) XXX.XXX LBS
+ Minimum Landing Fuel 013.000 LBS
+ Alternate Fuel (200nm distance) 007.000 LBS
= Planned Landing Weight (PLW) XXX.XXX LBS (max 401.200 LBS)
+ Contingency Fuel (holding, taxi, etc.) 013.000 LBS
= Planned Takeoff Weight (PTOW) XXX.XXX LBS (max 513.700 LBS)
+ Flight Plan Fuel (fuel for route) XXX.XXX LBS
Flight Plan Fuel + 31.000 LBS = Total Fuel
 Total fuel = Enough fuel for route, 1h contingency (holding & taxi), problematic winds, alternate
fuel for 200nm and a minimum landing fuel (1h). Modify alternate value as needed.
 Load all wing tanks with same amount of fuel; inner tanks full  outer tanks  center tanks.
A330-300 Attachments:
A330-300 Optimum & Maximum Flight Level Charts:
A330-300 Fuel Planing Charts:
Flightplan
Fuel at
CI = 50
MZFW
385800 lbs
Fuel
Consumed
(lbs)
Break
Release to
Landing
Climb:
250 / 300 kt
M 0.78
Cruise:
M 0.80
Descend:
M 0.82
300 / 250 kt
Distance
(nm)
Fuel (lbs) at
FL 310
Fuel (lbs) at
FL 330
Fuel (lbs) at
FL 350
Fuel (lbs) at
FL 370
Fuel (lbs) at
FL 390
Fuel (lbs) at
FL 410
100 4800
200 7500
300 10200
400 12900
500 15600
1000 29000
1500 42500
2000 56000
2500 69500 95% 90% 88% 87% 85%
3000 82900 of Of Of Of of
3500 96400 FL310 FL310 FL310 FL310 FL310
4000 109800
4500 123300
5000 136800
5500 150200
6000 163700
6500 177100
7000 - - 171540 167728 165822 162010
7500 - - - - - 173485
Fuel planning notes A330-300:
Basic Operating Weight (OEW) 274.500 LBS
= Zero Fuel Weigh (ZFW) XXX.XXX LBS (max 385.800 LBS)
+ Payload (passengers & cargo) XXX.XXX LBS
+ Minimum Landing Fuel 013.000 LBS
+ Alternate Fuel (200nm distance) 005.000 LBS
= Planned Landing Weight (PLW) XXX.XXX LBS (max 412.300 LBS)
+ Contingency Fuel (holding, taxi, etc.) 013.000 LBS
= Planned Takeoff Weight (PTOW) XXX.XXX LBS (max 513.700 LBS)
+ Flight Plan Fuel (fuel for route) XXX.XXX LBS
Flight Plan Fuel + 28.000 LBS = Total Fuel
 Total fuel = Enough fuel for route, 1h contingency (holding & taxi), problematic winds, alternate
fuel for 200nm and a minimum landing fuel (1h). Modify alternate value as needed.
 Load all wing tanks with same amount of fuel; inner tanks full  outer tanks  center tanks.
A340-300 Attachments:
A340-300 Optimum & Maximum Flight Level Charts:
A340-300 Fuel Planing Charts:
Flightplan
Fuel
Only
MZFW
399000 lbs
Fuel
Consumed
(lbs)
Break
Release to
Landing
Climb:
250 / 300 kt
M 0.78
Cruise:
M 0.80
Descend:
M 0.82
300 / 250 kt
Distance
(nm)
　
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