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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 5800
200 8900
300 12000
400 15100
500 18200
1000 33800
1500 49300
2000 64800 95% 91% 88% 87% 86%
2500 80300 of of of of of
3000 95800 FL310 FL310 FL310 FL310 FL310
3500 111300
4000 126800
4500 142300
5000 157800
5500 173300
6000 188900
6500 204400
7000 219900
7500 235400
8000 250700
8500 - - 242400 234400 231700 229100
9000 - - - 248000 245200 242400
Fuel planning notes A340-300 (1kg = 2,205 lbs):
Basic Operating Weight (OEW) 287.000 LBS
= Zero Fuel Weigh (ZFW) XXX.XXX LBS (max 399.000 LBS)
+ Payload (passengers & cargo) XXX.XXX LBS
+ Minimum Landing Fuel 012.000 LBS
+ Alternate Fuel (200nm distance) 006.000 LBS
= Planned Landing Weight (PLW) XXX.XXX LBS (max 423.300 LBS)
+ Contingency Fuel (holding, taxi, etc.) 012.000 LBS
= Planned Takeoff Weight (PTOW) XXX.XXX LBS (max 609.600 LBS)
+ Flight Plan Fuel (fuel for route) XXX.XXX LBS
Flight Plan Fuel + 30.000 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.
A340-600 Attachments:
A340-600 Optimum & Maximum Flight Level Charts:
A340-600 Fuel Planing Charts:
Flightplan
Fuel
Only
MZFW
553400 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 4000
200 7600
300 11500
400 15300
500 19200
1000 38600
1500 58000
2000 77400
2500 96800 95% 92% 89% 88% 87%
3000 116200 Of Of of of of
3500 135600 FL310 FL310 FL310 FL310 FL310
4000 155000
4500 174500
5000 193800
5500 213200
6000 232600
6500 252000
7000 271500
7500 290900
8000 310200
8300 322000
8500 - 313100 303200 293300 290000 286700
9000 - - 321000 310600 307100 303600
9500 - - - - - 320500
Fuel planning notes A340-600:
Basic Operating Weight (OEW) 400.900 LBS
= Zero Fuel Weigh (ZFW) XXX.XXX LBS (max 553.400 LBS)
+ Payload (passengers & cargo) XXX.XXX LBS
+ Minimum Landing Fuel 017.500 LBS
+ Alternate Fuel (200nm distance) 008.000 LBS
= Planned Landing Weight (PLW) XXX.XXX LBS (max 584.200 LBS)
+ Contingency Fuel (holding, taxi, etc.) 017.500 LBS
= Planned Takeoff Weight (PTOW) XXX.XXX LBS (max 837.800 LBS)
+ Flight Plan Fuel (fuel for route) XXX.XXX LBS
Flight Plan Fuel + 43.000 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.
Attachments for all Airplanes:
Product Presentation
AP-3C Autopilot System
Introduction
• Chelton Aviation is a member of a worldwide
family of aerospace/marine/defense
electronics companies.
• Chelton products are original equipment on
Cessna, Piper, Mooney, Liberty, Pilatus,
Learjet, Embraer, Airbus, Boeing, Eurocopter,
Concorde, Eurofighter, and more.
• Chelton was founded in 1947 and is a
Subsidiary of Cobham plc, a $2 Billion
aerospace and defense conglomerate.
• Chelton Aviation Corp. produces advanced
autopilot flight control products.
• Based in Denton, Texas.
• Product development in Denton, Texas and
Gainesville, Florida.
• STC development and modification operations
in Denton, Texas.
• Manufacturing and repair facilities in Prescott,
Arizona and Denton, Texas.
Introduction
• New standard of reliability, precision, and quality.
• Surface mount solid-state electronics.
• Matched blend of the latest digital and analog
technologies.
• Time proven proprietary stabilization algorithms.
• Suitable for single and twin engine aircraft.
　
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