4. The Wide-Body Family (A300-600/A310) ...........................................................................64
4.1. Tanks and capacities ...................................................................................................64
4.2. Fuel Systems...............................................................................................................65
4.3. CG Travel during refueling...........................................................................................66
4.4. In-flight CG travel .........................................................................................................67
4.5. CG control system........................................................................................................67
C. Less Paper in the Cockpit Weight and Balance system..........69
1. Generalities........................................................................................................................69
2. User interface . general presentation.................................................................................70
WEIGHT AND BALANCE ENGINEERING
A. Generalities..............................................................................75
1. Definitions...........................................................................................................................75
1.1. Center of Gravity (CG) .................................................................................................75
1.2. Mean Aerodynamic Chord (MAC) ................................................................................75
2. Forces applied on flying aircraft..........................................................................................76
3. Influence of the CG position on performance......................................................................77
3.1. Impact on the stall speed .............................................................................................77
3.2. Impact on takeoff performance.....................................................................................79
3.3. Impact on in-flight performance....................................................................................84
3.4. Impact on landing performance....................................................................................87
3.5. Summary .....................................................................................................................88
3.6. Conclusion...................................................................................................................88
4. Certified limits design process ............................................................................................89
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