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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