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Refer to figure. 
Using the graph, and given the following parameters, what is the loaded centre of gravity of this aircraft?

BEM: 1100 kg 
BEM arm: 3.10 
Front pax: 150 kg 
Rear pax: 200 kg 
Fuel: 200 kg

  • A
    3.10 m
  • B
    2.94 m
  • C
    3.01 m
  • D
    2.98 m

Refer to figure.
We need to get the loaded aircraft mass = 1100 + 150 + 200 + 200 = 1650 kg
Start with the BEM (1100 kg) and BEM CG Arm (3.10).
Then add front pax (150 kg) and rear pax (200 kg).
Lastly, add fuel (200 kg) and match it with 1650 kg aircraft mass to get loaded CG.

Loaded CG: 2.98 m

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