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Refer to Annex -031-007.
The aeroplane has a Take-Off Mass of 58 000 kg. At this mass the range of allowable CG positions, as determined from graph, is:
  • A
    Forward limit 9.5% MAC aft limit 26.1% MAC
  • B
    Forward limit 8.2% MAC aft limit 26.2% MAC
  • C
    Forward limit 8.0% MAC aft limit 26.5% MAC
  • D
    Forward limit 8.5% MAC aft limit 26.1% MAC

Draw a line representing the takeoff mass (58000 kg) and see where it will intersect the CG envelope, determine forward and aft CG.

Correct Answer: Forward limit 8.0% MAC aft limit 26.5%MAC

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