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Refer to figure.
The trim sheet for a twin-engined jet airplane is finalized using the following data:

CG for Zero Fuel Mass: 30%
MAC CG for Take-off Mass: 24%
MAC CG for Landing Mass: 26%

If the crew opts for flaps 15 for take-off, what would be the corresponding stabilizer trim setting?

  • A

    3.0

  • B

    3.25

  • C

    2.5

  • D

    4

Refer to figure.
Identify the take-off percentage of the Mean Aerodynamic Chord (MAC) at 24% with flaps set to 15. As the table only provides %MAC values at 22 and 26, interpolation between 3.5 and 3 results in an estimated value of 3.25.

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