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Refer to figure or CAP697 Figure 3.4.
Given the following information, what is the true airspeed?

Pressure altitude: 12 000 feet
Temperature: ISA
Power: 65%

  • A
    184 knots
  • B
    163 knots
  • C
    178 knots
  • D
    146 knots
Refer to figure.

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