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Refer to figure.
An aircraft is departing from an airfield that has a pressure altitude of 3000 ft with a purpose to climb to FL75. Given the following data determine the climb speed.

Aircraft mass: 3000 lbs
OAT at airfield: 25°C
OAT in FL75: 0°C

  • A

    90 kt

  • B

    120 kt

  • C

    110 kt

  • D

    100 kt

Refer to figure.
On the top left of the performance table, the following conditions are indicated:

  • POWER: Full throttle, 2700 RPM
  • MIXTURE: Full rich
  • WING FLAPS: Up
  • COWL FLAPS: As required
  • CLIMB SPEED: 110 kt all masses

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