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Refer to figure.
Given the following data, determine the maximum rate of climb of the aircraft.

Outside air temperature: 12°C
Pressure altitude: 9000 ft

  • A

    200 ft/min

  • B

    250 ft/min

  • C

    350 ft/min

  • D

    300 ft/min

Refer to figure.
In order to find the maximum rate of climb from the graph:

  1. Locate the outside air temperature of 12°C on the left lower side of the graph.
  2. Draw a line upwards from the point of outside air temperature of 12°C until the midway between the Pressure Altitude lines of 8000 ft and 10 000 ft.
  3. From that point draw a line towards the right until it intersects the rate of climb graph.
  4. From that intersection draw a line downwards and read a rate of climb of 200 ft/min.

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