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
Refer to figure.
In order to find the maximum rate of climb from the graph:
- Locate the outside air temperature of 12°C on the left lower side of the graph.
- 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.
- From that point draw a line towards the right until it intersects the rate of climb graph.
- From that intersection draw a line downwards and read a rate of climb of 200 ft/min.
Your Notes (not visible to others)
This question has appeared on the real examination, you can find the related countries below.
-
Austro Control1