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1. **What two things determine the term 'angle of attack'?**

2. **Which statement relates to Bernoulli's principle?**

3. **Refer to Figure 36 on page 38.**

Determine the approximate manifold pressure setting with 2,450 RPM to achieve 65 percent maximum continuous power at 6,500 feet with a temperature of 36 °F higher than standard.

Determine the approximate manifold pressure setting with 2,450 RPM to achieve 65 percent maximum continuous power at 6,500 feet with a temperature of 36 °F higher than standard.

4. **Refer to Figure 36 on page 38.**

Approximately what true airspeed should a pilot expect with 65 percent maximum continuous power at 9,500 feet and a temperature of 36 °F below standard?

Approximately what true airspeed should a pilot expect with 65 percent maximum continuous power at 9,500 feet and a temperature of 36 °F below standard?

5. **Refer to Figure 8 on page 10.**

What is the effect of a temperature increase from 35 to 50 °F on the density altitude if the pressure altitude remains at 3,000 feet MSL?

What is the effect of a temperature increase from 35 to 50 °F on the density altitude if the pressure altitude remains at 3,000 feet MSL?