(Refer to figure 36.) Approximately what true airspeed should a pilot expect with 65 percent maximum continuous power at 9,500 feet with a temperature of 36 °F below standard?

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(Refer to figure 38.) Determine the approximate ground roll distance after landing.

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OAT ………………………………………………………….. 90 °F
Pressure altitude ……………………………………….. 4,000 ft
Weight …………………………………………………… 2,800 lb
Tailwind component ……………………………………… 10 kts

 

(Refer to figure 36.) What is the expected fuel consumption for a 1,000-nautical mile flight under the following conditions?

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Pressure altitude ……………………………………….. 8,000 ft
Temperature ……………………………………………….. 22 °C
Manifold pressure …………………………………… 20.8” Hg
Wind …………………………………………………………. Calm

 

(Refer to figure 8.) Determine the pressure altitude at an airport that is 1,386 feet MSL with an altimeter setting of 29.97.

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