# Ground effect is most likely to result in which

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Ground effect is most likely to result in which problem?
(Refer to figure 36.) What fuel flow should a pilot expect at 11,000 feet on astandard day with 65 percent maximum continuous power?
Which combination of atmospheric conditions will reduce aircraft takeoff andclimb performance?
(Refer to figure 41.) Determine the approximate ground roll distance requiredfor takeoff.
(Refer to figure 8.) Determine the pressure altitude with an indicated altitude of1,380 feet MSL with an altimeter setting of 28.22 at standard temperature.
(Refer to figure 26.) Estimate the time en route from Addison (area 2) to DallasExecutive (area 3). The wind is from 300° at 15 knots, the true airspeed is 120knots, and the magnetic variation is 7° east.
(Refer to figure 37.) With a reported wind of south at 20 knots, which runway(10, 14, or 24) is appropriate for an airplane with a 13-knot maximum crosswindcomponent?
(Refer to figure 41.) Determine the total distance required for takeoff to clear a50-foot obstacle.
(Refer to figure 8.) Determine the pressure altitude at an airport that is 1,386 feetMSL with an altimeter setting of 29.97.
(Refer to figure 38.) Determine the approximate total distance required to landover a 50-foot obstacle.
What must a pilot be aware of as a result of ground effect?
(Refer to figure 41.) Determine the approximate ground roll distance requiredfor takeoff.
What effect, if any, does high humidity have on aircraft performance?
What is ground effect?
(Refer to figure 36.) What is the expected fuel consumption for a 1,000-nauticalmile flight under the following conditions?Pressure altitude 8,000 ftTemperature 22 °CManifold pressure 20.8 inches HgWind Calm70.1 gallons.(Refer to figure 37.) Determine the maximum wind velocity for a 45° crosswind ifthe maximum crosswind component for the airplane is 25 knots.v35 knots.(Refer to figure 39.) Determine the total distance required to land over a 50-footobstacle.
(Refer to figure 8.) What is the effect of a temperature decrease and a pressurealtitude increase on the density altitude from 90 °F and 1,250 feet pressurealtitude to 55 °F and 1,750 feet pressure altitude?
(Refer to figure 39.) Determine the total distance required to land over a 50-footobstacle.
Runway Hard surface

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