# FAA Aircraft Performance Test 2

This is a timed quiz. You will be given 60 seconds per question. Are you ready?

60

#### (Refer to Figure 38.) Determine the approximate landing ground roll distance. Pressure altitude.................Sea level Headwind..............................4 kts Temperature.............................Std

Correct!
Wrong!

#### (Refer to Figure 36.) What is the crosswind component for a landing on Runway 18 if the tower reports the wind as 220° at 30 knots?

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#### (Refer to Figure 40.) Determine the total distance required for takeoff to clear a 50-foot obstacle. OAT..........................................Std Pressure altitude.......................4,000 ft Takeoff weight..........................2,800 lb Headwind component..........................Calm

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#### (Refer to Figure 36.) What is the maximum wind velocity for a 30° crosswind if the maximum crosswind component for the airplane is 12 knots?

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#### (Refer to Figure 38.) Determine the total distance required to land over a 50-foot obstacle. Pressure altitude..............5,000 ft Headwind..........................8 kts Temperature.......................41 °F Runway.....................Hard surface

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#### (Refer to Figure 40.) Determine the approximate ground roll distance required for takeoff. OAT.........................................32 °C Pressure altitude........................2,000 ft Takeoff weight...........................2,500 lb Headwind component..........................20 kts

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#### (Refer to Figure 35.) Approximately what true airspeed should a pilot expect with full throttle at 10,500 feet with a temperature of 36 °F above standard?

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#### (Refer to Figure 38.) Determine the approximate landing ground roll distance. Pressure altitude.........................1,250 ft Headwind.....................................8 kts Temperature....................................Std

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#### (Refer to Figure 38.) Determine the total distance required to land over a 50-foot obstacle. Pressure altitude..............7,500 ft Headwind..........................8 kts Temperature.......................32 °F Runway.....................Hard surface

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#### (Refer to Figure 37.) Determine the total distance required to land. OAT.........................................Std Pressure altitude.....................10,000 ft Weight................................2,400 lbs Wind component.............................Calm Obstacle..................................50 ft

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#### (Refer(Refer to Figure 37.) Determine the approximate total distance required to land over a 50-foot obstacle. OAT.........................................90 °F Pressure altitude........................4,000 ft Weight...................................2,800 lbs Headwind component..........................10 kts to Figure 37.) Determine the approximate total distance required to land over a 50-foot obstacle.

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#### (Refer to Figure 37.) Determine the total distance required to land. OAT.........................................32 °F Pressure altitude........................8,000 ft Weight...................................2,600 lb Headwind component..........................20 kts Obstacle....................................50 ft

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#### (Refer to Figure 37.) Determine the total distance required to land. OAT.........................................90 °F Pressure altitude........................3,000 ft Weight...................................2,900 lbs Headwind component..........................10 kts Obstacle....................................50 ft

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#### (Refer to Figure 40.) Determine the total distance required for takeoff to clear a 50-foot obstacle. OAT......................................Std Pressure altitude..................Sea level Takeoff weight......................2,700 lb Headwind component......................Calm

Correct!
Wrong!

#### (Refer to Figure 38.) Determine the approximate landing ground roll distance. Pressure altitude......................5,000 ft Headwind...................................Calm Temperature..............................101 °F

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Wrong!

#### (Refer to Figure 36.) With a reported wind of north at 20 knots, which runway (6, 29, or 32) is acceptable for use for an airplane with a 13-knot maximum crosswind component?

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#### (Refer to Figure 40.) Determine the approximate ground roll distance required for takeoff. OAT........................................38 °C Pressure altitude.......................2,000 ft Takeoff weight..........................2,750 lb Headwind component..........................Calm

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#### A pilot and two passengers landed on a 2,100 foot east-west gravel strip with an elevation of 1,800 feet. The temperature is warmer than expected and after computing the density altitude it is determined the takeoff distance over a 50 foot obstacle is 1,980 feet. The airplane is 75 pounds under gross weight. What would be the best choice?

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#### (Refer to Figure 36.) 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 crosswind component?

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#### (Refer to Figure 36.) Determine the maximum wind velocity for a 45° crosswind if the maximum crosswind component for the airplane is 25 knots.

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Wrong!

#### (Refer to Figure 38.) Determine the total distance required to land over a 50-foot obstacle. Pressure altitude.........................3,750 ft Headwind....................................12 kts Temperature....................................Std

Correct!
Wrong!

#### (Refer to Figure 36.) What is the headwind component for a landing on Runway 18 if the tower reports the wind as 220° at 30 knots?

Correct!
Wrong!

#### (Refer to Figure 8.) 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?

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Wrong!