Extra Study 10

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

1,004 feet.

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

1,150 feet

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

1,400 feet

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

1,400 feet

Determine the total distance required to land. OAT = 90°F Pressure altitude = 3,000 ft Weight = 2,900 lb Headwind component = 10 kts Obstacle = 50 ft

1,725 feet

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

1,750 feet

Determine the approximate total distance required to land over a 50-ft. obstacle. OAT = 90°F Pressure altitude = 4,000 ft Weight = 2,800 lb Headwind component = 10 kts

1,775 feet

Determine the total distance required to land. OAT = Std Pressure altitude = 10,000 ft Weight = 2,400 lb Wind component = Calm Obstacle = 50 ft

1,925 feet

What fuel flow should a pilot expect at 11,000 feet on a standard day with 65 percent maximum continuous power?

11,2 gallons per hour

Approximately what true airspeed should a pilot expect with full throttle at 10,500 feet with a temperature of 36°F above standard?

165 KTS

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?

183 MPH

What is the crosswind component for a landing on Runway 18 if the tower reports the wind as 220° at 30 knots?

19 knots

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.

21.0" Hg.

What is the headwind component for a landing on Runway 18 if the tower reports the wind as 220° at 30 knots?

23 knots

What is the maximum wind velocity for a 30° crosswind if the maximum crosswind component for the airplane is 12 knots?

24 knots

Determine the maximum wind velocity for a 45° crosswind if the maximum crosswind component for the airplane is 25 knots.

35 knots

What is the expected fuel consumption for a 500-nautical mile flight under the following conditions? Pressure altitude = 4,000 ft Temperature = +29°C Manifold pressure = 21.3" Hg Wind = Calm

36.1 gallons

Determine the approximate landing ground roll distance. Pressure altitude = 1,250 ft Headwind = 8 kts Temperature = Std

366 feet.

Determine the approximate landing ground roll distance. Pressure altitude = Sea level Headwind = 4 kts Temperature = Std

401 feet

Determine the approximate landing ground roll distance. Pressure altitude = 5,000 ft Headwind = Calm Temperature = 101°F

545 feet.

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

650 feet

What is the expected fuel consumption for a 1,000-nautical mile flight under the following conditions? Pressure altitude = 8,000 ft Temperature = 22°C Manifold pressure = 20.8" Hg Wind = Calm

70.1 gallons

Determine the total distance required to land over a 50-ft. obstacle. Pressure altitude = 3,750 ft Headwind = 12 kts Temperature = Std

816 feet.

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

956 feet.

With a reported wind of south at 20 knots, which runway is appropriate for an airplane with a 13-knot maximum crosswind component?

Runway 14

With a reported wind of north at 20 knots, which runway is acceptable for use for an airplane with a 13-knot maximum crosswind component?

Runway 32

If an emergency situation requires a downwind landing, pilots should expect a faster

groundspeed at touchdown, a longer ground roll, and the likelihood of overshooting the desired touchdown point.