HW 10
What is the crosswind component for a landing on Runway 18 if the tower reports the wind as 220° at 30 knots? A.30 knots. B.19 knots.
.Answer B is correct.
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? A.183 MPH.
Answer A is correct.
Determine the approximate landing ground roll distance.Pressure altitude = 5,000 ftHeadwind = CalmTemperature = 101°F A.545 feet.
Answer A is correct.
Determine the approximate landing ground roll distance.Pressure altitude = Sea levelHeadwind = 4 ktsTemperature = Std A.401 feet.
Answer A is correct.
Determine the total distance required for takeoff to clear a 50-foot obstacle.OAT = StdPressure altitude = 4,000 ftTakeoff weight = 2,800 lbHeadwind component = Calm A.1,750 feet.
Answer A is correct.
Determine the total distance required to land over a 50-ft. obstacle.Pressure altitude = 3,750 ftHeadwind = 12 ktsTemperature = Std A.816 feet.
Answer A is correct.
What is the headwind component for a landing on Runway 18 if the tower reports the wind as 220° at 30 knots? A.23 knots.
Answer A is correct.
If an emergency situation requires a downwind landing, pilots should expect a faster A.groundspeed at touchdown, a longer ground roll, and the likelihood of overshooting the desired touchdown point.
Answer A is correct. A downwind landing, in an emergency or other situation, will result in a faster groundspeed at touchdown, which means a longer ground roll, which in turn increases the likelihood of overshooting the desired touchdown point.
What is the expected fuel consumption for a 500-nautical mile flight under the following conditions?Pressure altitude = 4,000 ftTemperature = +29°CManifold pressure = 21.3" Hg Wind = Calm A.31.4 gallons. B.36.1 gallons.
Answer B is correct
Approximately what true airspeed should a pilot expect with full throttle at 10,500 feet with a temperature of 36°F above standard? A.159 KTS. B.165 KTS.
Answer B is correct.
Determine the approximate ground roll distance required for takeoff.OAT = 38°CPressure altitude = 2,000 ftTakeoff weight = 2,750 lbHeadwind component = Calm A.1,800 feet. B.1,150 feet.
Answer B is correct.
Determine the approximate landing ground roll distance.Pressure altitude = 1,250 ftHeadwind = 8 ktsTemperature = Std A.275 feet. B.366 feet
Answer B is correct.
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. A.19.8" Hg. B.21.0" Hg.
Answer B is correct.
Determine the total distance required for takeoff to clear a 50-foot obstacle.OAT = StdPressure altitude = Sea levelTakeoff weight = 2,700 lbHeadwind component = Calm A.1,700 feet. B.1,400 feet.
Answer B is correct.
Determine the total distance required to land over a 50-foot obstacle.Pressure altitude = 7,500 ftHeadwind = 8 ktsTemperature = 32°FRunway = Hard surface A.1,205 feet. B.1,004 feet.
Answer B is correct.
What fuel flow should a pilot expect at 11,000 feet on a standard day with 65 percent maximum continuous power? A.10.6 gallons per hour. B.11.2 gallons per hour.
Answer B is correct.
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? A.Runway 29. B.Runway 32.
Answer B is correct.
With a reported wind of south at 20 knots, which runway is appropriate for an airplane with a 13-knot maximum crosswind component? A.Runway 24. B.Runway 14.
Answer B is correct.
Determine the approximate ground roll distance required for takeoff.OAT = 32°CPressure altitude = 2,000 ftTakeoff weight = 2,500 lbHeadwind component = 20 kts A.1,000 feet. B.850 feet. C.650 feet.
Answer C is correct.
Determine the approximate total distance required to land over a 50-ft. obstacle.OAT = 90°FPressure altitude = 4,000 ftWeight = 2,800 lbHeadwind component = 10 kts A.1,525 feet. B.1,950 feet. C.1,775 feet.
Answer C is correct.
Determine the maximum wind velocity for a 45° crosswind if the maximum crosswind component for the airplane is 25 knots. A.29 knots. B.25 knots. C.35 knots.
Answer C is correct.
Determine the total distance required to land over a 50-foot obstacle.Pressure altitude = 5,000 ftHeadwind = 8 ktsTemperature = 41°FRunway = Hard surface A.1,076 feet. B.837 feet. C.956 feet.
Answer C is correct.
Determine the total distance required to land.OAT = 90°FPressure altitude = 3,000 ftWeight = 2,900 lbHeadwind component = 10 ktsObstacle = 50 ft A.1,450 feet. B.1,550 feet. C.1,725 feet.
Answer C is correct.
What is the maximum wind velocity for a 30° crosswind if the maximum crosswind component for the airplane is 12 knots? A.20 knots. B.16 knots. C.24 knots.
Answer C is correct.
