Private Pilot, Aircraft Performance, Chapter 8 Aircraft Performance - Weight and Balance, chapter 8 aircraft performance, ASA Test Prep 2025 Private Pilot Chapter 9: "Enroute Flight", Private Pilot - Aircraft Performance/Aircraft Performance

Private Pilot, Aircraft Performance, Chapter 8 Aircraft Performance - Weight and Balance, chapter 8 aircraft performance, ASA Test Prep 2025 Private Pilot Chapter 9: "Enroute Flight", Private Pilot - Aircraft Performance/Aircraft Performance, Enroute flight, FAA, ASA Private Pilot ch. 4, 6, 7, 11, airspace (Enroute Flight) Exam All Versions  Private Pilot, Aircraft Performance Answered  Chapter 8 Aircraft Performance - Weight and Balance Answered  Chapter 8 aircraft performance Answered  ASA Test Prep 2025 Private Pilot Chapter 9: "Enroute Flight" Answered  Private Pilot - Aircraft Performance/Aircraft Performance Answered  Enroute flight Answered  FAA, ASA Private Pilot ch. 4, 6, 7, 11, airspace (Enroute Flight) Answered pg. 2 (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? A) Runway 10. B) Runway 14. C) Runway 24. B) Runway 14. (Refer to Figure 35.) 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" HgWind Calm A) 60.2 gallons. B) 70.1 gallons. C) 73.2 gallons. B) 70.1 gallons. pg. 3 What effect does high density altitude have on aircraft performance? A) It increases engine performance. B) It reduces climb performance. C) It increases takeoff performance. B) It reduces climb performance. (Refer to Figure 37.) Determine the total distance required to land.OAT 32°FPressure altitude 8,000 ftWeight 2,600 lbHeadwind component 20 ktsObstacle 50 ft A) 850 feet. B) 1,400 feet. C) 1,750 feet. B) 1,400 feet. (Refer to Figures 32 and 33.) What effect does a 35-gallon fuel burn (main tanks) have on the weight and balance if the airplane weighed 2,890 pounds and the MOM/100 was 2,452 at takeoff? pg. 4 A) Weight is reduced by 210 pounds and the CG is aft of limits. B) Weight is reduced by 210 pounds and the CG is unaffected. C) Weight is reduced to 2,680 pounds and the CG moves forward. A) Weight is reduced by 210 pounds and the CG is aft of limits. (Refer to Figure 37.) Determine the total distance required to land.OAT StdPressure altitude 10