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
,Private Pilot, Aircraft PePrivate Pilot, Aircrafformance - Weight and Bal t Prep 2025 All Versions 2026-03-10
• (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
1,000nautical 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. 1
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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?
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.
pg. 3
Page 3 of 145 Private Pilot, Aircraft Performance - Weight and Balance, Enroute flight, FAA, ASA Test Prep 2025 All Versions.docxPage 3
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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
,Private Pilot, Aircraft PePrivate Pilot, Aircrafformance - Weight and Bal t Prep 2025 All Versions 2026-03-10
• (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
1,000nautical 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. 1
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pg. 2
Page 2 of 145 Private Pilot, Aircraft Performance - Weight and Balance, Enroute flight, FAA, ASA Test Prep 2025 All Versions.docxPage 2
, \
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?
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.
pg. 3
Page 3 of 145 Private Pilot, Aircraft Performance - Weight and Balance, Enroute flight, FAA, ASA Test Prep 2025 All Versions.docxPage 3
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