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Private Pilot Aircraft Performance Weight and Balance Enroute Flight FAA ASA Test 2025/ 2026 Study Guide

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Study resource for Private Pilot FAA/ASA training, 2025/ 2026, covering aircraft performance, weight and balance, and enroute flight planning. Includes key aviation concepts and exam-focused practice to support pilot certification preparation and safe flight operations.

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Private
Private
Private
Pilot,
Pilot,
Pilot,
Aircraft
Aircraft
Aircraft
Performance
Performance
Performance
- -Weight
-Weight
Weightand
and
and
Balance,
Balance,
Balance,
Enroute
Enroute
Enroute
flight,
flight,
flight,
FAA,
FAA,
FAA,
ASA
ASA
ASA
Test
Test
Test
Prep
Prep
Prep
2025
2025
2025
All
All
All
Versions.docxhttps://www.stuvia.com/user/stuviaun
Versions.docxhttps://www.stuvia.com/user/stuviaun
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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. 1

Private
Private
Private
Pilot,
Pilot,
Pilot,
Aircraft
Aircraft
Aircraft
Performance
Performance
Performance
- -Weight
-Weight
Weightand
and
and
Balance,
Balance,
Balance,
Enroute
Enroute
Enroute
flight,
flight,
flight,
FAA,
FAA,
FAA,
ASA
ASA
ASA
Test
Test
Test
Prep
Prep
Prep
2025
2025
2025
All
All
All
Versions.docxhttps://www.stuvia.com/user/stuviaun
Versions.docxhttps://www.stuvia.com/user/stuviaun
Versions.docxhttps://www.stuvia.com/user/stuviaun

,Private
Private
Private
Pilot,
Pilot,
Pilot,
Aircraft
Aircraft
Aircraft
Performance
Performance
Performance
- -Weight
-Weight
Weightand
and
and
Balance,
Balance,
Balance,
Enroute
Enroute
Enroute
flight,
flight,
flight,
FAA,
FAA,
FAA,
ASA
ASA
ASA
Test
Test
Test
Prep
Prep
Prep
2025
2025
2025
All
All
All
Versions.docxhttps://www.stuvia.com/user/stuviaun
Versions.docxhttps://www.stuvia.com/user/stuviaun
Versions.docxhttps://www.stuvia.com/user/stuviaun




(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. 2

Private
Private
Private
Pilot,
Pilot,
Pilot,
Aircraft
Aircraft
Aircraft
Performance
Performance
Performance
- -Weight
-Weight
Weightand
and
and
Balance,
Balance,
Balance,
Enroute
Enroute
Enroute
flight,
flight,
flight,
FAA,
FAA,
FAA,
ASA
ASA
ASA
Test
Test
Test
Prep
Prep
Prep
2025
2025
2025
All
All
All
Versions.docxhttps://www.stuvia.com/user/stuviaun
Versions.docxhttps://www.stuvia.com/user/stuviaun
Versions.docxhttps://www.stuvia.com/user/stuviaun

,Private
Private
Private
Pilot,
Pilot,
Pilot,
Aircraft
Aircraft
Aircraft
Performance
Performance
Performance
- -Weight
-Weight
Weightand
and
and
Balance,
Balance,
Balance,
Enroute
Enroute
Enroute
flight,
flight,
flight,
FAA,
FAA,
FAA,
ASA
ASA
ASA
Test
Test
Test
Prep
Prep
Prep
2025
2025
2025
All
All
All
Versions.docxhttps://www.stuvia.com/user/stuviaun
Versions.docxhttps://www.stuvia.com/user/stuviaun
Versions.docxhttps://www.stuvia.com/user/stuviaun




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

Private
Private
Private
Pilot,
Pilot,
Pilot,
Aircraft
Aircraft
Aircraft
Performance
Performance
Performance
- -Weight
-Weight
Weightand
and
and
Balance,
Balance,
Balance,
Enroute
Enroute
Enroute
flight,
flight,
flight,
FAA,
FAA,
FAA,
ASA
ASA
ASA
Test
Test
Test
Prep
Prep
Prep
2025
2025
2025
All
All
All
Versions.docxhttps://www.stuvia.com/user/stuviaun
Versions.docxhttps://www.stuvia.com/user/stuviaun
Versions.docxhttps://www.stuvia.com/user/stuviaun

, Private
Private
Private
Pilot,
Pilot,
Pilot,
Aircraft
Aircraft
Aircraft
Performance
Performance
Performance
- -Weight
-Weight
Weightand
and
and
Balance,
Balance,
Balance,
Enroute
Enroute
Enroute
flight,
flight,
flight,
FAA,
FAA,
FAA,
ASA
ASA
ASA
Test
Test
Test
Prep
Prep
Prep
2025
2025
2025
All
All
All
Versions.docxhttps://www.stuvia.com/user/stuviaun
Versions.docxhttps://www.stuvia.com/user/stuviaun
Versions.docxhttps://www.stuvia.com/user/stuviaun




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 10,000 ftWeight 2,400 lbWind component
CalmObstacle 50 ft


A) 750 feet.
B) 1,925 feet.
C) 1,450 feet.

B) 1,925 feet.

(Refer to Figure 38.) Determine the approximate landing ground roll
distance.Pressure altitude 5,000 ftHeadwind CalmTemperature 101°F


A) 495 feet.
B) 545 feet.
C) 445 feet.

B) 545 feet.

(Refer to Figure 8.) What is the effect of a temperature decrease and a
pressure altitude increase on the density altitude from 90°F and
1,250 feet pressure altitude to 55°F and 1,750 feet pressure altitude?


A) 1,700-foot increase.
B) 1,300-foot decrease.
C) 1,700-foot decrease.



pg. 4

Private
Private
Private
Pilot,
Pilot,
Pilot,
Aircraft
Aircraft
Aircraft
Performance
Performance
Performance
- -Weight
-Weight
Weightand
and
and
Balance,
Balance,
Balance,
Enroute
Enroute
Enroute
flight,
flight,
flight,
FAA,
FAA,
FAA,
ASA
ASA
ASA
Test
Test
Test
Prep
Prep
Prep
2025
2025
2025
All
All
All
Versions.docxhttps://www.stuvia.com/user/stuviaun
Versions.docxhttps://www.stuvia.com/user/stuviaun
Versions.docxhttps://www.stuvia.com/user/stuviaun

Document information

Uploaded on
June 30, 2026
Number of pages
145
Written in
2025/2026
Type
Exam (elaborations)
Contains
Questions & answers
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