Complete
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Private Pilot - Aircraft
Performance/Aircraft Performance
(Refer to figure 8.) What is the effect of a temperature increase from 35 to 50 °F
on the density altitude if the pressure altitude remains at 3,000 feet MSL?
a) 1,300-foot increase.
b) 1,000-foot increase.
c) 1,100-foot decrease.
b) 1,000-foot increase.
(Refer to figure 38.) Determine the approximate landing ground roll distance.
Pressure altitude - 5,000 ft
Headwind - Calm
Temperature- 101 F
a) 445 feet.
b) 545 feet.
c) 495 feet.
b) 545 feet.
pg. 1
2026-2027: Private Pilot - Aircraft Performance-
Private
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Performance
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1 ofPerformance-
21 Aircraft Performance.pdf- (exam preparation).
,Complete
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(Refer to figure 38.) Determine the approximate landing ground roll distance.
Pressure altitude-Sea level
Headwind-4 kts
Temperature-Std
a) 490 feet.
b) 356 feet.
c) 401 feet.
c) 401 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 decrease.
b) 1,300-foot decrease.
c) 1,700-foot increase.
a) 1,700-foot decrease.
pg. 2
2026-2027: Private Pilot - Aircraft Performance-
Private
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Performance
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2 ofPerformance-
21 Aircraft Performance.pdf- (exam preparation).
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(Refer to Figure 40.) What is the approximate ground roll distance necessary for
takeoff under the following conditions? OAT - 90°F, Pressure altitude - 4,000 ft,
Takeoff weight - 2,600 lb, Headwind component - 20 kts
a) 600 feet.
b) 800 feet.
c) 1,000 feet.
b) 800 feet.
Ground effect is most likely to result in which problem?
a) Settling to the surface abruptly during landing.
b) Becoming airborne before reaching recommended takeoff speed.
c) Inability to get airborne even though airspeed is sufficient for normal takeoff
needs.
b) Becoming airborne before reaching recommended takeoff speed.
(Refer to figure 38.) Determine the approximate landing ground roll distance.
Pressure altitude-1,250 ft
pg. 3
2026-2027: Private Pilot - Aircraft Performance-
Private
Aircraft
Pilot -Page
Performance
Aircraft
3 ofPerformance-
21 Aircraft Performance.pdf- (exam preparation).
Private Pilot
review
- Aircraft
with chapter-based
Performance- Aircraft
questionsPerformance.pdf=
and accurate
Page answers.
1Includes
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accurately Private
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andPerformance-
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Aircraft Perfo
Private Pilot - Aircraft
Performance/Aircraft Performance
(Refer to figure 8.) What is the effect of a temperature increase from 35 to 50 °F
on the density altitude if the pressure altitude remains at 3,000 feet MSL?
a) 1,300-foot increase.
b) 1,000-foot increase.
c) 1,100-foot decrease.
b) 1,000-foot increase.
(Refer to figure 38.) Determine the approximate landing ground roll distance.
Pressure altitude - 5,000 ft
Headwind - Calm
Temperature- 101 F
a) 445 feet.
b) 545 feet.
c) 495 feet.
b) 545 feet.
pg. 1
2026-2027: Private Pilot - Aircraft Performance-
Private
Aircraft
Pilot -Page
Performance
Aircraft
1 ofPerformance-
21 Aircraft Performance.pdf- (exam preparation).
,Complete
Private Pilot
review
- Aircraft
with chapter-based
Performance- Aircraft
questionsPerformance.pdf=
and accurate
Page answers.
2Includes
of 21 2026//2027
accurately Private
reviewedPilot
questions
- Aircraft
andPerformance-
verified answers.
Aircraft Perfo
(Refer to figure 38.) Determine the approximate landing ground roll distance.
Pressure altitude-Sea level
Headwind-4 kts
Temperature-Std
a) 490 feet.
b) 356 feet.
c) 401 feet.
c) 401 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 decrease.
b) 1,300-foot decrease.
c) 1,700-foot increase.
a) 1,700-foot decrease.
pg. 2
2026-2027: Private Pilot - Aircraft Performance-
Private
Aircraft
Pilot -Page
Performance
Aircraft
2 ofPerformance-
21 Aircraft Performance.pdf- (exam preparation).
, Complete
Private Pilot
review
- Aircraft
with chapter-based
Performance- Aircraft
questionsPerformance.pdf=
and accurate
Page answers.
3Includes
of 21 2026//2027
accurately Private
reviewedPilot
questions
- Aircraft
andPerformance-
verified answers.
Aircraft Perfo
(Refer to Figure 40.) What is the approximate ground roll distance necessary for
takeoff under the following conditions? OAT - 90°F, Pressure altitude - 4,000 ft,
Takeoff weight - 2,600 lb, Headwind component - 20 kts
a) 600 feet.
b) 800 feet.
c) 1,000 feet.
b) 800 feet.
Ground effect is most likely to result in which problem?
a) Settling to the surface abruptly during landing.
b) Becoming airborne before reaching recommended takeoff speed.
c) Inability to get airborne even though airspeed is sufficient for normal takeoff
needs.
b) Becoming airborne before reaching recommended takeoff speed.
(Refer to figure 38.) Determine the approximate landing ground roll distance.
Pressure altitude-1,250 ft
pg. 3
2026-2027: Private Pilot - Aircraft Performance-
Private
Aircraft
Pilot -Page
Performance
Aircraft
3 ofPerformance-
21 Aircraft Performance.pdf- (exam preparation).
