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AVIA 455 - Aircraft Performance Final Exam Chapter 1,2,3, 7, 8, 9, 10, 14-19 Newest 2026 Questions and Correct Detailed Answers Already Graded A+ AVIA 455 - Aircraft Performance Final Exam Chapter 1,2,3, 7, 8, 9, 10, 14-19 Newest 2026 Questions and C

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AVIA 455 - Aircraft Performance Final Exam Chapter 1,2,3, 7, 8, 9, 10, 14-19 Newest 2026 Questions and Correct Detailed Answers Already Graded A+

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AVIA 455 - Aircraft Performance Final Exam
Chapter 1,2,3, 7, 8, 9, 10, 14-19 Newest 2026
Questions and Correct Detailed Answers Already
Graded A+

2.13 With increasing altitude, the power required curve moves:

(a) up and to the right

(b) down and to the right

(c) up and to the left

(d) down and to the left - CORRECT ANSWER-(a) up and to the right



2.14 For a piston engine airplane at a constant mass, AOA, and configuration, an
increase of altitude will require:

(a) increased power but the same TAS

(b) increased power and TAS

(c) lower power but increased TAS

(d) the same power but an increased TAS - CORRECT ANSWER-(b) increased
power and TAS



2.15 For a piston engine airplane at a constant altitude, AOA, and configuration,
an increased mass will require:

,(a) more power and speed

(b) more power but the same speed

(c) the same power but more speed

(d) more power but less speed - CORRECT ANSWER-(a) more power and speed



2.16 The region of reversed command means:

(a) a lower airspeed requires more thrust

(b) the thrust required is independent of airspeed

(c) a thrust reduction results in acceleration

(d) a momentary increase of airspeed has no influence on the thrust required -
CORRECT ANSWER-(a) a lower airspeed requires more thrust




2.17 At speeds below Vimd:

(a) the airplane can only be controlled in level flight

(b) a lower speed requires more thrust

(c) a higher speed requires more thrust

(d) the airplane cannot be controlled manually - CORRECT ANSWER-(b) a lower
speed requires more thrust



2.18 In which of the following conditions is thrust equal to drag?

,(a) in a descent at constant IAS

(b) in level flight at constant IAS

(c) in level flight accelerating

(d) in a climb at constant IAS - CORRECT ANSWER-(b) in level flight at constant
IAS



2.19 How does Cl vary with altitude?

(a) it increases with increased altitude

(b) it decreases with increased altitude

(c) it remains constant with increased altitude

(d) it decreases with decreased altitude - CORRECT ANSWER-(c) it remains
constant with increased altitude



2.20 Maximum horizontal speed occurs when:

(a) thrust = minimum drag

(b) thrust does not increase with increasing speed

(c) maximum thrust = total drag

(d) thrust = maximum drag - CORRECT ANSWER-(c) maximum thrust = total
drag

, 2.21 The maximum IAS for a piston airplane in level flight is attained at the:

(a) lowest practical altitude

(b) optimum cruise altitude

(c) service ceiling

(d) practical ceiling - CORRECT ANSWER-(a) lowest practical altitude



1.1 A jet aeroplane flying for max endurance has a mass decrease, because of fuel
used, by 5% from its original mass, the change to the fuel consumption per hour
from that at the original mass is:

(a) increase by 5%

(b) decrease by 5%

(c) increase by 10%

(d) decrease by 10% - CORRECT ANSWER-(b) decrease by 5%



1.6 At a constant thrust setting and altitude the fuel flow of a jet engine:

(a) decreases with decreasing OAT

(b) increases slightly with increasing speed

(c) is independent of speed

(d) decreases slightly with increasing speed - CORRECT ANSWER-(b) increases
slightly with increasing speed

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