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by: Teri Sims

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# FAA Exam Prep Chapter One Pt. 1 AVED 1114

Marketplace > Oklahoma State University > Aerospace Engineering > AVED 1114 > FAA Exam Prep Chapter One Pt 1
Teri Sims
OK State
GPA 3.4

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25 questions from Chapter One test pool questions with answer sheet.
COURSE
Theory of Flight
PROF.
Tyler Muse
TYPE
Class Notes
PAGES
8
WORDS
CONCEPTS
Theory of Flight, FAA, Private Pilot, OSU, Oklahoma State University, Answer Sheet, questions, test prep, AVED 1222
KARMA
25 ?

1 review
Elaina Gonzalez

## Popular in Aerospace Engineering

This 8 page Class Notes was uploaded by Teri Sims on Wednesday March 9, 2016. The Class Notes belongs to AVED 1114 at Oklahoma State University taught by Tyler Muse in Winter 2016. Since its upload, it has received 48 views. For similar materials see Theory of Flight in Aerospace Engineering at Oklahoma State University.

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Date Created: 03/09/16
Wednesday, March 9, 2016 Chapter One FAA Test Questions Pt. 1 w/ Answer Sheet Theory of Flight 1. What is one purpose of wing ﬂaps? A. To enable the pilot to make steeper approaches to a landing without increasing the airspeed. B. To relieve the pilot of maintaining continuous pressure on the controls. C. To decrease wing area to vary the lift. 2. One of the main functions of ﬂaps during approach and landing is to _____ A. Decrease the angle of descent without increasing the airspeed. B. Permit a touchdown at a higher indicated airspeed. C. Increase the angle of descent without increasing the airspeed. 3. What is the purpose of the rudder on an airplane? A. To control yaw. B. To control overbanking tendency. C. To control roll. 4. Which is not a primary ﬂight control? A. Flaps. B. Stabilator. C. Ailerons. 1 Wednesday, March 9, 2016 5. The elevator controls movement around which axis? A. Longitudinal. B. Lateral. C. Vertical. 6. Which statement is true concerning primary ﬂight controls? A. The effectiveness of each control surface increases with speed because there is more ﬂow over them. Only when all three primary ﬂight controls move in sequence do the airﬂow B. and pressure distribution change over and around the airfoil. C. Primary ﬂight controls include ailerons, rudder, elevator, and trim systems. 7. Which of the following is true concerning ﬂaps? A. Flaps are attached to the leading edge of the wing and used to increase wing lift. B. Flaps allow an increase in the angle of descent without increasing airspeed. C. Flaps are high drag devices deployed from the wings to reduce lift. 8. Which device is a secondary ﬂight control? A. Spoilers. B. Ailerons. C. Stabilators. 2 Wednesday, March 9, 2016 9. Trim systems are designed to do what? A. They relieve the pilot of the need to maintain constant back pressure on the ﬂight controls. B. They are used during approach and landing to increase wing lift. C. They move in the opposite direction from one another to control roll. 10. The four forces acting on an airplane in ﬂight are _____ A. Lift, weight, thrust, and drag. Lift, weight, gravity, and thrust. B. C. Lift, gravity, power, and friction. 11. When are the four forces that act on an airplane in equilibrium? A. During unaccelerated level ﬂight. B. When the aircraft is accelerating. C. When the aircraft is at rest on the ground. 12. What is the relationship of lift, drag, thrust, and weight when the airplane is in straight-and-level ﬂight? Lift equals weight and thrust equals drag. A. B. Lift, weight, and drag equal thrust. C. Lift and weight equal thrust and drag. 3 Wednesday, March 9, 2016 13. Which statement relates to Bernoulli’s principle? A. For every action, there is an equal and opposite reaction. B. An additional upward force is generated as the lower surface of the wing deﬂects air downward. C. Air traveling faster over the curved upper surface of an airfoil causes lower pressure on the top surface. 14. The term “angle of attack” is deﬁned as the angle between the ____ A. Chord line of the wing and the relative wind. B. Airplane’s longitudinal axis and that of the air striking the airfoil. C. Airplane’s center line and the relative wind. 15. The term “angle of attack” is deﬁned as the angle ____ A. Between the wing chord lone and the relative wind. B. Between the airplane’s climb angle and the horizon. C. Formed by the longitudinal axis of the airplane and the chord line of the wing. 16. Angle of attack is deﬁned as the angle between the chord line of an airfoil and the ____ A. Direction of the relative wind. B. Pitch angle of an airfoil. C. Rotor plane of rotation. 4 Wednesday, March 9, 2016 17. (Refer to image above) The acute angle A is the angle of _____ A. Incidence. B. Attack. Dihedral. C. 18. The angle between the chord line of an airfoil and the relative wind is known as the angle of ____ A. Lift. B. Attack. C. Incidence. 5 Wednesday, March 9, 2016 19. The angle of attack at which an airplane wing stalls will ______ A. Increase if the CG is moved forward. B. Change with an increase in gross weight. C. Remain the same regardless of gross weight. 20. As altitude increase, the indicated airspeed at which a given airplane stalls in a particular conﬁguration will ______ A. Decrease as true airspeed decreases. Decrease as true airspeed increases. B. C. Remain the same regardless of altitude. 21. In what ﬂight condition must an aircraft be placed in order to spin? A. Partially stalled with one wing low. B. In a steep diving spiral. C. Stalled. 22. During a spin to the left, which wing(s) is/are stalled? A. Both wings are stalled. B. Neither wing is stalled. C. Only the left wing is stalled. 23. How will frost on the wings of an airplane affect takeoff performance? A. Frost will disrupt the smooth ﬂow of air over the wing, adversely affecting its lifting capability. B. Frost will change the camber of the wing, increasing its lifting capability. 6 Wednesday, March 9, 2016 C. Frost will cause the airplane to become airborne with a higher angle of attack, decreasing the stall speed. 24. Why is frost considered hazardous to ﬂight? A. Frost changes the basic aerodynamic shape of the airfoils, thereby increasing lift. B. Frost slows the airﬂow over the airfoils, thereby increasing control effectiveness. C. Frost spoils the smooth ﬂow of air over the wings, thereby decreasing lifting capability. 25. How does frost affect the lifting surfaces of an airplane on takeoff? A. Frost may prevent the airplane from becoming airborne at normal takeoff speed. B. Frost will change the camber of the wing, increasing lift during takeoff. C. Frost may cause the airplane to become airborne with a lower angle of attack at a lower indicated airspeed.  7 Wednesday, March 9, 2016 Answers 1. A 2. C 3. A 4. A 5. B 6. A 7. B 8. A 9. A 10.A 11. A 12. A 13. C A 14. 15.A 16. A 17. B 18. B 19.C 20.C 21. C 22. A 23. A 24.C 25.A 8

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