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FREE AND STUDY GAMES ABOUT 6 ASSEMBLY AND RIGGI
EXAM QUESTIONS
Actual Qs and Ans Expert-Verified Explanation
This Exam contains:
-Guarantee passing score -82 Questions and Answers -format set of multiple-choice -Expert-Verified Explanation
Question 1: Where is the buttock line or buttline of an aircraft?
Answer:
A width measurement left or right of, and parallel to, the vertical centerline.Question 2: A tension regulator in the flight control cable system of a large all-metal aircraft is used primarily to
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retain a set tension.Question 3: During inspection of the flight control system of an airplane equipped with differential-type aileron control, side-to-side movement of the control stick will cause
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each aileron to have a greater up travel (from the streamlined position) than down travel.
Question 4: The universal propeller protractor can be used to measure
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degrees of flap travel.
Question 5: What is the purpose of the free-wheeling unit in a helicopter drive system?
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It disengages the engine from the main rotor when engine RPM is less than rotor RPM.Question 6: When a fiber or nylon insert-type self-locking nut can be threaded on a bolt or stud through the insert with only the fingers, it should be
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rejected.
Question 7: When the lift of an airfoil increases, the drag will
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also increase.Question 8: The acute angle formed by the chord line of a wing and the relative wind is known as the
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angle of attack.Question 9: Buffeting is the intermittent application of forces to a part of an airplane. It is caused by
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an unsteady flow from turbulence.Question 10: Excessive wear on both of the sides of a control cable pulley groove is evidence of
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pulley misalignment.
Question 11: The chord of a wing is measured from
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leading edge to trailing edge.Question 12: Proper wing twist in a sheet metal constructed wing can usually be checked by utilizing a
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bubble level and special fixtures described by the manufacturer.
Question 13: An airplane which has good longitudinal stability should have a minimum tendency to
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pitch.Question 14: In rotorcraft external-loading, the ideal location of the cargo release is where the line of action passes
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through the center of gravity at all times.Question 15: When inspecting a control cable turnbuckle for proper installation, determine that
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the safety wire ends are wrapped a minimum of four turns around the terminal end shanks.Question 16: A universal propeller protractor used to measure the degrees of aileron travel should be zeroed
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with the aileron in the NEUTRAL position.Question 17: As the angle of attack of an airfoil increases, the center of pressure will
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move toward the leading edge.Question 18: An airplane's center of lift is usually located aft of its center of gravity
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so that the airplane will have a nose-heavy tendency.
Question 19: The vertical flight of a helicopter is controlled by
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collective pitch changes.Question 20: Movement of an airplane along its lateral axis (roll) is also movement
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around or about the longitudinal axis controlled by the ailerons.
Question 21: If the right wing of a monoplane is improperly rigged to a greater angle of incidence than designated in the manufacturer's specifications, it will cause the
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airplane to be off balance both laterally and directionally.Question 22: An airplane is controlled directionally about its vertical axis by the
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rudder.Question 23: If a pilot reports that an airplane flies left wing heavy, this condition may be corrected by
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increasing the angle of incidence of the left wing, or decreasing the angle of incidence of the right wing, or both.Question 24: After repairing or re-covering a rudder, the surface should be rebalanced
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to manufacturer's specifications.
Question 25: The purpose of the vertical fin is to provide
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directional stability.Question 26: When installing a castle nut, start alignment with the cotter pin hole at the
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minimum recommended torque plus friction drag torque.Question 27: Where does the breakage of control cable wires occur most frequently?
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Breakage usually occurs where cables pass over pulleys and through fairleads.Question 28: Movement of the cockpit control toward the nosedown position during a ground operational check of the elevator trim tab system will cause the trailing edge of the trim tab to move in which direction?
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Upward regardless of elevator position.