BUAD 341 FINAL EXAM PAPER 1 2026
QUESTIONS AND SOLUTIONS 100% CORRECT
◉ 8228.
Other than the manufacturer maintenance manual what other
document could be used to determine the primary flight control
surface deflection for an imported aircraft that is reassembled after
shipment?
A— Aircraft Type Certificate Data Sheet
B— Import manual for the aircraft
C— The certificate of airworthiness issued by the importing country.
Answer: Aircraft type certificate data sheet
◉ 8229. If a pilot reports that an airplane flies left wing heavy, this
condition may be corrected by?
A. increasing the angle of incidence of the left wing, or decreasing
the angle of incidence of the right wing or both
B. Increasing the dihedral angle of the left wing or decreasing the
dihedral angle of the right wing, or both
,C. adjusting the dihedral angle of the left wing so that differential
pressure between the upper and lower wing surfaces is increased.
Answer: increasing the angle of incidence of the left wing, or
decreasing the angle of incidence of the right wing or both
◉ 8230 If the vertical fin of a single engine, propeller-driven
airplane is rigged properly, it will generally be parallel to
A. The longitudinal axis but not the vertical axis
B. The vertical axis but not the longitudinal axis
C. Both the longitudinal and vertical axes. Answer: The vertical axis
but not the longitudinal axis
◉ (8231)-An airplane which has good longitudinal stability should
have a minimum tendency to?
a. roll
b. pitch
c. yaw. Answer: pitch
, ◉ (8232)-As the angle of attack of an airfoil increases, the center of
pressure will?
a. move toward the trailing edge
b. remain stationary because both lift and drag components increase
proportionally to increased angle of attack.
c. move toward the leading edge. Answer: move toward the leading
edge
◉ (8233)-The angle of incidence is that acute angle formed by?
a. the angular difference between the setting of the main airfoil and
the auxiliary airfoil (horizontal stabilizer) in reference to the
longitudinal axis of the aircraft.
b. a line parallel to the wing chord and a line parallel to the
longitudinal axis of the aircraft
c. a line parallel to the wing from root to tip and a line parallel to the
lateral axis of the aircraft.. Answer: a line parallel to the wing chord
and a line parallel to the longitudinal axis of the aircraft
◉ (8234)-An airplane's center of lift is usually located aft of its
center of gravity?
QUESTIONS AND SOLUTIONS 100% CORRECT
◉ 8228.
Other than the manufacturer maintenance manual what other
document could be used to determine the primary flight control
surface deflection for an imported aircraft that is reassembled after
shipment?
A— Aircraft Type Certificate Data Sheet
B— Import manual for the aircraft
C— The certificate of airworthiness issued by the importing country.
Answer: Aircraft type certificate data sheet
◉ 8229. If a pilot reports that an airplane flies left wing heavy, this
condition may be corrected by?
A. increasing the angle of incidence of the left wing, or decreasing
the angle of incidence of the right wing or both
B. Increasing the dihedral angle of the left wing or decreasing the
dihedral angle of the right wing, or both
,C. adjusting the dihedral angle of the left wing so that differential
pressure between the upper and lower wing surfaces is increased.
Answer: increasing the angle of incidence of the left wing, or
decreasing the angle of incidence of the right wing or both
◉ 8230 If the vertical fin of a single engine, propeller-driven
airplane is rigged properly, it will generally be parallel to
A. The longitudinal axis but not the vertical axis
B. The vertical axis but not the longitudinal axis
C. Both the longitudinal and vertical axes. Answer: The vertical axis
but not the longitudinal axis
◉ (8231)-An airplane which has good longitudinal stability should
have a minimum tendency to?
a. roll
b. pitch
c. yaw. Answer: pitch
, ◉ (8232)-As the angle of attack of an airfoil increases, the center of
pressure will?
a. move toward the trailing edge
b. remain stationary because both lift and drag components increase
proportionally to increased angle of attack.
c. move toward the leading edge. Answer: move toward the leading
edge
◉ (8233)-The angle of incidence is that acute angle formed by?
a. the angular difference between the setting of the main airfoil and
the auxiliary airfoil (horizontal stabilizer) in reference to the
longitudinal axis of the aircraft.
b. a line parallel to the wing chord and a line parallel to the
longitudinal axis of the aircraft
c. a line parallel to the wing from root to tip and a line parallel to the
lateral axis of the aircraft.. Answer: a line parallel to the wing chord
and a line parallel to the longitudinal axis of the aircraft
◉ (8234)-An airplane's center of lift is usually located aft of its
center of gravity?
