Fixed-Wing Aircraft MCQs December 5, 2025August 22, 2024 by u930973931_answers 40 min Score: 0 Attempted: 0/40 Subscribe 1. What is the primary function of an aircraftâs ailerons? (A) To control roll (B) To control pitch (C) To control yaw (D) To control thrust 2. Which component of a fixed-wing aircraft controls its pitch? (A) Ailerons (B) Elevators (C) Rudder (D) Flaps 3. What is the purpose of the rudder on a fixed-wing aircraft? (A) To control thrust (B) To control roll (C) To control pitch (D) To control yaw 4. In which axis of flight does the elevator control the aircraft? (A) Longitudinal axis (B) Yaw axis (C) Vertical axis (D) Lateral axis 5. Which aircraft component is primarily responsible for increasing lift during takeoff and landing? (A) Flaps (B) Rudder (C) Ailerons (D) Elevators 6. What does the term âairspeedâ refer to in aviation? (A) The speed of the aircraft relative to the air (B) The speed of the aircraft relative to the ground (C) The speed of the aircraftâs engines (D) The speed of the aircraft in a climb 7. What is the purpose of the wingâs dihedral angle? (A) To control yaw (B) To increase lift (C) To improve stability and reduce roll (D) To manage thrust 8. Which component helps to control the aircraftâs roll? (A) Ailerons (B) Rudder (C) Elevators (D) Flaps 9. What is the primary function of an aircraftâs landing gear? (A) To control pitch (B) To support the aircraft during landing and taxiing (C) To manage engine power (D) To increase lift 10. What does the term âV1â refer to in aviation? (A) The maximum climb speed (B) The stall speed (C) The takeoff decision speed (D) The cruising speed 11. Which instrument provides information about the aircraftâs altitude? (A) Attitude indicator (B) Airspeed indicator (C) Vertical speed indicator (D) Altimeter 12. What is the purpose of the aircraftâs trim system? (A) To increase lift during climb (B) To control engine power (C) To manage the aircraftâs speed (D) To reduce pilot workload by maintaining a desired flight attitude 13. Which of the following is a characteristic of a swept-wing aircraft? (A) Greater maneuverability at low speeds (B) Increased lift at low speeds (C) Enhanced low-speed stability (D) Improved high-speed performance and reduced drag 14. What is the function of the aircraftâs horizontal stabilizer? (A) To manage yaw (B) To control roll (C) To maintain pitch stability (D) To increase lift 15. What is âstall speedâ in aviation? (A) The minimum speed at which an aircraft can maintain controlled flight (B) The maximum speed of the aircraft (C) The speed at which the aircraft takes off (D) The speed at which the aircraft lands 16. Which of the following best describes the âcenter of gravityâ (CG) in an aircraft? (A) The point where the aircraftâs drag is minimized (B) The point where the aircraftâs lift is generated (C) The point where the aircraftâs thrust is produced (D) The point where the aircraftâs weight is balanced 17. What does the term âdragâ refer to in aviation? (A) The thrust produced by the engines (B) The lift generated by the wings (C) The aerodynamic force that opposes the aircraftâs motion through the air (D) The weight of the aircraft 18. What is the purpose of aircraft wing flaps? (A) To reduce engine noise (B) To control roll (C) To manage yaw (D) To increase lift and drag during takeoff and landing 19. In which axis of flight does the aileron control the aircraft? (A) Longitudinal axis (B) Lateral axis (C) Vertical axis (D) Yaw axis 20. What does the term âcruising speedâ refer to in aviation? (A) The speed during takeoff (B) The speed at which an aircraft maintains efficient flight for a prolonged period (C) The speed during climb (D) The speed during landing 21. What is the primary purpose of the aircraftâs vertical stabilizer? (A) To increase lift (B) To control pitch (C) To manage roll (D) To control yaw and provide directional stability 22. What does the term âangle of attackâ refer to? (A) The angle between the aircraftâs longitudinal axis and the horizon (B) The angle between the wing chord line and the relative airflow (C) The angle of the aircraftâs landing gear (D) The angle between the wing and the fuselage 23. What is the function of the aircraftâs throttle? (A) To control the aircraftâs altitude (B) To manage the pitch of the aircraftâs wings (C) To control the engine power and, consequently, the aircraftâs speed (D) To adjust the ailerons 24. What is the term for the aerodynamic force that acts perpendicular to the direction of motion? (A) Drag (B) Lift (C) Thrust (D) Weight 25. Which instrument displays the aircraftâs rate of climb or descent? (A) Airspeed indicator (B) Altimeter (C) Vertical speed indicator (D) Heading indicator 26. What does the term âpayloadâ refer to in aviation? (A) The cargo and passengers carried by the aircraft (B) The total weight of the aircraft including fuel (C) The weight of the aircraftâs engines (D) The weight of the aircraftâs fuel 27. Which aircraft control surface is used to balance the aircraft during flight? (A) Ailerons (B) Elevators (C) Rudder (D) Flaps 28. What is the purpose of a âyawâ control in an aircraft? (A) To control the aircraftâs altitude (B) To adjust the aircraftâs direction left or right (C) To manage the aircraftâs speed (D) To balance the aircraftâs roll 29. What is the effect of increasing the aircraftâs speed on the lift generated by its wings? (A) Lift decreases with speed (B) Lift increases with speed (C) Lift remains constant (D) Lift becomes zero 30. What does âtakeoff distanceâ refer to in aviation? (A) The distance needed to reach cruising altitude (B) The distance traveled during landing (C) The distance required for an aircraft to become airborne (D) The distance covered during a glide 31. What is the purpose of the aircraftâs âspoilersâ? (A) To manage pitch (B) To increase engine thrust (C) To control roll (D) To reduce lift and increase drag 32. What does the term âflap settingâ refer to? (A) The angle at which the wing flaps are deployed (B) The speed of the aircraftâs engines (C) The angle of attack of the wings (D) The aircraftâs cruising altitude 33. Which instrument measures the aircraftâs true airspeed? (A) Vertical speed indicator (B) Altimeter (C) Mach meter (D) Airspeed indicator 34. What is the function of the aircraftâs âautopilotâ system? (A) To control the aircraftâs flight path automatically (B) To manage the aircraftâs fuel consumption (C) To adjust the aircraftâs landing gear (D) To control the aircraftâs thrust 35. What does the term âmach numberâ represent? (A) The ratio of the aircraftâs speed to the speed of sound (B) The aircraftâs cruising altitude (C) The ratio of lift to drag (D) The aircraftâs rate of climb 36. Which control surface adjusts the aircraftâs angle of attack during flight? (A) Elevators (B) Ailerons (C) Rudder (D) Flaps 37. What does the term âstallâ mean in aviation? (A) A condition where the aircraftâs wings lose lift due to excessive angle of attack (B) The engineâs loss of power (C) The aircraftâs uncontrolled descent (D) The aircraftâs rapid acceleration 38. What is the function of the aircraftâs âwingletsâ? (A) To control the aircraftâs yaw (B) To increase lift during takeoff (C) To reduce drag and improve fuel efficiency (D) To manage engine power 39. Which component of the aircraftâs propulsion system is responsible for converting fuel energy into thrust? (A) Propeller (B) Engine (C) Wing (D) Rudder 40. What does the term âtakeoff thrustâ refer to? (A) The maximum power produced by the engine during takeoff (B) The minimum speed required for takeoff (C) The distance needed to take off (D) The altitude reached during takeoff