FAA Repairman Certificate – Light-Sport Aircraft (LSA) Inspection – Gyroplane Exam Practice Test Questions And Correct Answers (Verified Answers) Plus Rationales 2026 Q&A | Instant Download Pdf
- What is the primary source of lift for a gyroplane?
- Propeller thrust
- Unpowered rotor blades
- Fixed wings
- Engine exhaust gases
Rationale: In a gyroplane, lift is generated by unpowered rotor
blades that autorotate due to the aircraft's forward motion.
- What term describes the rotation of the rotor blades caused by air
- Propulsion
- Autorotation
- Induced drag 1 / 4
moving upward through the rotor system?
- Gyroscopic precession
Rationale: Autorotation occurs when upward airflow through the
rotor system causes the blades to spin freely, generating lift.
- Which component provides forward thrust in a gyroplane?
- The propeller
- The rotor system
- The tail fin
- The cyclic pitch control
Rationale: In a gyroplane, an engine-driven propeller provides
forward thrust, while the rotor provides lift.
4. During autorotation, the rotor blades are driven by:
- The engine
- The cyclic control
- The upward flow of air through the rotor disc
- The rudder
Rationale: Autorotation occurs because the air moving upward
through the rotor disc drives the rotor blades.
- Which type of airframe is most commonly used in light-sport
- Wooden
- Steel monocoque
- Tubular aluminum or steel frame
- Composite sandwich shell 2 / 4
gyroplanes?
Rationale: Most LSA gyroplanes use lightweight tubular metal
frames for strength and simplicity.
6. The thrust line in a gyroplane should ideally:
- Pass below the center of gravity
- Pass above the center of gravity
- Pass close to the center of gravity
- Be perpendicular to the center of gravity
Rationale: A thrust line near the center of gravity ensures stability
and reduces pitch oscillations.
- What is the function of the pre-rotator in a gyroplane?
- Provides lift during flight
- Spins up the rotor before takeoff
- Controls yaw
- Acts as a brake for the rotor
Rationale: The pre-rotator is used to bring the rotor blades up to
speed before takeoff to shorten takeoff distance.
- What happens if the engine fails in a gyroplane during flight?
- The aircraft stalls
- The rotor stops spinning
- The aircraft continues to autorotate and can glide safely
- The propeller provides lift
Rationale: Gyroplanes can glide safely in autorotation even if the
engine fails, as the rotor continues spinning. 3 / 4
9. The cyclic control in a gyroplane changes:
- Engine power
- The pitch angle of the rotor blades cyclically
- The tail rudder position
- The propeller thrust
Rationale: The cyclic control tilts the rotor disc by changing blade
pitch cyclically, controlling direction.
10. The rudder in a gyroplane is primarily used to:
- Change altitude
- Control yaw
- Control roll
- Adjust lift
Rationale: The rudder controls yaw, or left-right movement, by
changing airflow over the vertical stabilizer.
- What determines the rotor blade’s lift at a given airspeed?
- Propeller RPM
- Angle of attack and airspeed
- Rotor hub angle
- Weight of the gyroplane
Rationale: Lift depends on airspeed and the rotor blade’s angle of
attack.
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