PRIVATE HELICOPTER TEST PREP ACTUAL EXAM PAPER
2026 QUESTIONS WITH ANSWERS GRADED A+
● Rotorcraft. Answer: Aircraft using rotating wings for lift
● Helicopter. Answer: Rotorcraft with powered main rotor
● Main Rotor. Answer: Large rotating blades providing lift
● Tail Rotor. Answer: Small rotor counteracting torque
● Rotor System. Answer: Complete assembly of rotating components
● Rotor Blade. Answer: Airfoil-shaped rotating wing
● Rotor Hub. Answer: Central component connecting blades
● Rotor Mast. Answer: Vertical shaft supporting rotor system
● Rotor Head. Answer: Assembly at top of mast
● Fully Articulated Rotor. Answer: Blades can flap, lead-lag, and feather
● Semi-Rigid Rotor. Answer: Blades flap and feather only
● Rigid Rotor. Answer: Blades only feather
● Flapping. Answer: Blade up and down movement
● Lead-Lag. Answer: Blade forward and backward movement
● Feathering. Answer: Blade pitch angle change
● Collective Pitch Control. Answer: Changes pitch of all blades equally
● Cyclic Pitch Control. Answer: Changes pitch during rotation cycle
● Swashplate. Answer: Mechanism translating control inputs to rotor
● Stationary Swashplate. Answer: Non-rotating lower portion
2026 QUESTIONS WITH ANSWERS GRADED A+
● Rotorcraft. Answer: Aircraft using rotating wings for lift
● Helicopter. Answer: Rotorcraft with powered main rotor
● Main Rotor. Answer: Large rotating blades providing lift
● Tail Rotor. Answer: Small rotor counteracting torque
● Rotor System. Answer: Complete assembly of rotating components
● Rotor Blade. Answer: Airfoil-shaped rotating wing
● Rotor Hub. Answer: Central component connecting blades
● Rotor Mast. Answer: Vertical shaft supporting rotor system
● Rotor Head. Answer: Assembly at top of mast
● Fully Articulated Rotor. Answer: Blades can flap, lead-lag, and feather
● Semi-Rigid Rotor. Answer: Blades flap and feather only
● Rigid Rotor. Answer: Blades only feather
● Flapping. Answer: Blade up and down movement
● Lead-Lag. Answer: Blade forward and backward movement
● Feathering. Answer: Blade pitch angle change
● Collective Pitch Control. Answer: Changes pitch of all blades equally
● Cyclic Pitch Control. Answer: Changes pitch during rotation cycle
● Swashplate. Answer: Mechanism translating control inputs to rotor
● Stationary Swashplate. Answer: Non-rotating lower portion