Module 12 Practice Questions - EASA Part-66 Module 12 - Helicopter Aerodynamics, Structures And Systems Exam

Retreating blade stall is the primary aerodynamic limitation that establishes which helicopter performance boundary?

Maximum hover ceiling out of ground effect Never-exceed forward speed (VNE) Maximum gross weight Minimum autorotation rotor RPM

Correct Answer:

Never-exceed forward speed (VNE)

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