Quick Links Take a Practice Exam Contribute to the Site About this Site Privacy Policy Terms & Conditions New User Log In Examine My Cookies Contact WebMaster   Exams4Pilots Forum Forum Home - Latest News - Testimonials - Tips & Tricks - Stuck Mike - Bug Reports - Feature Request	SiteMap You are here: home->pvt_plt->H703->2.3.3.2.8.A.1 3328 The purpose of the lead-lag (drag) hinge in a three-bladed, fully articulated helicopter rotor system is to compensate for A) coning. B) geometric unbalance. * C) Coriolis effect.

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