Quick Links Take a Practice Exam Contribute to the Site Browse the Exams About this Site Privacy Policy Terms & Conditions Site Map 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->amg->J01->J.8.4.8.8.A.1 8488 The purpose of aircraft wing dihedral is to A) increase longitudinal stability. B) increase lift coefficient of the wing. C) increase lateral stability.

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