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->sp_inst->H302->Z.0.0.3.6.A.1 0036 The purpose of aircraft wing dihedral angle is to * A) increase lateral stability. B) increase longitudinal stability. C) increase lift coefficient of the wing.

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