Module 17 Propeller Practice Questions - UK CAA Part-66 AME Module 17 - Propeller Exam

To ensure the root section produces maximum thrust while the tip section produces zero drag To allow the centrifugal force to pull the blade into coarse pitch automatically at high engine RPM To equalize the mechanical bending stress caused by engine exhaust gas impingement To maintain a relatively constant angle of attack along the blade despite increasing rotational linear velocity toward the tip