CAA NZ CPL Theory - Principles Of Flight & Aircraft Performance Practice Questions - CAA NZ CPL Theory - Principles Of Flight & Aircraft Performance (New Zealand) Exam

Increases wing camber and max lift coefficient (CL max), allowing a lower landing speed and steeper descent path Decreases total drag while keeping lift constant to extend glide range Shifts the center of pressure rearward to decrease elevator control load Increases critical angle of attack to prevent premature stall