Flying Magazine

MAY 10, 2024

gross weight is reduced. 2: A stall occurs when the smooth airflow over the unmanned airplane’s wing is disrupted and the lift degenerates rapidly. the maximum allowable operating weight. CG is shifted rearward to the aft CG limit. airplane is subjected to maneuvers other than straight-and-level flight. visual observer C.

Weight-Shift-Control 114

Weight-Shift-Control Air Traffic Control Aeronautical Decision-Making Density Altitude 114

Pilot Institute

MAY 4, 2024

Aircraft Weight and Limitations An aircraft’s weight affects inertia and stopping distance. The POH lists landing distances for specific gross weights. Smaller aircraft may only have short field landing distances for maximum gross weight. x V SO (or POH recommendation) by around 500 feet AGL.

Weight-Shift-Control 52

Weight-Shift-Control Runway Approach Descent 52

Pilot Institute

SEPTEMBER 18, 2024

A smaller bank angle will result in more lift, while an increased bank angle will reduce the lift. As an aircraft banks, lift is divided into horizontal and vertical components. The horizontal component of lift causes the aircraft to turn. Combining both components of lift, the total lift required increases.

Lift 52

Lift Aileron Drag Pilot 52

Pilot Institute

MARCH 29, 2024

Lift : The aerodynamic force generated due to airflow over the wings. Weight : The force gravity exerts on the aircraft. The aircraft’s deceleration reduces the airflow over the wings, which reduces lift. When the lift force is less than the force of gravity, the aircraft descends. Why does this happen?

Lift 52

Lift Rudder Drag AGL 52