What year did Cessna reduce the maximum flap deflection on the 210 series aircraft?

Cessna reduced the maximum flap deflection on the 210 series aircraft in 1966. This change was made to improve the aircraft's handling characteristics during flight, particularly during takeoff and landing. By adjusting the flap deflection, Cessna aimed to enhance performance and safety, ensuring pilots had better control over the aircraft under different conditions. This modification reflects the manufacturer’s ongoing commitment to improving aircraft design based on feedback and performance evaluations over time, showcasing the evolution of aircraft technologies and the importance of safety in aviation practices.