What is the maximum take-off weight for smaller aeroplanes under part 135?

The maximum take-off weight for smaller aeroplanes operating under Part 135 is set at 8,618 kg (about 19,000 lbs). This weight limit is established to ensure that aircraft used for certain operations, particularly those classified as on-demand charter and commuter operations, meet specific safety and operational criteria.

This regulation is critical for maintaining safety standards within the aviation industry, allowing operators to manage risk effectively. The weight limit reflects considerations around aircraft performance, load-carrying capacity, and operational limitations for smaller aircraft. It distinguishes these aircraft from larger commercial airliners, which operate under different regulatory frameworks with higher weight thresholds.

Understanding this specific weight limitation is essential for pilots and operators involved in Part 135 operations, as exceeding this weight can lead to regulatory violations and potential safety risks during flight operations.