In aircraft design, the horizontal tail plays a crucial role in ensuring longitudinal stability. A thorough understanding and analysis of the loads acting on this component is essential to the overall integrity of the aircraft structure. This underscores the importance of carefully considering various design requirements and the associated operational conditions.

The process of load analysis presents a significant challenge. By integrating principles of aerodynamics and structural engineering, a systematic approach is necessary. This process allows for the effective management of extensive datasets while enhancing our comprehension of the interplay between aerodynamics and structural components.

Furthermore, facilitating clear communication with other teams and certification authorities can introduce its own complexities, but it also promotes collaboration and innovation within the design process.

This paper presents a methodical approach to load computations through a simple hand calculation, striking a balance between speed and accuracy, which is particularly beneficial during the initial stages of aircraft development. While this methodology is broadly applicable, we will exemplify its use with a focused case study of a horizontal tail for a single-propeller engine aircraft, thus demonstrating its practical application. We look forward to engaging in this analytical journey of design exploration.