Drones, which entered our lives with the development of technology, are used in many areas that make our lives easier today. It is seen the effect of drones in photography, cargo transportation, mapping, defense industry, and agricultural sectors. In order for the drones used in these areas to fulfil the desired task, the mechanical and static structure of the drone is of great importance along with the software and electronic cards used. It is possible to perform the desired task in a mechanically stable and optimized air vehicle with integrated payloads. In particular, most of the electronic equipment and payloads of the drone are integrated on the parts that make up the body. For this reason, it is inevitable to examine the effect of both equipment and payloads on whether the drone can perform the desired task or not. In this study, the static analysis of the parts made of carbon fiber material forming the construction of the body of the uniquely designed drone is carried out. These analyses were performed in terms of the total deformation, the strain, and the stress with different mesh structures such as multizone, tetrahedrons, and hex dominant method mesh were performed on the body parts. The results obtained indicated that the body parts of the uniquely designed drone presented in this study can be produced by using carbon fiber materials and they will be suitable for different missions.