Where is the shock absorber located in the boom components?

The shock absorber is typically located at the top of the boom to help manage the dynamic forces experienced during flight and landing. This positioning allows the shock absorber to effectively dampen vibrations and stresses as they occur, providing stability and absorbing shock loads that could affect the structural integrity and performance of the boom and, by extension, the helicopter itself.

Placing the shock absorber at the top contributes to optimizing the overall balance and performance of the aircraft, as it can directly interact with the forces exerted during operation. The top location is strategically advantageous, as it helps to mitigate the impact of forces throughout the boom and leverage the natural structural design of the aircraft.

The other locations mentioned would not serve the function of improving stability as effectively; for example, placing it at the bottom could result in less effective dampening of the longitudinal and lateral movements, while mid-section placement might not maximize its effectiveness regarding force transfer throughout the boom structure.