What is the typical load distribution rule on a CH-47 when using multiple hooks?

The typical load distribution rule on a CH-47 when using multiple hooks primarily focuses on ensuring the aircraft's balance and stability during flight. By placing the heaviest load in the center, it helps to maintain a lower center of gravity and reduces the risk of instability that can occur with heavier loads positioned toward the front or rear of the aircraft. This configuration allows for a more balanced distribution of weight across the aircraft, which is crucial for flight safety and performance.

Positioning the lightest load at the aft hook ensures that the rear of the aircraft remains light enough to avoid excessive tail heaviness, which can adversely affect the lift characteristics and control of the helicopter. This approach to load distribution mitigates the risk of uneven weight shift during flight, enhancing overall handling and operational effectiveness.

The practice of balancing loads on a helicopter, especially in the case of the CH-47, is a critical part of flight operations and is guided by safety protocols to ensure a stable flight path. This arrangement also assists with precise maneuverability and allows for the effective application of navigation and operational missions.