Abstract This paper presents a methodology for the conceptual design of a Maneuver Load Control system taking into account the airframe flexibility. The system. when switched on. is able to minimize the bending moment augmentation at a wing station near the wing root during an unsteady longitudinal maneuver. https://www.roneverhart.com/Jumbo-New-Spin-Tuz-Karabiber-De-irmeni-14-cm/