Vou pros Balcãs ser Traficante de Armas da Silva

“The most likely cause, based on the available tracking data, ATC audio, weather context, and the physics of the final trajectory, is this: The Learjet 60 penetrated the core of a strong convective cell (tops reported near 47,000 ft while the aircraft was around 35,000 ft). Inside the cell it encountered a rapid updraft-to-downdraft transition that drove the nose down. The aircraft then accelerated past its Mach limits, entered Mach tuck (the aerodynamic nose-down force that becomes strong once a Learjet is overspeed at high altitude), and developed a steep spiral. Descent rates exceeded 30,000 ft/min and the final attitude was near-vertical. Recovery was not possible once that sequence was established. Ice was reported by the crew and may have added workload or minor performance degradation, but at approximately –47 °C classic structural icing is improbable and is not required to explain the observed behavior. Claims of an isolated negative-G pushover specifically shearing the horizontal stabilizer are aerodynamically possible in severe turbulence but remain secondary and unconfirmed; the dominant, data-supported chain is cell penetration → upset → overspeed/Mach tuck → unrecoverable dive. The critical decision was the failure to deviate around a cell that was visible on radar and associated with ground stops at FLL. Once inside the core, the margin for recovery disappeared within roughly 30 seconds.”