What happened
On May 26, 2026, a Cessna 206G, registration YV1172, was performing a flight from Guiria Aerodrome to the Uon-Quen indigenous community in Bolívar State. The aircraft, operated for private use, departed Uon-Quen at 16:35 UTC carrying eight occupants, including the pilot, five passengers, and two children.
During the final approach to Guiria, while flying under Visual Flight Rules (VFR) at an altitude of 6,500 feet, the pilot encountered windshear. This meteorological phenomenon caused an immediate loss of lift and destabilized the aircraft's approach. As the aircraft dropped below the glide path, the pilot attempted an emergency landing short of the runway threshold to minimize potential injuries.
The pilot shut down the engine during the maneuver. The aircraft traveled approximately 20 meters before the nose gear struck an obstacle and fractured. This impact caused the aircraft to overturn. All eight occupants escaped without injury, though the aircraft sustained significant structural damage.
The investigation
The Venezuelan investigation authority (JIAAC) conducted a technical examination of the wreckage and reviewed all relevant documentation. Investigators inspected the airworthiness certificates, maintenance logs from the certified maintenance organization (SKY DREAMS AVIATION C.A.), and the pilot's commercial licenses and medical certifications, all of which were found to be valid at the time of the accident.
Physical inspections focused on several key areas:
- Nose Gear: The assembly was found detached from its mounting fittings. Significant fractures were identified in the drag link, the upper trunnion, and the fork. Damage was also noted on the steering bungee, shimmy damper, and the steering bungee support fitting.
- Fuselage: Structural damage included buckling (wrinkling) of the fuselage skin on both the left and right sides near station 18.4, as well as damage to the forward fuselage bulkheads.
- Engine and Propeller: The McCauley propeller sustained damage to the blades, hub, and spinner. While the engine itself showed no signs of mechanical failure or leaks, the upper engine cowling was damaged.
- Empennage and Wings: Damage was observed on the vertical and horizontal stabilizers, as well as the elevator and rudder. On the left wing, the wingtip and leading edge were damaged.