What happened
During the evening hours, an aircraft departed from a private, unlit airstode. The pilot had previously landed on a road/landing strip at approximately 18:30, using vehicle headlights to assist with visibility, and departed again around 19:00 after dropping off a passenger. The flight path headed toward a rural area characterized by rolling hills and low population density.
Witnesses in the vicinity reported hearing the aircraft take off, followed by the sound of the engine failing, and subsequently hearing an impact within a nearby grape vineyard. An investigation of the crash site determined that the aircraft type impacted the terrain in a nose-down orientation. There were 0 fatalities reported in the provided text, though the specific injury count was not detailed.
Findings
Maintenance documentation indicated that the aircraft's last annual inspection took place roughly 12 months and 299.5 flight hours before the crash. Approximately five months prior to the accident, a certified repair station had identified 15 specific grounding discrepancies that required attention. These issues included structural concerns such as cracks in the wing lower skins, loose wing spar bolts, and loose rivets on the right-hand flap, as well as mechanical failures like an inoperative stall warning, leaking hydraulic components, and a frayed elevator trim cable.
While the pilot had addressed the cracked nose cowling and potentially the turbine inlet temperature gauge, many other identified faults remained unaddressed. Notably, the pilot had been operating the aircraft with a non-functional landing gear retraction system for approximately four months. Post-accident inspections confirmed that several of these documented discrepancies were still present on the aircraft at the time of the crash, although investigators could not establish a direct causal link between these specific mechanical issues and the engine failure and subsequent impact.