Accident Overview
A Cessna 421 experienced an inflight breakup. Investigation revealed that the left outboard portion of the elevator assembly, including the balance weight, separated from the aircraft first. This separation led to empennage flutter and the subsequent in-flight breakup of the empennage.
Structural Findings
Examination of the wreckage showed that the left elevator outboard hinge and its support structure exhibited evidence of hinge overtravel. The left horizontal stabilizer front spar had failed downward. Rivets attaching the left outboard hinge to the rear spar of the left stabilizer were sheared. Additionally, the left elevator center hinge had been pulled off the rear spar.
Maintenance History
Approximately 100 flight hours before the accident, maintenance was performed to address a loose left elevator balance weight and to repair a damaged stiffener in the center structure of the horizontal stabilizer. Post-accident examination confirmed that the balance weight was tight and the stiffener repair was intact.