The
National Transportation Safety Board (NTSB) opened an investigation into the crash and was joined by
National Oceanic and Atmospheric Administration vessels in the search for wreckage. A side-scan sonar was deployed by the
University of Washington Applied Physics Laboratory and discovered large debris below the surface that were identified as being similar to the plane. The NTSB worked with the US Navy to recover the wreckage using an
ROV and a recovery barge. The aircraft had no
flight data recorder nor a
cockpit voice recorder, and was not required to carry them. It was, however, equipped with a
Ground Proximity Warning System. It had just passed a 100-hour inspection before the crash. Further recovery efforts took place on September 26, 2022; this search resulted in most of the wreckage and multiple bodies being recovered. On October 24, 2022, the NTSB released an update on its investigation, stating that the horizontal stabilizer
actuator had separated into two pieces at a threaded assembly fitting, which could be a contributing factor to the crash. The NTSB said that the actuator lock ring was missing from the wreckage. On October 25, 2022, Viking Air issued a service letter requiring DHC-3 Otter operators to inspect the aircraft and verify that the lock ring is properly installed. The following day, on October 26, 2022, the NTSB issued urgent safety recommendations to the FAA and
Transport Canada urging all DHC-3 Otter operators to inspect the horizontal stabilizer actuator lock ring and report their findings to the respective agencies. The NTSB also recommended the immediate grounding of all DHC-3 seaplanes until further notice, citing concern that more will crash.
Final report On September 29, 2023, the NTSB released its final report on the crash, stating that the probable cause was the loss of control of the plane due to the unthreading of the clamp nut from the horizontal stabilizer trim actuator barrel due to a missing lock ring, which resulted in the horizontal stabilizer moving to an extreme trailing-edge-down position rendering the airplane’s pitch uncontrollable. ==References==