On October 2, 2022, about 0900 central daylight time, a Scoda Aeronautica LTDA, Super Petrel LS, N892SP, was substantially damaged when it was involved in an accident near Perma, Montana. The pilot sustained serious injuries and later in the day succumbed to those injuries. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight. According to the trailing pilot, he was following the accident pilot on an impromptu low-level flight over a river. Without incident, they departed Polson Airport, Polson, MT, about 0800, as a flight of two. He reported that about an hour later, while trailing the accident airplane and flying westbound about 50 feet above the river, he saw the lead airplane abruptly pitch up, descend to the right, and impact the water. A still image from a video captured by the trailing pilot showed that the accident airplane was about the height of the powerline poles shortly before the airplane pitched up (see Figure 1).

Figure 1. Photo of power pole and line in relation to accident airplane before impact, with added depiction of the powerline over the river (courtesy of witness) The trailing pilot added that he did not see the powerline before the accident airplane impacted the wire. A witness who responded to the accident site reported that the pilot stated to him that he had flown over the river near the accident area before, but forgot about the powerline during the accident flight.

Figure 2. Map depiction of wreckage site in relation to powerlines According to the power company, the “H” configured 2-pole structure on the north side of the river is about 50 ft above the ground (agl) and the structure on the south side of the river is about 55 ft agl, with a lineal span of 1026 ft. They estimated that the distribution powerline spanned above the water between 40 and 80 ft agl and that the line was not marked at the time of the accident. The airplane came to rest upright on a gravel bar that was about 4 ft below the water level and about 540 feet southwest of the northern power pole structure (see Figure 2). The engine and cabin were submerged with the wings and aft fuselage being above water. The tailcone was partially separated midspan; the empennage was inverted and partially submerged in the water. The airplane sustained substantial damage to the fuselage and both wings. The trailing pilot stated that the pilot did not report any mechanical anomalies concerning the airplane or engine during the accident flight. The auditioned video was consistent with the airplane and engine operating without any anomalies. Sanders County Medical Examiner & Coroner’s Office performed the pilot’s autopsy and reported his cause of death as multiple blunt force injuries. The autopsy identified moderate-to-severe and severe aortic atherosclerosis, with no other significant natural disease. The FAA Bioaeronautical Sciences Research Laboratory, Oklahoma City, Oklahoma, performed toxicological testing of specimens from the pilot, which were negative for performance-impairing drugs or alcohol.