Clatskanie, OR, USA
N925DP
PFLUGRADT Kitfox
The airline transport pilot of the experimental, amateur-built airplane reported that, while flying about 800 ft above a river during a personal flight, he advanced the throttle to climb then the engine started to lose power. He elected to land on a nearby island, during which the airplane nosed over. Postaccident examination of the airplane revealed that the throttle cable set screw on the aft side of the throttle body arm had backed out of its original position and was no longer securing the throttle cable. As a result, the cable moved freely with no corresponding motion on the throttle body arm. This would have also resulted in the pilot's inability to adjust the engine power from the cockpit throttle control. Maintenance records revealed that the pilot built and installed the throttle body arm about 7 months and 204 flight hours before the accident. In addition, a vernier-style throttle cable was installed about 6 months and 159 flight hours before the accident. It is likely that the set screw was improperly secured during one of the previous maintenance events and came loose during operation, which released its hold on the throttle cable.
On March 20, 2018, about 1315 Pacific daylight time, an experimental Pflugradt Kitfox Super Sport airplane, N925DP, experienced a partial loss of engine power and collided with terrain near Clatskanie, Oregon. The airline transport pilot was not injured and the airplane sustained substantial damage to the right wing. The airplane was registered to and operated by the pilot as a Title 14 Code of Federal Regulations Part 91 personal flight. Visual meteorological conditions prevailed, and no flight plan was filed. The flight originated from Pacific City State Airport (PFC), Pacific City, Oregon at 1200 and was destined for Pearson Field Airport (VUO), Vancouver, Washington The pilot reported that he departed from PFC and he followed the coast and Columbia river en route to VUO. About 800 ft above the Columbia river, he advanced the throttle to climb when the engine started to lose power. The pilot elected to land on a nearby treeless island in the river. The airplane landed uneventfully, and during the landing roll, the main wheels sunk into the ground and the airplane nosed over and came to rest on its back. Postaccident examination of the airplane by a Federal Aviation Administration Inspector revealed that the throttle cable was loose at the throttle body attachment arm. When manipulated, the cable moved freely with no corresponding motion on the throttle body arm. The cable set screw on the aft side of the throttle body arm backed slightly out of its original position and was no longer securing the throttle cable. Review of the maintenance logbooks revealed the the throttle body arm was built by the owner and was installed on the airplane on July 30, 2017, at 1,092.5 hours, which is about 204 hours prior to the accident. In addition, a vernier style throttle cable was installed on August 30, 2017 at 1,137 hours, about 159 hours prior to the accident.
A partial loss of engine power due to an improperly secured throttle cable set screw.
Source: NTSB Aviation Accident Database
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