N2510H is a 1979 Piper PA-18-150. It is a fixed-wing single-engine aircraft with 2 seats, powered by a Lycoming 0-320 series rated at 180 horsepower. The registration is active, with the registrant based in Alexandria, MN. Its standard airworthiness certificate was issued in Sep 1979. It has been registered to its current owner since Dec 2019. This page also carries 1 NTSB event.
- 47 years old
- 1 of 2,081 Piper PA-18-150
2019
1979
That's everything on file so far — TailWiki checks the FAA registry daily and adds new entries as N2510H's record changes.
On August 15, 2020, about 1307 central daylight time, a Piper PA18, N2510H, was destroyed when it was involved in an accident near Brandon, Minnesota. The pilot and one passenger sustained minor injuries. The airplane was being operated as a Title 14 Code of Federal Regulations (CFR) Part 91 personal flight.
According to the pilot, he had landed to the south and turned around to take off to the north from his private grass runway. He reported that the engine lost power shortly after the airplane became airborne. He contemplated landing on the remaining runway as he thought that the engine regained power. Due to the length of runway, he elected to continue the takeoff, but because of the obstacles at the departure end of the runway, he turned the airplane toward a wheat field. While maneuvering toward the field, the landing gear struck a 4-foot-high steel post attached to a fence in the field. The airplane came to rest upright in the field. After the occupants exited, a postcrash fire consumed the airplane.
Examination of the accident site revealed that the airplane struck the steel post about 4-ft above the ground. The airplane came to rest about 150 ft from the impact with the post. Evidence at the site showed that the airplane rotated about 90° to the right before it struck the ground. Although a postimpact fire consumed most of the airplane, all flight control continuities were confirmed. Engine control continuity was established. Due to the extensive fire damage, the engine could not be rotated, and a detailed examination was not possible.
According to the carburetor icing probability chart in Federal Aviation Administration Special Airworthiness Information Bulletin CE-09-35, with a temperature of 18ºC and a dew point of 2ºC (+16 dew point depression), the airplane was operating within the range of serious icing in glide power.
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About the Piper PA-18-150
About the modelThe Super Cub — a two-seat tandem taildragger developed from the J-3 with far more power. A backcountry, bush and glider-towing aircraft, prized for short-field performance.