Accident Summary
During climb to cruise altitude at 2,800 feet, the pilot reported a loss of engine power. The pilot trimmed the airplane for best glide speed and selected a beach area for landing. Emergency procedures were attempted, including engine restart efforts, but these were unsuccessful. The airplane touched down successfully, but during the landing roll it encountered a large pool of standing water, causing the nose gear to collapse.
Examination Findings
A post-accident examination revealed that the nose gear had collapsed, the engine mounts were broken, and the right wing was damaged and detached from the fuselage. Fuel recovery showed 17 gallons in the right fuel tank and 10 gallons in the left fuel tank. Further examination found no blockage in the exhaust system, no defects with either magneto, and a functional check of the engine was accomplished. The pilot did not report any mechanical malfunctions prior to the accident.
Weather Conditions
At the time of the accident, the nearest weather facility reported clouds at 2,500 feet, temperature 29°C, and dew point 24°C. The conditions were stated to be favorable for the formation of ice. According to Advisory Circular 20-113, pilots are advised to remain alert for indications of induction system icing during takeoff and climb-out, especially when relative humidity is above 50 percent or when visible moisture is present.