Aviation Accident Summaries

Aviation Accident Summary LAX96LA167

LAKE HAVASU CTY, AZ, USA

Aircraft #1

N9177E

Maule M-5-235C

Analysis

The pilot owned and operated the seaplane and had flown it for 803 hours. During the dark nighttime cruise flight, the engine began surging and then gradually lost power. The pilot planned to make a forced landing at the shoreline of the Colorado River; however, during landing the airplane slid on the grass bank and impacted a 3-foot-high tree trunk. The airplane was subsequently examined, and the following discrepancies were found: (1) Sediment was observed in the fuel filter and carburetor; (2) The number 3 cylinder intake valve was found open and stretched in excess of 0.200 inches; (3) No compression was obtained from the number 3 cylinder; (4) The engine oil was black in color; (5) The magneto's drive end seal bearing was found leaking oil; (6) The left set of points were oil fouled, and the right set of points had oil on the contacts and were coked up; and (7) The left distributor gear was missing a gear tooth.

Factual Information

On April 13, 1996, at 2210 hours mountain standard time, a Maule, M-5-235C, N9177E, owned and operated by the pilot, experienced a partial loss of engine power during cruise flight. The pilot made a forced landing on a river bank near Lake Havasu City, Arizona. The float equipped airplane was substantially damaged. Neither the commercial pilot nor the two passengers were injured. Visual meteorological conditions prevailed during the dark nighttime personal flight, and no flight plan was filed. The flight originated from the Colorado River, near Bullhead, Arizona, at 2150. According to the pilot, when he was about 12 minutes from reaching Lake Havasu, his airplane's engine began surging, and then gradually lost power. The pilot planned to make a forced landing on the bank of the river. However, upon touchdown the pilot discovered that he had landed so close to the shoreline that the airplane slid on a grass bank and then impacted a 3-foot-high tree trunk. The airplane was subsequently examined by the Federal Aviation Administration and by an independent airplane mechanic. The following observations were made in verbal and written inspection reports: (1) Sediment was found in the fuel filter and carburetor; (2) The number 3 cylinder intake valve was found open and stretched in excess of 0.200 inches; (3) No compression was obtained from the number 3 cylinder; (4) The engine oil was black in color; (5) The magneto's drive end seal bearing was found leaking oil into the magneto; (6) The left set of points were oil fouled, and the right set of points had oil on the contacts and were coked up; and (7) The left distributor gear was missing a gear tooth.

Probable Cause and Findings

the pilot-owner's inadequate engine maintenance which resulted in a progressive ignition failure. Factors which contributed to the accident were the dark nighttime light condition and the presence of hidden obstructions in the forced landing area.

 

Source: NTSB Aviation Accident Database

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