Aviation Accident Summaries

Aviation Accident Summary LAX02LA169

STOCKTON, CA, USA

Aircraft #1

N51716

Enstrom F-28C

Analysis

During the takeoff sequence, a gust of wind pushed the helicopter into a water tower near the refueling pad. The pilot had been drying trees in an orchard and landed in a parking lot to refuel. During takeoff from the parking lot, the main rotor blades struck the tank and the helicopter fell to the ground. It impacted in a flat attitude before rolling onto its side. Rain accumulation had reduced the pilot's visibility through the windshield. The pilot was not able to attain any visual cues on the wind velocity and directional information from inside the helicopter. High obstructions surrounded the takeoff area and were located within 15 feet of the rotor diameter.

Factual Information

On May 19, 2002, about 1720 Pacific daylight time, an Enstrom F-28C, N51716, collided with a water tower during takeoff about 10 miles northeast of Stockton, California. The owner was operating the helicopter on a local flight under the provisions of 14 CFR Part 91. The airline transport pilot, the sole occupant, sustained serious injuries; the helicopter was substantially damaged. Day visual meteorological conditions prevailed, and no flight plan had been filed. The pilot reported that he had been flying over an orchard to dry cherry trees. The winds were gusty and there were intermittent rain showers. He landed in a parking lot and refueled. The parking lot was surrounded by several high obstacles including power lines, lighting poles, and water tanks. All of these were within 15 feet of the rotor blades as the helicopter sat on the ground. Rain had accumulated on the windscreen, which reduced visibility. The pilot was unable to detect the current wind velocity at the location. During the takeoff sequence, a gust of wind pushed the helicopter into a water tower near the refueling pad. The main rotor blades struck the tank and the helicopter fell to the ground. The pilot stated that the helicopter had impacted in a flat attitude before rolling over on its side. Water from the breached tank poured onto the airframe. There was no post crash fire.

Probable Cause and Findings

The pilot's failure to maintain an adequate clearance from the water tower during takeoff. Also causal was the pilot's selection of a confined area for the landing and subsequent takeoff.

 

Source: NTSB Aviation Accident Database

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