Aviation Accident Summaries

Aviation Accident Summary GAA18CA506

Ridgeway, PA, USA

Aircraft #1

N89ZC

Hughes 369

Analysis

The pilot reported that, after a high reconnaissance of the area, he descended the helicopter to about 30 ft above power lines to inspect them while flying about 30 to 35 knots. While patrolling, he climbed over an identified crossing line and then initiated a descent. During the descent, the passenger spotted a previously unseen power line in their flightpath, so the pilot "pulled hard aft cyclic with right pedal," but the main rotor blades struck the power line. The helicopter's main rotor system began vibrating, but the pilot was able to land without further incident. The helicopter sustained substantial damage to the main rotor blades. The pilot reported that there were no preaccident mechanical failures or malfunctions with the helicopter that would have precluded normal operation.

Factual Information

The helicopter pilot reported that, after a high reconnaissance the helicopter was descended to about 30 ft above the power lines for the powerline inspection, while flying about 30-35 knots. While patrolling, they climbed over an identified crossing line, and then descended back down. During the decent , the passenger spotted a previously unseen power line in their flight path so the pilot "pulled hard aft cyclic with right pedal" but the main rotor blades struck the power line. The helicopter acquired a vibration in the main rotor system, but pilot was able to land without further incident. The helicopter sustained substantial damage to the main rotor blades. The pilot reported that there were no preaccident mechanical failures or malfunctions with the helicopter that would have precluded normal operation.

Probable Cause and Findings

The pilot's failure to maintain clearance from power lines during an aerial observation flight.

 

Source: NTSB Aviation Accident Database

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