Aviation Accident Summaries

Aviation Accident Summary CEN09CA368

Wellington, CO, USA

Aircraft #1

N5462N

GROB G103

Analysis

Same as Factual Information

Factual Information

The pilot reported that the initial takeoff roll was normal, but that after a premature takeoff due to wind gusts and thermals the glider controls became ineffective. The pilot attempted to pull the tow line release knob and reported that the tow line “back-released,” resulting in the glider entering a stall. During the impact with terrain, the glider's empennage separated partially, just aft of the fuselage. Examination of the tow line release mechanism and glider systems revealed no mechanical anomalies.

Probable Cause and Findings

The pilot’s failure to maintain control of the glider during takeoff.

 

Source: NTSB Aviation Accident Database

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