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NTSB Reports

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At about 1720 Eastern time, the airplane was substantially damaged in an off-field landing. The student pilot was fatally injured, and the flight instructor sustained serious injuries. Visual conditions prevailed. The airplane took off at about 1641, and began maneuvers consistent with training. At about 1718, the airplane was on an easterly track when it entered a right descending 270-degree turn from about 2100 feet msl. The last ADS-B target was observed at 1719, descending through 1075 feet msl at a groundspeed of 64 knots. The accident site's elevation was about 1000 feet. Examination revealed the fuel boost pump switch lever was fractured but the remaining portion was in the "ON" position. The left fuel tank was breached; the right fuel tank remained intact and contained about a pint of aviation fuel. Grass blighting was evident along the wreckage path. One propeller blade was "unremarkable," while the other was bent aft around the engine. Neither blade exhibited leading edge gouging or polishing. The fuel selector valve's position was not reported.
机译:在大约1720年的东部时间,飞机在野外着陆中受到严重损坏。学生飞行员致命受伤,飞行教练持续严重伤害。视觉条件占上风。飞机在大约1641年起飞,并开始与培训一致的演习。在大约1718年,飞机在东风轨道上,当它进入约2100英尺MSL的正确下降270度转弯时。在1719中观察到最后的ADS-B靶标,在64个结的底部下降到1075英尺MSL。意外网站的海拔约1000英尺。检查显示燃料升压泵开关杆被破裂,但剩余部分处于“ON”位置。左燃料箱被突破;右燃料箱保持完整并包含在一品脱的航空燃料。沿着残骸路径很明显草丛。一个螺旋桨刀片是“不起眼的”,而另一个是在发动机周围弯曲的船尾。叶片都没有表现出领先的边缘凿孔或抛光。没有报道燃油选择阀的位置。

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    《Aviation safety 》 |2021年第9期| 26-29| 共4页
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