University of Texas, 7777 Knight Road, Houston, TX 77054, United States.
Accid Anal Prev. 2015 Apr;77:113-9. doi: 10.1016/j.aap.2015.01.021. Epub 2015 Feb 18.
Accidents in twin-engine aircraft carry a higher risk of fatality compared with single engine aircraft and constitute 9% of all general aviation accidents. The different flight profile (higher airspeed, service ceiling, increased fuel load, and aircraft yaw in engine failure) may make comparable studies on single-engine aircraft accident causes less relevant. The objective of this study was to identify the accident causes for non-commercial operations in twin engine aircraft. A NTSB accident database query for accidents in twin piston engine airplanes of 4-8 seat capacity with a maximum certified weight of 3000-8000lbs. operating under 14CFR Part 91 for the period spanning 2002 and 2012 returned 376 accidents. Accident causes and contributing factors were as per the NTSB final report categories. Total annual flight hour data for the twin engine piston aircraft fleet were obtained from the FAA. Statistical analyses employed Chi Square, Fisher's Exact and logistic regression analysis. Neither the combined fatal/non-fatal accident nor the fatal accident rate declined over the period spanning 2002-2012. Under visual weather conditions, the largest number, n=27, (27%) of fatal accidents was attributed to malfunction with a failure to follow single engine procedures representing the most common contributing factor. In degraded visibility, poor instrument approach procedures resulted in the greatest proportion of fatal crashes. Encountering thunderstorms was the most lethal of all accident causes with all occupants sustaining fatal injuries. At night, a failure to maintain obstacle/terrain clearance was the most common accident cause leading to 36% of fatal crashes. The results of logistic regression showed that operations at night (OR 3.7), off airport landings (OR 14.8) and post-impact fire (OR 7.2) all carried an excess risk of a fatal flight. This study indicates training areas that should receive increased emphasis for twin-engine training/recency. First, increased training should be provided on single engine procedures in the event of an engine failure. Second, more focus should be placed on instrument approaches and recovery from unusual aircraft attitude where visibility is degraded. Third, pilots should be made aware of appropriate speed selection for inadvertent flights in convective weather. Finally, emphasizing the importance of conducting night operations under instrument flight rules with its altitude restrictions should lead to a diminished proportion of accidents attributed to failure to maintain obstacle/terrain clearance.
双引擎飞机事故的死亡率比单引擎飞机高,占通用航空事故的 9%。不同的飞行剖面(更高的空速、飞行上限、增加的燃料负荷以及发动机故障时的飞机偏航)可能使对单引擎飞机事故原因的可比研究相关性降低。本研究的目的是确定双引擎飞机非商业运营中的事故原因。对 2002 年至 2012 年期间,在 14 CFR 第 91 部规定下运行的最大认证重量为 3000-8000 磅、容纳 4-8 名乘客的双活塞引擎飞机的 NTSB 事故数据库查询返回了 376 起事故。事故原因和促成因素按照 NTSB 最终报告的类别。从 FAA 获得了双引擎活塞飞机机队的年度总飞行小时数据。采用卡方检验、Fisher 精确检验和逻辑回归分析进行统计分析。在 2002-2012 年期间,无论是综合致命/非致命事故还是致命事故率都没有下降。在目视天气条件下,最大数量 n=27(27%)的致命事故归因于故障,未能遵循单引擎程序是最常见的促成因素。在能见度降低的情况下,恶劣的仪表进近程序导致了最严重的致命坠机事故。遭遇雷暴是所有事故原因中最致命的,所有乘客都受了致命伤。在夜间,未能保持与障碍物/地形的净空距离是最常见的事故原因,导致 36%的致命坠机事故。逻辑回归的结果表明,夜间飞行(OR 3.7)、场外着陆(OR 14.8)和事故后火灾(OR 7.2)都存在致命飞行的额外风险。本研究表明,在双引擎培训/近期培训方面,应重点关注一些培训领域。首先,应在发动机故障时提供更多关于单引擎程序的培训。其次,应更加重视仪表进近和在能见度降低时从异常飞机姿态恢复的情况。第三,应让飞行员意识到在意外的对流天气中选择适当速度的重要性。最后,强调根据仪表飞行规则进行夜间操作并遵守高度限制的重要性,应能降低因未能保持与障碍物/地形的净空距离而导致的事故比例。