Hicks J E, Adams B H
Aviat Space Environ Med. 1980 Sep;51(9 Pt 2):1043-9.
A methodology for identification of crashworthiness deficiencies in Army aircraft is discussed. The methodology provides for injury and impact data to be extracted from accident reports using a specially-developed injury coding system. Personnel injuries are costed through a technique which provides for consideration of each injury based on its relative severity as determined by medical examination. Crash injury causes are identified and ranked according to the magnitude of their effect and probability of occurrence. The technique is designed to provide recommendations as to the most urgent crashworthiness research/development/procurement efforts for consideration by aircraft systems managers and aviation research laboratories. An application of the methodology to an operational Army aircraft is shown. Results typically available are discussed. Recommendations are made as to the use of the methodology and to additional investigation aids which would improve the future identification of crash hazards.
讨论了一种用于识别陆军飞机抗坠毁性缺陷的方法。该方法通过使用专门开发的伤害编码系统，从事故报告中提取伤害和撞击数据。通过一种技术对人员伤害进行成本核算，该技术考虑根据医学检查确定的相对严重程度来考量每一处伤害。识别出坠机伤害原因，并根据其影响程度和发生概率进行排序。该技术旨在为飞机系统管理人员和航空研究实验室提供关于最紧迫的抗坠毁性研究/开发/采购工作的建议。展示了该方法在一架现役陆军飞机上的应用。讨论了通常可获得的结果。就该方法的使用以及有助于改进未来坠机危险识别的其他调查辅助手段提出了建议。
