Fatigue issues in aircraft maintenance and repairs

摘要: Many design considerations are involved in ensuring structural integrity of Boeing jet transports, which have common features validated by extensive analyses, tests, and service performance. Designing for continued the presence damage such as fatigue or corrosion is an evolutionary process. Performance demands, increasing complexity, aging fleet reassessments required development standards suitable application large teams engineers. This presentation focused on methods with special emphasis practical reliability considerations. Durability evaluations based quantitative ratings incorporate test data reduction performance predictions. Fatigue detection assessments estimates coupled to growth residual strength evaluations. Data presented airline operators check forms permit efficient maintenance planning achieve levels.