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Cessna 180-Series AD: Recurring Tail Inspection

机译:CESSNA 180系列广告:经常性尾部检查

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The reality is that the fleet of Cessna singles is aging, and a new FAA airworthiness directive is a reminder that focused airframe inspections might be the best defense against corrosion and structural failure. The latest is FAA AD 2020-21-22, which became effective on Dec. 7, 2020. The issue began with a report of cracks found in the tailcone and horizontal stabilizer attachment structure on a Cessna 185. The FAA then discovered similar conditions on 29 additional Textron Cessna 180- and 185-series airplanes, and determined that the combination of the attachment structure design and high loads during landing contributes to the development of cracks in the tailcone and horizontal stabilizer attachment structure. The meat of the original NPRM (Notice of Proposed Rulemaking) from May 2020 and this ultimate AD require inspecting the tailcone and horizontal stabilizer for corrosion, cracks and loose or sheared rivets and repairing or replacing damaged parts as necessary. The inspection (and repair if needed) can ultimately avoid a failure of the horizontal stabilizer/tail-cone attachment, and worst case-a tail separation in flight. The AD also includes 182A-D models, which was challenged by AOPA and others.
机译:现实是塞斯纳单身队的队伍正在老化,新的FAA适航指令是一个提醒人们,以至于集中的机身检验可能是对抗腐蚀和结构失败的最佳防御。最新的是FAA AD 2020-21-22,该公司于2020年12月7日生效。该问题始于塞斯纳185上的尾机和水平稳定器附件结构中发现的裂缝报告。FAA随后发现了类似的条件29额外的Textron Cessna 180-和185系列飞机,并确定着陆期间连接结构设计和高负荷的组合有助于尾机和水平稳定器附接结构的裂缝的发展。原始NPRM的肉(拟议的统治通知)于5月20日起,该终极广告需要检查旋钮,裂缝和松散或剪切铆钉的尾机和水平稳定器,并根据需要修复或更换损坏部件。检查(以及修理,如果需要)最终可能最终避免水平稳定器/尾锥附件的故障,以及最坏的情况 - 飞行中的尾部分离。该广告还包括182A-D模型,由AOPA和其他人挑战。

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