Aircraft Flight Operation Regulations Article 285-28
After December 20, 2010, an operator may not operate a turbine-powered transport category airplane with a type certificate issued after January 1, 1958, and either a maximum type certificated passenger seating capacity of 30 or more, or a maximum type certificated payload capacity of 7,500 pounds or more, unless the following requirements have been met:1. The maintenance programme for the airplane includes damage-tolerance-based inspections and procedures for aircraft structure susceptible to fatigue cracking that could contribute to a catastrophic failure. These inspections and procedures must take into account the adverse affects repairs, alterations, and modifications may have on fatigue cracking and the inspection of this aircraft structure; and2. The damage-tolerance-based inspections and procedures aforementioned in the preceding subparagraph, including any revisions, must be approved by the state of design. The operator must incorporate the damage-tolerance-based inspections and procedures in CAA-approved maintenance programme.
中文原文 航空器飛航作業管理規則第285-28條
航空器使用人應於中華民國九十九年十二月二十日以前符合下列規定，始得操作於中華民國四十七年一月一日以後型別檢定之最大座位數三十座以上或最大酬載七千五百磅以上之渦輪發動機之運輸類飛機：
一、航空器使用人之維護計畫應包括飛機結構受疲勞裂痕影響可能導致毀滅性失效之結構容損基礎之檢查及程序。
該檢查及程序應考慮修理、改裝或技術修改對疲勞裂痕之負面影響及飛機結構之檢查。
二、前款結構容損基礎之檢查及程序之訂定或修訂，應經航空器設計國民航主管機關核准；航空器使用人應將該訂定或修訂之檢查及程序納入維護計畫中，經報請民航局核准後實施。
一、航空器使用人之維護計畫應包括飛機結構受疲勞裂痕影響可能導致毀滅性失效之結構容損基礎之檢查及程序。
該檢查及程序應考慮修理、改裝或技術修改對疲勞裂痕之負面影響及飛機結構之檢查。
二、前款結構容損基礎之檢查及程序之訂定或修訂，應經航空器設計國民航主管機關核准；航空器使用人應將該訂定或修訂之檢查及程序納入維護計畫中，經報請民航局核准後實施。