超輕型載具發展於休閒運動用途為主，台灣現有超輕法規，並無設計製造與通過驗證的相關法規，在自製超輕飛機上，從設計、建造、操作至維護等，均參酌美國自製飛機法規來辦理。本研究目的在於協助建立並完成一本土個人設計第二級超輕型載具之結構驗證工作，將根據台灣現有民航法規07-03A與相關作業流程進行驗證工作，並輔以符合性方法與應用標準規劃所需的結構驗證計畫。本研究根據國外早期發展文獻建立驗證方法，分析超輕飛機結構之設計，並在本地規劃與進行具有可行性且具有可信度的驗證實驗。

Ultra-Light Vehicle (ULV) is developed for recreation purposes. Currently, there is no suitable regulation in Taiwan to fit ULV design and certification. A self-made ULV should apply American Society for Testing and Materials (ASTM) Regulation for design, construction, operation and maintenance. This research tries to establish a personal design Class II ULV in structure verification under CAA Regulation 07-03A and its relative procedures to access ULV qualification using stress tests for regulation conformation in structure. This research adopts some earlier development literatures to create a feasible method for experiment and verification.

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