Light aircraft wing dihedral angle measuring clamp

The utility model discloses a light aircraft wing dihedral angle measuring clamp which comprises a whole panel matched with the front end of a wing, the panel is provided with a positioning structure and a clamping groove, the positioning structure is matched with an oil filler cap, and the clamping groove is used for positioning a measuring instrument. The panel is positioned on the wing through the matching of the panel and the front end of the wing and the matching of the positioning structure and the oil filler cap. Afterwards, the measuring instrument is positioned in the clamping groove, the measuring instrument can accurately measure the dihedral angle of the wing, and the technical problem that in the prior art, due to the fact that the standing angles of measuring personnel are different, and the position of the measuring instrument is inaccurate, the measuring result error is large is solved. 本实用新型公开了一种轻型飞机机翼上反角测量夹具，包括一整块与机翼前端吻合的面板，面板上设有定位结构和卡槽，定位结构与加油口盖吻合，卡槽用于定位测量仪器。本发明利用面板与机翼前端的吻合，以及，定位结构与加油口盖的吻合，