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My RV-7A
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Date:  6-2-2008
Number of Hours:  1.50
Manual Reference:  Sec 6 page 3 Dwg 3
Brief Description:  Dimpling the understructure components

Dimpled all of the spars and ribs using the pneumatic squeezer. While dimpling the HS-603PP Rear Spar, I managed to allow the squeezer to strike the spar twice, causing a second dimple hole to be created close to the original (see center of image). Because of the holes are close together and redrilling would not look good. I am considering replacing the part since it may fracture under the stress of flight. I verify with Vans to make sure.
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