Inspected left weldment mounting hole to spar alignment and decided the clearances were enough. Removed the weldment and measured the largest dimension of each of the holes. Also examined the alignment of the holes between the weldment and the side of the fuselage. Sent information and questions to Deene.
Test fit right weldment and used two holes as the initial alignment. Verified rivet clearance holes were adequate. Verified alignment of remaining holes to the spar were close enough for filing to fit. Inspected alignment of holes between mount and fuselage and decided they might not be close enough. Included information in email to Deene.