What was found
WHILE PERFORMING LT ENGINE DRAG FITTINGS CLAMP-UP & DIAGONAL BRACE INSPECTIONS MAINTENANCE FOUND OUTER WING LT UPPER SKIN & DRAG FITTINGS CORROSION & TOOL MARKS AT HOLES 2-5, 7-9, 11-14, 16 & 18. C/W ERA 589123-14AD.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
WHILE PERFORMING LT ENGINE DRAG FITTINGS CLAMP-UP & DIAGONAL BRACE INSPECTIONS MAINTENANCE FOUND OUTER WING LT UPPER SKIN & DRAG FITTINGS CORROSION & TOOL MARKS AT HOLES 2-5, 7-9, 11-14, 16 & 18. C/W ERA 589123-14AD.