As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LH WING REAR SPAR HAS VERIFIED CORROSION AROUND LT SPOILER RETURN HYDRAULIC FITTING. MECHANICALLY BLENDED TWO SPOTS OF MILD/MODERATE CORROSION IN LT WHEEL WELL ON LT WING REAR SPAR AROUND LH SPOILER RETURN HYDRAULIC FITTING IAW SRM 51-10-01. FOUND BLENDED AREAS TO BE OUT OF LIMITS PER SRM 51-70-02. REPAIRED CORRODED AREAS IAW ENGINEERING MEMO DQ26483M1/