As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
WHILE REMOVING THE RIGHT LEADING EDGE STRUCTURE, FOUND CORROSION ON THE LOWER FRONT SPAR AT WS 810. REMOVED CORROSION, BLENDED AREA WITHIN LIMITS IAW SRM 57-20-01, FIGURE 101, DETAIL III. REPAIRED IAW ED 47224REA30. TREATED PRIMED AREA IAW AMM 51-21-04 AND 51-21-00.