As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INNER STRUCTURE AT THE R2 DOOR BETWEEN BS 967 AND 986.5 HAS CORROSION AT FASTENER HOLE LOCATIONS. ACFT GROUNDED. REMOVED CORROSION AND CHECKED LIMITS, ORIGINAL MAT .080, REMOVED MATERIAL .003, REMAINING MATERIAL .077 FOUND WITHIN LIMITS IAW SRM 53-70-15. APPLIED ALODINE IAW SRM 51-20-01. APPLIED PRIMER IAW SRM 51-20-01. REMOVED AND INSTALLED FASTENERS IAW SRM 51-40-02, APPLIED TOPCOAT IAW AMM 51-05-01.