As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
AFTER TOP PANEL REMOVAL, CORROSION ON STIFFERNERS OF THE TOP PANEL WAS FOUND ON FWD PASSENGER DOOR. STIFFENERS (3 EAS) WERE REPLACED AND STIFFERNERS (2 EAS) WERE REMOVED AND CLEANED AND AFTER STIFFENER WERE CLEANED AND DVI WAS PERFORMED AND NOT CORROSION WAS FOUND AND SAME STIFFERNERS (2 EAS) WERE INSTALLED ON TOP PANEL OF FWD PASSENGER DOOR PER SRM 51-42-06-001-001-A01, SRM 51-21-06-001-001-A01, SRM 51-12-00-001-001-A01,