As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION ON MID CAP ANGLE AND LOWER ANGLE KICK PLATE AT PASSENGER DOOR FUSELAGE FRAME, BTW FS 310.00 TO FS 349.00. MID CAP ANGLE AND LOWER ANGLE KICK PLATE AT PASSENGER DOOR FUSELAGE FRAME, BTW FS 310.00 TO FS 349.00 WERE EVALUATED AND FOUND EXCESSIVE CORROSION PER SRM 53-00-00-101-001-A01 AND WERE REPLACED PER SRM 51-41-02-001-001-A01 AND SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01