As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
ASD UPPER AFT ANGLE HAS CORROSION. REMOVED CORROSION AT ASD AFT UPPER ANGLE FUSELAGE SIDE IAW SRM 53-21-23-101-001-A01. BLENDED AREA IS OUT OF ALLOWABLE LIMITS IAW SRM 53-21-23-101-001-A01. R & R ANGLE ON ASD UPPER AFT IAW SRM 51-42-06-001-001-A01.