As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
AFTER REMOVAL ANGLE FLOOR SUPPORT CORROSION WAS FOUND AT CROSSBEAM BETWEEN BL 0 TO LBL 9 ON FUSELAGE STA 280. CROSSBEAM BETWEEN BL 0 TO LBL 9 ON FUSELAGE STA 280.0 WAS REPLACED PER SRM 51-42-06-001-001-A01, SRM 51-42-06-001-001-A01, SRM 51-42-13-001-001-A01