As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION FOUND ON SUPPORT ANGLE AT DOOR 4 RT STA 1681, RBL 56. MAJOR REPAIR ACCOMPLISHED: AFTER CORROSION REMOVAL FOUND TO BE BEYOND LIMITS AND FOUND A CRACK IN THE FUSELAGE FRAME INNER CHORD AT BS 1681.5 JUST ABOVE STRINGER 17R. REMOVED AND REPAIRED IAW INSTRUCTIONS.