As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RT SIDE CABIN INNER CREASEBEAM FROM STA 900-1040 HAS CORROSION. BLENDED CORRODED AREA IAW SRM 51-10-02. ORIGINAL THICKNESS OF CHORD IS 0.75" IAW SRM 53-40-13 FIG 1 ( SHEET 2 ). AFTER REMOVED CORROSION ON 3 SPOTS MATERIAL REMAINING IS .035" ALL AREAS FOUND OUT OFF LIMITS IAW SRM 53-40-13 FIG 101 DETAIL VII. REMOVED AND REPLACED CREASE BEAM IAW SRM 51-40-05 AND 51-40-02. MAJOR REPAIR.