As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON THE FUSELAGE EXTERNAL PLATING AT FUSELAGE STATION 902, LONGERONS 14,17 AND 18 RIGHT. REPAIR ACCOMPLISHED CORROSION REMOVAL AND DETERMINED TO BE WITH LIMITATION IN ACCORDANCE WITH THE DOUGLAS STRUCTURAL REPAIR MANUAL AND BOEINGS FAX TIN-MIA-02-00012H.