As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LOWER FUSELAGE SKIN FOUND CRACKED AND CORRODED AT FRAME 14A BETWEEN STRINGERS 25 AND 26. THE DAMAGED AREA MEASURES /75 INCH BY .75 INCH. MAINTENANCE REMOVED DAMAGED AND INSTALLED EXTERNAL DOUBLER REPAIR IAW FAIRCHILD DORNIER REPAIR DESIGN APPROVAL SHEET RAS-328-53-1736 AND SERVICE PROBLEM REPORT MODOO33371. (M)