As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
1 INCH BY 2 INCH HOLE PUNCTURED IN SKIN BETWEEN FRAME 20-21 AND STRINGERS 28-29 ON R-H SIDE OF FWD FUSELAGE APPROX 5 INCHES FWD OF AFT AVIONICS ACCESS DOOR. MAJOR REPAIR ACCOMPLISHED. REPLACED STRINGER. FABRICATED & INSTALLED EXTERNAL SKIN DOUBLER.