As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING 4-DAY CHECK A 3.5 INCH CRACK WAS FOUND IN LT FUSELAGE SKIN 4 INCHES ABOVE WING ROOT BETWEEN WINDOWS 11 AND 12, BETWEEN BS 500D+10 AND BS 520, STR 12 LT. MAINTENANCE CUTOUT DAMAGE IN LT FUSELAGE SKIN BETWEEN BS 500D+10 AND BS 520, STR 12 LT. PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST. FABRICATED A REPAIR DOUBLER AND TRIPLER; INSTALLED REPAIR PARTS IAW AWA E.R. 03-5331-04191-RA1.