As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE EXTERIOR STA 58 AT L19R SKIN CRACKED 3 PLACES. REMOVED PREVIOUS DOUBLER AND FILLER. CUT OUT DAMAGE TO 1.6 IN DIAMETER. NDT VERIFY CRACKS CONTAINED IAW NDT SPM 06-10-01. FABRICATED NEW DOUBLER FROM 6AL-4V TITANIUM AND FILLER FROM 7075-T6 0.050 IAW DC9 SRM 53-04 FIG 38 LOCATED AND DRILLED IAW DC9 SRM 51-10-4. INSTALLED IAW DC9 SRM 51-30-5, 51-30-2, P-125 R.