As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE SKIN CRACK AT CANTED FRAME STA 1303 RIGHT SIDE 4 INCHES ABOVE LONGERON 14. CRACK IS APPROXIMATELY 1 INCH LONG. STOP DRILLED CRACK PER SRM 53-01 FIG 2 SHT 3. HFEC INSPECTION SHOWS CRACK CONTAINED. FABRICATED AND INSTALLED DOUBLER PER SRM 53-01 FIG 2 SHEET 3. APPLIED TOPCOAT PER SRM51-10-03B. JOB COMPLETE.