As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION FOUND A 2 INCH CRACK IN RT LOWER FUSELAGE SKIN AT STA 680, STRINGER 28R. THE CRACKED AREA AND FASTENERS WERE REMOVED IAW SRM 51-30-2, PAGE 2 AND 53-30-3, PAGE 14E. DOUBLER AND FILLER WERE INSTALLED IAW SRM 53-30-3, PAGE 14E.