As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACK IN THE FUSELAGE SKIN AT RIGHT SIDE FUSELAGE STA 727 A-1 BETWEEN STR 14 AND STR 15. CRACK REPAIRED BY REMOVING DAMAGED AREA. FABRICATED REPAIR DOUBLER AND INSTALLED WITH RIVETS WET WITH SEALANT IAW SRM 51-30-3, FIG 1 AND SRM 51-30-1. (X)