As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION TYPE:C2 CRACK ON EXTERIOR FUSE SKIN AT STA 1740 L19R. CUT OUT DAMAGED AREA ON FUSELAGE SKIN AT STA 1740 L19R IAW SRM 53-02-01 FIG 7. FABRICATED AND INSTALLED REPAIR DOUBLER, FINGER DOUBLER, AND FILLER AT STA 1740 L19R IAW SRM 53-02-01 FIG 7.