As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION TYPE:C3 REPAIR SURVEY OF THE PRESS FUSELAGE AREA FOUND FUSELAGE EXTERIOR SKIN EXISTING DOUBLER HAS SHORT ED FASTENER AT STA 1750 L14L. REMOVED EXISTING DOUBLER IAW SRM 51-1-20D AND FOUND 2 INCH CRACK IN SKIN, CUT OUT DAMAGED AREA IAW SRM 53-02-01 FIG 7. FABRICATED AND INSTALLED REPAIR FILLER, FINGER DOUBLERS AND DOUBLER IAW DWG 5772706-19, AND SRM 53-02-01-0 FIG 007.