As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING ACCOMPLISHMENT OF EA5330-04213 OP2, FOUND HFEC CRACK INDICATIONS ON 3 FASTENER HOLES AND AN EXTERNAL 0.3" SKIN CRACK AT THE L1 UPPER FORWARD CORNER. MAJOR REPAIR ACCOMPLISHED. REPAIRED EXTERNAL FUSELAGE SKIN AT L1 DOOR UPPER FORWARD CORNER IAW EA5330-04213 AND ECRA 5331-01687. ACCOMPLISHED HFEC -NO CRACKS. INSTALLED DOUBLER AND TRIPLER.