As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING THE STRUCTURAL INSPECTION IT WAS FOUND AT FORWARD FUSELAJE, THE SKIN LH SIDE WITH EXISTING OIL CAN. THE OIL CAN WAS LOCATED COMMON TO AN EXISTING REPAIR AS PER SRM 53-10-01 REPAIR 64P AT FR12 BETWEEN STRINGER 21L AND STRINGER 23L. ALSO, THERE WERE TWO DENTS CLOSE TO THE REPAIR AND OIL CAN. THE DAMAGES WERE REPAIRED BY INSTALLING AN EXTERNAL DOUBLER REPAIR AS PER E.O. # COO-EO-2021-12923 R01, ETD2021-190-018705-A AND APROVED UNDER ANAC FORM F-200 PROVIDED BY EMB.