What was found
AT FAR 121 ACCEPTANCE INSPECTION, DETERMINED LEFT FUSELAGE TO HAVE LARGE FLAT DENT AT FUSELAGE STATION 198.6 AND STRINGER 6L. REPAIRED WITH FLUSH PATCH IAW MANUFACTURER'S STRUCTURAL REPAIR MANUAL. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AT FAR 121 ACCEPTANCE INSPECTION, DETERMINED LEFT FUSELAGE TO HAVE LARGE FLAT DENT AT FUSELAGE STATION 198.6 AND STRINGER 6L. REPAIRED WITH FLUSH PATCH IAW MANUFACTURER'S STRUCTURAL REPAIR MANUAL. (M)