What was found
EXTERIOR FUSELAGE SKIN, 12 INCHES FWD OF FRAME 10 HAD TWO DENTS, 6 AND 10 INCHES ABOVE THE LAP SEAM. REPAIRED THE AREA IAW EO A300-5330-69533-A, AND REO-G21522, REV IR.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
EXTERIOR FUSELAGE SKIN, 12 INCHES FWD OF FRAME 10 HAD TWO DENTS, 6 AND 10 INCHES ABOVE THE LAP SEAM. REPAIRED THE AREA IAW EO A300-5330-69533-A, AND REO-G21522, REV IR.