As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE SKIN DAMAGED AT BS 132.5 BETWEEN STRINGERS 24 - 30R. DAMAGE MEASURES 12 INCHES CIRCUMFERENTIAL BY 2.25 INCHES FORE & AFT AND 1.5 INCHES OUTWARD DEFLECCTION, DAMAGE IS APPOX 6 INCHES FROM LOWER EDGE OF SKIN AND AT L/E. REPAIRED IAW EO B767-5330-63407-A.