As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
PERFORMED OPEN HOLE HFEC INSPECTION OF ALL FASTENER HOLES (5 EA) AT THE FORWARD SERVICE DOOR CUTOUT AFT LOWER CORNER ,FOUND 01 EA CRACK ON THE FASELAGE SKIN OF THE NO.4 FASTENER HOLE, THE CRACK LOCATIONED AT 2 O'CLOCK,THE LENGTH OF CRACK IS ABOUT 0.12 INCH, THE CRACK FASTENER HOLE ON FUSELAGE SKIN AT THE FORWARD SERVICE DOOR CUTOUT AFT LOWER CORNER REPAIRED AS PER B767-400 SRM 53-10- 01-2R-1 REV 75.00 MAY-14-2025 (1193178)