What was found
HFEC INSPECTION FOUND APPROX 1 INCH CRACK THROUGH STOP DRILLED HOLE ON L1 DOOR SKIN UPPER HINGE CUTOUT RADIUS. REPAIRED IN ACCORDANCE WITH EN 048-11 APPROVED BY BOEING ODAS.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
HFEC INSPECTION FOUND APPROX 1 INCH CRACK THROUGH STOP DRILLED HOLE ON L1 DOOR SKIN UPPER HINGE CUTOUT RADIUS. REPAIRED IN ACCORDANCE WITH EN 048-11 APPROVED BY BOEING ODAS.