What was found
A HOLE WAS FOUND IN THE FUSELAGE SKIN BETWEEN STA 368-375 AND STR 20L-21L. THE HOLE MEASURED APPROX 3 INCHES DIAMETER AND HAD SEVERAL LARGE CRACKS EMINATING FROM THE HOLE. THE DAMAGED SKIN WAS TRIMMED OUT TO AN APPROX 8 FWD/AFT BY 7 CIRCUMFERENTIAL HOLE. TIME LIMITED REPAIR PER B767-300 SRM 53-00-01, FIG. 201 EXCEPT INSTALL DOUBLER AND FASTENERS AS SHOWN IN FIG; PERMANENT REPAIR - CONTACT LIAISON ENGINEERING - LIMITED TO 12 MONTHS SERVICE; VISUAL INSPECT EVERY 1000 FLIGHT CYCLES.