What was found
-AD- OPEN HOLE HFEC INSPECTION FOUND 01 EA THROUGH CRACK AT 10 O'CLOCK POSITION AT #3 FASTENER LOCATION AND 01 EA THROUGH CRACK AT 4 O'CLOCK AT #4 FASTENER LOCATION ON THE FUSELAGE SKIN LAYER ONLY AT THE FORWARD ENTRY DOOR CUTOUT AFT LOWER CORNER AS MARK. (LOOKING FROM O/B TO I/B). CRACK WAS FOUND DURING NDT INSPECTION. REPAIR IS REQUIRED PRIOR TO FURTHER FLIGHT. AMOC TO AD 24-05-03 MAY BE REQUIRED. REFER TO AA 5331- 01288. ACCOMPLISHED THE REPAIR TRANSFER TO W/C 5331-01288-02. THIS IS A CATEGORY B REPAIR. INSPECTIONS SHALL BE CONDUCTED AT 3,000 FLIGHT CYCLES INTERVALS, COMMENCING FROM WHICHEVER OCCUR FIRST: EITHER 6,000 MAXIMUM FLIGHT CYCLES AFTER REPAIR INSTALLATION OR 37,500 FLIGHT CYCLES SINCE AIRPLANE DELIVERY PER B767-300 SRM 53-10-01-2R-1 FIG 202 REV 127.00 MAR-18-2025. (LP #0883850)