What was found
UPON AIRCRAFT ARRIVAL AND WHILST POSITIONING LOADER AT AFT CARGO DOOR FOR UNLOADING EQUIPMENT STRUCK THE AIRCRAFT AT FRAME 58 AND STGR 46RH AND 45RH CAUSING A PUNCTURE TO THE FUSELAGE. CORRECTIVE ACTION: ACCOMPLISHED SECTION 1 TIME LIMITED REPAIR IAW ERA 609873-14 REV ORIGINAL. ACCOMPLISH SECTION 2 PERMANENT REPAIR WITHIN 2 FLIGHT CYCLES. ERA 609873-14 REV ORIGINAL MATCHES PRI 609873-14 REV ORIGINAL, REV 1, REV 2 AND ALL RII COMPLIED WITH. ON 11JUL23, C/W ER/A 609873-14 REV ORIGINAL SECTION II PERMANENT REPAIR. (LP 3483441)