What was found
DURING A D2 CHECK AT MIA, CORROSION WAS FOUND ON THE UPPER SURFACE OF STRINGER 23L BETWEEN STA321 AND STA 338. REPAIR WAS PERFORMED PER EC/RA 5311-02093. ON OR BEFORE AIRCRAFT REACHES 7500 0 TOTAL AIRCRAFT FLIGHT CYCLES, PERFORM AN INSPECTION PER PART2 OF ECRA 5311-02093. PLANNING TO CONTACT EG. AFTER 72000 CYCLES BUT BEFORE 73000 CYCLES FOR THE INSPECTION REQUIREMENTS. ON OR BEFORE A/C REACHES 75000 TOTAL A/C FLIGHT CYCLES, PERFORM AN INSPECTION PER PART 2 ECRA 5311-02093. PLANNING TO CONTACT EG. AFTER 72000CYCLES BUT BEFORE 73000 CYCLES FOR INSPECTION. REPAIR WAS PERFORMED PER EC/RA 5311-02093. ON OR BEFORE AIRCRAFT REACHES 75000 TOTAL AIRCRAFT FLIGHT CYCLES, PERFORM AN INSPECTION PER PART2 OF ECRA 5311-02093. PLANNING TO CONTACT EG. AFTER 72000 CYCLES BUT BEFORE 73000 CYCLES FOR THE INSPECTION REQUIREMENTS TOMC-APPROVAL FROM SC1ELBYC COMMENT INSPECTIONS CREATED BY AUTODIP PENDING AIRCRAFT RECORDS AUDIT & UPDATE. IMSPECTION C/W TOMC APPROVED : QC REVIEWED TOMC APPROVED : QC REVIEWED