What was found
POSSIBLE INTERIOR SKIN CORROSION ON WASH, SKIN AND RIVETS BUCKLED FROM STA 360 TO STA 400 AROUND S-26 LEFT APPROX. [EXTERIOR SKIN CIRCLED] FLEET CYCLE LOG PAGE 9780955. INITIATE A 2ND DTA DIP FOR "PLANNING TO CONTACT ENGINEERING AFTER 16 MONTHS, BUT BEFORE 17 MONTHS FOR PERMANENT REPAIR INSTRUCTIONS". THIS L/P FOR DIPS ONLY. DAMAGED STR SECTION TRIMMED OUT AND NEW SECTION SPLICED IN PER ECRA 5311-02618. SEE FLEET CYCLE L/P 9780955 FOR DETAILS OF WORK ACCOMPLISHED. CONTACT ENGINEERING AFTER 16 MONTHS, BUT BEFORE 17 MONTHS FOR PERMANENT REPAIR INSTRUCTIONS.? PLACED ON A 2ND DTA DIP PER ECRA 5311-02618 FOR ?PLANNING TO TOMC-APPROVAL FROM SC1ELBYC COMMENT QC REVIEWED QC REVIEWED INSPECTIONS CREATED BY AUTODIP PENDING AIRCRAFT RECORDS AUDIT & UPDATE.