What was found
IN MAINTENANCE, FOUND SKIN CRACK, FUSELAGE LT SIDE AFT OF UPPER WING TO BODY FAIRING, 1 INCH LONG. VERIFIED BY HFEC AND MARKED ENDS. REPAIRED WITH BLIND RIVET REPAIR PER SRM 53-30-3, FIG 6, INSPECT BLIND RIVET REPAIR AT 3000 FLT CYC THEN 2500 FLT CYC THERE AFTER. REPLACE WITH SOLID RIVET REPAIR IF LOOSE RIVET FOUND OR AT 10,000 FLT CYC.