What was found
LEFT UPPER WING, REMOVED CORROSION AT REAR SPAR, 69.5\ O/B OF BBL 70.5. REMOVED APROX .020\ MAT AND ALODINE AREA. CORR DID NOT GO INTO FASTENER. FASTENER OKAY. INSPECTED REWORK AREA WBL 150.5, .016 INCH MATERAL REMOVED FOR CORROSION FROM .424 INCH ORIG THICKNESS, FASTENER NOT AFFECTED, NO LAMINAR CORROSION FOUND, USING 757 NDT PART 4 51 00 00 AND AVO ESC120524-5325-1.