What was found
LEFT WING OTBD FLAP, OTBD FWD HINGE BRACKET, WING SIDE, LOWER OTBD STUD ATTACH SPOT FACE FOUND CORROSION. REWORKED & FOUND EXCEEDED LIMIT IAW MM 57-44-09. EXISTING THICKNESS 0.421", MATERIAL REMOVED, FWD FACE 0.009" & AFT FACE 0.009", REMAINING THICKNESS 0.403" & MINIMUM ALLOWABLE THICKNESS 0.408". NEW REPAIR SHIM FABRICATED & INSTALLED IAW EA 1-5750-T0325482 PT 1 STEP 1. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100. REFER TO WRI 57503736 FOR WORK DETAILS.