What was found
LEFT WING OTBD FLAP, INBD FWD HINGE, WING SIDE, LOWER MOUNT INBD HOLE SURFACE CORROSION. CORROSION REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-08. EXISTING THICKNESS 0.437 INCHES, MATERIAL REMOVED FWD SIDE 0.006 INCHES, AFT SIDE 0.016 INCHES, REMAINING THICKNESS 0.415 INCHES, MIN ALLOWABLE THICKNESS 0.423 INCHES. REPAIR SHIM FABRICATED & INSTALLED IAW EA 1-5750-T0325375 PART 1 STEP 1. CORROSION REPAIR REFER TO WRI 57507886 FOR WORK DETAILS. REFER CLASSIFIED AS MINOR IAW GMM 6-2-100.