What was found
LEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, UPPER MOUNT INBD HOLE, SURFACE CORROSION. REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING THICKNESS 0.711", MATERIAL REMOVED 0.006", REMAINING THICKNESS 0.705", MINIMUM ALLOWABLE THICKNESS 0.720". REPAIR SHIM FABRICATED & INSTALLED IAW EA 1-5750-T0319681 PART 1. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.