What was found
LEFT WING OTBD FLAP, INBD FORWARD HINGE BRACKET LOWER OTBD STUD HOLE SPOTFACE, FOUND CORRODED. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-08, REV 72. EXISTING THICKNESS 0.415", REMAINING THICKNESS 0.384". MATERIAL REMOVED: FWD 0.002"AND AFT 0.029", MINIMUM ALLOWABLE THICKNESS 0.423". REWORKED CARRIED OUT IAW EA 1-5750-157159, PART 1, STEPS 1, 2, 3, AND 6. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.