What was found
RT WING (WING SIDE) OTBD FLAP, INBD HINGE SIDE LOAD FITTING SURFACE, FOUND CORRODED. REWORKED IAW CMM 20-11-02 REV 72. UPPER EXISTING THICKNESS: 0.412", MATERIAL REMOVED: 0.005", REMAINING THICKNESS: 0.407". LOWER EXISTING THICKNESS: 0.403", MATERIAL REMOVED: 0.006", REMAINING THICKNESS: 0.397". REPAIR ACCOMPLISHED IAW EA NR 1-5750-160028, PART 1, STEPS 3, 4, 5 AND 7. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.