What was found
LT WING (WING SIDE) OTBD FLAP, INBD HINGE SIDE LOAD FITTING SURFACE FOUND CORRODED. REWORKED IAW CMM 20-11-02, REV 72. UPPER EXISTING THICKNESS: 0.400", MATERIAL REMOVED: 0.004", REMAINING THICKNESS: 0.396". LOWER EXISTING THICKNESS: 0.387", MATERIAL REMOVED: 0.004", REMAINING THICKNESS: 0.383". REPAIR ACCOMPLISHED IAW EA 1-5750-160021, PART 1, STEPS 5, 6 AND 8. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 114.