What was found
RIGHT WING OTBD FLAP, INBD FORWARD HINGE BRACKET SIDE LOAD FITTING ATTACH SURFACE FOUND CORRODED. REWORKED IAW CMM 57-44-08, REV 72. EXISTING THICKNESS UPPER 0.393", LOWER 0.392", REMAINING THICKNESS UPPER 0.390", LOWER 0.389. MATERIAL REMOVED: UPPER 0.003", LOWER 0.003". SHIM FABRICATED AND INSTALLED IAW CMM 57-44-08, REV 72. REPAIR CARRIED OUT IAW EA 1-5750-157157, PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.