As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION ON RT WING HINGE ARM FITTING AND TOP SKIN PANEL. REPAIR PERFORMED BY BLEND OUT IAW EA 6-5722-103262 AND RAS/BAE/1003079/2006 ISSUE "A" (ALTERNATE MATERIAL DAN 26H30 IN PLACE OF 7150-T651 FOR STIFFENER A572-42583-203) AND RAS/BAE/1003026/2006 ISSUE "A" (CORROSION BLEND OUT).