As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RIGHT WING, LOWER SKIN AT REAR SPAR, WBL 708 HAS EXFOLIATION. CORROSION WAS REMOVED BY BLENDING TO A 0.111 INCH MINIMUM THICKNESS FROM ORIGINAL THICKNESS OF 0.193 INCHES. REWORKED AREA WAS SHOT PENNED, ALODINED & PRIMED. STAGE 1 STATIC STRENGTH APPROVAL REQUIRED BY 25 MAR 2017.