As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LEFT WING VERTICAL ANGLE INBOARD OF MID SPAN DEFLECTION CONTROL RIB IS CRACKED. REMOVED VERTICAL ANGLE INBOARD OF MID SPAN DEFLECTION CONTROL RIB FOR REPLACEMENT. INSTALLED A NEW ANGLE INBOARD OF MID SPAN DEFLECTION CONTROL RIB PER SRM 51-40-02.. REFINISHED PAINT PER AMM51-21-99.