As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LEFT WING TRAILING EDGE ATTACH ANGLE BETWEEN DEFLECTION CONTROL RIB AND TRANSVERSE WEB CRACKED / [01] REMOVED LEFT WING TRAILING EDGE ATTACH ANGLE BETWEEN DEFLECTION CONTROL RIB AND TRANSVERSE WEB CRACKED AND INSTALLED NEW ATTACH ANGLE P/N 115A6260-1 IAW SRM 51-40-02-0G-0.;[02] VERIFIED CORRECTIVE ACTION #1