As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LEFT WING INTERNAL LE AIR LOAD RIB IS CRACKED AT THE UPPER ATTACHMENT AT ILES 500.0 VERIFIED WITH HFEC. REPLACED LOWER CHORD FOR UPPER ATTACH POINT IAW SRM 57-41-09 & SRM 51-40-02. TREATED & PAINTED WITH CIC PROTECTION IAW SRM 51-20-01 & SRM 53-50-01.