What was found
LEFT WING TRAILING EDGE INBOARD OF THE DEFLECTOR BEAM AROUND REAR SPAR STA 261, THE FIXED UPPER PANEL CENTER AFT TRIANGLE SHAPED STIFFENER CRACKED AT THE LOWER ATTACH. R & R PANEL IAW SRM & DWG.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT WING TRAILING EDGE INBOARD OF THE DEFLECTOR BEAM AROUND REAR SPAR STA 261, THE FIXED UPPER PANEL CENTER AFT TRIANGLE SHAPED STIFFENER CRACKED AT THE LOWER ATTACH. R & R PANEL IAW SRM & DWG.