What was found
LEFT WING UPPER TE PANEL AFT SUPPORT ANGLE CRACKED AT TRANSVERSE WEB ATTACH POINT ABOVE NR 1 PYLON AFT TIP. R & R ANGLE IAW SRM.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT WING UPPER TE PANEL AFT SUPPORT ANGLE CRACKED AT TRANSVERSE WEB ATTACH POINT ABOVE NR 1 PYLON AFT TIP. R & R ANGLE IAW SRM.