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