What was found
RIGHT WING UPPER TE PANEL, CTR SUPPORT ANGLE CRACKED AT TRANSVERSE WEB ATTACH POINT, ABOVE NR 2 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.
RIGHT WING UPPER TE PANEL, CTR SUPPORT ANGLE CRACKED AT TRANSVERSE WEB ATTACH POINT, ABOVE NR 2 PYLON AFT TIP. R & R ANGLE IAW SRM.