What was found
SUPPLEMENTAL INFORMATION: (RIGHT WING) UPPER T/E PANEL SUPPORT CRACKED AT TRANSVERSE WEB LOWER ATTACH POINT ABOVE #2 PYLON AFT TIP / REMOVED AND REPLACED THE UPPER T/E SUPPORT AT THE TRANVERSE WEB IAW SRM 51-40-02-0G-0
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
SUPPLEMENTAL INFORMATION: (RIGHT WING) UPPER T/E PANEL SUPPORT CRACKED AT TRANSVERSE WEB LOWER ATTACH POINT ABOVE #2 PYLON AFT TIP / REMOVED AND REPLACED THE UPPER T/E SUPPORT AT THE TRANVERSE WEB IAW SRM 51-40-02-0G-0