What was found
LEFT WING UPPER T/E SUPPORT ANGLE CRACKED ABOVE NR1 PYLON AFT TIP AT TRANSVERSE WEB ATTACH POINT. REMOVED AND REPLACED ANGLE IAW SOPM.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT WING UPPER T/E SUPPORT ANGLE CRACKED ABOVE NR1 PYLON AFT TIP AT TRANSVERSE WEB ATTACH POINT. REMOVED AND REPLACED ANGLE IAW SOPM.