What was found
LEFT WING T/E, AFT SUPPORT ANGLE CRACKED FORM UPPER T/E PANEL ABOVE NR 1 ENGINE STRUT. REMOVED AND REPLACED ANGLE IAW SOPM AND SRM.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT WING T/E, AFT SUPPORT ANGLE CRACKED FORM UPPER T/E PANEL ABOVE NR 1 ENGINE STRUT. REMOVED AND REPLACED ANGLE IAW SOPM AND SRM.