What was found
(LEFT WING) UPPER T/E PANEL SUPPORT ANGLE CRACKED ABOVE NR 1 PYLON AFT TIP ON AFT SIDE OF TRANSVERSE BEAM. 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 PANEL SUPPORT ANGLE CRACKED ABOVE NR 1 PYLON AFT TIP ON AFT SIDE OF TRANSVERSE BEAM. REMOVED AND REPLACED ANGLE IAW SOPM.