As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LEFT WING FRONT SPAR LOWER CHORD ANGLE LOWER SECTION WHERE L/E PANELS ATTACH, CORROSION ON TWO SECTIONS APPROX BETWEEN WS 383.0 AND 477.0. FABRICATED AND INSTALLED REPAIR PLATE 18.375 X 2.875 INCHES. INSTALLED PER AVITAS EO AVHM-0186 RO-1FORM 337 FILED BY AVBORNE.