What was found
CORROSION FOUND AT MANY PLACES ON LADDER PLATE OF STRESS PANEL 522AT. COMPLIED WITH HFEC INSPECTION ON REWORKED AREAS IAW RD8-57-114. NO CRACK INDICATION FOUND. REPAIRED IAW RD8-57-114.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CORROSION FOUND AT MANY PLACES ON LADDER PLATE OF STRESS PANEL 522AT. COMPLIED WITH HFEC INSPECTION ON REWORKED AREAS IAW RD8-57-114. NO CRACK INDICATION FOUND. REPAIRED IAW RD8-57-114.