What was found
STRESS PANEL LADDER PLATE IS CRACKED ON OTBD AFT CORNER OF PANEL 622AT. REMOVED DAMAGE IAW RD8-57-2375. COMPLIED WITH HFEC INSPECTION. NO FURTHER DAMAGE FOUND. REPAIRED DAMAGE IAW RD8-57-6133.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
STRESS PANEL LADDER PLATE IS CRACKED ON OTBD AFT CORNER OF PANEL 622AT. REMOVED DAMAGE IAW RD8-57-2375. COMPLIED WITH HFEC INSPECTION. NO FURTHER DAMAGE FOUND. REPAIRED DAMAGE IAW RD8-57-6133.