What was found
FWD INBD CORNER OF STRESS PANEL LADDER PLATE IS CRACKED AT PANEL 622AT. REMOVED DAMAGE AND REPLACED WITH NEW PART FABRICATED IAW RD 8-57-2287. COMPLIED WITH BOND TEST AND HFEC INSPECTION. NO OTHER CRACKS NOTED.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FWD INBD CORNER OF STRESS PANEL LADDER PLATE IS CRACKED AT PANEL 622AT. REMOVED DAMAGE AND REPLACED WITH NEW PART FABRICATED IAW RD 8-57-2287. COMPLIED WITH BOND TEST AND HFEC INSPECTION. NO OTHER CRACKS NOTED.