What was found
LADDER PLATE FOUND CRACKED UNDER STRESS PANEL 622AT. CUTOUT DAMAGE IAW RD8-57-2387 AND FABRICATED NEW PART IAW RD8-57-2387. HFEC INSPECTION DONE ON REPAIRED AREA. NO DEFECTS NOTED.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LADDER PLATE FOUND CRACKED UNDER STRESS PANEL 622AT. CUTOUT DAMAGE IAW RD8-57-2387 AND FABRICATED NEW PART IAW RD8-57-2387. HFEC INSPECTION DONE ON REPAIRED AREA. NO DEFECTS NOTED.