What was found
THE FUSELAGE SKIN IS DENTED BETWEEN FS 605 AND FS621 BETWEEN STRINGERS 22L AND 23L. TRIMMED OUT DAMAGED FUSELAGE SKIN. FRABRICATED REPAIR DOUBLER FROM 2024-T3.063" AND INSTALLED I/A/W WVAC EO 601R-53-3328A.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
THE FUSELAGE SKIN IS DENTED BETWEEN FS 605 AND FS621 BETWEEN STRINGERS 22L AND 23L. TRIMMED OUT DAMAGED FUSELAGE SKIN. FRABRICATED REPAIR DOUBLER FROM 2024-T3.063" AND INSTALLED I/A/W WVAC EO 601R-53-3328A.