What was found
FUSELAGE FRAME AT STA 580 IS DENTED AND CRACKED BETWEEN STR 16R-17R. REMOVED DAMAGED AREA, NO CRACK FOUND. FABRICATED REPAIR PART FROM 7075-T6 .063 AL PER SRM 51-40-3. TREATED, PRIMED AND INSTALLED PER SRM 51-40-3 FIG 1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE FRAME AT STA 580 IS DENTED AND CRACKED BETWEEN STR 16R-17R. REMOVED DAMAGED AREA, NO CRACK FOUND. FABRICATED REPAIR PART FROM 7075-T6 .063 AL PER SRM 51-40-3. TREATED, PRIMED AND INSTALLED PER SRM 51-40-3 FIG 1.