What was found
CRACK - STRINGER, FWD UPPER FUSELAGE INTERNAL STRUCTURE STA 870 - STA 890, S-8L(<P>REPAIR DAMAGE AREA IAW EI NO T2021A53M-870 REV 1. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK - STRINGER, FWD UPPER FUSELAGE INTERNAL STRUCTURE STA 870 - STA 890, S-8L(<P>REPAIR DAMAGE AREA IAW EI NO T2021A53M-870 REV 1. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)