What was found
CRACK - STRINGER, FWD UPPER FUSELAGE INTERNAL STRUCTURE STA 950 - STA 980+30, S-9L(<P>ACCOMPLISHED EI NO T2021A53M-872, REV 1 AND EI ATTACH TO WO NO 5670098 (367). JOB COMPLETED AND CONDITION CHK 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 950 - STA 980+30, S-9L(<P>ACCOMPLISHED EI NO T2021A53M-872, REV 1 AND EI ATTACH TO WO NO 5670098 (367). JOB COMPLETED AND CONDITION CHK NORMAL.</P>)