As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACK FOUND APPROX 1.125" LONG AT STR13AL BETWEEN BS1654-1674 WHILE ACCOMPLISHING EA 5380-01178 OPS 001 SKIN INSPECTION. FUSELAGE SKIN CRACK REPAIRED BETWEEN STA1654-1674 STR 13AL IAW SRM 53-80-01 REPAIR 7 FIG 201 DETAIL VII CAT B REPAIR. REF TABLE 202 FOR IQ REQUIREMENTS AND FREQUENCY.