What was found
CRACK ON FUSELAGE SKIN COMMON TO THE AFT ENTRY DOOR CUTOUT, STA 986.5+2" AND BETWEEN S-7L TO S-8L. PERFORMED REPAIR PER SRM.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON FUSELAGE SKIN COMMON TO THE AFT ENTRY DOOR CUTOUT, STA 986.5+2" AND BETWEEN S-7L TO S-8L. PERFORMED REPAIR PER SRM.