What was found
CRACKED FWD UPPER CORNER ON FUSELAGE SKIN AT FWD SERVICE DOOR JAMB CORNER. REPAIR WAS ACOMPLISHD IAW SRM 53-05, FIG 112.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACKED FWD UPPER CORNER ON FUSELAGE SKIN AT FWD SERVICE DOOR JAMB CORNER. REPAIR WAS ACOMPLISHD IAW SRM 53-05, FIG 112.