What was found
FUSELAGE SKIN UPPER SPLICE PLATE BETWEEN FRAMES 80 AND 81 WAS CRACKED. PERFORMED A PERMANENT REPAIR IAW SRM 51-40-02
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE SKIN UPPER SPLICE PLATE BETWEEN FRAMES 80 AND 81 WAS CRACKED. PERFORMED A PERMANENT REPAIR IAW SRM 51-40-02