What was found
INSPECTION FOUND A 2.25 INCH CRACK IN RT FUSELAGE SKIN AT STA 745 BETWEEN STRINGERS 15R AND 16R. THE CRACKED AREA WAS REMOVED AND A DOUBLER WAS INSTALLED IAW SRM 51-30-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 2.25 INCH CRACK IN RT FUSELAGE SKIN AT STA 745 BETWEEN STRINGERS 15R AND 16R. THE CRACKED AREA WAS REMOVED AND A DOUBLER WAS INSTALLED IAW SRM 51-30-2.