What was found
INSPECTION FOUND A 3" CRACK IN UPPER FUSELAGE SKIN AT STA 178, WL 243, LBL 1.5. THE CRACKED DOUBLER WAS REMOVED AND A NEW DOUBLER WAS INSTALLED IAW SOEING DRAWING #65-45800 AND SRM 51-40-02.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 3" CRACK IN UPPER FUSELAGE SKIN AT STA 178, WL 243, LBL 1.5. THE CRACKED DOUBLER WAS REMOVED AND A NEW DOUBLER WAS INSTALLED IAW SOEING DRAWING #65-45800 AND SRM 51-40-02.