What was found
INSPECTION FOUND A .5 INCH CRACK IN FUSELAGE TO BELTFRAME CLIP AT STA 616, S7L TO S8L. THE CLIP WAS REMOVED AND REPLACED IAW SRM 51-40-02.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .5 INCH CRACK IN FUSELAGE TO BELTFRAME CLIP AT STA 616, S7L TO S8L. THE CLIP WAS REMOVED AND REPLACED IAW SRM 51-40-02.