What was found
INSPECTION FOUND A 1 INCH CRACK IN FUSELAGE CLIP TIE AT STA 300, STRINGER 29L. THE CLIP WAS REMOVED, A NEW CLIP WAS FABRICATED AND INSTALLED IAW SRM 51-10-1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1 INCH CRACK IN FUSELAGE CLIP TIE AT STA 300, STRINGER 29L. THE CLIP WAS REMOVED, A NEW CLIP WAS FABRICATED AND INSTALLED IAW SRM 51-10-1.