What was found
INSPECTION FOUND A 1.5 INCH CRACK IN FRAME TO FUSELAGE SKIN CLIP AT STA 1307 BETWEEN STRINGER 15R AND 16R. A NEW SKIN CLIP WAS INSTALLED IAW SRM 51-30-5.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1.5 INCH CRACK IN FRAME TO FUSELAGE SKIN CLIP AT STA 1307 BETWEEN STRINGER 15R AND 16R. A NEW SKIN CLIP WAS INSTALLED IAW SRM 51-30-5.