What was found
DURING INSPECTION OF THE INTERNAL FUSELAGE, CORROSION WAS FOUND ON THE SHEAR TIE, BS 880, STRINGER 30 JUST AFT OF GROUND AIR CONNECTION. REPAIRED THE SHEAR TIE IAW DWG 140N2002 AND SRM 53-30-07.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING INSPECTION OF THE INTERNAL FUSELAGE, CORROSION WAS FOUND ON THE SHEAR TIE, BS 880, STRINGER 30 JUST AFT OF GROUND AIR CONNECTION. REPAIRED THE SHEAR TIE IAW DWG 140N2002 AND SRM 53-30-07.