What was found
FOUND FUSELAGE FLOOR SUPPORT STRUCTURE FORWARD LT BUTT STRAP CORRODED. REMOVED CORRODED BUTT STRAP AND INSTALLED NEW PART PER EMB120 SRM STANDARD PRACTICES, CH 51-40-02. AIRCRAFT TOTAL CYCLES, 19,871.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FOUND FUSELAGE FLOOR SUPPORT STRUCTURE FORWARD LT BUTT STRAP CORRODED. REMOVED CORRODED BUTT STRAP AND INSTALLED NEW PART PER EMB120 SRM STANDARD PRACTICES, CH 51-40-02. AIRCRAFT TOTAL CYCLES, 19,871.