What was found
RIGHT AFT EMERGECY EXIT AFT FUSELAGE FRAME HAS CHAFE DAMAGE FROM SCREW HEAD. REMOVED DAMAGED FRAME. INSTALLED NEW SERVICEABLE FRAME P/N 120-26331-001 IAW EMBRAER EMB 120 SRM 51-10-02 PART 3 AND 51-40-02.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RIGHT AFT EMERGECY EXIT AFT FUSELAGE FRAME HAS CHAFE DAMAGE FROM SCREW HEAD. REMOVED DAMAGED FRAME. INSTALLED NEW SERVICEABLE FRAME P/N 120-26331-001 IAW EMBRAER EMB 120 SRM 51-10-02 PART 3 AND 51-40-02.