What was found
AFT CABIN FUSELAGE CTL III FLOOR PANEL SUPPORT ANGLE HAS CORROSION AT FRAME 86, Y= 739. R & R SUPPORT ANGLE 170-66796-001 IAW SRM 51-41-02 WO 6213171I3 & EO E175-5300-100 REV IR WO 1834035.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AFT CABIN FUSELAGE CTL III FLOOR PANEL SUPPORT ANGLE HAS CORROSION AT FRAME 86, Y= 739. R & R SUPPORT ANGLE 170-66796-001 IAW SRM 51-41-02 WO 6213171I3 & EO E175-5300-100 REV IR WO 1834035.