What was found
RIGHT FUSELAGE HAS CRACKED ANGLE JUST FWD OF R1 DOOR AT FS 294.5 BETWEEN STR 12-13 RT. ACFT GROUNDED. REMOVED ANGLE STIFFENER IAW SRM 51-40-02 LOCATED AND DRILLED NEW ANGLE STIFFENER IAW SRM 51-40-05, INSTALLED IAW SRM 51-40-02.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RIGHT FUSELAGE HAS CRACKED ANGLE JUST FWD OF R1 DOOR AT FS 294.5 BETWEEN STR 12-13 RT. ACFT GROUNDED. REMOVED ANGLE STIFFENER IAW SRM 51-40-02 LOCATED AND DRILLED NEW ANGLE STIFFENER IAW SRM 51-40-05, INSTALLED IAW SRM 51-40-02.