What was found
RIGHT FUSELAGE HAS CRACKED ANGLE JUST FWD OF R1 DOOR AT BS 294.5 BETWEEN S9-10R. ACFT GROUNDED. REMOVED ANGLE STIFFENER IAW SRM 51-40-02, INSTALLED FABRICATED ANGLE STIFFENER 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 BS 294.5 BETWEEN S9-10R. ACFT GROUNDED. REMOVED ANGLE STIFFENER IAW SRM 51-40-02, INSTALLED FABRICATED ANGLE STIFFENER IAW SRM 51-40-02.