What was found
INTERIOR FUSELAGE STIFFENER BRACKET CRACKED 4.5 INCH LENGTH FWD OF STA 291 BETWEEN STRINGERS 12R AND 13R. REMOVED DAMAGED ANGLE, LOCATED DRILLED AND INSTALLED A REPLACEMENT STIFFENER IAW SRM 51-40-02 PG 30 DETAIL 1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INTERIOR FUSELAGE STIFFENER BRACKET CRACKED 4.5 INCH LENGTH FWD OF STA 291 BETWEEN STRINGERS 12R AND 13R. REMOVED DAMAGED ANGLE, LOCATED DRILLED AND INSTALLED A REPLACEMENT STIFFENER IAW SRM 51-40-02 PG 30 DETAIL 1.