What was found
INTERIOR FUSELAGE STIFFENER BRACKET CRACKED 1 INCH LENGTH FWD OF STA 291 BETWEEN STRINGERS 11R AND 12R. REMOVED DAMAGED ANGLE, LOCATED DRILLED AND INSTALLED A REPLACEMENT STIFFENER IAW SRM 51-40-02 PG 3 DETAIL 1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INTERIOR FUSELAGE STIFFENER BRACKET CRACKED 1 INCH LENGTH FWD OF STA 291 BETWEEN STRINGERS 11R AND 12R. REMOVED DAMAGED ANGLE, LOCATED DRILLED AND INSTALLED A REPLACEMENT STIFFENER IAW SRM 51-40-02 PG 3 DETAIL 1.