What was found
INTERIOR FUSELAGE STIFFENER BRACKET CRACKED 1.5 INCHES IN LENGTH FWD OF STA 291 BETWEEN STRINGERS 10R AND 11R. 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 1.5 INCHES IN LENGTH FWD OF STA 291 BETWEEN STRINGERS 10R AND 11R. REMOVED DAMAGED ANGLE, LOCATED, DRILLED AND INSTALLED A REPLACEMENT STIFFENER IAW SRM 51-40-02 PG 30 DETAIL 1.