What was found
LEFT WING DEFLECTION RIB TAB AND TRAILING EDGE PANEL STIFFENER HAVE DAMAGE FROM ATTACH BOLTS. / REPAIRED LEFT WING DEFLECTION RIB AND T/E PANEL STIFFENER IAW SRM 57-51-02-2R-1 AND SRM 57-51-02-2R-4 A55799
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT WING DEFLECTION RIB TAB AND TRAILING EDGE PANEL STIFFENER HAVE DAMAGE FROM ATTACH BOLTS. / REPAIRED LEFT WING DEFLECTION RIB AND T/E PANEL STIFFENER IAW SRM 57-51-02-2R-1 AND SRM 57-51-02-2R-4 A55799