What was found
WING STRUT FAIRING CHAFING ON FUSELAGE SKIN AFT OF RT WING STRUT LOWER FITTING. DAMAGE WAS SUBMITTED TO MFG FOR REPAIR APPROVAL. AREA WAS REPAIRED IAW MFG ENGINEERING REPAIR INSTRUCTIONS S-208B0060/01RDA.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
WING STRUT FAIRING CHAFING ON FUSELAGE SKIN AFT OF RT WING STRUT LOWER FITTING. DAMAGE WAS SUBMITTED TO MFG FOR REPAIR APPROVAL. AREA WAS REPAIRED IAW MFG ENGINEERING REPAIR INSTRUCTIONS S-208B0060/01RDA.