What was found
C CHECK - NACELLE PANEL 414AL HAS A CHAFED INTERNAL RIB UPPER AFT END OF PANEL. REMOVED DAMAGED RIB FROM PANEL, MATCH DRILLED NEW RIB TO PANEL AND INSTALLED NEW RIB IAW SRM 51-42-05.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
C CHECK - NACELLE PANEL 414AL HAS A CHAFED INTERNAL RIB UPPER AFT END OF PANEL. REMOVED DAMAGED RIB FROM PANEL, MATCH DRILLED NEW RIB TO PANEL AND INSTALLED NEW RIB IAW SRM 51-42-05.