What was found
RIGHT NACELLE PANEL 424AR HAS BROKEN RIB ANGLE. REMOVED DAMAGED STIFFENER, REF SRM 51-42-05. INSTALLED, DRILLED, LOCATED NEW STIFFENER REF SRM 51-42-05. RESTORED FINISH, REF SRM 51-42-05. SEALED STIFFENER REF SRM 51-23-00.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RIGHT NACELLE PANEL 424AR HAS BROKEN RIB ANGLE. REMOVED DAMAGED STIFFENER, REF SRM 51-42-05. INSTALLED, DRILLED, LOCATED NEW STIFFENER REF SRM 51-42-05. RESTORED FINISH, REF SRM 51-42-05. SEALED STIFFENER REF SRM 51-23-00.