What was found
INNER REINFORCEMENT SKIN AT LAV SERVICE PANEL CORRODED. (MAJOR REPAIR) (LEVEL 2 CORROSION). COMPLIED WITH FABRICATION, ALODINE PRIMED AND INSTALLED FILLER AND EXTERNAL DOUBLER IAW SRM 53-23-60.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INNER REINFORCEMENT SKIN AT LAV SERVICE PANEL CORRODED. (MAJOR REPAIR) (LEVEL 2 CORROSION). COMPLIED WITH FABRICATION, ALODINE PRIMED AND INSTALLED FILLER AND EXTERNAL DOUBLER IAW SRM 53-23-60.