As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING ROUTINE C-CHECK AND CPCP INSPECTION, CORROSION OF THE EXTERIOR PLATING WAS IDENTIFIED AT FUSELAGE STATION 296 BETWEEN LONGERONS 34 AND 35 RIGHT. THE CORRODED AREA WAS CUT OUT AND REPAIR WAS ACCOMPLISHED BY FABRICATION AND INSTALLATION OF A FILLER AND EXTERNAL DOUBLER IAW DOUGLAS STRUCTURAL REPAIR MANUAL 53-2-1. (M)