As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FWD FUSELAGE SECTION, RT ECS BAY CUTOUT FRAME FOR ACCESS DOOR CRACKED WITH CORROSION AT STAND OFF ATTACH POINT JUST FORWARD OF FORWARD HINGE ARM ATTACH POINT, TOP FWD OF O/B FRAME FORMER, TM3. REMOVED AND REPLACED CRACKED AND CORRODED CHORD ON O/B SIDE OF RT ECS BAY CUTOUT.