As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
REPAIRED THE CORRODED AREAS OF THE FUSELAGE SKIN LOCATED UNDER AND ADJACENT TO THE AFT CHIN FAIRING (WING-TO FUSELAGE FAIRING) BY BLENDING CORRODED AREAS, PERFORMING NDT AND REPORTING FOR REPAIR DISPOSITION, FABRICATING AND INSTALLING REPAIR DOUBLERS IN ACCORDANCE WITH AEROSPACE QUALITY RESEARCH & DEVELOPMENT MRO ENGINEERING REPAIR ORDER.