What was found
ANGLE IN THE LEFT WHEEL WELL SHOWS SIGNS OF CORROSION FOR THE PRESSURE SENSITIVE FLOW LIMITER ABOVE THE TRANSFER CYLINDER ACCUMALATOR ON THE KEEL WEB.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
ANGLE IN THE LEFT WHEEL WELL SHOWS SIGNS OF CORROSION FOR THE PRESSURE SENSITIVE FLOW LIMITER ABOVE THE TRANSFER CYLINDER ACCUMALATOR ON THE KEEL WEB.