What was found
DAILY INSPECTION FOUND CRACK ON LEFT AUXILIARY VERTICAL FIN AT ATTACH POINT (4 INCH) SPIDER. THIS IS A PROBLEM THAT WAS CORRECTED MANY YEARS AGO ON 206L-1 SERIES.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DAILY INSPECTION FOUND CRACK ON LEFT AUXILIARY VERTICAL FIN AT ATTACH POINT (4 INCH) SPIDER. THIS IS A PROBLEM THAT WAS CORRECTED MANY YEARS AGO ON 206L-1 SERIES.