What was found
DURING ACCEPTANCE INSPECTION, FOUND LT WING UPPER SKIN CORROSION TO BE .130 DEEP AT XRS=75 AND 18 INCHES OF REAR SPAR.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING ACCEPTANCE INSPECTION, FOUND LT WING UPPER SKIN CORROSION TO BE .130 DEEP AT XRS=75 AND 18 INCHES OF REAR SPAR.