What was found
INSPECTION FOUND A 1 INCH CRACK IN RT HORIZONTAL UPPER SKIN. THE CRACK WAS LOCATED APPROXIMATELY 15 INCHES OUTBOARD FROM FUSELAGE. THE CRACKED AREA WAS REMOVED AND A FIBERGLASS OVERLAY REPAIR WAS INSTALLED IAW SRM 51-40-9 AND 51-20-3.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1 INCH CRACK IN RT HORIZONTAL UPPER SKIN. THE CRACK WAS LOCATED APPROXIMATELY 15 INCHES OUTBOARD FROM FUSELAGE. THE CRACKED AREA WAS REMOVED AND A FIBERGLASS OVERLAY REPAIR WAS INSTALLED IAW SRM 51-40-9 AND 51-20-3.