What was found
DURING A SCHEDULED AD92-06-09 AREA 'A' INSPECTION OF THE LEFT ENGINE MOUNT TRUSS ASSEMBLY REVEALED A .300 INCH CRACK IN THE TOP OF THE OUTBOARD FORWARD UPPER COWL ATTACH BRACKET. THE CRACK WAS REPAIRED BY WELDING.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING A SCHEDULED AD92-06-09 AREA 'A' INSPECTION OF THE LEFT ENGINE MOUNT TRUSS ASSEMBLY REVEALED A .300 INCH CRACK IN THE TOP OF THE OUTBOARD FORWARD UPPER COWL ATTACH BRACKET. THE CRACK WAS REPAIRED BY WELDING.