What was found
DURING POWER PLANT INSPECTION. ENGINE TRUSS WAS NOTED TO BE CRACKED AT THE LOWER LEFT ENGINE SHOCK MOUNT ATTACH POINT IN THE WELDED AREA (GUSSET TUBE).
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING POWER PLANT INSPECTION. ENGINE TRUSS WAS NOTED TO BE CRACKED AT THE LOWER LEFT ENGINE SHOCK MOUNT ATTACH POINT IN THE WELDED AREA (GUSSET TUBE).