What was found
ON 100 HR INSPECTION, FOUND CRACK ON LOWER NR 2 ALTERNATOR ATTACH POINT. SUSPECT DEFECT CASTING OF PART. RECOMENDATION WOULD BE TO MAKE THE PART FROM BILLET ALUMINUM.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
ON 100 HR INSPECTION, FOUND CRACK ON LOWER NR 2 ALTERNATOR ATTACH POINT. SUSPECT DEFECT CASTING OF PART. RECOMENDATION WOULD BE TO MAKE THE PART FROM BILLET ALUMINUM.