What was found
AT CYLINDER REPLACEMENT, FOUND PRIMER LINES NR 1, NR 3 CYLINDERS CRACKED (3/4 AROUND) UNDER ADEL CLAMP AREA. EVIDENCE OF FATIGUE AND CORROSION. (X)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AT CYLINDER REPLACEMENT, FOUND PRIMER LINES NR 1, NR 3 CYLINDERS CRACKED (3/4 AROUND) UNDER ADEL CLAMP AREA. EVIDENCE OF FATIGUE AND CORROSION. (X)