What was found
CRACK IN WHEEL HALF (INNER) ALONG FLANGE APPROXIMATELY 3 INCHES LONG, P/N 3-1372, S/N 0217. RECOMMENDED INSPECT WHEEL HALF FLANGES FOR CRACKS PERIODICALLY USING DYE PENETRANT METHOD. RIGHT MAIN LANDING GEAR. ACFT TT: 3718.3 HOURS.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK IN WHEEL HALF (INNER) ALONG FLANGE APPROXIMATELY 3 INCHES LONG, P/N 3-1372, S/N 0217. RECOMMENDED INSPECT WHEEL HALF FLANGES FOR CRACKS PERIODICALLY USING DYE PENETRANT METHOD. RIGHT MAIN LANDING GEAR. ACFT TT: 3718.3 HOURS.