As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
GJT - RIGHT ENGINE TRUSS MOUNT CRACKED NEAR WELD AT UPPER OUTBOARD ATTACH POINT. AREA ''A''. CRACKED AT TYPICAL LOCATION AS IDENTIFIED IN AD 95-02-18, BEECH SB NR 2255 R6. REMOVED AND REPLACED THE TRUSS ASSEMBLY. THE REPETATIVE INSPECTIONS REQUIRED BY AD 95-02-18 ARE NOW TERMINATED BY INSTALLATION OF TRUSS P/N 129-910047-17. THE NEW TRUSS WILL BE DUE MAGNETIC PARTICLE INSPECTIONS AT 8,000 HOUR INTERVALS. (X)