What was found
INSPECTION TYPE:C+SI ENGINE NR 2 AFT MOUNT SUPPORT RIB RIGHT CHORD INSIDE THE VERTICAL FIN HAS CRACKED SUPPORT ANGLE APPROX 17 INCHS FROM TOP OF CHORD. REPLACED CRACKED ANGLE IAW DRAWING NO.65-17553
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION TYPE:C+SI ENGINE NR 2 AFT MOUNT SUPPORT RIB RIGHT CHORD INSIDE THE VERTICAL FIN HAS CRACKED SUPPORT ANGLE APPROX 17 INCHS FROM TOP OF CHORD. REPLACED CRACKED ANGLE IAW DRAWING NO.65-17553