What was found
INSPECTION FOUND 4 INCH CRACK RUNNING LONGITUDINALLY .3 INCH BELOW CENTER LEFT HAND ENGINE LEG ATTACHMENT BOLT HOLE. SUBMITTER RECOMMENDATIONS TO PREVENT RECURRENCE: INCREASE FOOT PRINT OF CUP P/N 206-032-315-113. (X)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND 4 INCH CRACK RUNNING LONGITUDINALLY .3 INCH BELOW CENTER LEFT HAND ENGINE LEG ATTACHMENT BOLT HOLE. SUBMITTER RECOMMENDATIONS TO PREVENT RECURRENCE: INCREASE FOOT PRINT OF CUP P/N 206-032-315-113. (X)