What was found
DURING ROUTINE INSPECTION A CRACK WAS DISCOVERED THROUGH THE STRENGTHENING RIB OF THE MOUNTING FLANGE. CRACK DEVELOPMENT IS A VERY COMMON FAILURE FOR THIS PART. SUGGEST A MORE ROBUST MATERIAL SUCH AS SS OR TITANIUM BE UTILIZED. (K)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING ROUTINE INSPECTION A CRACK WAS DISCOVERED THROUGH THE STRENGTHENING RIB OF THE MOUNTING FLANGE. CRACK DEVELOPMENT IS A VERY COMMON FAILURE FOR THIS PART. SUGGEST A MORE ROBUST MATERIAL SUCH AS SS OR TITANIUM BE UTILIZED. (K)