Service difficulty report · Thru Bolt

Difficulty date
December 17, 2007
Submitted
December 28, 2007
Operation
General aviation
Engine
Cont IO520C
Part
Thru Bolt
Part number
SA6419311075
Condition
Broken
Location
Crankcase
Stage of operation
IN
How discovered
V
Nature of condition
O
Precautionary procedure
K

As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.

What was found

INSTALLING ALL NEW SA641931-10.75 LOT NR K070059179, REV E THRU BOLTS IN ENGINE. AFTER TORQUE, WITHIN A FEW HOURS THE THRU BOLT SNAPPED, AT THE OIL RING GROOVE. THIS IS THE THIRD THRU BOLT THAT HAS SNAPPED AFTER TORQUE, AND SETTING. PROBABLE CAUSE, IS IMPROPER HEAT TREATING DURING OR AFTER PLATING. (K)