Service difficulty report · Crankcase · Beech A36

Difficulty date
March 5, 2019
Submitted
July 30, 2019
Operation
General aviation
Aircraft
N871CS
Make and model
Beech A36
Aircraft serial
E2291
Aircraft time
2,058 hours
Engine
Cont IO550B
Engine time
2,058 hours
Part
Crankcase
Part serial
675193
Condition
Cracked
Location
Engine
Part time
2,058 hours
Component
Engine · Cont · IO550B
Stage of operation
CR
How discovered
O
Nature of condition
Y
Precautionary procedure
A

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

What was found

DEPARTED (MEZ) TO (JBR) ON A VFR FLIGHT, EXPERIENCED ROUGH RUNNING ENGINE, LOSS OF OIL PRESSURE, AND SUBSEQUENT ENGINE FAILURE APPROXIMATELY 40 MINUTES INTO THE FLIGHT. THE PILOT LANDED IN AN OPEN FIELD. INVESTIGATION REVEALED THE ENGINE FAILED TO A MAIN BEARING FAILURE THAT RESULTED IN A BROKEN CRANKSHAFT. DURING TEAR DOWN INSPECTION IT WAS NOTED THAT THE MAIN BEARING SADDLE NEAR THE CRANKSHAFT COUNTER WEIGHT APPEARED TO HAVE CRACKED IN THE THROUGH BOLT AREA AND HOLE FOR THE THROUGH BOLT WAS OUT-OF-ROUND WITH THE MATING SURFACES OF THE BEARING SADDLE SHOWED SIGNS OF FRETTING.

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