Service difficulty report · Crankcase · Cessna T310R

Difficulty date
May 13, 2022
Submitted
August 19, 2022
Operation
General aviation
Aircraft
N314BB
Make and model
Cessna T310R
Aircraft serial
310R1836
Aircraft time
5,252 hours
Engine
Cont TSIO520BB
Engine time
5,611 hours
Propeller
Hartzl PHCC3YF2
Part
Crankcase
Part number
CASTING642001
Part serial
MATCH9B956PL
Condition
Destroyed
Location
Rh Engine
Component
Engine · Cont · TSIO520BB
Component part number
TSIO520BB
Stage of operation
CR
How discovered
V
Nature of condition
Z, Y, T
Precautionary procedure
A

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

What was found

AFTER CLIMBING TO 12000 FT FROM KCYS, THE AIRCRAFT TRANSITIONED TO CRUISE TO PREPARE FOR AERIAL SURVEY WORK. SHORTLY THEREAFTER, THE RE HAD A VIBRATION, POWER LOSS, AND STOPPAGE. THE AIRCRAFT WAS LANDING BACK AT KCYS WITHOUT INCIDENT. AFTER THE COWLING WAS REMOVED, A HOLE WAS NOTICED IN THE TOP OF THE CASE UNDER THE LH MAGNETO. THE LH MAGNETO WAS BROKEN FROM ITS MOUNT AND THE BEARING SURFACE OF A PISTON ROD COULD BE SEEN PROTRUDING FROM THE CASE. THE CRS THAT HAD OVERHAULED THE ENGINE 142.5 HOURS AGO REMOVED THE ENGINE FROM THE AIRCRAFT AND TRANSPORTED THE ENGINE TO THEIR FACILITY FOR TEARDOWN/INVESTIGATION. TEARDOWN OF THE ENGINE REVEALED THAT THE #2 CRANK BEARING (BETWEEN #2 AND #3) OIL JOURNAL PASSAGE WAS OBSTRUCTED BY A FOREIGN OBJECT. THE OBJECT RESTRICTED OIL FLOW WHICH CAUSED THE BEARINGS TO OVERHEAT, RESULTING IN FAILURE. THE ENGINE CRS NOTED THAT THE CRANKCASE HAD BEEN REPAIRED AT A DIFFERENT CRS. THE ENGINE CRS DID STATE THAT THEIR PROCEDURES REQUIRED THAT EACH OIL JOURNAL WAS REQUIRED TO HAVE A BRUSH RUN THROUGH AND FOR AIR TO BE BLOWN THROUGH. THE CRS STATED THAT IF THE BRUSH HAD BEEN RUN THROUGH THE JOURNAL, THEN THE OBSTRUCTION WOULD HAVE BEEN DISCOVERED.

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