SDR 2015F00077

Service difficulty report · Filter Adapter · Cessna 402C

Difficulty date
June 12, 2015
Submitted
June 12, 2015
Operation
General aviation
Filed by
8PCR980B
Pinnacle Aircraft Engines LLC
Make and model
Cessna 402C
Engine
Cont TSIO520VB
Engine time
3,649 hours
Part
Filter Adapter
Part number
653491
Condition
Cracked
Location
Engine Oil Pump
Part time
3,649 hours
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

ENGINE RECEIVED FOR OVERHAUL; 3649.4 HOURS SFRM. OIL FILTER ADAPTER WAS FOUND TO BE CRACKED DURING ROUTINE INSPECTION AT ENGINE REPAIR. THE CRACK WAS LOCATED AT LOWER LEFT MOUNTING STUD BORE SPOT-FACE AT THE 10 O'CLOCK POSITION. IT APPEARS THAT THE CRACK ORIGINATED AT A SHARP EDGE, CREATED WHEN THE SPOT-FACING OPERATION WAS PERFORMED DURING PART MANUFACTURE. TOTAL CRACK LENGTH WAS APPROXIMATELY 2 INCHES. THE CRACK HAD PENETRATED INTO THE OIL PRESSURE CHAMBER OF THE ADAPTER. THIS AREA SHOULD BE CHECKED FOR A CRACK, ESPECIALLY IF A SHARP EDGE AS DESCRIBED ABOVE IS PRESENT. SHARP EDGES IN THIS LOCATION SHOULD BLENDED SMOOTH TO PREVENT A STRESS RISER IN THE ALUMINUM CASTING.

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