Service difficulty report · Cylinder · Cessna 180A

Difficulty date
March 5, 2015
Submitted
August 5, 2015
Operation
General aviation
Make and model
Cessna 180A
Aircraft time
4,067 hours
Engine
Cont IO470D
Part
Cylinder
Part number
AEC631397TISN70
Condition
Delaminated
Location
Inside Barrel
Part time
252 hours
Stage of operation
IN
How discovered
9
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

(CAN) DURING A ROUTINE INSPECTION, HIGH METAL CONTENT FOUND IN ENGINE OIL SCREEN. CONTINUED INSPECTION OF THE ENGINE FOUND CYLINDER NR 4 NOT ABLE TO OBTAIN HIGHER THAN 10 PSI ON A COMPRESSION TEST. PRIMARY LOSS OF COMPRESSION OBSERVED FROM CRANKCASE BREATHER, PISTON RINGS. CYLINDER NR 4 REMOVED TO INVESTIGATE FURTHER. IT WAS OBSERVED THAT THE NICKEL/CARBIDE FINISH OF THE CYLINDER BARREL HAS DELAMINATED FROM THE CYLINDER WALL. IT WAS DETERMINED THAT THE CYLINDER WAS THE SOURCE OF THE METAL FOUND IN THE OIL SCREEN. LOSS OF MATERIAL FROM CYLINDER WALL WARRANTED FURTHER INSPECTION TO EVALUATE DAMAGE TO THE REST OF THE ENGINE AND ASSOCIATED COMPONENTS FOR CONTAMINATION. ENGINE REMOVED AND SENT TO O/H FACILITY FOR A DETAILED INSPECTION. DISASSEMBLY AND INSPECTION CONCLUDED THAT THE CONTAMINATION RESULTED IN DAMAGE TO THE PISTON, FROM SUBJECT CYLINDER, OIL PUMP ASSEMBLY, MAIN AND CONNECTING ROD BEARINGS. IT WAS ALSO ADVISED THAT ALL OTHER ENGINE OIL SUBJECTED ITEMS BE SENT FOR INSPECTION/FLUSH, PROP, GOVERNOR, OIL COOLER.

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