SDR 98ZZZX2185

Service difficulty report · Cylinder · Beech 58

Difficulty date
May 24, 1998
Submitted
March 26, 2000
Operation
Air carrier
Aircraft
N5565D
Make and model
Beech 58
Aircraft serial
TH1552
Engine
Cont IO550C
Part
Cylinder
Condition
Cracked
Location
Cylinder Head
Part time
880 hours
Stage of operation
IN
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

SEVENTY HOURS AGO, THIS ENGINE HAD TWO CRACKED CYLINDER HEADS. THE CRACKS WERE IN THE AREA BETWEEN THE TOP SPARK PLUG HOLE AND THE FUEL INJECTOR BOSS. THIS INSPECTION SHOWED ANOTHER CRACK. THE OPPOSITE ENGINE HAD FOUR CRACKED HEADS AT THIS TIME AND ONE CRACKED HEAD PREVIOUSLY. ALL CRACKS WERE NEARLY IDENTICAL. TCM'S ANALYTICAL INSPECTION REVEALED THE CRACK STARTED IN THE AREA BEHIND (AS YOU FACE THE CRANKSHAFT WITH THE CYLINDER INSTALLED) THE FUEL INJECTOR BOSS. ALL CRACKED HEADS WERE DATE STAMPED 3-95 ON A ROCKER ARM SHAFT SUPPORT AND HAD 'REV K' CAST INTO THE HEAD. THE PREVIOUS ENGINES ON THIS AIRCRAFT RAN TO 1,675 HOURS WITHOUT PROBLEMS. THE AFFECTED ENGINES WERE FACTORY REBUILT.

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