Service difficulty report · Spark Plug · Beech 76

Difficulty date
July 2, 2005
Submitted
August 3, 2005
Operation
General aviation
Make and model
Beech 76
Aircraft time
12,809 hours
Engine
Lyc LIO360A1G6
Part
Spark Plug
Part number
URHM38E
Condition
Cracked
Location
Engine
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

DURING ROUTINE SCHEDULED 100 HR, 1 SPARK PLUG APPEARED BENT WHILE INSTALLED IN CYLINDER. UPON REMOVAL, CONFIRMED BY INSPECTION THAT SPARK PLUG BODY HAD SEPARATED AT NECKED DOWN AREA OF METAL BODY OF PLUG ON IGNITION LEAD SIDE OF GASKET SEALING SURFACE. AFFECTED AREA APPEARED TO HAVE OVERHEATED AND METAL WAS DISCOLOURED, METAL OVERHEATING RESULTED IN CRACK. ALL PWGS INSPECTED, ONE OTHER FOUND WITH OVERHEATING BUT NOT CRACKED, BOTH REPLACED. OVERHEATING NOT CAUSED BY ENG CONDITION, SUGGEST MANUFACTURER DEFECT. SLOWLY PHASING OUT THE USE OF AUTOLITE SPARK PLUGS TO AVOID SIMILAR SITUATIONS, PLUGS ARE BEING INSPECTED FLEETWIDE FOR THIS CONDITION DURING SCHEDULED MX AND SWITCHING TO CHAMPION BRAND.

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