Service difficulty report · Spark Plug · Beech P35

Difficulty date
September 23, 2026
Submitted
September 25, 2026
Operation
General aviation
Aircraft
N1721G
Make and model
Beech P35
Aircraft serial
D6944
Aircraft time
3,464 hours
Engine
Cont IO470N
Engine time
349 hours
Part
Spark Plug
Part number
URHB32S
Condition
Separation
Location
Nr 4 Cylinder
Part time
60 hours
Stage of operation
CR
How discovered
O
Nature of condition
R, E
Precautionary procedure
B, A

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

What was found

DURING CRUISE FLIGHT, THE AIRCRAFT EXPERIENCED AN IMMEDIATE PARTIAL LOSS OF ENGINE POWER ACCOMPANIED BY SEVERE ENGINE ROUGHNESS. AN EMERGENCY WAS DECLARED, AND THE AIRCRAFT LANDED SAFELY WITHOUT FURTHER INCIDENT. POST-FLIGHT MAINTENANCE INSPECTION REVEALED THAT THE NR 4 CYLINDER BOTTOM AVIATION SPARK PLUG, A TEMPEST URHB32S (FINE WIRE, LOT CODE 11WA), SUFFERED A CATASTROPHIC STRUCTURAL FAILURE. THE SPARK PLUG COMPLETELY SEPARATED BETWEEN THE PLUG'S SEAT ASSEMBLY AND THE HEXAGONAL NUT IN FLIGHT. THE REMAINING PLUGS FROM THE SAME LOT CODE ARE BEING REMOVED FROM SERVICE. THE CYLINDER THREADS AND INTERIOR ARE UNDERGOING A BORESCOPE INSPECTION FOR SECONDARY MECHANICAL OR THERMAL DAMAGE.

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