NTSB CAROL · Event
Event CEN23LA313
Registry · N34KP
FAA Aircraft Registry record.
Make / Model
PERKINS KENNETH E PIETENPOL
Year of manufacture
2000 · 23 years old at event
Engine
FORD CONVERSION (60 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
20000519
ADS-B equipped
Yes — Mode-S A3BBE4
Registrant of record
ROLLER RICHARD D
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
A loss of engine power due to lead fouling of a spark plug.
Factual narrative
On July 19, 2023, about 0615 central daylight time, an Pietenpol Aircamper airplane, N34KP, was substantially damaged when it was involved in an accident near Gardner, Kansas. The pilot sustained minor injuries. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight. The pilot reported that shortly after takeoff, the engine started “missing” on one cylinder. The pilot reversed course back toward Gardner Municipal Airport (K34), Gardner, Kansas. The airplane was initially able to maintain altitude; however, as he approached the airport, the airplane began to descend. The engine ran rough and then lost all power. The pilot executed a forced landing to a construction site; the airplane nosed over and sustained substantial damage to both wings and the fuselage. A witness reported that he heard the airplane’s engine “cutting out” as the airplane descended to the field and then nosed over after landing. The airplane was equipped with an in-line, four-cylinder, liquid cooled Ford Model A engine with an owner-fabricated, electronic-type ignition system. A postaccident examination of the engine revealed that the No. 3 cylinder spark plug did not produce spark during field test with a Champion spark plug service unit cleaner and tester. Further examination revealed the No. 3 cylinder spark plug’s firing end contained hard cinder-like deposits, consistent with lead fouling when compared to the Champion Aviation Service Manual AV6-R. The spark plug functioned normally after its firing end was cleaned of the deposits. The other three spark plugs exhibited various degrees of lead deposits, but functioned when tested. The pilot reported that he used 100LL aviation fuel in the engine. Review of the engine logbooks revealed that the spark plugs were replaced during the last condition inspection and had accrued about 18.7 hours of service. There were no other preimpact mechanical malfunctions or failures with the engine or airframe that would have precluded normal operation. The pilot reported that shortly after takeoff, the engine started to run rough. The pilot reversed course back toward the departure airport when the roughness increased and then the engine lost all power. The pilot performed a forced landing to a field and the airplane nosed over, which resulted in substantial damage to the wings and fuselage. An examination of the engine revealed that the No. 3 cylinder spark plug’s firing end contained hard, cinder-like deposits, consistent with lead fouling. When tested, the No. 3 cylinder spark plug did not spark; however, after it was cleaned, the spark plug functioned normally. No other mechanical anomalies with the engine or airframe were noted that would have precluded normal operation. The pilot reported that he used 100LL aviation fuel in the engine. It is likely that the loss of power was due to the lead fouling on the No. 3 cylinder spark plug. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
Hierarchical cause / factor breakdown from the FAA bulk avdata database. Each finding tagged C (Cause) or F (Factor).
- — Aircraft-Aircraft power plant-Ignition system-Spark plugs/igniters-Failure
Verbatim from NTSB's published report. Source file
NTSB_2023_CEN23LA313.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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