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ERA24LA195

2024-04-27 · Dunbar, Pennsylvania, United States · None · 1 aircraft · Status: Completed

Airport VVS

Current FAA registration · N601DR

Make / Model
ZENITH ZODIAC 601 XL
Year of manufacture
2015 · 9 years old at event
Engine
AMA/EXPR UNKNOWN ENG
Seats / Engines
2 seats · 1 engine
Last airworthiness date
20150512
ADS-B equipped
Yes — Mode-S A7CB51

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

A total loss of engine power as a result of an improperly fabricated fuel-air mixture cable bracket. Contributing was the pilot’s decision to fly the airplane with a known mechanical engine issue, and the presence of another airplane that was back taxiing on the runway while the pilot was attempting to maneuver the airplane for landing.

Factual narrative

The pilot reported that the purpose of the flight was to test cooling plenum changes that he had recently made to the experimental amateur-built airplane’s automotive conversion engine. After takeoff on the planned flight in the airport traffic pattern, the pilot heard over the radio that another airplane was inbound to the airport for touch-and-go landings, so he flew away from the airport and performed ground reference maneuvers. Shortly after, the pilot returned to the traffic pattern, entering on the upwind leg. Upon turning onto the crosswind leg, his engine began to “sputter”, so he made a 180° turn to land on the opposite direction of the same runway. About that time, he noticed that the other airplane was back taxiing on the runway. He elected to not land on the parallel taxiway due to its condition and out of concern for a possible collision with another aircraft. The pilot overflew the other airplane on the runway, and shortly thereafter his airplane’s engine lost power completely as he neared the end of the runway. About that time the pilot was turning the airplane left, but could feel it slowing, so he leveled the wings and landed straight ahead, perpendicular to the runway. The airplane subsequently traveled over a grass embankment and contacted trees, resulting in substantial damage to the right wing and fuselage structure. The pilot stated that following the accident, an examination of the engine revealed that a bracket for the fuel/air mixture cable had “bent and overextended,” which resulted in the engine’s fuel/air mixture becoming excessively lean. The pilot stated that he had fabricated the bracket during a recent engine replacement and knew that a new bracket would need to be refabricated but had not completed the task it before the accident flight. Based on this information, it is likely that the loss of engine power was the result of the improperly fabricated bracket, which resulted in an excessively lean mixture to the airplane’s engine. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12

NTSB Findings

FAA avdata. C = Cause, F = Factor.

  • — Aircraft-Aircraft power plant-Engine controls-Mixture control-Design
  • — Personnel issues-Task performance-Maintenance-Fabrication-Pilot
  • — Personnel issues-Action/decision-Info processing/decision-Decision making/judgment-Pilot
  • — Environmental issues-Physical environment-Object/animal/substance-Aircraft-Contributed to outcome

Verbatim from NTSB's published report. Source file NTSB_2024_ERA24LA195.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.