NTSB CAROL · Event
Event SEA04LA046
Aircraft involved
Probable cause & findings
The pilot's inadequate evaluation of deteriorating weather conditions (increasing rain) and his failure to maintain the proper rate of descent on landing (long/hard touchdown). Contributing factors were carburetor icing conditions and rain.
Factual narrative
On February 28, 2004, at 1553 Pacific standard time, a Jerome Q-2 homebuilt aircraft, N143GJ, registered to and being flown by a private pilot sustained substantial damage during a hard landing at the Portland-Hillsboro airport, Hillsboro, Oregon. The pilot was uninjured. Visual meteorological conditions prevailed and no flight plan had been filed. The flight, which was personal, was operated under 14CFR91 and originated at Hillsboro approximately 1530. The pilot reported that the Revmaster 2100DQ engine, a Volkswagen automobile engine modified for aircraft use, had just undergone maintenance work for a sticking valve and this was the first flight following that maintenance. He departed Hillsboro airport on runway 20 in light drizzle and flew a circuit in the pattern at the airport without problems. While climbing out on the second circuit, the pilot encountered "...heavy rain that obscured my vision...," and shortly thereafter the engine began running rough. The pilot, suspecting carburetor icing, applied carburetor heat. The reduced power condition continued and the pilot was cleared to land on runway 20 by the air traffic control tower. He reported that he executed a rapid descent and subsequently landed hard during which the left canard broke at the fuselage attach point and the aircraft came to rest near the midpoint of the 4,049 foot long asphalt runway (refer to attached NTSB Form 6120.1/2). The aviation surface weather observation for Hillsboro airport reported at 1553 the following meteorological conditions: Ceiling 2,700 foot broken, 3,100 foot overcast, 6 miles visibility in light rain and mist, temperature/dew point 8/6 degrees Celsius respectively and winds from 220 degrees magnetic at 10 knots (refer to Attachment WX-I). The temperature/dew point readings at the time of the accident were consistent with carburetor icing conditions (refer to Attachment CI-I). The pilot reported that the Revmaster 2100DQ engine, a Volkswagen automobile engine modified for aircraft use, had just undergone maintenance work for a sticking valve and this was the first flight for the homebuilt aircraft following that maintenance. He took off in light drizzle, flew one circuit in the pattern and was climbing out for a second approach when he encountered heavy rain. The aircraft's engine began to run rough and the pilot applied carburetor heat but the partial power loss continued. He then received clearance to land and executed a rapid descent to a hard landing coming to rest near the midpoint of the 4,049 foot long asphalt runway. The temperature/dew point at the time of the accident at the site was 8/6 degrees Celsius respectively, and serious carburetor icing conditions existed. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2004_SEA04LA046.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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Related research
What the literature says.
Academic papers and agency reports matching this event's aircraft type or causal vocabulary (icing, maintenance). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- Embry-Riddle Scholarly Commons 2023 · Faculty research project
Reconfigurable Guidance and Control Systems for Emerging On-Orbit Servicing, Assembly, and Manufacturing (OSAM) Space Vehicles
Dynamic response to emergent situations is a necessity in the on-orbit servicing, assembly, and manufacturing (OSAM) field, because traditional on-orbit guidance and control (G&C) cannot respond effic…
- Embry-Riddle Scholarly Commons 2019 · Journal article (IJAAA)
Satellite Maintenance: An Opportunity to Minimize the Kessler Effect
Recently, there has been an emphasis on the growing problem of orbital debris. While the advantages of placing satellites into space are numerous, advances in satellite technology combined with the gr…
- Embry-Riddle Scholarly Commons 2015 · Conference paper
The Implementation of Safety Management Systems in Maintenance Operations
Literature for Safety Management Systems (SMS) that apply to flight operations is abundant, but there is a limited supply of SMS-related literature for maintenance operations.
- Embry-Riddle Scholarly Commons 2026 · Journal article (IJAAA)
From Reactive to Predictive: A hybrid Trust-Mediated Adoption Framework for Data-Driven Maintenance in Distributed-Authority Aviation Environments
Modern aviation maintenance operates within increasingly data-intensive technological environments, yet the operational integration of predictive maintenance into routine decision-making remains incon…
- NASA NTRS 2026 · Contractor Report (CR)
Icing Physics Studies Using the 3D SIDRM Test Article: 2023 Icing Tests Analysis
In-flight icing is an important safety issue and is a factor that affects aircraft design and performance. Newer regulations are driving a need for improvements in airframe and engine icing simulation…
- arXiv 2025 · arXiv preprint
Multi-Agent Deep Reinforcement Learning for UAV-Assisted 5G Network Slicing: A Comparative Study of MAPPO, MADDPG, and MADQN
The growing demand for robust, scalable wireless networks in the 5G-and-beyond era has led to the deployment of Unmanned Aerial Vehicles (UAVs) as mobile base stations to enhance coverage in dense urb…
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