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WPR24FA226

2024-07-06 · Eatonville, Washington, United States · Fatal · 1 aircraft · Status: In work

Airport 2W3

Current FAA registration · N3464D

Make / Model
CHAMPION 7GCBC
Year of manufacture
1969 · 55 years old at event
Engine
LYCOMING 0-290 SERIES (140 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
19860506
ADS-B equipped
Yes — Mode-S A3D680

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Factual narrative

On July 6, 2024, at about 2122 Pacific daylight time, a Champion 7GCBC, N3464D, was substantially damaged when it was involved in an accident near Swanson Airport (2W3), Eatonville, Washington. The pilot and passenger were fatally injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight. A witness, who was located about 500 ft southwest of the departure end of runway 16 at 2W3, stated that he heard the airplane perform an engine run-up and then take off. The airplane overflew his location at an altitude that was lower than he expected. The witness added that after the airplane flew out of his line of sight, he heard the airplane’s engine “cut out,” followed by the sound of a crash. Two additional witnesses, who were about 1,900 ft northwest of the accident site, observed the accident airplane flying southbound. Both witnesses described the airplane as being about 10 ft above the treetops and lower than an adjacent ridgeline. The witnesses said that the airplane was slow as it maintained a nose high attitude, and the engine was producing smooth and continuous power. The airplane then performed a turn to the left, rolled inverted, and disappeared out of their line of sight below a tree canopy. The witnesses added that the sound of the engine stopped before the airplane impacted the trees. Figure 1: The location of the witnesses with a depiction of the airplane’s approximate flight path. The airplane came to rest in a nose down attitude within a forested area about 0.5 nm south of the departure end of runway 16. All major components of the airplane were accounted for at the accident site. The airplane exhibited extensive impact damage and aft crush deformation to the forward portion of the fuselage and leading edges of both wings. The wings remained partially attached to the fuselage and the tail section was folded upward and to the left. Both the engine and propeller were buried in the ground beneath the wreckage. The accident site was at an elevation of 803 ft mean sea level (msl), with rising mountainous terrain located to the south and east that varied in elevation between 1,200 ft and 1,400 ft msl. Figure. 2: A depiction of the terrain around the accident site. The wreckage was recovered to a secure location for further examination. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12

NTSB Findings

FAA avdata. C = Cause, F = Factor.

  • — Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Angle of attack-Capability exceeded
  • — Personnel issues-Task performance-Use of equip/info-Aircraft control-Pilot
  • — Aircraft-Aircraft oper/perf/capability-Aircraft capability-Climb capability-Capability exceeded
  • — Environmental issues-Physical environment-Object/animal/substance-Tree(s)-Contributed to outcome

Verbatim from NTSB's published report. Source file NTSB_2024_WPR24FA226.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.