NTSB CAROL · Event
Event SEA96LA126
Aircraft involved
Probable cause & findings
failure of the electrically driven hydraulic pump; and the absence of the main landing gear over-center downlock springs, which were not installed by the previous owner/builder.
Factual narrative
On June 18, 1996, approximately 1915 hours mountain daylight time, a homebuilt Price Berkut, N538AJ, registered to and being flown by a private pilot, was substantially damaged when the landing gear collapsed on landing roll on runway 18 at the Jackson Hole airport, Jackson, Wyoming. The pilot was uninjured. No flight plan was in effect and visual meteorological conditions existed at the time. The flight, which was personal, was to have been operated under 14CFR91, and originated from Sioux City, Iowa, approximately 1500. The pilot reported that approaching the Jackson Hole airport while in turbulence the landing gear "transition" light (indicating hydraulic pump operation) illuminated even though the gear was presumed to be retracted. When the pilot attempted to lower the landing gear they remained retracted. He then manually lowered the gear and the nose landing gear green "down and locked" light illuminated but the corresponding main gear lights did not. The pilot attempted side load maneuvers and high "G" pull-ups to attempt to lock the main landing gear without success and the corresponding main gear green lights remained out. He then executed an approach and landing during which the main landing gear collapsed on rollout and the aircraft impacted several runway light during the subsequent ground slide. The pilot reported in a subsequent telephone conversation that the electrically driven hydraulic motor which operates the landing gear had burned out. Additionally, he reported that the over-center downlock springs which insure the main landing achieving a down-and-locked condition when the hydraulic system has failed, were not installed in the aircraft by the owner/builder from whom he purchased the aircraft. The pilot submitted only pages 1 through 4 of the NTSB Form 6120.1/2 and did not include a narrative history of flight. As the pilot approached his destination, the landing gear 'transition' light illuminated indicating operation of the hydraulic pump, although the landing gear was still retracted. When the pilot lowered the landing gear, they failed to extend. He then manually lowered the gear, but was unable to obtain green 'down and locked' indicator lights for the main gear. During the landing, the main gear collapsed, and the aircraft impacted several runway lights. Postcrash examination revealed that the electrically driven hydraulic pump had burned out. Additionally, the over-center downlock springs, which were to assist in manually locking the gear into a down-and-locked condition during manual extension, had never been installed by the builder/previous owner. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1996_SEA96LA126.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 (stall, turbulence). 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 2021 · Journal article (IJAAA)
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When dealing with CFD simulations the turbulent nature is seen on most of the engineering flows and these flows need to be solved.
- arXiv 2020 · arXiv preprint
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- NASA NTRS 2019 · Conference Paper
Prediction of stall and post-stall behavior of airfoils at low and high Reynolds numbers
An interactive boundary-layer method, together with the e(super n)-approach to the calculation of transition, has been used to predict the stall and post-stall behavior of airfoils at low and high Rey…
- arXiv 2026 · arXiv preprint
Direct Numerical Simulations of Ice-Ocean Boundary Turbulence
Turbulent heat and freshwater transport at ice-ocean interfaces controls glacier and iceberg melt rates, yet the underlying physics remains poorly constrained.
- NASA NTRS 2026 · Conference Paper
Computational Analysis of Steady State Aerodynamics of Transonic Truss-Braced Wing Configuration in Deep Stall
This study presents a computational investigation of steady state aerodynamics of the Subsonic Ultra-Green Aircraft Research (SUGAR) Transonic Truss-Braced Wing (TTBW) configuration over a wide range …
- Embry-Riddle Scholarly Commons 2025 · Journal article (JAAER)
Political Turbulence and Aviation Safety: A Cross-National Analysis of Political Stability's Effects on Aviation Accidents
To what extent does political stability affect aviation safety? This research aims to link domestic political conditions and public safety through the consideration of aviation accident frequency.
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