NTSB CAROL · Event
Event LAX97LA035
Registry · N207YK
FAA Aircraft Registry record.
Make / Model
S C AEROSTAR S A YAK-52
Year of manufacture
1996 · 0 years old at event
Engine
VEDENEYEV M14P (350 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
20141105
ADS-B equipped
Yes — Mode-S A1AE34
Registrant of record
GRIFA NATHANIEL ARICK
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
loss of engine power due to an undetermined internal carburetor malfunction. A factor relating to the accident was: the directions that were use for reassembly of the aircraft were written only in Russian.
Factual narrative
On November 1, 1996, at 1200 hours Pacific standard time, an Aerostar SA Yak 52, N207YK, collided with an airport building and a perimeter fence during a rejected takeoff attempt at the Fullerton Municipal Airport, Fullerton, California. The rejected takeoff was precipitated by a loss of engine power just after liftoff. Visual meteorological conditions prevailed at the time and no flight plan was filed. The aircraft sustained substantial damage. The certificated commercial pilot was not injured. The flight originated at the time of the accident as a local area test flight. The aircraft is a new production airplane which was manufactured in Romania, then shipped in a crate to the United States. This was the first flight following reassembly of the aircraft. According to the pilot, the aircraft had been run on the ground for 50 minutes and had completed a high speed taxi test. Following liftoff from runway 24, the engine quit as the aircraft reached 50 feet in altitude. The pilot landed on the runway, but had insufficient pavement to stop prior to colliding with a building and a fence at the departure end of the runway. In a telephone interview, the pilot reported that the airplane has a 9-cylinder radial engine with a pressure carburetor. He believed that the carburetor malfunctioned. The aircraft was examined by an Federal Aviation Administration (FAA) airworthiness inspector from the Long Beach, California, Flight Standards District Office. The inspector reported that a Russian factory trained technician came from another importer of the aircraft and provided technical assistance. During examination of the airplane, the carburetor was removed from the engine and another serviceable one installed in it's place. The engine was then started and exercised through the normal power range with no problems noted. The technician stated that disassembly of the carburetor requires special tools available only at the factory. The inspector reported that the directions for disassembling the aircraft are used as a checklist/reference for reassembling the aircraft, and that the directions are written only in Russian. The Russian tech from San Diego said that ". . . the factory did not do one or two steps on the checklist." The aircraft was a new production airplane, which was manufactured in Romania, then was disassembled and shipped in a crate to the United States. This was the first flight following reassembly of the aircraft. The aircraft had been run on the ground for 50 minutes, and a high speed taxi test had been completed. Shortly after takeoff, a loss of engine power occurred. The pilot landed on the runway, but insufficient runway was remaining to stop before colliding with a building and a fence at the departure end of the runway. The powerplant was a Russian manufactured 9-cylinder radial engine with a pressure carburetor. The pilot said he believed that the carburetor malfunctioned. The aircraft was examined by an FAA airworthiness inspector with the assistance of a Russian factory trained technician. The carburetor was removed from the engine and a used/serviceable one was installed in its place. The engine was then started and exercised through the normal power range with no problem noted. The technician stated that disassembly of the carburetor required special tools available only at the factory. The inspector reported that the directions for disassembling the aircraft were used as a checklist/reference for reassembling the aircraft, and that the directions were written only in Russian. The Russian technician said that '. . . the factory did not do one or two steps on the checklist.' Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1996_LAX97LA035.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). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- 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 …
- arXiv 2023 · arXiv preprint
Automating Bird Diverter Installation through Multi-Aerial Robots and Signal Temporal Logic Specifications
This paper tackles the task assignment and trajectory generation problem for bird diverter installation using a fleet of multi-rotors.
- arXiv 2023 · arXiv preprint
Variation of Critical Crystallization Pressure for the Formation of Square Ice in Graphene Nanocapillaries
Two-dimensional square ice in graphene nanocapillaries at room temperature is a fascinating phenomenon and has been confirmed experimentally.
- arXiv 2023 · arXiv preprint
Polycrystallinity enhances stress build-up around ice
Damage caused by freezing wet, porous materials is a widespread problem, but is hard to predict or control. Here, we show that polycrystallinity makes a great difference to the stress build-up process…
- arXiv 2022 · arXiv preprint
Enhanced Prediction of Three-dimensional Finite Iced Wing Separated Flow Near Stall
Icing on three-dimensional wings causes severe flow separation near stall. Standard improved delayed detached eddy simulation (IDDES) is unable to correctly predict the separating reattaching flow due…
- Embry-Riddle Scholarly Commons 2021 · Journal article (JAAER)
Analysis on the Negative Emotional, Physiological, and Cognitive Responses Elicited from of the Activation of a Stall Alarm
Failing to identify an aerodynamic stall can lead to the inability of an aircraft to sustain flight. To warn pilots of an impending or fully-developed stall, many aircraft have safety devices installe…
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