NTSB CAROL · Event
Event LAX83LA312
Registry · N1WA
FAA Aircraft Registry record.
Make / Model
CIRRUS DESIGN SF50
Year of manufacture
2024
Engine
WILLIAMS FJ33-5A
Seats / Engines
7 seats · 1 engine
Last airworthiness date
20240502
ADS-B equipped
Yes — Mode-S A001F7
Registrant of record
MCNABBVILLE LLC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Factual narrative
THE ACFT WAS ON AN EXTERNAL LOAD OPERATION TO AIRLIFT LOADS OF CEMENT. THE CEMENT WAS BEING POURED FOR BASE PILINGS FOR POWER LINE TOWERS ON ROUGH TERRAIN. WHILE CARRYING A 3100 LB LOAD OF CEMENT ON A 40 FT LINE, THE HELICOPTER HAD JUST MOVED TO A POSITION TO START POURING. WHILE STABLIZED IN A HOVER, THE PLT HEARD 3 COMPRESSOR STALLS. THE HELICOPTER YAWED & BEGAN LOSING ALTITUDE. THE PLT MOVED THE ACFT FORWARD FOR THE SAFETY OF WORKERS BELOW. THE PLT CONTINUED FORWARD, RELEASED THE EXTERNAL LOAD, CONTINUED AN AUTOROTATION INTO A RAVINE & LANDED ON SOFT, UNEVEN GROUND. PRIOR TO TOUCHDOWN, THE HELICOPTER BEGAN MAKING UNCONTROLLABLE TURNS. THE MAIN ROTOR STRUCK A LARGE BOULDER. SHORTLY AFTER LANDING, A FIRE ERUPTED IN THE ENG COMPARTMENT WHICH SUBSEQUENTLY COSUMED THE HELICOPTER. AN EXAM OF THE WRECKAGE, INCLUDING THE ENG, REVEALED NO PREIMPACT, MECHANICAL PROBLEM. THE PINION GEAR OF THE 90 DEG GEAR BOX EXHIBITED SOME BACKLASH WEAR. THE ELEVATION OF THE CRASH SITE WAS APRX 3000 FT. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1983_LAX83LA312.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…
Browse the full corpus — academia portal ↗