NTSB CAROL · Event
Event LAX83FA122
Registry · N761RG
FAA Aircraft Registry record.
Make / Model
CESSNA T210M
Engine
CONT MOTOR TSIO-520 SER (300 hp)
Seats / Engines
6 seats · 1 engine
Last airworthiness date
19780131
ADS-B equipped
Yes — Mode-S AA46BD
Registrant of record
BAS PART SALES LLC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Factual narrative
THE PILOT HAD FOUND WATER IN THE WING TANKS DURING HIS PREFLT BUT DID NOT DRAIN THE FUEL ACCUMULATOR TANKS AS HE WAS NOT AWARE OF THEIR EXISTENCE. THE ENGINE SPUTTERED AND QUIT AT 100 FT AGL, BUT THE PILOT WAS ABLE TO NEGOTIATE A LANDING ON THE ARPT. EXAMINATION REVEALED EXTENSIVE WATER IN BOTH FUEL TANK ACCUMULATORS, ENGINE DRIVEN FUEL PUMP OUTLET LINE TO THE FUEL SERVO AND THE FUEL MANIFOLD INLET LINE. THE CESSNA 210 OWNERS MANUAL STATES THAT IF WATER IS FOUND IN THE WING TANKS, THE ACCUMULATOR TANKS MUST BE DRAINED UNTIL THE WATER IS ELIMINATED. BOTH ACCUMULATOR TANKS ON THE ACFT WERE CAPPED WITH A QUICK REMOVAL TYPE CAP. THE EXTENDED ACCUMULATOR TANK DRAIN FITTINGS WERE NOT INSTALLED. LATER MODEL CESSNA 210 ACFT HAVE THE EXTERIOR DRAINS INSTALLED. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1983_LAX83FA122.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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