NTSB CAROL · Event
Event NYC83FA171
Registry · N90DD
FAA Aircraft Registry record.
Make / Model
PIPER PA-32-300
Engine
LYCOMING IO-540 SER (300 hp)
Seats / Engines
6 seats · 1 engine
Last airworthiness date
19790227
ADS-B equipped
Yes — Mode-S AC6D22
Registrant of record
BAS PART SALES LLC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Factual narrative
THE CARBURETOR HAD BEEN PREVIOUSLY REMOVED & REWORKED, THEN WAS REINSTALLED. AFTER THE INSTALLATION, WHICH INCLUDED A LEAK CHECK, THE PLT GOT INTO THE LEFT FRONT SEAT & THE PASSENGER/MECHANIC GOT INTO THE RIGHT FRONT SEAT. THE PLT PRIMED THE ENG, THEN MADE A START. AFTER STARTING, THE ENG RAN FOR APRX 20 SECONDS, THEN STOPPED. THE OCCUPANTS DISCUSSED THE PROBLEM & DECIDED THAT THE FUEL LINE WAS PROBABLY 'AIR BOUND.' A DECISION WAS MADE TO KEEP THE ENG RUNNING BY USING THE PRIMER. AFTER RESTARTING, THE ENG CONTINUED TO RUN, BY USE OF THE PRIMER, FOR 30 TO 40 SEC, THEN THE PLT OBSERVED A FIRE IN THE LOWER RIGHT CORNER OF THE COCKPIT. THE OCCUPANTS EVACUATED THE BURNING PLANE, BUT THE PLT FELL & THE PASSENGER RETURNED TO HELP. AT ABOUT THAT TIME, THE RIGHT WING TANK EXPLODED & BOTH OCCUPANTS WERE BURNED. AN EXAM REVEALED THAT THE MAIN FUEL LINE FROM THE GASCOLATOR TO THE CARBURETOR HAD BROKEN. THE PLT DIED TWO DAYS LATER. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1983_NYC83FA171.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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