NTSB CAROL · Event
Event LAX02LA062
Registry · N83517
FAA Aircraft Registry record.
Make / Model
PIPER PA-18-150
Seats / Engines
2 seats · 1 engine
Last airworthiness date
19770118
ADS-B equipped
Yes — Mode-S AB6D88
Registrant of record
AIR ADS INC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot failed to maintain directional control resulting in an inadvertent ground loop. A contributing factor was the tailwind.
Factual narrative
On January 5, 2002, about 1040 Pacific standard time, a Piper PA-18-150, N83517, ground looped at Reno-Tahoe Airport (RNO), Reno, Nevada. The private pilot/owner was operating the airplane under the provisions of 14 CFR Part 91. The pilot, the sole occupant, was not injured; the airplane sustained substantial damage. The personal local flight departed Reno about 1015. Visual meteorological conditions prevailed, and no flight plan had been filed. The pilot said he made one successful touch-and-go landing. About 300 feet from touchdown, he noticed he was experiencing a quartering left tailwind. He considered performing a wheel landing with partial flaps, but decided to make a full stall landing with full flaps. The touchdown was good, but during the landing roll the airplane began to veer to the right. He applied left rudder, but got no response. He then applied more left rudder and some left brake. The airplane immediately veered left at an angle of 45 degrees to the runway centerline. He reacted with right rudder and brake and the airplane turned to the right so that it was pointed 30 degrees to the right of the centerline. As the airplane reached the centerline, the airplane ground looped. The left axle broke and the left spar sustained substantial damage. The airplane ground looped during routine pattern work. The pilot made one successful touch-and-go landing. About 300 feet from touchdown, he noticed he was experiencing a quartering left tailwind. He considered performing a wheel landing with partial flaps, but decided to make a full stall landing with full flaps. The touchdown was good, but during the landing roll the airplane began to veer to the right. He applied left rudder, but got no response. He then applied more left rudder and some left brake. The airplane immediately veered left at an angle of 45 degrees to the runway centerline. He reacted with right rudder and brake and the airplane turned to the right so that it was pointed 30 degrees to the right of the centerline. As the airplane reached the centerline, the airplane ground looped. The left axle broke and the left spar sustained substantial damage. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2002_LAX02LA062.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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