NTSB CAROL · Event
Event NYC03LA108
Registry · N1514X
FAA Aircraft Registry record.
Make / Model
PIPER PA-28R-200
Year of manufacture
1975 · 28 years old at event
Engine
LYCOMING IO-360-C1C (200 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
19750618
ADS-B equipped
Yes — Mode-S A0D0E0
Registrant of record
RABIDOU GARY R JR
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot’s failure to maintain airspeed, resulting in an inadvertent stall.
Factual narrative
On May 15, 2003, at 1215 eastern daylight time, a Piper PA-28R-200, N1514X, was substantially damaged while landing at the Montgomery County Airpark, Gaithersburg, Maryland. The certificated private pilot was not injured. Visual meteorological conditions prevailed and no flight plan was filed for the local personal flight conducted under 14 CFR Part 91. According to the pilot, he was conducting touch and go's to runway 14, a 4,201-foot long, 75-foot wide asphalt runway. On the seventh landing, the pilot elected to perform a simulated power-off, "gliding approach," to the runway. While on the downwind leg, abeam the approach end of the runway, the pilot reduced the throttle to 1,000 rpm's, performed the landing checklist, and added one notch of flaps. He then turned on to the base leg at an airspeed of 80 mph. As the turn on to the final approach leg was made, at an altitude of 350 feet agl, the airspeed began to decrease to 70 mph, and the pilot added power. About 1/4-mile short of the runway, the airspeed decreased to 60 mph, "presumably because of loss of 10 knot headwind," and the airplane stalled. The airplane descended into a grass field short of the runway, and came to rest upright. The winds recorded at a nearby airport, about the time of the accident, were from 040 degrees at 5 knots. While on the final approach leg of a simulated forced landing, the airspeed began to decrease to 70 mph, and the pilot added power. About 1/4-mile short of the runway, the airspeed decreased to 60 mph, "presumably because of loss of 10 knot headwind," and the airplane stalled. The airplane descended into a grass field short of the runway, and came to rest upright. The winds recorded at a nearby airport, about the time of the accident, were from 040 degrees at 5 knots. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2003_NYC03LA108.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 ↗