NYC03LA108
2003-05-15 · Gaithersburg, Maryland, United States · None · 1 aircraft · Status: Completed
Airport GAI
Current FAA registration · N1514X
- 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
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
Matched on aircraft type or causal vocabulary (stall). All research papers
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- 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…