LAX00LA204
2000-05-24 · TONOPAH, Nevada, United States · None · 1 aircraft · Status: Completed
Airport KTPH
Current FAA registration · N3700T
- Make / Model
- PIPER PA-28R-180
- Engine
- LYCOMING I0360 SER (180 hp)
- Seats / Engines
- 4 seats · 1 engine
- Last airworthiness date
- 19670701
- ADS-B equipped
- Yes — Mode-S A43635
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's failure to attain the proper rotation airspeed during initial takeoff and his improper aborted takeoff procedures.
Factual narrative
On May 24, 2000, at 0930 hours Pacific daylight time, a Piper PA-28R-180, N3700T, landed hard after an aborted takeoff during initial climb at Tonopah, Nevada. The commercial pilot and his passenger were not injured. The airplane owned and operated by the pilot, sustained substantial damage during the hard landing. The pilot did not file a flight plan, and the airplane was being flown under the provisions of 14 CFR Part 91. The pilot was destined for Willits, California, when the accident occurred. Visual meteorological conditions prevailed at the time of the accident. The pilot stated that he departed Willits at 0630, and continued on to Tonopah where he landed on runway 33. He described the winds at the time as "light." He said he taxied to the fuel pump and topped off the fuel tanks. After refueling the airplane, he taxied to runway 33 for departure. He stated he did a run-up and magneto check, which appeared to be normal. He said he taxied onto the active runway approximately 0930. He said the winds were light and the temperature was about 70 to 75 degrees. On the takeoff roll he said he pulled the airplane off prematurely as the airplane felt "like it was in ground effect." The pilot said at that point, he felt he needed to abort the takeoff to prevent a stall. He said the airplane dropped several feet onto the concrete runway, damaging the main gear and wings. The pilot told investigators that he did not have an engine problem but that the takeoff seemed "mushy." A hard landing ensued when the pilot aborted the takeoff just after liftoff from the runway. According to the pilot, he had just refueled his airplane following a cross-country flight to the accident airport. The engine run-up and magneto check before takeoff was normal. As he taxied onto the runway, he noted that the winds were light and temperature was in the 70's. The pilot said that during the takeoff roll, he believed he pulled the airplane off the runway prematurely, as the airplane felt like it was in ground effect. He aborted the takeoff to prevent the airplane from stalling, and the airplane dropped several feet onto the runway, damaging the wings and main gear. The pilot stated there were no engine malfunctions during the flight. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2000_LAX00LA204.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
Search this event elsewhere
External sources are reported, not agency: signal that something happened, not fact about what happened.
- TallyAero Live Wire Aviation press
- NTSB CAROL Agency ↗
- NTSB Docket Agency ↗
- Aviation Safety Network Aviation press ↗
- Kathryn's Report Aviation press ↗
- Aviation Herald Aviation press ↗
- AVweb Aviation press ↗
- Pilots of America Community ↗
- Reddit /r/flying Community ↗
- FlightAware Aviation press ↗
- AOPA accident database Aviation press ↗
- Google News News ↗
- DuckDuckGo News ↗
Related research
Matched on aircraft type or causal vocabulary (stall). All research papers
- 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…