NTSB CAROL · Event
Event LAX00LA266
Registry · N67603
FAA Aircraft Registry record.
Make / Model
BOEING 737-10
Seats / Engines
230 seats · 2 engines
ADS-B equipped
Yes — Mode-S A8F476
Registrant of record
BOEING CO
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's in-flight decision to continue the takeoff and his subsequent delayed decision to abort the takeoff after he noted that the airplane was unable to climb out of ground effect.
Factual narrative
On July 15, 2000, at 1530 hours Pacific daylight time, a Cessna 152, N67603, collided with the airport perimeter fence and nosed over during an aborted takeoff from runway 31L at the Reid-Hillview Airport, San Jose, California. The airplane, operated by Interwings Corp., and rented by the pilot under 14 CFR Part 91, sustained substantial damage. The private pilot and pilot-rated passenger were not injured. Visual meteorological conditions existed for the personal cross-country flight, which was originating at the time of the accident. The flight was scheduled to stop in Sacramento and Napa, California, with a return to the Reid-Hillview airport. No flight plan was filed. In the pilot's written statement to the Safety Board, he stated that the purpose of the cross-country flight was to build up flight time for his commercial certificate. Prior to the flight he performed a weight and balance for the airplane, and noted that the center of gravity was within the manufacturer's specified limits. The pilot stated, "everything was normal" with the preflight and run-up. On the takeoff roll he waited until the airplane had reached 60 knots before he rotated because he had a heavy passenger onboard and wanted to make sure he had enough airspeed for the climb out. After the airplane lifted off the runway, the pilot pulled back on the yoke, but the airplane settled back on the runway. The pilot continued the takeoff and kept the airplane on the ground until the airspeed reached 65 knots. The airplane lifted off the runway and stayed in ground effect and did not climb. The pilot decided at that point to land; however, there was no remaining runway left. He made an attempt to return to land on runway 13R due to houses located off the departure end of the runway. He stated that the airplane did not have the altitude and struck the airport perimeter fence. He stated that he heard the stall warning horn as the airplane collided with the fence. The pilot stated there were no discrepancies with the engine power output; the airplane was just not gaining altitude. A witness to the accident stated that he heard a power reduction during takeoff and observed the airplane in takeoff configuration, but not gaining altitude. After the airplane crossed over the departure end of the runway it was still at a low altitude. He saw the pilot attempt to land straight ahead and then make a left turn to land on runway 13R. The witness stated that the airplane was in a steep bank and low altitude and thought he saw the left wing of the airplane strike the ground. The airplane leveled off and landed in a field. It impacted a ditch and nosed over onto the airport perimeter fence that separates the airport from the Donald J. Meyer Elementary School. No discrepancies were noted with the preflight and weight and balance computations. On the takeoff roll the pilot elected to build up airspeed for the climb out due to a heavy passenger. When the airplane lifted off the ground he pulled back on the yoke, but the airplane settled back onto the runway. He continued the takeoff roll, built up more airspeed, and noted that when the airplane lifted off the runway it stayed in ground effect and did not climb. He noted that there was not enough remaining runway to land and come to a stop safely, and could not land straight ahead due to houses at the departure end. He attempted to return to an opposite runway and heard the stall warning horn as the airplane collided with the airport perimeter fence. The pilot reported no discrepancies with engine power output; the airplane was just unable to gain altitude. A witness heard a power reduction during the initial climb and noted the airplane was not gaining altitude. After crossing over the departure end of the runway at a low altitude, he saw the airplane make a left turn to land on the runway and saw the left wing contact the ground. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2000_LAX00LA266.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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