NTSB CAROL · Event
Event LAX02LA064
Aircraft involved
Probable cause & findings
the pilot's failure to maintain an adequate airspeed while maneuvering in an attempt to gain altitude, which resulted in an inadvertent stall/mush. The high density altitude was a factor in the accident.
Factual narrative
On January 11, 2002, at 1320 Pacific standard time, a Piper PA-22-108, N4895Z, collided with the ground during the takeoff initial climb near Tehachapi, California. The personal flight was operated by the pilot/owner under the provisions of 14 CFR Part 91. The airplane was substantially damaged; the private pilot and passenger received minor injuries. Visual meteorological conditions prevailed, and no flight plan had been filed. The flight originated about 1310, and was destined for Scottsdale, Arizona. According to a sheriff's deputy, who witnessed the accident, the airplane departed runway 29, and barely cleared power lines during the initial climb. The airplane performed two 360-degree turns south of the airport and stalled, impacting in a field about 4,200 mean sea level (msl). The airport is located at 3,993 feet msl. Post accident examination by a Federal Aviation Administration inspector determined that the fuel tanks were full at the time of departure. The density altitude was calculated about 5,000 feet msl. The pilot reported that there were no mechanical malfunctions. The pilot's recommendation as to how the accident could have been prevented was with less weight and cooler temperatures. The airplane stalled and descended to the ground while maneuvering to gain altitude shortly after takeoff. According to a sheriff's deputy, who witnessed the accident, the airplane departed runway 29, and barely cleared power lines during the initial climb. The airplane performed two 360-degree turns south of the airport and stalled, impacting in a field about 4,200 msl. The airport is located at 3,993 feet msl. Post accident examination by an FAA inspector determined that the fuel tanks were full at the time of departure. The density altitude was calculated about 5,000 feet msl. The pilot reported that there were no mechanical malfunctions. The pilot's recommendation as to how the accident could have been prevented was taking off with less weight and at cooler temperatures. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2002_LAX02LA064.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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