LAX07CA194
2007-06-26 · Fresno, California, United States · Minor · 1 aircraft · Status: Completed
Airport FCH
Current FAA registration · N1054E
- Make / Model
- AERONCA 7AC
- Year of manufacture
- 1946 · 61 years old at event
- Engine
- CONT MOTOR A&C65 SERIES (65 hp)
- Seats / Engines
- 2 seats · 1 engine
- Last airworthiness date
- 19560512
- ADS-B equipped
- Yes — Mode-S A01A30
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
the pilot's failure to maintain an adequate airspeed, which resulted in a stall.
Factual narrative
On June 26, 2007, about 1945 Pacific daylight time, an Aeronca 7AC, N1054E, collided with terrain at Fresno Chandler Executive Airport, Fresno, California. The pilot was operating the airplane under the provisions of 14 CFR Part 91. The private pilot and one passenger sustained minor injuries; the airplane sustained substantial damage. The cross-country personal flight departed Fresno about 1945, with a planned destination of Selma, California. Visual meteorological conditions prevailed, and no flight plan had been filed. The pilot stated in a written report that he departed runway 30 after rotating at 60 mph. During the initial climb the right wing dropped and he attempted to recover. The airplane impacted the ground approximately 60 feet north of the runway end. The pilot stated that the winds at the time of the accident were 280 degrees at 10 knots, gusting to 20 knots. The pilot stated that the airplane and engine had no mechanical failures or malfunctions during the flight, and that he believed holding a higher air speed during climb out could have prevented the accident. The airplane impacted terrain after it stalled during the takeoff initial climb. The pilot stated in a written report that he departed runway 30 after rotating at 60 mph. He said that he did not maintain adequate airspeed during the climb. The right wing dropped and he attempted to recover; however, the airplane impacted the ground approximately 60 feet north of the runway end. The pilot stated that the winds at the time of the accident were 280 degrees at 10 knots, gusting to 20 knots. He reported that the airplane and engine had no mechanical failures or malfunctions during the flight, and that he believed holding a higher air speed during climb out could have prevented the accident. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2007_LAX07CA194.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.
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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…