NTSB CAROL · Event
Event LAX03LA120
Aircraft involved
Probable cause & findings
The pilot's failure to obtain/maintain an adequate airspeed, which resulted in a stall/mush.
Factual narrative
On March 30, 2003, at 1816 Pacific standard time, a Beech 19A, N7610R, collided with terrain at the departure end of runway 14 at Harris Ranch Airport, Coalinga, California, during the takeoff initial climb. The owner operated the flight under the provisions of 14 CFR Part 91. The private pilot and the passenger/owner were not injured. The airplane sustained substantial damage. Visual meteorological conditions prevailed, and no flight plan had been filed. The pilot stated in the Pilot/Operator Aircraft Accident Report (NTSB Form 6120.1/2) that he set 10 degrees of flaps for takeoff from the relatively short runway. He rotated at 60 mph, and once the airplane was airborne he noticed that the "aircraft was slow to climb." He leveled the nose and gradually raised the flaps. The airplane settled, collided with the ground, and came to rest just past the end of the runway in an onion field. The pilot said that the aural stall warning was operating throughout the attempted climb out. The Beechcraft Musketeer Sport III, Model 19A, Owner's Manual states that there are 3 flap settings; 15 degrees, 25 degrees, and 35 degrees. It states the following takeoff procedure, "After the airplane breaks ground, lower the nose slightly and let the airplane accelerate to the desired climb speed." Additionally, takeoff speed for 15 degrees of flaps is 60 mph, and 75 mph for no flaps. At the direction of the National Transportation Safety Board investigator-in-charge the airplane's engine was inspected and ran by a licensed airframe and power plant mechanic. The mechanic reported that the engine operated to what he would consider a normal level of performance. During the takeoff initial climb the airplane collided with terrain at the departure end of the runway. The pilot set 10 degrees of flaps for takeoff from the 2,820-foot runway. He rotated at 60 mph and once the airplane was airborne he noticed that the "aircraft was slow to climb." He leveled the nose, and gradually raised the flaps. The airplane settled, collided with the ground, and came to rest just past the end of the runway in an onion field. The pilot said the aural stall warning was operating throughout the attempted climb out. The Beechcraft Musketeer Sport III, Model 19A, Owner's Manual states that there are 3 flap settings; 15 degrees, 25 degrees, and 35 degrees. It states the following takeoff procedure, "After the airplane breaks ground, lower the nose slightly and let the airplane accelerate to the desired climb speed." Additionally, takeoff speed for 15 degrees of flaps is 60 mph, and 75 mph for no flaps. No anomalies were found during a post accident test run of the engine. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2003_LAX03LA120.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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