NTSB CAROL · Event
Event LAX04LA124
Aircraft involved
Probable cause & findings
A partial loss of engine power for undetermined reasons during takeoff.
Factual narrative
On February 13, 2004, about 1540 Pacific standard time, a Cessna 172N, N5107K, experienced a partial loss of engine power during takeoff from runway 24 at the Cable Airport, Upland, California. The pilot aborted the takeoff and attempted to stop on the available runway. The airplane sustained substantial damage when it overran the runway's departure end, impacted a flatbed trailer, and came to rest on uneven terrain against a berm about 43 yards from the runway. Cable Air, Inc., operated the airplane. The private pilot and one passenger sustained minor injuries; the second passenger was not injured. Visual meteorological conditions prevailed, and no flight plan had been filed for the local area personal flight. The flight was performed under the provisions of 14 CFR Part 91, and it was originating at the time of the mishap. In the pilot's completed "Aircraft Accident Report," NTSB Form 6120.1/2, he indicated that prior to taking off he performed a preflight inspection of the airplane. He performed a runup and determined that the airplane was in proper working condition and worthy of flight. During the takeoff roll, the pilot again observed that the engine instruments were still "looking good." However, after climbing for several seconds the pilot heard the engine lose power. According to the pilot, he observed that the engine's tachometer had decreased to 1,400 rpm, and he opined that the airplane was not going to continue flying. Therefore, he aborted the climb and lowered the wing flaps. Cable Airport management personnel verbally reported to the National Transportation Safety Board investigator that skid marks were noted on the departure end of the runway leading to the accident airplane. There were about 156 feet of skid marks on the runway, which led to 128 feet of skid-like marks in the dirt. Under the direction of the Safety Board investigator, the airplane was recovered from the accident site and was examined under Federal Aviation Administration (FAA) supervision. In summary, the FAA inspector reported that on February 17, the accident airplane's engine was removed from N5107K, and it was installed on another Cessna 172 airframe that was awaiting an engine overhaul. After removing and replacing several impact-damaged components, the engine was run up to 2,400 rpm. With the exception of a minor vibration due to the fact that the crankshaft was bent, the engine operated normally. The reason for the partial engine power loss, as reported by the pilot, was not ascertained. The engine lost partial power just after the airplane lifted off the runway and the pilot aborted the takeoff and attempted to land on the remaining runway. The airplane touched down on the runway, overran its departure end, impacted a flatbed trailer, and came to rest on uneven terrain against a berm about 43 yards from the runway. The pilot reported that the airplane appeared to have been in proper working condition and worthy of flight during his preflight and pretakeoff inspections. However, after climbing for several seconds he heard the engine lose power, and its tachometer decreased to 1,400 rpm. The pilot believed that the airplane was not going to continue flying so he elected to abort the takeoff. To ascertain the reason for the power loss, the accident airplane's engine was removed from the airplane and installed on another airframe. After removing and replacing several impact-damaged engine accessories/components, the engine was run up to 2,400 rpm. With the exception of a minor vibration due to the fact that the crankshaft was bent, the engine operated normally. The reason for the partial engine power loss, as reported by the pilot, was not ascertained. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2004_LAX04LA124.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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