LAX01LA097
2001-02-14 · Petaluma, California, United States · None · 1 aircraft · Status: Completed
Airport O69
Current FAA registration · N8286P
- Make / Model
- PIPER PA-24-250
- Year of manufacture
- 1963 · 38 years old at event
- Engine
- LYCOMING 0-540 SERIES (250 hp)
- Seats / Engines
- 4 seats · 1 engine
- Last airworthiness date
- 19630524
- ADS-B equipped
- Yes — Mode-S AB51CB
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
Failure of non-airframe and powerplant mechanic/certificated owners to properly install a new mixture cable that became entangled in the nose landing gear during its extension for landing, resulting in a loss of engine power.
Factual narrative
On February 14, 2001, at 1230 hours Pacific standard time, a Piper PA-24-250, N8286P, experienced a loss of power during landing at the Petaluma Muni Airport, Petaluma, California. The airplane collided with a tree and impacted the ground 100 yards short of the runway. The airplane was owned and operated by the private pilot under the provisions of 14 CFR Part 91 as a personal flight, and sustained substantial damage. The pilot was not injured. Visual meteorological conditions prevailed. No flight plan had been filed. The flight departed the Sonoma County Airport, Santa Rosa, California, at 1145, and was scheduled to terminate at the Petaluma airport. An inspector from the Federal Aviation Administration (FAA) interviewed the pilot. The pilot stated that he conducted the prelanding checklist on downwind for runway 11, which included reducing power and lowering the landing gear. He saw the instrument panel flex forward and the engine began to run rough. He attempted to add power, but there was not a corresponding power increase. The pilot stated that he set the airplane up for best glide and continued the flight to the airport. About 300 yards from the end of runway 29 the airplane struck a tree. The airplane continued over a street and fence, where it came to rest about 150 yards from the departure end of runway 29. In the pilot's written statement to the Safety Board he indicated that the landing gear stopped about halfway down and then he felt a "severe" vibration. After the engine quit he continued in the pattern to set up for an emergency landing in an open field on airport property. The airplane was inspected on scene by an FAA inspector. He visually inspected the fuel tanks. Each outboard fuel tank had half a tank of fuel, and the main fuel tanks were full. During the inspection of the airplane, the FAA inspector noted that the mixture cable was entangled in the nose landing gear. When the landing gear was lowered, it pulled the mixture cable "out of its holder," which allowed the engine to be in a full lean position. The pilot informed the FAA inspector that he and his two partners had recently installed the mixture, throttle, and propeller cables. The FAA inspector reported that the pilot and his partners were not certified airframe and power plant (A & P) mechanics. He further noted that a certificated A & P mechanic had not returned the airplane to service. A review of the airplane logbook by the Safety Board investigator disclosed that the last entry was made on September 18, 2000. During landing, the engine lost power. The airplane collided with trees, and made a hard landing in an open dirt field in the ensuing forced landing. On the downwind leg for landing, the pilot lowered the landing gear, and the engine began to run rough. He noted that the landing gear stopped about halfway down. He attempted to add power, but did not receive a corresponding power increase, and set up for an emergency landing. A visual external examination of the engine revealed that the mixture cable was entangled in the nose landing gear. When the landing gear was lowered the mixture cable was pulled out of its sleeve, which allowed the engine to be in a full lean position. Mixture, throttle, and propeller cables were recently installed by the pilot and his two partners. The pilot and his partners were not certificated A & P mechanics, and a certified mechanic had not returned the airplane to service after the cable installation. The last entry in the logbook was made 6 months prior to the accident,. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2001_LAX01LA097.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.
- TallyAero Live Wire Aviation press
- NTSB CAROL Agency ↗
- NTSB Docket Agency ↗
- Aviation Safety Network Aviation press ↗
- Kathryn's Report Aviation press ↗
- Aviation Herald Aviation press ↗
- AVweb Aviation press ↗
- Pilots of America Community ↗
- Reddit /r/flying Community ↗
- FlightAware Aviation press ↗
- AOPA accident database Aviation press ↗
- Google News News ↗
- DuckDuckGo News ↗
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…