NTSB CAROL · Event
Event LAX95LA287
Aircraft involved
Probable cause & findings
a forced landing into unsuitable terrain due to an engine failure for undetermined reasons.
Factual narrative
On August 10, 1995, at 1350 hours Pacific daylight time, the pilot of an Avid Mark IV, N16CN, experienced a loss of engine power shortly after takeoff from the airport at Chino, California. Visual meteorological conditions existed at the time for the local personal flight. The aircraft sustained substantial damage and the pilot received no injuries. The pilot indicated in his accident report that prior to departure he put 4 gallons of auto fuel in the right tank and went through a normal preflight checklist. He departed from runway 21 and shortly after takeoff, the engine began to run rough. The pilot attempted to circle back to the airport to land on runway 26. However, the engine continued to lose power and when the pilot realized he wasn't going to make the runway, he elected to land in a nearby field. During the approach, the aircraft collided with some telephone power lines and came to rest inverted in the field. The pilot stated in his report that he performed some work on the engine prior to the flight. The work included tension and tracking the speed reduction belt, checking the timing (35 degrees btdc at 4,500 rpm), and safety-wiring the propeller. He also indicated that he would never use an auto conversion in an airplane again. He did not state what the specific engine problem was. THE PILOT PERFORMED SOME WORK ON THE ENGINE AND THE PROPELLER AND ADDED 4 GALLONS OF AUTOMOBILE FUEL TO THE RIGHT TANK PRIOR TO DEPARTURE. AFTER TAKEOFF, THE PILOT EXPERIENCED A ROUGH RUNNING ENGINE. HE ATTEMPTED A RETURN TO THE AIRPORT BUT THE ENGINE CONTINUED TO LOSE POWER. DURING THE FORCED LANDING TO AN OPEN FIELD, THE AIRCRAFT COLLIDED WITH SOME TELEPHONE LINES AND CRASHED INVERTED. THE PILOT DID NOT STATE WHAT THE SPECIFIC PROBLEM FOR THE LOSS OF POWER WAS. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1995_LAX95LA287.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 (engine failure). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- arXiv 2022 · arXiv preprint
Multi-level Adaptation for Automatic Landing with Engine Failure under Turbulent Weather
This paper addresses efficient feasibility evaluation of possible emergency landing sites, online navigation, and path following for automatic landing under engine-out failure subject to turbulent wea…
- NASA NTRS 2019 · Conference Paper
Simulation of Liquid Rocket Engine Failure Propagation Using Self-Evolving Scenarios
Traditional probabilistic risk assessment approaches often require failure scenarios to be explicitly defined through event sequences that are then quantified as part of the integrated analysis.
- NASA NTRS 2019 · Conference Paper
Rocket engine failure detection using system identification techiques
The theoretical foundation and application of two univariate failure detection algorithms to Space Shuttle Main Engine (SSME) test firing data is presented.
- NASA NTRS 2019 · Conference Paper
Rocket engine failure detection using system identification techniques
The theoretical foundation and application of two univariate failure detection algorithms to Space Shuttle Main Engine (SSME) test firing data is presented.
- NASA NTRS 2019 · Technical Memorandum (TM)
A simulator investigation of engine failure compensation for powered-lift STOL aircraft
A piloted simulator investigation of various engine failure compensation concepts for powered-lift STOL aircraft was carried out at the Ames Research Center.
- Semantic Scholar 2019 · Article (AIAA Scitech 2019 Forum)
Impact of Engine Failure Constraints on the Initial Sizing of Hybrid-Electric GA Aircraft
Potential advantages of hybrid-electric aircraft are fuel savings, lower emissions, and reduced noise. Since these aircraft generally apply multiple power sources, they can also be designed to sustain…
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