LAX02LA132
2002-04-10 · Gila Bend, Arizona, United States · Serious · 1 aircraft · Status: Completed
Airport E63
Aircraft involved
Probable cause & findings
The failure of the engine for undetermined reasons.
Factual narrative
On April 10, 2002, about 0830 mountain standard time, an unregistered, experimental homebuilt Cox Aeros Ltd. Skyranger, collided with the ground during a forced landing at Gila Bend, Arizona. The owner/operator was operating the airplane under the provisions of 14 CFR Part 91. The private pilot sustained minor injuries and the passenger sustained serious injuries; the airplane sustained substantial damage. The purpose of the flight was to practice touch-and-go landings. Day visual meteorological conditions prevailed, and no visual flight rules (VFR) flight plan had been filed. Through a written statement, the pilot stated that after departing runway 22 to practice touch-and-go's, approximately 300 yards beyond the end of the runway a computer malfunction resulted in instant shutdown of the engine; consequently, the pilot made a forced landing in the rough, desert terrain. The pilot further stated that upon touchdown, the nosegear collapsed and the cowling and windshield were damaged. The speed of the airplane was between 40-45 miles per hour. According to a local law enforcement report, the pilot had departed to the west from the municipal airport. The runway is oriented 040/220 degrees, according to the Southwest U.S. Airport/Facility Directory. About 150 to 200 feet above the ground (agl), the engine lost power and a forced landing ensued. According to the engine manufacturer, if the computer does not receive power from the battery, the engine will quit. The two-place ultralight trainer airplane was registered with the United States Ultralight Association but the owner/operator did not apply for a waiver as required by Federal Aviation Regulations Part 103. An unregistered, experimental homebuilt aircraft collided with the ground during a forced landing after an engine failure. The airplane was not issued a waiver as required for operation by Part 103 of the Federal Aviation Regulations. After departing to practice touch-and-go's the engine lost power; consequently, the pilot made a forced landing in the rough, desert terrain. Upon touchdown, the nosegear collapsed and the cowling and windshield were damaged. The speed of the airplane was between 40-45 miles per hour. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2002_LAX02LA132.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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Related research
Matched on aircraft type or causal vocabulary (engine failure). All research papers
- 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…