LAX04CA024
2003-10-25 · Fresno, California, United States · None · 1 aircraft · Status: Completed
Airport FCH
Current FAA registration · N738YL
- Make / Model
- CESSNA 172N
- Year of manufacture
- 1978 · 25 years old at event
- Engine
- LYCOMING 0-320 SERIES (180 hp)
- Seats / Engines
- 4 seats · 1 engine
- Last airworthiness date
- 19780202
- ADS-B equipped
- Yes — Mode-S A9EAF4
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
the pilot's inadequate fuel management, which resulted in fuel starvation and a loss of engine power. Also causal was the pilot's failure to follow engine out emergency procedures as defined by the pilot operating handbook.
Factual narrative
On October 25, 2003, at 1300 Pacific daylight time, a Cessna 172N, N7387YL, lost engine power during flight and made an emergency landing near Fresno Chandler Airport (FCH), Fresno, California. Carter Flygare, Inc., was operating the airplane under the provisions of 14 CFR Part 91. The pilot was not injured; the airplane sustained substantial damage. The flight departed Visalia Municipal Airport (VIS), Visalia, California, at 1230, and was en route to Sacramento Executive Airport (SAC), Sacramento, California. Day visual meteorological conditions prevailed and no flight plan had been filed. In a written statement, the pilot reported that after an uneventful departure, he was en route to Sacramento when the engine lost power. He applied carburetor heat and placed the mixture in the full forward position. He reported the engine power loss to Fresno Approach and requested to land at the nearest airport. He turned toward the airport while attempting restart procedures; the engine was unresponsive. While on final, the pilot realized that he was not going to make the airport and landed the airplane in a field. As the main wheels touched down, the airplane nosed over. The pilot did not report any mechanical malfunctions. The Federal Aviation Administration inspector reported that the fuel selector was on the left tank during the recovery. Approximately 1/2 gallon of fuel was recovered from the left fuel tank; approximately 20 gallons of fuel were recovered from the right tank. After the engine failure, the pilot did not switch fuel tanks. The pilot operating handbook for the Cessna 172N states that in the event of an engine failure, the pilot should move the fuel selector valve into the "BOTH" position. The engine lost engine power during flight and the airplane nosed over during an emergency landing in a field. The pilot reported that after an uneventful departure, he was en route when the engine lost power. He applied carburetor heat and placed the mixture in the full forward position. He turned toward a nearby airport while attempting restart procedures; the engine was unresponsive. While on final, the pilot realized that he was not going to make the airport and landed the airplane in a field. As the main wheels touched down, the airplane nosed over. The pilot did not report any preimpact mechanical malfunctions or failures. An FAA inspector examined the airplane and found the fuel selector on the left tank. Approximately 1/2 gallon of fuel was recovered from the left fuel tank; approximately 20 gallons of fuel were recovered from the right tank. After the engine failure, the pilot did not switch fuel tanks. The pilot operating handbook for the Cessna 172N states that in the event of an engine failure, the pilot should move the fuel selector valve into the "BOTH" position. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2003_LAX04CA024.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
Search this event elsewhere
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Related research
Matched on aircraft type or causal vocabulary (fuel starvation, 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…