NTSB CAROL · Event
Event ATL03LA036
Aircraft involved
Probable cause & findings
The pilot's mismanagement of the fuel supply that resulted in fuel starvation and the loss of engine power in both engines. A factor was a tree.
Factual narrative
On January 18, 2003, at 1307 eastern standard time, a Beech 65, N115HF, registered to JAP Air LLC, and operated by a private pilot, collided with the ground during a forced landing following a dual engine loss of power near Fitzgerald, Georgia. The personal flight operated under the provisions of Title 14 CFR Part 91 with an instrument flight plan filed. Visual weather conditions prevailed at the time of the accident. The airplane was substantially damaged. The pilot and his three passengers were not injured. The instrument flight departed Lawrenceville, Georgia, on January 18, 2003 at 1200. According to the pilot, prior to departing Lawrenceville, Georgia, the airplane had been topped off with fuel. The flight was uneventful until he switched fuel tanks from the main tanks to the auxiliary tanks near Macon, Georgia. Several minutes after the fuel selectors were switched the pilot reported a loss of left engine power. The pilot then switched back to the main tanks. The pilot declared an emergency and requested radar vectors to the nearest airport. While enroute to the nearest airport, the pilot switched back to the auxiliary tanks and shortly after, the right engine lost power. The pilot selected an open field and attempted a forced landing. During the attempted landing, the nose wheel assembly collapsed and the left wing assembly collided with a tree. According to the fixed base operator, Aircraft Specialist Jet Center, at Lawrenceville, Georgia, 160 gallons of fuel was purchased for the airplane three days prior to the accident. Their refueling records showed no additional refueling on the day of the accident. According to the Operator's Manual for this airplane, after takeoff and once level cruise has been established, the fuel supply for the engines should be changed from the main tanks to the auxiliary tanks. During the post-accident examination of both engines, they started and ran without any anomalies reported. A total of sixty gallons of fuel was recovered from the airplane during the recovery from the accident site. Examination of the airplane revealed nose wheel and left wing damage. The pilot did not report a mechanical problem with the airplane before the accident. The post-accident examination of the airplane failed to disclose a mechanical problem. According to the pilot, the flight was uneventful until he switched fuel tanks near Macon, Georgia. Several minutes after the fuel selectors were switched the pilot reported a loss of left engine power. The pilot declared an emergency and requested radar vectors to the nearest airport. While en route to the nearest airport, the right engine lost power. The pilot selected and open field and attempted a forced landing. During the forced landing, the nose wheel assembly collapsed, and the left wing collided with a tree. Both engines were test run after the accident and they operated without any anomalies. A total of sixty gallons of fuel was recovered from the airplane during the recovery from the accident site. The pilot did not report a mechanical problem with the airplane before the accident. The post-accident examination of the airplane failed to disclose a mechanical problem. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2003_ATL03LA036.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 (fuel starvation). 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 2026 · arXiv preprint
Trajectory Optimization of Morphing Aerial Vehicles Based on Mid-Fidelity Aeroservoelastic Models
Morphing aerial vehicles offer enhanced maneuverability and fuel efficiency compared to fixed-wing configurations. However, the trade-off between performance gains and control cost in dynamic, unstead…
- arXiv 2025 · arXiv preprint
Hovering efficiency optimization of the cycloidal propeller with end plates
Cycloidal propellers are known for their omnidirectional vectored thrust, enabling smooth transitions between hovering and forward flight, making them ideal for unmanned aerial vehicles (UAVs) and ele…
- arXiv 2025 · arXiv preprint
Shepherd Grid Strategy: Towards Reliable SWARM Interception
Modern unmanned aerial vehicle threats require sophisticated interception strategies that can overcome advanced evasion capabilities and operate effectively in contested environments.
- Embry-Riddle Scholarly Commons 2025 · Journal article (IJAAA)
Bibliometric Analysis with R Biblioshiny on Safety Behavior in Aviation
Safety behaviors in aviation are not limited to technical knowledge and skills in ensuring the safety of flight operations, but also include the attitudes, decision-making processes and collaborations…
- NASA NTRS 2024 · Accepted Manuscript (Version with final changes)
Inverse Modeling of the Initial Stage of the 1991 Pinatubo Volcanic Cloud Accounting for Radiative Feedback of Volcanic Ash
The way volcanic clouds evolve is very sensitive to the initial spatial 3D distributions of volcanic materials, which are often unknown. In this study, we conducted inverse modeling of the Mt.
- NASA NTRS 2024 · Reprint (Version printed in journal)
Comparative Analysis of Empirical and Machine Learning Models for Chla Extraction Using Sentinel-2 and Landsat OLI Data: Opportunities, Limitations, and Challenges
Remote retrieval of near-surface chlorophyll-a (Chla) concentration in small inland waters is challenging due to substantial optical interferences of various water constituents and uncertainties in th…
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