NTSB CAROL · Event
Event SEA97LA168
Aircraft involved
Probable cause & findings
The pilot mismanaged his fuel supply which led to fuel exhaustion and subsequent loss of engine power. Factors contributing to the accident were the lack of adequate altitude and airspeed to successfully execute an autorotation.
Factual narrative
On July 14, 1997, approximately 1220 mountain daylight time, a Bell 47G-3B, N8494E, registered to Roger & Michael Hall, and being flown by a commercial pilot doing business as Eagle Aviation, Inc., incurred substantial damage during a hard landing, following a total loss of power while returning to his fueling station, approximately 11 miles east of Idaho Falls, Idaho. The pilot sustained minor injuries. No flight plan had been filed and visual meteorological conditions existed at the time. The flight, which had just completed an aerial application run, was to have been operated under 14CFR137, and originated from a location adjacent to the spray site. The pilot reported that he "was spraying a potato field. As I made the last pass I looked down and noticed my gas gauge showing low. So I turned around and head(ed) back to the load truck." He continued reporting "I was over a sod field when the engine quit. At that time I was about 250 to 300 yd (yards) from the truck and at (sic) about 10 to 15 f(ee)t above the ground and at (sic) about 25 kts. He concluded reporting "When it quit I did not have the time to do any auto(rotation). It stopped and I hit the ground." An altitude of 15 feet (above ground) at an airspeed of 25 knots places the aircraft on the boundary of the envelope for a successful autorotation (refer to CHART I). An inspector from the Federal Aviation Administration's Flight Standards District Office, Salt Lake City, Utah, traveled to the site. His examination confirmed that the fuel tanks were empty. The pilot reported that upon making the last spray pass of a potato field he noted a low fuel state and turned back towards his refueling truck. At an altitude of 10-15 feet above ground and an airspeed of approximately 25 knots, the engine lost power. The pilot reported that 'when it quit I did not have the time to do any auto(rotation). It stopped and I hit the ground.' An FAA inspector confirmed the lack of fuel on board the aircraft following the accident. The height-velocity diagram for the Bell 47G-3B placed the aircraft on the boundary of the envelope for a successful autorotation at the altitude and speed at the time of the power loss. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1997_SEA97LA168.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
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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 exhaustion). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- AOPA Air Safety Institute 2023 · Safety advisor
Safety Advisor: Fuel Awareness
AOPA Air Safety Institute safety advisor on preventing fuel-exhaustion and fuel-starvation accidents in general aviation. Covers pre-flight fuel planning, reserve requirements (14 CFR 91.151, 91.167),…
- NASA NTRS 2019 · Abstract
U.S. Civil Rotorcraft Accidents, 1963 through 1997
The U.S. National Transportation Safety Board (NTSB) has recorded 8,436 rotorcraft accidents during the period mid - 1963 through the end of 1997.
- NASA NTRS 2019 · Contractor Report (CR)
A study of carburetor/induction system icing in general aviation accidents
An assessment of the frequency and severity of carburetor/induction icing in general-aviation accidents was performed. The available literature and accident data from the National Transportation Safet…
- NASA NTRS 2018 · Other
Parachuting to Safety
NASA's Langley Research Center awarded Ballistic Recovery Systems, Inc., three Small Business Innovation Research (SBIR) contracts to research and develop a new, low cost, lightweight recovery system …
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