NTSB CAROL · Event
Event SEA96LA154
Registry · N248B
FAA Aircraft Registry record.
Make / Model
PIPER PA-28-180
Engine
LYCOMING O&VO-360 SER (180 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
19750528
ADS-B equipped
Yes — Mode-S A24DD0
Registrant of record
FOTHERINGHAM JACK
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
the pilot's inadequate preflight of the airplane, and subsequent fuel exhaustion due to an inadequate supply of fuel, which resulted in loss of engine power and an emergency landing. Uneven terrain in the emergency landing area was a related factor.
Factual narrative
On July 12, 1996, at 2015 mountain daylight time, an amphibian Colonial C-1, N248B, leased to and operated by the pilot, experienced a loss of engine power. The pilot initiated a forced landing to an open field near Halls Crossing, Utah, where during the forced landing, the airplane collided with the terrain and came to rest inverted. Visual meteorological conditions prevailed at the time and no flight plan was filed. The private pilot received minor injuries, and the passenger was not injured. The flight originated from Taylor, Arizona, with a fuel stop at Gallup, New Mexico. The flight departed from Gallup approximately two hours prior to the accident. The pilot reported that at Gallup, approximately 11 gallons of fuel was added to bring the total fuel capacity to 22 gallons. The pilot stated that the fuel totalizer indicated 22 gallons, however, the cockpit panel fuel gauge read a conflicting amount. The pilot stated that previous to this flight, there had been a conflict between the gauges. At this time, the pilot used a dip stick to verify the fuel quantity. The pilot stated that the fuel totalizer indicated the correct quantity. On the day of the accident, the pilot reported that he did not have the dip stick with him and he did not visually check the fuel level. The pilot stated that he felt that the fuel totalizer was correct. The pilot stated that after passing over the north end of Lake Powell at 1,000 feet above ground level and with the airport in sight, the engine suddenly quit. The pilot was unable to restart the engine and a forced landing was made to an open area. The airplane belly landed and then bounced approximately 15 feet in the air. The airplane rolled to the left and touched down again inverted. The pilot stated during a telephone interview that there was no fuel spillage or fuel smell at the accident site. The pilot's written statement reports "fuel starvation." The pilot reported that about 1,000 feet above ground level and with the airport in sight, the engine suddenly quit. He was unable to restart the engine, and a forced landing was made in an open area. The airplane belly landed, bounced, and became airborne, then it rolled to the left and touched down again inverted. The pilot stated that after the accident, there was no smell of fuel or fuel spillage. He stated that 11 gallons of fuel had been added at the last refueling to bring the total fuel capacity to 22 gallons for this leg of the flight. There had been a conflicting indication of quantity between the fuel totalizer and the cockpit fuel gauge. The pilot stated that he felt that the totalizer was correct; however, there were indications that he did not verify this either visually or with a dip stick. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1996_SEA96LA154.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 exhaustion, 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.
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Experimental flight test vibration measurements and nondestructive inspection on a USCG HC-130H aircraft
This paper presents results of experimental flight test vibration measurements and structural inspections performed by the Federal Aviation Administration's Airworthiness Assurance NDI Validation Cent…
- Embry-Riddle Scholarly Commons 2016 · Journal article (IJAAA)
The Military Learner: The Acceptance of New Training Technology for C-130 Aircrews
The problem in this qualitative embedded single-case study was that business and military organizations have shrinking budgets, which has caused conflicting priorities for training funds.
- 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 2026 · Presentation
Low Altitude RA Virtual Pilot Tabletop: Preliminary Results Summary
A virtual tabletop activity was conducted in support of NASA Airspace Operations and Safety Program’s (AOSP) Air Traffic Management and Safety (ATMS) project.
- arXiv 2025 · arXiv preprint
Next-Generation Aerial Robots -- Omniorientational Strategies: Dynamic Modeling, Control, and Comparative Analysis
Conventional multi-rotors are under-actuated systems, hindering them from independently controlling attitude from position.
- arXiv 2024 · arXiv preprint
High-fidelity study of three-dimensional turbulent transonic buffet on wide-span infinite wings
Turbulent transonic buffet is an aerodynamic instability causing periodic oscillations of lift/drag in aerospace applications.
Browse the full corpus — academia portal ↗