DEN00LA090
2000-05-18 · BOULDER, Utah, United States · None · 1 aircraft · Status: Completed
Airport NONE
Aircraft involved
Probable cause & findings
The pilot's failure to take timely remedial action when he realized a low fuel state. Factors were fuel exhaustion and low airspeed.
Factual narrative
On May 18, 2000, approximately 1000 mountain daylight time, an Eagle DW-1, N8803H, registered to and operated by Parowan Crop Dusting Services, Inc., was substantially damaged when it landed hard at Boulder, Utah. The commercial pilot, the sole occupant aboard, was not injured. Visual meteorological conditions prevailed, and no flight plan had been filed for the local aerial application flight being conducted under Title 14 CFR Part 137. The flight originated at Parowan, Utah, approximately 0510. According to the pilot's accident report, he departed Parowan with a full load of chemical (165 gallons of Malathion ULV) and full fuel (60 gallons) en route to Boulder (total payload approximately 1700 pounds). The route of flight was south to Huricane Mesa, east to Bryce Canyon and Escalante, thence to Boulder. Towards the end of the aerial application (1,100+ acres), wind velocity began increasing and, noticing that the fuel gauge registered 1/8 to 1/4 fuel remaining, the pilot turned towards Escalante, where he planned to land and refuel. Over Boulder, the fuel gauge indicated empty. The pilot briefly considered landing at Boulder, but decided the unimproved airstrip was inadequate. Five miles from Escalante and 2 miles past Boulder, the pilot realized the terrain ahead was not conducive to a forced landing. He turned back towards the Boulder airstrip. The engine lost power 1/2-mile from the airstrip. Activating the boost pump resulted in 2 seconds of engine power, enough for the airplane to cross the runway threshold. Airspeed had deteriorated to 60 mph and the airplane landed hard. The nose started to "dip" and the pilot applied full nose up elevator. The airplane continued to nose over, crushing the vertical stabilizer. The pilot departed Parowan, Utah, with a full load of chemical (165 gallons of Malathion ULV) and full fuel (60 gallons) en route to Boulder, Utah, (total payload approximately 1700 pounds). Towards the end of the aerial application (1,100+ acres), wind velocity began increasing and, noticing that the fuel gauge registered 1/8 to 1/4 fuel remaining, the pilot turned towards Escalante, where he planned to land and refuel. Over Boulder, the fuel gauge indicated empty. The pilot briefly considered landing at Boulder, but decided the unimproved airstrip was inadequate. Five miles from Escalante and 2 miles past Boulder, the pilot realized the terrain ahead was not conducive to a forced landing. He turned back towards the Boulder airstrip. The engine lost power 1/2-mile from the airstrip. Activating the boost pump resulted in 2 seconds of engine power, enough for the airplane to cross the runway threshold. Airspeed had deteriorated to 60 mph and the airplane landed hard. The nose started to 'dip' and the pilot applied full nose up elevator. The airplane continued to nose over, crushing the vertical stabilizer. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2000_DEN00LA090.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
Search this event elsewhere
External sources are reported, not agency: signal that something happened, not fact about what happened.
- TallyAero Live Wire Aviation press
- NTSB CAROL Agency ↗
- NTSB Docket Agency ↗
- Aviation Safety Network Aviation press ↗
- Kathryn's Report Aviation press ↗
- Aviation Herald Aviation press ↗
- AVweb Aviation press ↗
- Pilots of America Community ↗
- Reddit /r/flying Community ↗
- FlightAware Aviation press ↗
- AOPA accident database Aviation press ↗
- Google News News ↗
- DuckDuckGo News ↗
Related research
Matched on aircraft type or causal vocabulary (icing, fuel exhaustion). All research papers
- 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…
- arXiv 2026 · arXiv preprint Enabling Beyond-Visual-Line-of-Sight Drones Operation over Open RAN 5G Networks with Slicing
Among the foretold claims of the transition from 5G to 6G, Beyond-Visual-Line-of-Sight (BVLoS) drone operation has emerged as a prominent Internet-of-Robots enabler.
- NASA NTRS 2026 · Contractor Report (CR) Icing Physics Studies Using the 3D SIDRM Test Article: 2023 Icing Tests Analysis
In-flight icing is an important safety issue and is a factor that affects aircraft design and performance. Newer regulations are driving a need for improvements in airframe and engine icing simulation…
- arXiv 2025 · arXiv preprint Multi-Agent Deep Reinforcement Learning for UAV-Assisted 5G Network Slicing: A Comparative Study of MAPPO, MADDPG, and MADQN
The growing demand for robust, scalable wireless networks in the 5G-and-beyond era has led to the deployment of Unmanned Aerial Vehicles (UAVs) as mobile base stations to enhance coverage in dense urb…
- NASA NTRS 2025 · Presentation NASA Icing Update – March 2025
This NASA Icing Update was prepared for presentation to the SAE International AC-9C Inflight Icing Technology Committee. This update includes the following topics: planned Rotational Icing Scaling tes…
- Embry-Riddle Scholarly Commons 2025 · Journal article (JAAER) A Mathematical Model on the Temporal Dynamics of Aviation Competitive Pricing
This study investigates the competitive dynamics of airport pricing using U.S. airport data to validate the findings. It employs linear and nonlinear ordinary differential equation models to analyze t…