DEN89LA105
1989-04-09 · MORGAN, Utah, United States · None · 1 aircraft · Status: Completed
Airport 42U
Current FAA registration · N7847U
- Make / Model
- CESSNA 172F
- Year of manufacture
- 1964 · 25 years old at event
- Engine
- CONT MOTOR 0-300 SER (145 hp)
- Seats / Engines
- 4 seats · 1 engine
- Last airworthiness date
- 19640925
- ADS-B equipped
- Yes — Mode-S AAA2C2
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
INADEQUATE SERVICING OF THE AIRCRAFT BY THE PILOT, PARTIAL BLOCKAGE OF THE FUEL LINE AND FUEL FILTER, AND FUEL STARVATION. CONTRIBUTING FACTORS WERE: THE DOWNWARD SLOPING RUNWAY AND A FENCE.
Factual narrative
DRG FLT AT 10,500' MSL, THE ENG LOST POWER & WOULD NOT RESTART. THE PLT MADE A FORCED LANDING ON RWY 21 AT A NEARBY ARPT. THE RWY WAS ONLY 3800' LONG & HAD A RPRTD DOWNWARD SLOPE OF 1.5 DEG. THE WIND WAS ESTIMATED TO BE FROM 270 DEG AT 10 KTS. THE PLT RPRTD THAT DRG THE LANDING, THE ACFT TOUCHED DOWN AT ABOUT MIDFIELD & HE WAS UNABLE TO STOP ON THE REMAINING RWY. AFTER GOING OFF THE DEPARTURE END, IT HIT A FENCE & WAS DAMAGED. A POST ACDNT EXAM REVEALED THERE WAS SEVEN GAL OF FUEL REMAINING. A CHECK OF THE FUEL SYSTEM REVEALED EVIDENCE THAT THE MAIN FUEL LINE & FUEL FILTER WERE RESTRICTING FUEL FLOW. THE PLT RELATED THAT THIS ACFT HAD A SIMILAR PROBLEM PREVIOUSLY & HE HAD DRAINED A CONSIDERABLE AMOUNT OF WATER FROM THE FUEL SYSTEM. AUTOMOTIVE FUEL WAS BEING USED IN THE ACFT. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1989_DEN89LA105.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 starvation). All research papers
- 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…
- arXiv 2024 · arXiv preprint An energy-stable phase-field model for droplet icing simulations
A phase-field model for three-phase flows is established by combining the Navier-Stokes (NS) and the energy equations, with the Allen-Cahn (AC) and Cahn-Hilliard (CH) equations and is demonstrated ana…