NTSB CAROL · Event
Event WPR11TA087
Registry · N6774B
FAA Aircraft Registry record.
Make / Model
PIPER PA-18-150
Year of manufacture
1956 · 55 years old at event
Engine
LYCOMING 0-320 SERIES (180 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
19560515
ADS-B equipped
Yes — Mode-S A8F89F
Registrant of record
LEGACY AVIATION AND SALES LLC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
A total loss of engine power for undetermined reasons.
Factual narrative
On January 2, 2011, about 1315 mountain standard time, a Piper PA-18-180, N6774B, experienced a gear collapse during a forced landing about 10 miles southeast of Shoshoni, Wyoming. The commercial pilot and his passenger were not injured, but the airplane, which was owned by STP Aviation LLP, and operated by the United States Department of Agriculture, sustained substantial damage. The local Public Use wildlife aerial observation flight, which departed Riverton Municipal Airport, Riverton, Wyoming, about four hours prior to the accident, was being operated in visual meteorological conditions. No flight plan had been filed. According to the pilot, during the aerial observation flight, the engine suddenly stopped producing power. He therefore checked the fuel selector, applied carburetor heat, made sure the magneto switch was on both, and tried to restart the engine. Because the engine did not restart, he made the decision to make a forced landing on the rough, brush-covered terrain. Although the touchdown was successful, during the landing roll, the airplane went off a low bank, and upon contacting the terrain at the bottom of the bank, the main landing gear support structure failed allowing both gear struts to fold outward. During the accident sequence, the left wing lift strut was bent to the extent that it had to be replaced. A postaccident examination of the airplane's fuel system determined that it had more than one hour of fuel remaining (10+ gallons). As part of the examination process, the engine was test run for several minutes with no sign of any anomaly. The investigation also determined that the ambient temperature and dew point (temperature of ten degrees F/dew point of one degree F) were outside the range at which carburetor icing would be expected in maneuvering flight. At the end of the investigation, no other fuel system or engine anomalies had been found, and the reason for the loss of engine power was not able to be determined. According to the pilot, during a wildlife aerial observation flight, the engine suddenly stopped producing power. The pilot checked the fuel selector and magnetos and applied carburetor heat. Because he was unable to get the engine started again, he executed a forced landing on rough/uneven terrain. During the landing roll, the airplane went off a low bank, contacted the terrain at the bottom of the bank, and sustained substantial damage. At the time of the accident, the airplane had about one hour of fuel remaining, and the postaccident inspection, which included a successful engine run, did not find any anomalies that would have contributed to a loss of power. The ambient temperature and dew point were outside of the range at which carburetor icing would be expected to occur. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
Hierarchical cause / factor breakdown from the FAA bulk avdata database. Each finding tagged C (Cause) or F (Factor).
- — Environmental issues-Physical environment-Terrain-Sloped/uneven-Contributed to outcome
- — Environmental issues-Physical environment-Terrain-Rough terrain-Contributed to outcome
- C Not determined-Not determined-(general)-(general)-Unknown/Not determined - C
Verbatim from NTSB's published report. Source file
NTSB_2011_WPR11TA087.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 (icing). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- 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…
- 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…
- 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…
- 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…
- NASA NTRS 2024 · Presentation
NASA Icing Update – Oct 2024
This presentation provides a status update on select NASA icing research activities for the SAE AC-9C Icing Technical Committee Meeting on Oct 21, 2024.
Browse the full corpus — academia portal ↗