NTSB CAROL · Event
Event ANC06CA071
Registry · N714JE
FAA Aircraft Registry record.
Make / Model
CESSNA A185F
Year of manufacture
1983 · 23 years old at event
Engine
CONT MOTOR IO 520 SERIES (285 hp)
Seats / Engines
6 seats · 1 engine
Last airworthiness date
19910129
ADS-B equipped
Yes — Mode-S A98BB6
Registrant of record
ALLRED MARK
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The loss of engine power for an undetermined reason, which resulted in an emergency landing and an in-flight collision with trees.
Factual narrative
The private pilot was conducting a local area round-robin flight to various lakes practicing water landings under Title 14, CFR Part 91. According to the pilot, while in cruise flight, the engine lost power. The pilot said he activated the boost pump, the engine produced power again for a few seconds, and then quit completely. He reported that during the forced landing to a small lake, the airplane struck trees and landed short of the lake. The airplane's wings received structural damage. During interviews, the mechanic who removed the airplane's wings for transport, told the NTSB investigator-in-charge (IIC) he didn't find any fuel in the wing fuel tanks. Another mechanic who removed the airplane's engine told the IIC the fuel system, including the gascolator, was intact with no signs of fuel leakage. The mechanic also said he removed less than 1 gallon of fuel from the airplane's header tank. The mechanic further stated that a visual inspection of the engine compartment did not disclose any evidence of a fuel leak. A visual examination of the airplane's exterior by the IIC did not disclose any evidence of fuel staining. In a written statement to the NTSB dated June 22, the pilot indicated that according to his fuel consumption calculations, there should have been enough fuel onboard for the proposed flight. The pilot also wrote that after recovering the airplane, he saw "fuel staining on the belly indicating fuel leaking from the gascolator." The private pilot was conducting a local area round-robin flight to various lakes practicing water landings under Title 14, CFR Part 91. According to the pilot, while in cruise flight, the engine lost power. The pilot said he activated the boost pump, the engine produced power again for a few seconds, and then quit completely. He reported that during the forced landing to a small lake, the airplane struck trees and landed short of the lake. The airplane's wings received structural damage. During interviews, the mechanic who removed the airplane's wings for transport, told the NTSB investigator-in-charge (IIC) he didn't find any fuel in the wing fuel tanks. Another mechanic who removed the airplane's engine told the IIC the fuel system, including the gascolator, was intact with no signs of fuel leakage. The mechanic also said he removed less than 1 gallon of fuel from the airplane's header tank. The mechanic further stated that a visual inspection of the engine compartment did not disclose any evidence of a fuel leak. A visual examination of the airplane's exterior by the IIC did not disclose any evidence of fuel staining. In a written statement to the NTSB dated June 22, the pilot indicated that according to his fuel consumption calculations, there should have been enough fuel onboard for the proposed flight. The pilot also wrote that after recovering the airplane, he saw "fuel staining on the belly indicating fuel leaking from the gascolator." Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2006_ANC06CA071.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 ↗