ERA15CA209
2015-05-08 · Balsam Grove, North Carolina, United States · None · 1 aircraft · Status: Completed
Current FAA registration · N5981T
- Make / Model
- CESSNA 150D
- Engine
- CONT MOTOR 0-200 SERIES (100 hp)
- Seats / Engines
- 2 seats · 1 engine
- Last airworthiness date
- 19640622
- ADS-B equipped
- Yes — Mode-S A7BDAC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's decision to attempt an off airport takeoff, and failure to maintain adequate clearance during the initial climb in crosswind conditions, which resulted in a collision with trees.
Factual narrative
The pilot\owner of the airplane reported that he experienced a total loss of engine power and performed an uneventful forced landing to a road. The reason for the engine failure was later attributed to a blocked fuel vent tube. After landing, the pilot added additional fuel to the airplane, conducted a normal engine run-up, and noted about 1,500 feet of straight roadway available to takeoff from. He elected to depart from the road to the west, which was toward a valley. During the initial climb, the airplane encountered a sudden crosswind, and struck tree branches, which resulted in substantial damage to the left outboard wing and right inboard horizontal stabilizer. The pilot was able to continue the flight and landed at his destination without further incident. He also reported that he did not experience any malfunctions or failures during the accident takeoff that would have precluded normal operation of the airplane. The airplane had been operated for about 17 hours since its most recent annual inspection, which was performed about 7 months prior. Winds reported at an airport that was located about 20 miles northeast of the accident site, about the time of the accident, were from 140 degrees at 7 knots. The pilot\owner of the airplane reported that he experienced a total loss of engine power and performed an uneventful forced landing to a road. The reason for the engine failure was later attributed to a blocked fuel vent tube. After landing, the pilot added additional fuel to the airplane, conducted a normal engine run-up, and noted about 1,500 feet of straight roadway available to takeoff from. He elected to depart from the road to the west, which was toward a valley. During the initial climb, the airplane encountered a sudden crosswind, and struck tree branches, which resulted in substantial damage to the left outboard wing and right inboard horizontal stabilizer. The pilot was able to continue the flight and landed at his destination without further incident. He also reported that he did not experience any malfunctions or failures during the accident takeoff that would have precluded normal operation of the airplane. The airplane had been operated for about 17 hours since its most recent annual inspection, which was performed about 7 months prior. Winds reported at an airport that was located about 20 miles northeast of the accident site, about the time of the accident, were from 140 degrees at 7 knots. . Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
FAA avdata. C = Cause, F = Factor.
- C Personnel issues-Action/decision-Info processing/decision-Decision making/judgment-Pilot - C
- C Personnel issues-Task performance-Use of equip/info-Aircraft control-Pilot - C
- — Environmental issues-Conditions/weather/phenomena-Wind-Crosswind-Not specified
Verbatim from NTSB's published report. Source file
NTSB_2015_ERA15CA209.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.
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Related research
Matched on aircraft type or causal vocabulary (engine failure). All research papers
- arXiv 2022 · arXiv preprint Multi-level Adaptation for Automatic Landing with Engine Failure under Turbulent Weather
This paper addresses efficient feasibility evaluation of possible emergency landing sites, online navigation, and path following for automatic landing under engine-out failure subject to turbulent wea…
- NASA NTRS 2019 · Conference Paper Simulation of Liquid Rocket Engine Failure Propagation Using Self-Evolving Scenarios
Traditional probabilistic risk assessment approaches often require failure scenarios to be explicitly defined through event sequences that are then quantified as part of the integrated analysis.
- NASA NTRS 2019 · Conference Paper Rocket engine failure detection using system identification techiques
The theoretical foundation and application of two univariate failure detection algorithms to Space Shuttle Main Engine (SSME) test firing data is presented.
- NASA NTRS 2019 · Conference Paper Rocket engine failure detection using system identification techniques
The theoretical foundation and application of two univariate failure detection algorithms to Space Shuttle Main Engine (SSME) test firing data is presented.
- NASA NTRS 2019 · Technical Memorandum (TM) A simulator investigation of engine failure compensation for powered-lift STOL aircraft
A piloted simulator investigation of various engine failure compensation concepts for powered-lift STOL aircraft was carried out at the Ames Research Center.
- Semantic Scholar 2019 · Article (AIAA Scitech 2019 Forum) Impact of Engine Failure Constraints on the Initial Sizing of Hybrid-Electric GA Aircraft
Potential advantages of hybrid-electric aircraft are fuel savings, lower emissions, and reduced noise. Since these aircraft generally apply multiple power sources, they can also be designed to sustain…