ERA11CA485
2011-09-05 · Beaufort, North Carolina, United States · Minor · 1 aircraft · Status: Completed
Airport MRH
Current FAA registration · N334JH
- Make / Model
- HAINES JOSEPH E SHA-GLASAIR
- Year of manufacture
- 1987 · 24 years old at event
- Engine
- LYCOMING 0-320 SERIES (180 hp)
- Seats / Engines
- 2 seats · 1 engine
- Last airworthiness date
- 19880628
- ADS-B equipped
- Yes — Mode-S A3A57B
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's improper fuel management, which resulted in a loss of engine power due to fuel starvation.
Factual narrative
Prior to the flight the pilot preflighted the airplane. He checked the oil quantity and sumped the fuel tanks for water. Start up and taxi was normal. After takeoff the pilot raised the wing flaps and turned to the right. While rolling out of the turn the engine coughed, ran, and then quit. The airplane at this time was approximately 150 feet above ground level. The pilot tried to land on one of the airport's other runways but, he did not have enough altitude or airspeed to complete his turn to final. He then landed the airplane on an unpaved portion of the airport and impacted heavy brush. The airplane structure was substantially damaged. When asked about the engine failure by a Federal Aviation Administration inspector, the pilot advised that the engine failed due to fuel starvation because he had not put any fuel in the wing tanks, and forgot to feed from the header tank. The pilot stated that he conducted a preflight inspection of the airplane, which included checking the fuel tanks for water. The startup and taxi were normal. After takeoff, the pilot raised the wing flaps and turned to the right. While rolling out of the turn, the engine coughed, ran, and then lost power. The airplane was about 150 feet above ground level. The pilot tried to land on another runway, but he did not have enough altitude or airspeed to complete his turn to final approach. He landed on an unpaved portion of the airport and impacted heavy brush, and the airplane structure sustained substantial damage. The pilot said that the engine lost power due to fuel starvation because he had not put any fuel in the wing tanks and forgot to switch the fuel feed to the header tank. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
FAA avdata. C = Cause, F = Factor.
- C Aircraft-Fluids/misc hardware-Fluids-Fuel-Fluid management - C
- C Personnel issues-Task performance-(general)-(general)-Pilot - C
Verbatim from NTSB's published report. Source file
NTSB_2011_ERA11CA485.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
Search this event elsewhere
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Related research
Matched on aircraft type or causal vocabulary (fuel starvation, 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…