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Atlas / NTSB / CEN14LA290

NTSB CAROL · Event

Event CEN14LA290

2014-06-04 Fort Worth, Texas, United States Airport · 2TE2 Serious 1 aircraft Status: Completed

Registry · N8DT

FAA Aircraft Registry record.

Make / Model

AIRBUS HELICOPTERS INC AS350B3

Year of manufacture

2024

TCDS

H9EU · AIRBUS HELICOPTERS

Engine

SAFRAN ARRIEL 2D (952 hp)

Seats / Engines

7 seats · 1 engine

Last airworthiness date

20240830

ADS-B equipped

Yes — Mode-S AADD88

Registrant of record

DT EQUIPMENT LEASING LLC

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

The non-certificated pilot’s inadequate preflight planning, which resulted in a loss of engine power during takeoff due to fuel exhaustion.

Factual narrative

On June 4, 2014, about 1800 central daylight time, an experimental, amateur-built Tuenis Starduster TOO SA300, N8DT, sustained substantial damage when it impacted tress and terrain after a loss of engine power during takeoff from the Flying Oaks Airport (2TE2), Fort Worth, Texas. The non-certificated pilot and passenger received serious injuries. The airplane was registered to and operated by the pilot individual under the provisions of the 14 Code of Federal Regulations Part 91 as a personal flight. Visual meteorological conditions prevailed at the time of the accident, and no flight plan was filed. The airplane was departing 2TE2 about 1800. The airplane departed runway 15 (2,800 feet by 150 feet, turf). Shortly after takeoff, the engine lost power and the pilot turned the airplane 180 degrees. He was unable to return to the runway, and the pilot attempted to land on a 1/4 mile long driveway that paralleled the runway. During the forced landing, the airplane struck a tree, and then impacted the driveway about 65 feet from the tree impact, and came to rest about 131 feet from the initial tree impact. A witness reported that she heard the engine sputter and lose power before it impacted the ground. The passenger was able to free himself from the wreckage, but the pilot in the rear seat had to be extricated by first responders who separated the fuselage aft of the pilot's seat. A Federal Aviation Administration inspector arrived at the accident site about 4 hours after the accident. The examination of the accident site revealed that the airplane's propeller and spinner had separated from the engine. There was minimal impact damage to the propeller blades and spinner, and there were no signatures of rotational damage consistent with an engine developing power. He observed no evidence of a fuel spill or fuel odor in the debris path. He removed the top wing fuel tank cap and there was no evidence of fuel. He checked the fuselage fuel tank for fuel and none was observed. There was no evidence of fuel leaks or fuel staining. He reported that the fuel tanks were intact and not breached. The following morning he returned to the accident site and checked the fuel tanks again with an inspection camera and confirmed that there was no fuel in the fuel tanks. The wreckage was moved with a tractor and the ground was checked for evidence of fuel, but none was observed within the wreckage area. The airplane was registered to the pilot. A bill of sale indicated that he purchased the airplane on January 27, 2014. Maintenance records indicated that the last conditional inspection of the airplane was conducted on December 9, 2013, with a reading tachometer time of 406.71 hours. The recording tachometer time at the accident site was 421.46 hours. The pilot was not a registered pilot and he did not hold a FAA medical certificate. The pilot's flight experience is unknown. The airplane's recording tachometer indicated that it had flown about 15 hours since the last conditional maintenance inspection. The pilot did not provide the National Transportation Safety Board (NTSB) a completed NTSB Accident Form 6120.1. Shortly after takeoff, the airplane's engine lost power. The pilot attempted to return to the runway but was unable to reach it so he attempted to land on a 1/4-mile-long driveway that paralleled the runway, but the airplane struck a tree and impacted the driveway. Postaccident examination revealed that the airplane's propeller and spinner had separated from the engine and had sustained minimal impact damage: there were no signatures of rotational damage consistent with the engine developing power at the time of impact. The airplane's fuel tanks were examined and no fuel was observed. The fuel tanks were not breached during the impact, and there was no evidence of fuel leaks or fuel stains at the accident site. The pilot was not a registered pilot and did not hold a Federal Aviation Administration medical certificate. The pilot's flight experience is unknown. 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).

  • C Aircraft-Fluids/misc hardware-Fluids-Fuel-Fluid level - C
  • C Aircraft-Fluids/misc hardware-Fluids-Fuel-Inadequate inspection - C
  • C Personnel issues-Task performance-Planning/preparation-Fuel planning-Pilot - C
  • C Personnel issues-Experience/knowledge-Experience/qualifications-Qualification/certification-Pilot - C

Verbatim from NTSB's published report. Source file NTSB_2014_CEN14LA290.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.

Related research

What the literature says.

Academic papers and agency reports matching this event's aircraft type or causal vocabulary (fuel exhaustion, maintenance). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.

Browse the full corpus — academia portal ↗