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Atlas / NTSB / CEN10CA239

NTSB CAROL · Event

Event CEN10CA239

2010-05-05 Fort Worth, Texas, United States Airport · AFW None 1 aircraft Status: Completed

Registry · N265RA

FAA Aircraft Registry record.

Make / Model

REMOS AIRCRAFT GMBH G-3/600

Year of manufacture

2007 · 3 years old at event

Engine

ROTAX 912ULS SERIES (100 hp)

Seats / Engines

2 seats · 1 engine

Last airworthiness date

20080324

ADS-B equipped

Yes — Mode-S A29308

Registrant of record

ROCKHOLD RICHARD A

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

The student pilot’s loss of control and the instructor’s delayed remedial action.

Factual narrative

Shortly after takeoff the student pilot experienced trouble controlling the light sport airplane. The flight instructor took over the controls and, believing that the airplane’s flight controls might have been malfunctioning, elected to land on the remaining runway. The fiberglass airplane impacted the runway hard, which resulted in a propeller strike and the collapse of the nose landing gear and left main landing gear. The airplane came to rest on the runway in an upright and left-wing-low position. Following an engine shutdown, the instructor and student were able to exit unassisted. Around the time of the accident the wind was shifting back and forth from a quartering headwind to a quartering tailwind. A Federal Aviation Administration inspector examined the airplane and reported that no preimpact anomalies were noted with the airplane’s flight controls. Shortly after takeoff the student pilot experienced trouble controlling the light sport airplane. The flight instructor took over the controls and, believing that the airplane’s flight controls might have been malfunctioning, elected to land on the remaining runway. The fiberglass airplane impacted the runway hard, which resulted in a propeller strike and the collapse of the nose landing gear and left main landing gear. The airplane came to rest on the runway in an upright and left-wing-low position. Following an engine shutdown, the instructor and student were able to exit unassisted. Around the time of the accident the wind was shifting back and forth from a quartering headwind to a quartering tailwind. A Federal Aviation Administration inspector examined the airplane and reported that no preimpact anomalies were noted with the airplane’s flight controls. 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 Personnel issues-Task performance-Use of equip/info-Aircraft control-Student pilot - C
  • C Personnel issues-Action/decision-Action-Delayed action-Instructor/check pilot - C
  • Environmental issues-Conditions/weather/phenomena-Wind-Variable wind-Effect on equipment

Verbatim from NTSB's published report. Source file NTSB_2010_CEN10CA239.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 (loss of control). 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 ↗