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Atlas / NTSB / ERA13CA338

NTSB CAROL · Event

Event ERA13CA338

2013-07-28 Shirley, New York, United States Airport · HWV None 1 aircraft Status: Completed

Aircraft involved

Probable cause & findings

The pilot's loss of control during an aborted takeoff as a result of his failure to properly configure the elevator trim prior to flight.

Factual narrative

The pilot reported to a Federal Aviation Administration inspector that, after completing a preflight inspection of the airplane and an engine run up, he taxied the airplane for departure. As the airplane rotated off the runway, the pilot noted that the control yoke felt "heavy." Approximately 25 feet above the ground, the pilot elected to abort the takeoff, and pitched the airplane's nose down. The airplane contacted the runway, bounced, and became airborne again. As the airplane touched down a second time in a nose-down attitude, the propeller struck the runway and the nose landing gear collapsed. The airplane skidded off the right side of the runway and came to rest inverted, resulting in substantial damage to the vertical stabilizer, right wing, and engine firewall. Postaccident examination of the airplane revealed that the elevator trim wheel was set approximately halfway between the neutral trim and full nose-down trim positions. The pilot reported to a Federal Aviation Administration inspector that, after completing a preflight inspection of the airplane and an engine run up, he taxied the airplane for departure. As the airplane rotated off the runway, the pilot noted that the control yoke felt "heavy." Approximately 25 feet above the ground, the pilot elected to abort the takeoff, and pitched the airplane's nose down. The airplane contacted the runway, bounced, and became airborne again. As the airplane touched down a second time in a nose-down attitude, the propeller struck the runway and the nose landing gear collapsed. The airplane skidded off the right side of the runway and came to rest inverted, resulting in substantial damage to the vertical stabilizer, right wing, and engine firewall. Postaccident examination of the airplane revealed that the elevator trim wheel was set to the nose-down position, which accounted for the "heavy" feeling of the flight controls the pilot experienced during the takeoff. 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-Aircraft oper/perf/capability-Performance/control parameters-Pitch control-Not attained/maintained - C
  • C Personnel issues-Action/decision-Action-Forgotten action/omission-Pilot - C
  • C Aircraft-Aircraft systems-Flight control system-Elevator control system-Related operating info - C

Verbatim from NTSB's published report. Source file NTSB_2013_ERA13CA338.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 ↗