Skip to content

Atlas / NTSB / CEN20LA234

NTSB CAROL · Event

Event CEN20LA234

2020-06-17 Pine Bluff, Arkansas, United States Serious 1 aircraft Status: Completed

Aircraft involved

Probable cause & findings

The pilot’s exceedance of the airplane’s critical angle of attack, which led to an aerodynamic stall and a loss of airplane control. Contributing was a partial loss of engine power for undetermined reasons.

Factual narrative

On June 17, 2020, about 1800 central daylight time, an Air Tractor AT-402 airplane, N1532H, was substantially damaged when it was involved in an accident near Pine Bluff, Arkansas. The pilot was seriously injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 137 aerial application flight. The pilot reported that he was spraying applicant over a field and that a partial loss of engine power occurred when he began the first climbing turn to reverse course and make a second pass. The airplane subsequently descended and impacted terrain in a near-vertical attitude. The pilot also reported that the airplane owner had previously told him that the engine could potentially have 15% less power and had a history of engine problems. Maintenance log entries did not show a history of engine problems. Postaccident examination of the engine and its components discovered multiple signatures of rotational scoring and rubbing. The fuel control unit, fuel pump, starting flow control unit, overspeed governor, and propeller governor showed no preimpact anomalies but did show signs of contamination consistent with the presence of agricultural fertilizer. The engine case and components were damaged by impact. The pilot reported that, during an aerial application flight, a partial loss of engine power occurred while he was performing the first climbing turn to reverse course. The airplane subsequently descended and impacted terrain in a nearvertical attitude. Postaccident examination of the engine and its components revealed no preimpact anomalies. The reason for the partial loss of engine power could not be determined with the available evidence for this accident investigation. Given the airplane’s near-vertical descent, it is likely that the pilot exceeded the airplane’s critical angle of attack during the climbing turn, which resulted in an aerodynamic stall and a loss of airplane control from which the pilot was unable to recover. 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).

  • Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Angle of attack-Capability exceeded
  • Aircraft-Aircraft power plant-(general)-(general)-Unknown/Not determined
  • Personnel issues-Task performance-Use of equip/info-Aircraft control-Pilot

Verbatim from NTSB's published report. Source file NTSB_2020_CEN20LA234.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 (stall, 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 ↗