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Atlas / NTSB / CEN25LA404

NTSB CAROL · Event

Event CEN25LA404

2025-09-30 Watertown, Wisconsin, United States Airport · RYV None 1 aircraft Status: Completed

Registry · N814

FAA Aircraft Registry record.

Make / Model

CIRRUS DESIGN SR20

Year of manufacture

2003 · 22 years old at event

Engine

CONT MOTOR IO-360 SER (300 hp)

Seats / Engines

4 seats · 1 engine

Last airworthiness date

20030130

ADS-B equipped

Yes — Mode-S AB1837

Registrant of record

WISCONSIN AVIATION-FOUR LAKES INC

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

The flight instructor’s failure to maintain control of the airplane following the student pilot’s bounced landing. Contributing to the accident was the flight instructor’s delayed remedial action which resulted in diminished airplane performance during the go-around.

Factual narrative

The flight instructor and student pilot were conducting a primary instruction flight. The flight instructor reported that the surface wind was calm as they approached the airport to land. The flight instructor stated that the student pilot allowed the airplane to be “slightly high and fast” while on short final approach, but the airplane then joined a normal descent path as it continued toward the runway. The flight instructor estimated that the airplane was 5-10 knots faster than a normal landing speed as it flew over the runway identification numbers. At that point, the flight instructor told the student to reduce engine power to idle, transition his sight picture down the runway, and allow the airplane to decelerate during the landing flare. The airplane bounced upon touchdown, ballooned, descended, and then bounced a second time before the flight instructor took control of the airplane from the student pilot. The flight instructor then increased engine power, increased right rudder input, and pitched for a level attitude to increase airspeed for a go-around. The airplane did not accelerate and bounced for a third time, this time with the stall warning horn audible. The flight instructor reduced the wing flaps from 100% to 50% to gain additional airspeed while flying in ground effect, but she noted that the airplane had ineffective roll and yaw control. She reduced engine power to idle as the airplane drifted left, struck a runway edge light, and departed off the left side of the runway. The airplane then entered an area of high vegetation where it spun around to a stop. The airplane’s aft fuselage sustained substantial damage during the accident. The flight instructor did not report any preimpact mechanical malfunctions or failures that would have precluded normal operation of the airplane. 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-Pitch control-Not attained/maintained
  • Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Lateral/bank control-Not attained/maintained
  • Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Yaw control-Not attained/maintained
  • Personnel issues-Action/decision-Action-Delayed action-Instructor/check pilot
  • Personnel issues-Task performance-Use of equip/info-Aircraft control-Instructor/check pilot

Verbatim from NTSB's published report. Source file NTSB_2025_CEN25LA404.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, go-around). 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 ↗