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ERA15CA122

2015-01-31 · Bushnell, Florida, United States · Minor · 1 aircraft · Status: Completed

Airport 9FL1

Current FAA registration · N40EV

Make / Model
EVOLUTION AIRCRAFT INC REVO
Engine
ROTAX 912ULS SERIES (100 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
20121005
ADS-B equipped
Yes — Mode-S A4AAC0

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

The pilot's failure to maintain airspeed during approach in variable wind, which resulted in the airplane exceeding its critical angle of attack and experiencing an aerodynamic stall.

Factual narrative

The pilot of the special light sport weight shift aircraft stated that he was attempting to land at a private airstrip for a breakfast fly-in. The pilot had to perform two go-arounds due to other traffic in the airport traffic pattern. During the third attempt, while on final approach to runway 9, the pilot extended his glidepath due to another aircraft back-taxiing on the 3,415-foot-long turf runway. The pilot intended to land further down the runway; however, the airspeed decreased when he extended the glidepath. There was also a wind shift when the aircraft was about 15 feet above the runway, which caused it to stall and impact the runway. The aircraft subsequently came to rest inverted on the runway. Examination of the wreckage by a Federal Aviation Administration inspector revealed substantial damage to both wings. The inspector did not observe any preimpact mechanical malfunctions, nor did the pilot report any. The pilot added that the wind was variable at 9 knots, gusting to 12 knots. The recorded wind information at an airport located about 17 miles from the accident site was similar, indicating variable wind from 020 to 090 degrees at 8 knots. The pilot of the special light sport weight shift aircraft stated that he was attempting to land at a private airstrip for a breakfast fly-in. The pilot had to perform two go-arounds due to other traffic in the airport traffic pattern. During the third attempt, while on final approach to runway 9, the pilot extended his glidepath due to another aircraft back-taxiing on the 3,415-foot-long turf runway. The pilot intended to land further down the runway; however, the airspeed decreased when he extended the glidepath. There was also a wind shift when the aircraft was about 15 feet above the runway, which caused it to stall and impact the runway. The aircraft subsequently came to rest inverted on the runway. Examination of the wreckage by a Federal Aviation Administration inspector revealed substantial damage to both wings. The inspector did not observe any preimpact mechanical malfunctions, nor did the pilot report any. The pilot added that the wind was variable at 9 knots, gusting to 12 knots. The recorded wind information at an airport located about 17 miles from the accident site was similar, indicating variable wind from 020 to 090 degrees at 8 knots. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12

NTSB Findings

FAA avdata. C = Cause, F = Factor.

  • C Personnel issues-Task performance-Use of equip/info-Aircraft control-Pilot - C
  • C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Airspeed-Not attained/maintained - C
  • — Environmental issues-Conditions/weather/phenomena-Wind-Variable wind-Effect on operation

Verbatim from NTSB's published report. Source file NTSB_2015_ERA15CA122.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.

Related research

Matched on aircraft type or causal vocabulary (stall, go-around). All research papers