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January 31, 2015 · Evolution Aircraft REVO · N40EV

Bushnell, FL

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
January 31, 2015
Injury Outcomes
1 injury (1 minor injury), 1 uninjured
Location
Bushnell, FL
Aircraft
Evolution Aircraft REVO (2012)
Tail Number
N40EV
Operator
Allen Gadoury
Injuries
Minor
Aircraft Damage
Substantial
NTSB Number
ERA15CA122

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.

NTSB Probable Cause

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.

Full 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.

Flight

Event TypeAccident
Event Time10:42 EST
Nearest AirportFlying W Airranch (0nm N)
Runway09
Runway Length3415 ft
Runway Width100 ft
Flight Plan FiledNone
Flight Plan ActivatedNo
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftEvolution Aircraft REVO
Tail NumberN40EV
Aircraft CategoryWsft
DamageSubstantial
OperatorAllen Gadoury
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsRotax · 912ULS · Reciprocating · 100
Seats2

People & Injuries

Injury Summary1 injury (1 minor injury), 1 uninjured
Fatal0
Serious0
Minor1
Uninjured1
Total2
Crew 1Age 64 · Third Class · None

Conditions

ConditionsVMC
LightDaylight
Wind50° @ 8 kt
Visibility10 sm
CeilingNone
Temperature / Dew Point63 F / 45 C
Altimeter30.31 inHg
Observation Time15:53
Weather SourceWFAC

Appendix: Source Data