Pilot Debrief

AIRBORNE WINDSPORTS Edge XT-912L near Mokuleia, HI — 2022-11-05

Final reportANC23FA003
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Date
2022-11-05
Location
Mokuleia, HI, USA
Airport
HDH
Aircraft
AIRBORNE WINDSPORTS Edge XT-912L
Registration
N444EZ
Category
Trike
Highest injury
Fatal
Fatalities
2
Phase of flight
Maneuvering

Probable cause

Structural failure of the wing for undetermined reasons, which resulted in a loss of control.

NTSB narrative

**This report was modified on January 22, 2025. Please see the docket for this accident to view the original report.** The flight instructor and student were conducting a local area discovery flight in the weight-shift-control light sport aircraft. An onboard video of the accident flight and ADS-B data revealed that about 28 minutes into the flight the aircraft entered a right turn as the flight instructor stated another way for them to lose altitude was to “do spirals.” The aircraft then continued a tight descending right turn, and the descent rate and airspeed rapidly increased to near the aircraft’s maneuvering limitations for both bank angle and airspeed. As the aircraft rolled out of the right turn and near a wings-level attitude, three of the battens connecting the left-wing fabric to the wing structure released at the trailing edge. The left wing subsequently began to flutter, and the aircraft rapidly rolled left and entered a spiral dive, from which the pilot was unable to recover before impact with terrain. A Service Instruction issued by the aircraft manufacturer listed three different factors that can cause the hinged batten to unload: 1) damage to the latch from incorrect loading of the fitting, 2) overtension of the batten within the pocket, and 3) operation outside the placarded limitation of the aircraft. While the investigation was not able to determine the state of battens before the accident, a performance study determined that the aircraft banked near its maximum recommended bank angle of 60° and near its maximum maneuvering speed of 73 kts in a right turn during the descent. The battens that separated during the flight were not recovered and therefore could not be examined. Postaccident examinations of the airframe and engine revealed no additional evidence of preimpact mechanical malfunctions or failures that would have precluded normal operation. The parachute pin was removed and the parachute was partially deployed. It is likely that the parachute was deployed without enough altitude remaining to fully open and arrest the descent. Ethanol was detected at low levels in the flight instructor’s liver and muscle tissue specimens collected during a postmortem examination. Some or all of the small amounts of detected ethanol may have been from postmortem production, and it is unlikely that ethanol effects contributed to the crash.

Analysis

Primary failure mode
Mechanical failure
First missed decision gate
Instructor could have avoided excessive bank angle during maneuvers.

NTSB coding

Evidence available

  • Video
  • ADS-B / radar
  • Photos
  • 18 docket documents
View NTSB final reportView NTSB docket

Docket documents18

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