Airborne Windsports Edge XT-912L accident near Mokuleia, Hawaii, November 5, 2022
On November 5, 2022 at about 6:11 pm local time, a 2016 Airborne Windsports Edge XT-912L (weight-shift aircraft), registered N444EZ, was substantially damaged in an accident during maneuvering near Mokuleia, Hawaii (Dillingham Airfield). It was an instructional flight under general aviation rules (Part 91). 2 people were killed. The weather was visual conditions (good weather).
The NTSB's probable cause their words, unchanged
Structural failure of the wing for undetermined reasons, which resulted in a loss of control.
Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.
What the record shows
- Date
- November 5, 2022 · about 6:11 pm local time
- Place
- Mokuleia, Hawaii · Dillingham Airfield · map
- Type
- Accident
- Injuries
- 2 people were killed.
- Weather
- visual conditions (good weather)
- Aircraft
- Airborne Windsports Edge XT-912L, built 2016
- Registration
- N444EZ · no longer on the register · serial XT-912-0508
- Damage
- Substantial damage
- Flight
- Instructional flight · general aviation rules (Part 91)
The NTSB's narrative final · quoted from the NTSB record
**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.
The complete narrative as the NTSB published it. The NTSB's docket holds the report as a PDF and any photographs, statements and other documents from the investigation.
The factual record from the NTSB's investigation tables, in plain English
What happened, in order
- Aircraft structural failure during maneuvering defining event
The NTSB's findings
- Aircraft › Aircraft structures › Wing structure › Flight surfaces (wing) › Failure
- Aircraft › Aircraft oper/perf/capability › Performance/control parameters › (general) › Attain/maintain not possible
Pilot
- Certificate: flight instructor, sport pilot
- Ratings: single-engine land; instructor: sport pilot
- Flight time: 450 hours in all; 450 in this make and model; 30 in the last 90 days; 9 in the last 30 days; 430 as pilot in command
- Last flight review: January 31, 2022
- Medical certificate: None
- Seat: frt
- Injury: fatal
Dual student
- Flight time: 0 hours in all; 0 in this make and model
- Seat: rear
- Injury: fatal
The aircraft
- Airframe total time: 1,455.2 hours
- Last inspection: 100-hour inspection, August 11, 2022
- Maximum gross weight: 992 lb
- Seats: 2
- Landing gear: fixed
- Engine: Rotax 912UL (piston); 0 hours total
- Operator: Naluventures LLC
The flight
- Departed from: PHDH Mokuleia HI at 5:40 pm
- Flight plan: none
Weather at the time
- Light: daylight
- Wind: from 130° at 3 knots
- Visibility: 10 statute miles
- Sky: broken clouds at 6,000 ft; scat at 4,900 ft
- Temperature: 77°F (25°C), dew point 63°F (17°C)
- Altimeter: 30.13 inHg
- Observation at 7:55 am from PHHI, 13 miles away
Weather report (METAR): PHHI 051755Z AUTO 07007KT 10SM FEW200 SCT220 25/17 A3013 RMK AO2 SLP192 T02460173 10246 20237 52013 $=
Injuries
| Fatal | Serious | Minor | None | |
|---|---|---|---|---|
| Flight crew | 1 | |||
| Passengers | 1 |
Documents from the investigation the NTSB's docket: the evidence folder behind the report
18 documents, released by the NTSB on November 14, 2024. View them here, or download them; the NTSB redacts some personal details before release, and this site shows the NTSB's own titles rather than its file names.
Everything on this page comes from the NTSB's public records. The narrative, probable cause and findings are the NTSB's own words; the coded tables behind the report are written out in plain English, with pilots' ages, home towns and medical details left out. The documents and photographs are the NTSB's docket, shown as the NTSB released them. This site's own text never names anyone involved. A preliminary report can change; the final report usually follows one to two years later, and the page is refreshed when it does.
