Amateur-built SILENT 2 ELECTRO accident near Wallis, Texas, July 22, 2023
On July 22, 2023 at about 9:00 pm local time, a 2014 amateur-built SILENT 2 ELECTRO (glider), registered N64JG, was substantially damaged in an accident during maneuvering near Wallis, Texas. It was a personal flight under general aviation rules (Part 91). No one was hurt; 1 person was on board or involved. The weather was visual conditions (good weather).
The NTSB's probable cause their words, unchanged
The failure of the tail boom structure due to cyclic torsion overloading as of a result of flutter in the empennage. The reason for the flutter could not be determined.
Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.
What the record shows
- Date
- July 22, 2023 · about 9:00 pm local time
- Place
- Wallis, Texas · map
- Type
- Accident
- Injuries
- No one was hurt; 1 person was on board or involved.
- Weather
- visual conditions (good weather)
- Aircraft
- Amateur-built SILENT 2 ELECTRO, built 2014
- Registration
- N64JG · registry record · serial 2067
- Damage
- Substantial damage
- Flight
- Personal flight · general aviation rules (Part 91)
The NTSB's narrative final · quoted from the NTSB record
After completing a cross-country flight, the pilot set up his final glide at 79 knots (kts), the top of the normal operating airspeed range, to descend from 6,000 ft. About 4,000 ft, the pilot experienced a severe vibration and shaking of the glider. The pilot stated that the glider did not sustain a bird strike or encounter severe turbulence. The pilot deployed the spoilers to slow the glider for possible elevator flutter and the vibration stopped when the glider reached about 60 kts. The pilot verified glider control and slowly increased the airspeed, at which time the vibration returned. The pilot slowed the glider again and proceeded to land. The straight-in landing was uneventful, and the glider rolled to a stop. After exiting the glider, the pilot noticed the composite tail boom structure was cracked in multiple locations. A materials examination of the tail boom structure revealed a damage pattern in the aft portion of the tail boom that contained multiple cracks orientated at ±45° relative to the transverse plane, consistent with torsion loading in both clockwise and counterclockwise rotation directions. Thus, a flutter event likely produced high alternating torsion loads on the fuselage and subsequent damage. The examination found no clear evidence of preexisting damage or weakness that would have led to reduced stiffness of the fuselage structure. The glider sustained a vibration event consistent with flutter while operating below the design maneuvering airspeed. The vibrations dissipated as the glider slowed, which also was consistent with flutter. Flutter could occur due to operation outside of the design flight envelope, loose flight controls, changes in control surface mass, or reduced stiffness in the control panel, wing, stabilizer, or fuselage. Based on the available evidence, the reason for the flutter event could not be determined.
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 › Fuselage › Fuselage main structure › Failure
- Not determined › Not determined › (general) › (general) › Unknown/Not determined
Pilot
- Certificate: commercial pilot
- Ratings: multi-engine land; single-engine land; instrument: airplane; instrument: helicopter; rotorcraft: glider; rotorcraft: helicopter
- Flight time: 5,000 hours in all; 64 in this make and model; 4,800 as pilot in command
- Last flight review: March 10, 2022
- Medical certificate: BasicMed (without waivers/limitations)
- Seat: sngl
- Injury: no injuries
The aircraft
- Airframe total time: 370 hours
- Last inspection: condition inspection, May 13, 2023
- Maximum gross weight: 660 lb
- Seats: 1
- Landing gear: retractable
- Engine: Lz Design FES-SIL-100 (electric); 0 hours total
The flight
- Flight plan: none
Weather at the time
- Light: daylight
- Sky: a few clouds at 6,000 ft
- Temperature: 98°F (37°C), dew point 0°F (-18°C)
Injuries
| Fatal | Serious | Minor | None | |
|---|---|---|---|---|
| Flight crew | 1 |
Documents from the investigation the NTSB's docket: the evidence folder behind the report
5 documents, released by the NTSB on November 7, 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.
| # | Document | What it is | |
|---|---|---|---|
| 1 | Materials Laboratory Factual Report 24-049 | PDF, 12 pages | View Download |
| 2 | Pilot/operator Aircraft Accident Report, NTSB Form 6120.1 | PDF, 9 pages | View Download |
| 3 | Pilot Statement | PDF, 1 page | View Download |
| 4 | Excerpt from Flight Manual | PDF, 2 pages | View Download |
| 5 | Investigation Photographs | PDF, 3 pages | View Download |
The same docket at the NTSB · documents without a copy here are fetched from the NTSB when you open them.
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.
