Silverlight Aviation LLC AR-1 accident near Heber City, Utah, December 16, 2020
On December 16, 2020 at about 9:17 pm local time, a 2020 Silverlight Aviation LLC AR-1 (gyroplane), an amateur-built aircraft,, registered N261MD, was substantially damaged in an accident during initial climb near Heber City, Utah (Heber Valley Airport). It was a personal flight under general aviation rules (Part 91). 1 person was killed. The weather was visual conditions (good weather).
The NTSB's probable cause their words, unchanged
The pilot’s failure to follow the procedures for takeoff in the Pilot Operating Handbook, which resulted in a loss of control and collision with the terrain. Contributing to the accident was the pilot’s failure to receive additional training in the gyroplane.
Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.
What the record shows
- Date
- December 16, 2020 · about 9:17 pm local time
- Place
- Heber City, Utah · Heber Valley Airport · map
- Type
- Accident
- Injuries
- 1 person was killed.
- Weather
- visual conditions (good weather)
- Aircraft
- Silverlight Aviation LLC AR-1, built 2020, amateur-built
- Registration
- N261MD · no longer on the register · serial 0048
- Damage
- Substantial damage
- Flight
- Personal flight · general aviation rules (Part 91)
The NTSB's narrative final · quoted from the NTSB record
The pilot conducted a takeoff after receiving systems familiarization from an experienced gyroplane pilot, who was not a certified flight instructor. The system familiarization included procedures on how to operate the gyroplane on the ground and in flight. According to the pilot’s, medical records, his weight was close to but less than the minimum weight indicated in the Pilot’s Operating Handbook (POH) for the front seat occupant. Recorded engine data indicated that the pilot applied 100% power to the engine during the takeoff, which he maintained for the duration of the flight. A security video recording showed that, shortly after liftoff, the gyroplane pitched nose-up and down multiple times, followed by an abrupt nose-up attitude and an abrupt gain in altitude. About 3 seconds later the gyroplane banked right. Shortly after the right turn, the gyroplane began to descend and rotated about the vertical axis. The gyroplane then pitched nose down and impacted terrain. The POH stated that maximum power at minimum takeoff weight can cause an abrupt climb rate and recommended 80% power when being operated by a pilot at the minimum weight. The POH also warned against any maneuver resulting in a low-G (near weightless) condition and stated that it could result in a catastrophic loss of lateral roll control in conjunction with rapid main rotor RPM decrease. The noted effects of these POH warnings are consistent with the gyroplane’s maneuvers captured on the security video. The employee of the gyroplane manufacturer who conducted the flight training with the accident pilot reported that during training, he had issues with excessive power applications and over-controlling the gyroplane. He reported that the pilot needed additional transition time and training in the gyroplane. The employee offered the pilot additional training, but the pilot declined.
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
- Loss of control in flight during initial climb defining event
The NTSB's findings
- Personnel issues › Task performance › Use of equip/info › Aircraft control › Pilot
- Personnel issues › Experience/knowledge › Training › Training with equipment › Pilot
- Personnel issues › Action/decision › Action › Incorrect action performance › Pilot
- Aircraft › Aircraft oper/perf/capability › Performance/control parameters › Powerplant parameters › Incorrect use/operation
Pilot
- Certificate: flight instructor, commercial pilot
- Ratings: multi-engine land; single-engine land; instructor: airplane single-engine; instructor: instrument airplane; instrument: airplane; rotorcraft: gyroplane
- Flight time: 2,900 hours in all; 2.5 in this make and model
- Medical certificate: Class 3 (with waivers/limitations)
- Seat: frt
- Injury: fatal
The aircraft
- Airframe total time: 0 hours
- Last inspection: condition inspection, September 22, 2020; 0 hours since
- Maximum gross weight: 1,260 lb
- Seats: 2
- Landing gear: fixed
- Engine: Rotax 915iS (piston); 0 hours total
The flight
- Flight plan: none
- Runway 22, 6,898 ft by 75 ft
Weather at the time
- Light: daylight
- Wind: from 290° at 4 knots
- Visibility: 10 statute miles
- Temperature: 36°F (2°C), dew point 19°F (-7°C)
- Altimeter: 30.25 inHg
- Observation at 2:56 pm from KPVU, 21 miles away
Weather report (METAR): KPVU 162156Z 29004KT 10SM FEW060 BKN200 02/M07 A3025 RMK AO2 SLP262 T00171067
Injuries
| Fatal | Serious | Minor | None | |
|---|---|---|---|---|
| Flight crew | 1 |
Documents from the investigation the NTSB's docket: the evidence folder behind the report
16 documents, released by the NTSB on October 4, 2022. 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 | EFIS Device - Specialist's Factual Report | PDF, 2 pages | View Download |
| 2 | Mechanic/pilot Statement | PDF, 2 pages | View Download |
| 3 | Witness Reports | PDF, 6 pages | View Download |
| 4 | Interviews | PDF, 6 pages | View Download |
| 5 | Witness Video | video | View Download |
| 6 | Security Video #1 | video | View Download |
| 7 | Security Video #2 | video | View Download |
| 8 | Security Video #3 | video | View Download |
| 9 | ADS-B Data | map file | Download |
| 10 | ADS-B Excel Data | data file | Download |
| 11 | Airframe and Engine Examination Report | PDF, 26 pages | View Download |
| 12 | POH Excerpts | PDF, 3 pages | View Download |
| 13 | Rotax 915IS Data Sheet | PDF, 2 pages | View Download |
| 14 | Memo for Record Autopsy | PDF, 1 page | View Download |
| 15 | Statement of Party Representatives to NTSB Investigation | PDF, 2 pages | View Download |
| 16 | Toxicology Report | PDF, 1 page | 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.
