Amateur-built VANS RV6A accident near Aztec, Arizona, September 16, 2022
On September 16, 2022 at about 8:35 pm local time, a 2009 amateur-built VANS RV6A, registered N646RV, was destroyed in an accident during enroute (cruise) near Aztec, Arizona. It was a personal 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
The total loss of engine power for reasons that could not be determined based on available evidence. Contributing to the accident was the pilot’s decision to turn away from a suitable emergency landing surface, his failure to maintain adequate airspeed as the airplane neared the ground, and his exceedance of the airplane’s critical angle of attack, which resulted in an aerodynamic stall.
Source: NTSB aviation accident database, copy made November 2, 2026. Docket and reports at the NTSB.
What the record shows
- Date
- September 16, 2022 · about 8:35 pm local time · cases in 2022
- Place
- Aztec, Arizona · map
- Type
- Accident
- Injuries
- 2 people were killed.
- Weather
- visual conditions (good weather)
- Aircraft
- Amateur-built VANS RV6A, built 2009
- Registration
- N646RV · registry record · serial 20333
- Damage
- Destroyed
- Flight
- Personal flight · general aviation rules (Part 91)
The NTSB's narrative final · quoted from the NTSB record
The pilot and passenger were conducting a cross-country flight. Flight track data showed their flight close to and paralleling an interstate highway one to two miles away when the airplane started a controlled descent. During the descent the airplane made a turn away from the highway, made another turn to parallel the highway, and then made a turn angling toward the highway. The flight continued to descend until it impacted terrain about one mile from the highway. The airplane impacted flat desert terrain in a nose-low attitude and a post-impact fire ensued, which consumed most of the airplane wreckage. There were no reported radio calls from the pilot or witnesses to the accident. Investigators could not determine why the pilot initially turned away from the highway, which could have provided a suitable emergency landing surface. Examination of the engine and propeller found the propeller had broken aft and there were starter ring impact marks of an aft, non-rotational nature. Impact and fire damage prevented any examination of the fuel, air intake, electrical, and ignition systems. There were no signatures or conditions observed during the examination that would indicate there was any pre-accident catastrophic mechanical malfunction. Those findings and the controlled descent made by the airplane from cruise altitude are consistent with a loss of engine power before impact. The nose-down impact attitude is consistent with the airplane entering an aerodynamic stall at low altitude. The accident is consistent with a total loss of engine power for reasons that could not be determined based on available evidence. Contributing to the accident was the pilot’s decision to turn away from a suitable emergency landing surface, his failure to maintain adequate airspeed as the airplane neared the ground, and his exceedance of the airplane’s critical angle of attack, which resulted in an aerodynamic stall.
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 emergency descent
- Unknown or undetermined during enroute (cruise) defining event
- Fire/smoke (post-impact) during post (impact)
- Aerodynamic stall/spin during emergency descent
The NTSB's findings
- Aircraft › Aircraft power plant › Engine (reciprocating) › (general) › Unknown/Not determined other cases naming the engine
- Personnel issues › Action/decision › Info processing/decision › Decision making/judgment › Pilot
- Aircraft › Aircraft oper/perf/capability › Performance/control parameters › Altitude › Attain/maintain not possible
- Aircraft › Aircraft oper/perf/capability › Performance/control parameters › Airspeed › Not attained/maintained
Pilot
- Certificate: private
- Ratings: single-engine land
- Medical certificate: Class 3 (without waivers/limitations)
- Seat: left
- Injury: fatal
Passenger
- Seat: rgt
- Injury: fatal
The aircraft
- Airframe total time: 314 hours
- Last inspection: condition inspection, April 4, 2021
- Seats: 2
- Landing gear: fixed
- Engine: Lycoming O-320-E2C (piston); 0 hours total
- Fire on the ground
The flight
- Departed from: SDM San Diego CA at 7:10 pm
- Destination: OLS Nogales AZ
- Flight plan: none
Weather at the time
- Light: daylight
- Visibility: 3 statute miles
- Sky: clear
- Temperature: 94°F (34°C), dew point 56°F (13°C)
- Altimeter: 28.60 inHg
- Observation at 1:30 pm from GILA, 36 miles away
Weather report (METAR): 1:51 PM 94 °F 56 °F 28 % S 3 mph 0 mph 28.60 in 0.0 in Fair
Injuries
| Fatal | Serious | Minor | None | |
|---|---|---|---|---|
| Flight crew | 1 | |||
| Passengers | 1 |
Photographs from the investigation 11 pictures from the NTSB's docket, as the NTSB released them
Photo 1 – Accident Site
Photo 2 - Engine
Photo 3 – Aft Side of Engine
Photo 4 – Propeller Spinner
Photo 5 – Propeller Hub
Photo 6 – Propeller Blade Fragments
Photo 7 – Spark Plugs (Lycoming Photo)
Photo 8 – Cylinders and Pistons (Lycoming Photo)
Photo 9 – Right Engine Case (Lycoming Photo)
Photo 10 – Left Engine Case (Lycoming Photo)
Photo 11 – Camshaft and Piston Rods (Lycoming Photo)The NTSB's photographs with the NTSB's captions, at screen size. Open a picture to see it full size or to report one that should not be shown.
Documents from the investigation the NTSB's docket: the evidence folder behind the report
9 documents, released by the NTSB on April 25, 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 | Wreckage and Engine Examination Notes | PDF, 8 pages · our copy | View Download |
| 2 | Raw ADS-B Data | spreadsheet · our copy | Download |
| 3 | Opsvue Raw Data | spreadsheet · our copy | Download |
| 4 | ADS-B Final Flight Track | PDF, 1 page · our copy | View Download |
| 5 | Maintenance Records | PDF, 13 pages · our copy | View Download |
| 6 | Autopsy Memorandum | PDF, 1 page · our copy | View Download |
| 7 | Photos | PDF, 11 pages · our copy | View Download |
| 8 | Statement of Party Representatives to NTSB Investigation | PDF, 14 pages · our copy | View Download |
| 9 | Release of Aircraft Wreckage, NTSB Form 6120.15 | PDF, 2 pages · our copy | View Download |
Other NTSB records under N646RV the same tail number, which may have belonged to a different aircraft at the time
Connections how this case links to the rest of the register
- N646RV on the register today · the tail number may have moved to another aircraft since
- Engine: Lycoming O-320-E2C 11 aircraft carry this series today · as the NTSB recorded it
- Brown Field Municipal · departed from
- Nogales International · bound for
- Accidents and incidents in Arizona 2,985 since 1982 · 468 in the last ten years
- Arizona 8,431 aircraft registered
- Other NTSB records under N646RV 1 records · the number may have belonged to another aircraft at the time
The whole map of how records connect · these connections as data: /graph/accident/WPR22FA348.json.
The bigger picture in Aviation Analytics: accidents over time since 1982, by model, by phase of flight and conditions, by place and on the map.
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 does not name anyone involved, its policy at this time. A preliminary report can change; the final report usually follows one to two years later, and the page is refreshed when it does.
