Amateur-built VANS RV-7A accident near White Hills, Arizona, February 19, 2022
On February 19, 2022 at about 8:28 pm local time, a 2019 amateur-built VANS RV-7A, registered N787NV, was destroyed in an accident during maneuvering near White Hills, Arizona (Triangle Airpark 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 improper aerobatic maneuver leading to an airspeed that exceeded the airplane’s design limits, which resulted in rudder flutter and an in-flight breakup.
Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.
What the record shows
- Date
- February 19, 2022 · about 8:28 pm local time
- Place
- White Hills, Arizona · Triangle Airpark · map
- Type
- Accident
- Injuries
- 1 person was killed.
- Weather
- visual conditions (good weather)
- Aircraft
- Amateur-built VANS RV-7A, built 2019
- Registration
- N787NV · registry record · serial 72097
- Damage
- Destroyed
- Flight
- Personal flight · general aviation rules (Part 91)
The NTSB's narrative final · quoted from the NTSB record
The pilot was conducting a personal flight in his experimental, amateur-built airplane. The flight data revealed that the pilot made multiple 90-degree turns before the airplane’s flight path became established over a highway. The airplane then entered a maneuver that was consistent with an aileron roll where it lost about 1,000 ft of altitude. A few minutes later the airplane entered a maneuver consistent with a split-S. Security video near the accident site captured the airplane in a steep nose-down descent before impacting the ground near airport hangars. Several objects from the airplane were seen falling to the ground south of the accident site. In another security video, an image of the airplane showed that the left horizontal stabilizer and elevator and the vertical stabilizer and rudder had separated from the empennage. A portion of the right horizontal stabilizer and elevator remained attached to the empennage. The left wing tip and canopy also separated. The accident site debris field revealed that the rudder and rudder surface skin were the furthest separated components from the impact crater and main wreckage, indicating that the rudder was likely the first component to fail. The remaining separated components were found in the debris field. The airplane data revealed that the pilot entered the split-S maneuver at an airspeed that exceeded the published manufacturer’s airspeed for that maneuver. The airplane then rolled to an inverted position and pitched down causing the airspeed to increase dramatically. The last recorded data point, at an altitude about 3,199 ft, showed the airspeed was 248 KIAS (262 KTAS), well above the published never exceed speed of 200 knots. The high airspeed allowed rudder flutter to occur, resulting in an in-flight breakup and subsequent impact with terrain. A postaccident examination of the airframe revealed damage consistent with an in-flight rudder flutter event that resulted in an in-flight breakup and subsequent impact with terrain. There were no indications of any pre-existing cracks or anomalies with the airframe structures, and no pre-accident anomalies were observed that would have precluded normal control of the airplane.
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 oper/perf/capability › Performance/control parameters › Airspeed › Capability exceeded
- Aircraft › Aircraft oper/perf/capability › Performance/control parameters › Airspeed › Capability exceeded
- Personnel issues › Task performance › Use of equip/info › Aircraft control › Pilot
Pilot
- Certificate: airline transport pilot, flight instructor, commercial pilot, flight engineer
- Ratings: single-engine land; single-engine sea; instructor: airplane multi-engine; instructor: airplane single-engine; instrument: airplane
- Flight time: 25,200 hours in all; 25 in the last 90 days
- Medical certificate: Class 3 (with waivers/limitations)
- Seat: unk
- Injury: fatal
The aircraft
- Seats: 2
- Landing gear: fixed
- Engine: Lycoming YIO-360-M1B (piston); 0 hours total
The flight
- Departed from: BVU Boulder City NV at 9:15 pm
- Flight plan: none
Weather at the time
- Light: daylight
- Wind: from 050° at 6 knots
- Visibility: 10 statute miles
- Sky: clear
- Temperature: 68°F (20°C), dew point 16°F (-9°C)
- Altimeter: 30.11 inHg
- Observation at 1:35 pm from KBVU, 23 miles away
Weather report (METAR): KBVU 192135Z AUTO 05006KT 10SM CLR 20/M09 A3011 RMK AO2
Injuries
| Fatal | Serious | Minor | None | |
|---|---|---|---|---|
| Flight crew | 1 |
Documents from the investigation the NTSB's docket: the evidence folder behind the report
17 documents, released by the NTSB on April 10, 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.
