Raytheon Aircraft Company A36 accident near Greenville, North Carolina, March 14, 2025
On March 14, 2025 at about 11:49 am local time, a 2005 Raytheon Aircraft Company A36, registered N566C, was destroyed in an accident during initial climb near Greenville, North Carolina (Pitt-Greenville Airport). It was a personal flight under general aviation rules (Part 91). 2 people were killed. The weather was instrument conditions (cloud, fog or low visibility).
The NTSB's probable cause their words, unchanged
The pilot’s loss of airplane control shortly after climbing into instrument meteorological conditions due to spatial disorientation (somatogyral illusion).
Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.
What the record shows
- Date
- March 14, 2025 · about 11:49 am local time
- Place
- Greenville, North Carolina · Pitt-Greenville Airport · map
- Type
- Accident
- Injuries
- 2 people were killed.
- Weather
- instrument conditions (cloud, fog or low visibility)
- Aircraft
- Raytheon Aircraft Company A36, built 2005
- Registration
- N566C · registry record · serial E-3621
- Damage
- Destroyed
- Flight
- Personal flight · general aviation rules (Part 91)
The NTSB's narrative final · quoted from the NTSB record
The instrument-rated private pilot and passenger were departing on an instrument flight rules (IFR) flight. The weather conditions that preceded and persisted until the time of the takeoff consisted of low ceilings (300 ft), mist, and fog with instrument meteorological conditions (IMC) through most of the area. After departure, the pilot flew the runway heading and climbed briefly before turning right and descending to about 200 ft. The right turn then stopped and the airplane flew a relatively straight ground track and resumed the climb. While flying at an altitude of about 600 ft, with the airplane climbing at a vertical speed of about 1,800 feet per minute, the airplane continued for about a mile before entering another turn to the right. The airplane stopped climbing during this turn after it reached a peak altitude of 1,000 ft. Shortly after, the right turn progressively tightened as the airplane began a descending spiral. A witness observed the airplane rolling as it descended out of the clouds before impacting terrain. The airplane impacted the terrain at high-speed in a nearly 50° nose down, and steep right wing low attitude. Postaccident examination of the wreckage was limited by the level of impact-related damage and significant fragmentation. Within the wreckage that was examined, there was no indication of a preimpact mechanical malfunction or failure that would have precluded normal operation of the airframe or engine. Additionally, witness statements and impact signatures observed on the airplane’s propeller blades were consistent with the engine producing power at impact. The instrument-rated pilot had completed an instrument proficiency check about 2 months before the accident. Since then, he had accumulated additional experience that included flight in simulated and actual instrument meteorological conditions, and had conducted several instrument approaches, all in the accident airplane. While his flight logs suggested that he had some familiarity operating the airplane and its newly installed electronic flight instrumentation under instrument flight rules, the pilot’s overall level of proficiency could not be determined from available information. The airplane’s erratic flight track on the accident flight, which included arrested climbs, descents, and low altitude turns that culminated in a tightening turn and high-speed descent was indicative of the known effects of spatial disorientation, specifically the somatogyral illusion (graveyard spiral). During the initial climb, once the pilot entered the clouds and lost all outside visual cues, it would have been difficult to recognize and respond to spatial disorientation unless he was confident and assertive in his use of the airplane’s avionics package and flight instrumentation. The aortic plaque observed a postaccident autopsy of the pilot indicated some increased risk of an impairing or incapacitating cardiovascular event, although the magnitude of this risk was uncertain from the limited autopsy evidence. The limited qualitative toxicology results in tissue indicated that the pilot had used the sedating antihistamine medication diphenhydramine, but did not indicate the precise timing of his last use or whether he was experiencing associated impairing effects at the time of the accident. While the pilot had defective color vision, he had been approved for flight and there was no evidence to suggest that color vision played a role in the accident.
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 › Psychological › Perception/orientation/illusion › Spatial disorientation › Pilot
- Environmental issues › Conditions/weather/phenomena › Ceiling/visibility/precip › Low ceiling › Effect on personnel
- Environmental issues › Conditions/weather/phenomena › Ceiling/visibility/precip › Drizzle/mist › Effect on personnel
Pilot
- Certificate: private
- Ratings: single-engine land; instrument: airplane
- Flight time: 2,034 hours in all; 159 in this make and model; 1,788 as pilot in command
- Last flight review: January 12, 2025
- Medical certificate: BasicMed (with waivers/limitations)
- Seat: left
- Injury: fatal
Passenger
- Seat: left
- Injury: fatal
The aircraft
- Airframe total time: 1,085.4 hours
- Last inspection: annual inspection, July 3, 2024
- Maximum gross weight: 4,011 lb
- Seats: 4
- Landing gear: retractable
- Engine: Continental IO-550-39B (piston); 1,085 hours total
The flight
- Destination: VRB Vero Beach FL
- Flight plan: IFR
- Runway 2, 7,175 ft by 150 ft
Weather at the time
- Light: daylight
- Wind: from 070° at 6 knots
- Visibility: 10 statute miles
- Sky: not recorded at 500 ft; not recorded
- Temperature: 46°F (8°C), dew point 46°F (8°C)
- Altimeter: 30.08 inHg
- Observation at 7:50 am from PGV, 1 miles away
Weather report (METAR): KPGV 141150Z AUTO 07006KT 10SM 08/08 A3008 RMK AO2
Injuries
| Fatal | Serious | Minor | None | |
|---|---|---|---|---|
| Flight crew | 1 | |||
| Passengers | 1 |
Photographs from the investigation 4 pictures from the NTSB's docket, as the NTSB released them
Photograph 1 – Empennage near end of wreckage path. (NTSB)
Photograph 2 – Wreckage path left to right. (NTSB)
Photograph 3 – Wreckage path looking towards empennage. (NTSB)
Photograph 4 – Propeller damage after recovery. (NTSB)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
16 documents, released by the NTSB on September 8, 2026. 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.
