Piper PA-46-310P accident near Dawsonville, Georgia, December 3, 2013
On December 3, 2013, a 1987 Piper PA-46-310P, registered N87NF, was destroyed in an accident during enroute near Dawsonville, Georgia. It was a personal flight under general aviation rules (Part 91). 1 person was killed. The weather was instrument conditions (cloud, fog or low visibility).
The NTSB's probable cause their words, unchanged
The pilot’s in-flight loss of airplane control due to spatial disorientation while operating in dark night instrument meteorological conditions, which resulted in the exceedance of the airplane’s design stress limitations and a subsequent in-flight breakup. Contributing to the accident was the pilot’s distraction by the reported malfunction of the autopilot system.
Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.
What the record shows
- Date
- December 3, 2013
- Place
- Dawsonville, Georgia · map
- Type
- Accident
- Injuries
- 1 person was killed.
- Weather
- instrument conditions (cloud, fog or low visibility)
- Aircraft
- Piper PA-46-310P, built 1987 · all PA-46-310Ps on the register
- Registration
- N87NF · no longer on the register · serial 4608099
- Damage
- Destroyed
- Flight
- Personal flight · general aviation rules (Part 91)
The NTSB's narrative final · quoted from the NTSB record
The pilot filed an instrument flight rules flight plan for the flight and was communicating with an air route traffic control center controller en route. The controller verified that the pilot had the local weather information for the intended destination and then he queried the pilot about the airplane's heading (which was north of the direct heading), and the pilot reported that he was having trouble with the autopilot. He then asked the pilot if he was able to hold the assigned altitude of 8,000 ft mean sea level (msl), and the pilot responded that he could; however, the airplane descended below 8,000 ft msl, and the controller then issued an altitude of 7,000 ft msl and a heading of 200 degrees. There was no response from the pilot, and radar contact was lost. Shortly after, the airplane wreckage was found. According to air traffic control radar data, the airplane turned left and then right before entering a descending left turn. A trajectory and performance study determined that, during the flight's final 18 seconds, the airplane descended from about 8,000 to 2,200 ft msl, accelerated to about 300 knots indicated airspeed, and then broke up. According to the Pilot's Operating Handbook, the airplane's maximum operating limit speed was 172 knots. Examinations of the airframe, engines, and autopilot revealed no preimpact mechanical malfunctions that would have precluded normal operations, and there was no evidence of medical impairment that would have affected the pilot's performance. The pilot held an instrument rating; however, investigators were unable to determine the extent of the pilot's recent night or instrument flight experience. Although postaccident testing did not reveal any anomalies with the autopilot system, the pilot should have been able to disable the autopilot if it was experiencing a problem and then continue to fly the airplane. However, given the available data and his conversation with the controller, it is likely that the pilot became focused on the autopilot system and diagnosing the reported problem. Dark (moonless) night conditions prevailed for the flight, and, about the time of the accident, instrument meteorological conditions with restricted visibility due to rain prevailed. Given the pilot's distraction, the weather conditions encountered during the flight, and the sustained descending left turn, it is likely that the pilot experienced spatial disorientation and then lost 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
- Unknown or undetermined during enroute
- Loss of control in flight during enroute defining event
- Collision with terrain or object (not controlled flight into terrain) during uncontrolled descent
The NTSB's findings
- factor Aircraft › Aircraft systems › Auto flight system › Autopilot system › Not specified
- cause Personnel issues › Task performance › Use of equip/info › Aircraft control › Pilot
- cause Personnel issues › Psychological › Perception/orientation/illusion › Spatial disorientation › Pilot
- factor Personnel issues › Psychological › Attention/monitoring › (general) › Pilot
- cause Aircraft › Aircraft oper/perf/capability › Performance/control parameters › (general) › Not attained/maintained
- cause Environmental issues › Conditions/weather/phenomena › Light condition › Dark › Effect on operation
- cause Environmental issues › Conditions/weather/phenomena › Ceiling/visibility/precip › Low ceiling › Effect on equipment
Pilot
- Certificate: private
- Ratings: multi-engine land; single-engine land; instrument: airplane
- Flight time: 3,500 hours in all
- Medical certificate: Class 3 (with waivers/limitations)
- Seat: left
- Injury: fatal
The aircraft
- Airframe total time: 5,904.4 hours
- Last inspection: annual inspection, January 29, 2013
- Maximum gross weight: 4,101 lb
- Seats: 6
- Landing gear: retractable
- Engine: Pratt And Whitney PT6A-34 (turboprop); 0 hours total
- Operator: Culbair LLC
The flight
- Departed from: MMU Morristown NJ at 9:35 pm
- Destination: PDK Atlanta GA
- Flight plan: IFR
Weather at the time
- Light: night, dark
- Visibility: 4 statute miles
- Sky: overcast at 500 ft
- Temperature: 50°F (10°C), dew point 48°F (9°C)
- Altimeter: 29.86 inHg
- Observation at 11:53 pm from GVL, 12 miles away
Injuries
| Fatal | Serious | Minor | None | |
|---|---|---|---|---|
| Flight crew | 1 |
Documents from the investigation the NTSB's docket: the evidence folder behind the report
The docket, the folder of records gathered during an investigation (maintenance records, photographs, witness statements, examinations), has not been read from the NTSB for this case yet; the list appears here once it has. Open the docket at the NTSB.
Other NTSB records under N87NF the same tail number, which may have belonged to a different aircraft at the time
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.
