Mooney M20F accident near Villa Rica, Georgia, November 8, 2021
On November 8, 2021 at about 5:57 pm local time, a 1967 Mooney M20F, registered N3284F, was substantially damaged in an accident during maneuvering near Villa Rica, Georgia (Earl L Small JR Fld/Stockmar 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 maintain proper airspeed and his exceedance of the airplane’s critical angle of attack, which resulted in an aerodynamic stall and spin.
Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.
What the record shows
- Date
- November 8, 2021 · about 5:57 pm local time
- Place
- Villa Rica, Georgia · Earl L Small JR Fld/Stockmar · map
- Type
- Accident
- Injuries
- 1 person was killed.
- Weather
- visual conditions (good weather)
- Aircraft
- Mooney M20F, built 1967 · all M20Fs on the register
- Registration
- N3284F · registry record · serial 670377
- Damage
- Substantial damage
- Flight
- Personal flight · general aviation rules (Part 91)
The NTSB's narrative final · quoted from the NTSB record
The pilot was performing a personal flight. The airplane departed the traffic pattern, flew 2 miles north, and then turned and flew west for 1 mile. During the final 2 minutes of the flight, the airplane’s ground speed slowed from 102 to 49 mph. After the ground speed decreased to about 55 mph, the airplane abruptly turned left and rapidly descended. The final data return was recorded when the airplane was about 100 ft above ground level and 80 ft from the accident site. A home surveillance video that captured the final moments of the accident flight showed that the airplane was in a steep descending left bank before impacting the ground. Another home surveillance video captured the sound of the engine until impact. Postaccident examination of the airplane revealed no evidence of preimpact mechanical malfunctions that would have precluded normal operation. The propeller signatures, cut tree roots, audio recording, and engine data were all consistent with the engine producing power at the time of impact. The weight and balance of the airplane and flap configuration (either extended flaps of 15° or 33°) could not be determined. Nevertheless, according to the airplane owner’s manual, the airplane’s stall speed likely ranged from 62 to 68 mph. The exact weight and balance of the airplane and flap configuration between extended flaps of 15° or 33° could not be determined. Thus, the available evidence for this accident (the automatic dependent surveillance-broadcast (ADS-B) data, GPS data, and surveillance videos) showed that the pilot likely allowed the airplane’s airspeed to decay below the aerodynamic stall speed for any configuration, which caused the airplane’s critical angle of attack to be exceeded. As a result, the airplane entered an aerodynamic stall and spin from which the pilot was unable to recover.
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 maneuvering
- Aerodynamic stall/spin during maneuvering defining event
The NTSB's findings
- Aircraft › Aircraft oper/perf/capability › Performance/control parameters › Airspeed › Not attained/maintained
- Personnel issues › Task performance › Use of equip/info › Aircraft control › Pilot
- Aircraft › Aircraft oper/perf/capability › Performance/control parameters › Angle of attack › Not attained/maintained
Pilot
- Certificate: airline transport pilot, commercial pilot, flight engineer
- Ratings: multi-engine land; single-engine land; instrument: airplane
- Flight time: 18,440 hours in all; 11.2 in the last 90 days; 3 in the last 30 days
- Last flight review: December 10, 2020
- Medical certificate: Class 3 (with waivers/limitations)
- Seat: left
- Injury: fatal
The aircraft
- Airframe total time: 3,760 hours
- Last inspection: annual inspection, October 1, 2020
- Maximum gross weight: 2,740 lb
- Seats: 4
- Landing gear: retractable
- Engine: Lycoming IO-360-A1A (piston); 3,782 hours total
The flight
- Flight plan: none
- Runway 10/2, 4,500 ft by 50 ft
Weather at the time
- Light: daylight
- Wind: from 130° at 3 knots
- Visibility: 10 statute miles
- Sky: clear
- Temperature: 68°F (20°C), dew point 32°F (0°C)
- Altimeter: 30.29 inHg
- Observation at 12:55 pm from PUJ, 7 miles away
Weather report (METAR): KPUJ 081755Z AUTO 13003KT 10SM CLR 20/00 A3029 RMK AO2
Injuries
| Fatal | Serious | Minor | None | |
|---|---|---|---|---|
| Flight crew | 1 |
Documents from the investigation the NTSB's docket: the evidence folder behind the report
21 documents, released by the NTSB on August 30, 2023. 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 | Witness Statements | PDF, 4 pages | View Download |
| 2 | Visual Capture of Accident Flight - Final Moments | MOV file | Download |
| 3 | Audio Capture of Accident Flight - Final Moments | MOV file | Download |
| 4 | Weather Reports and Records | PDF, 2 pages | View Download |
| 5 | ADS-B Tabular Data | spreadsheet | Download |
| 6 | Flight Track Maps | PDF, 4 pages | View Download |
| 7 | GPS Factual Report | PDF, 5 pages | View Download |
| 8 | GPS Factual Report - Attachment 1 - Tabular Data | spreadsheet | Download |
| 9 | Wreckage Examination Summary | PDF, 17 pages | View Download |
| 10 | Pilot Logbook | PDF, 21 pages | View Download |
| 11 | Airframe Log Excerpts | PDF, 14 pages | View Download |
| 12 | Engine Log Excerpts | PDF, 10 pages | View Download |
| 13 | Propeller Log Excerpts | PDF, 8 pages | View Download |
| 14 | Engine Data Monitor - Specialist's Factual REPORT_ERA22FA050 | PDF, 6 pages | View Download |
| 15 | Attachment 1 to Engine Data Monitor - Specialist's Factual REPORT_ERA22FA050 - Tabular Data | data file | Download |
| 16 | Attachment 2 to Engine Data Monitor - Specialist's Factual REPORT_ERA22FA050 - Tabular Data | data file | Download |
| 17 | Airplane Owner's Manual Excerpt | PDF, 2 pages | View Download |
| 18 | Toxicological Report | PDF, 1 page | View Download |
| 19 | Memorandum for Record - Autopsy Results | PDF, 1 page | View Download |
| 20 | Statement of Party Representatives to NTSB Investigation | PDF, 9 pages | View Download |
| 21 | Release of Aircraft Wreckage, NTSB Form 6120.15 and Other Evidence Control Forms | PDF, 3 pages | 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.
