Amateur-built LEGACY RG accident near Gainesville, Georgia, November 17, 2018
On November 17, 2018 at about 11:35 pm local time, a 2015 amateur-built LEGACY RG, registered N8448J, was substantially damaged in an accident during approach (VFR pattern final) near Gainesville, Georgia (Lee Gilmer Memorial airport). It was an instructional flight under general aviation rules (Part 91). 1 person was killed and 1 person was seriously injured. The weather was visual conditions (good weather).
The NTSB's probable cause their words, unchanged
The pilots’ failure to execute a go-around when the nighttime autopilot-coupled approach became unstable, which resulted in a loss of control and subsequent impact with terrain. Also causal was the flight instructor's inadequate supervision of the pilot and his failure to perform remedial action. Contributing to the accident was the inadvertent application of pressure to the pitch control while the autopilot was engaged, which caused an out-of-trim condition that was not identified by either pilot and resulted in control difficulty when the autopilot was disengaged.
Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.
What the record shows
- Date
- November 17, 2018 · about 11:35 pm local time
- Place
- Gainesville, Georgia · Lee Gilmer Memorial · map
- Type
- Accident
- Injuries
- 1 person was killed and 1 person was seriously injured.
- Weather
- visual conditions (good weather)
- Aircraft
- Amateur-built LEGACY RG No Series, built 2015
- Registration
- N8448J · no longer on the register · serial L2K-338
- Damage
- Substantial damage
- Flight
- Instructional flight · general aviation rules (Part 91)
The NTSB's narrative final · quoted from the NTSB record
The pilot/owner and flight instructor were returning from a cross-country flight and arrived in the vicinity of the airport after dark in visual meteorological conditions. The flight instructor requested (to the air traffic controller) and was cleared for a practice GPS approach to the runway, which was equipped with precision approach path indicator (PAPI) lighting. Flight data indicated the approach was flown using the autopilot. Just after the airplane passed the final approach fix, the flaps were partially extended, the pitch attitude decreased, and the airplane descended below the glidepath. The autopilot commanded nose up elevator and the airplane returned to slightly above the glidepath where it remained stable for about 16 seconds, before drifting to nearly a full-scale course deviation above the glidepath. The autopilot commanded the elevator to nose down, and the electric pitch trim to near the full nose-down position. The autopilot was then disconnected. Although the autopilot can automatically disengage in the event of a system failure, no failures were observed in the recorded data. Therefore, it was likely that the autopilot was manually disengaged. About 15 seconds later, the flaps were extended to full and then fully retracted. The descent rate increased, and the airplane descended below the glidepath, until the recorded data ended when the airplane was about 0.3 mile from the runway. The airplane then struck trees, crossed over a road, and impacted the left side of a localizer antenna platform before coming to rest in the grass short of the runway. Examination of the wreckage and the recorded flight data did not reveal any preimpact electrical or mechanical anomalies that would have precluded normal operation. The pilot's guide for the autopilot system warned that with the autopilot engaged, a small amount of force on the pitch controls can result in the autopilot automatic trim entering an out-of-trim condition. As the airplane drifted above the glidepath, the autopilot attempted to command nose-down elevator, and the elevator servo met with some resistance, as evidenced by the increase in elevator servo torque, which was sufficient to activate the electric pitch trim. Given that there were no indications of a flight control malfunction, it is likely that one of the pilots was applying pressure to the elevator control in the cockpit, and the autopilot applied elevator trim to counteract that pressure, in its attempt to return to the glidepath. At the time the autopilot was disengaged, the pitch trim was full nose down, which likely resulted in an unexpected increase in the (forward) force the pilot felt on the control stick, making it more difficult to control the airplane. The airplane's nose-down tendency would have increased further when the flaps were subsequently extended to full. This would have resulted in an even greater forward force on the control stick. It is likely that the pilot decided to then retract the flaps fully, due to the increased nose-down force on the control stick. However, the flap retraction resulted in an increased descent rate, and the airplane descended farther below the glidepath. A witness and the flight instructor reported that the airplane rolled inverted before impact. The recorded flight data, which ended when the airplane was on the extended runway centerline about 0.3 mile from the runway and about 50 ft above the runway elevation, did not indicate that the airplane had rolled inverted. The struck trees were also located on the extended runway centerline, about 0.1 mile from the end of the runway. Therefore, it is unlikely that the airplane experienced any significant lateral course deviation or roll, between the end of the recorded data and the struck trees. It is likely that the roll occurred after the airplane struck the trees and before it impacted the localizer antenna platform. The flight instructor had limited memory of the accident flight. He recalled that the pilot/owner was flying the airplane during the approach; however, the investigation was unable to determine which pilot was manipulating the controls at the time of 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 approach (VFR pattern final) defining event
- Collision with terrain or object (not controlled flight into terrain) during uncontrolled descent
The NTSB's findings
- cause Aircraft › Aircraft oper/perf/capability › Performance/control parameters › Descent/approach/glide path › Not attained/maintained
- cause Personnel issues › Action/decision › Action › Lack of action › Pilot
- cause Personnel issues › Task performance › Use of equip/info › Aircraft control › Pilot
- cause Personnel issues › Psychological › Attention/monitoring › Monitoring other person › Instructor/check pilot
- factor Aircraft › Aircraft systems › Auto flight system › Autopilot trim servo › Unintentional use/operation
- Environmental issues › Conditions/weather/phenomena › Light condition › Dark › Effect on personnel
- Personnel issues › Action/decision › Info processing/decision › Identification/recognition › Pilot
- Personnel issues › Action/decision › Info processing/decision › Identification/recognition › Instructor/check pilot
- Personnel issues › Action/decision › Action › Lack of action › Instructor/check pilot
- Personnel issues › Task performance › Use of equip/info › Aircraft control › Instructor/check pilot
Pilot
- Certificate: private
- Ratings: single-engine land
- Flight time: 289 hours in all; 96 in this make and model
- Medical certificate: Class 3 (with waivers/limitations)
- Seat: left
- Injury: fatal
Flight instructor
- Certificate: airline transport pilot, flight instructor
- Ratings: multi-engine land; single-engine land; instructor: airplane multi-engine; instructor: airplane single-engine; instructor: instrument airplane; instrument: airplane
- Flight time: 7,500 hours in all; 52 in this make and model
- Medical certificate: Class 3 (with waivers/limitations)
- Seat: rgt
- Injury: serious injuries
The aircraft
- Airframe total time: 358 hours
- Last inspection: condition inspection, December 3, 2017; 149 hours since
- Seats: 2
- Landing gear: retractable
- Engine: Continental Motors IO-550-N8B (piston); 358 hours total
The flight
- Departed from: JZI Charleston SC at 10:28 pm
- Destination: GVL Gainesville GA
- Flight plan: none
- Runway 23, 5,500 ft by 100 ft
- A second pilot was aboard
Weather at the time
- Light: night
- Wind: from 130° at 3 knots
- Visibility: 10 statute miles
- Sky: clear
- Temperature: 52°F (11°C), dew point 39°F (4°C)
- Altimeter: 30.20 inHg
- Observation at 11:53 pm from GVL
Injuries
| Fatal | Serious | Minor | None | |
|---|---|---|---|---|
| Flight crew | 1 | 1 |
Documents from the investigation the NTSB's docket: the evidence folder behind the report
22 documents, released by the NTSB on October 9, 2020. 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.
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.
