Grumman G-164A accident near Toccoa, Georgia, June 29, 2024
On June 29, 2024 at about 10:40 pm local time, a 1971 Grumman G-164A, registered N7849, was substantially damaged in an accident during landing (landing roll) near Toccoa, Georgia (Toccoa Airport-Rg Letourneau F). It was a positioning flight under general aviation rules (Part 91). No one was hurt; 1 person was on board or involved. The weather was visual conditions (good weather).
The NTSB's probable cause their words, unchanged
The pilot’s failure to set the engine speed control fully forward during takeoff, resulting in an engine surge and subsequent loss of control during landing.
Source: NTSB aviation accident database, copy made November 2, 2026. Docket and reports at the NTSB.
What the record shows
- Date
- June 29, 2024 · about 10:40 pm local time · cases in 2024
- Place
- Toccoa, Georgia · Toccoa Airport-Rg Letourneau F · cases near this airport · map
- Type
- Accident
- Injuries
- No one was hurt; 1 person was on board or involved.
- Weather
- visual conditions (good weather)
- Aircraft
- Grumman G-164A, built 1971 · all G-164As on the register
- Registration
- N7849 · registry record · serial 797
- Damage
- Substantial damage
- Flight
- Positioning flight · general aviation rules (Part 91)
The NTSB's narrative final · quoted from the NTSB record
The pilot of the turbo propeller-powered agricultural airplane reported that, during takeoff for a cross-county flight, the engine rpm did not reach 100% but he continued the flight. Shortly after takeoff, the engine appeared to surge and the pilot decided to return to the departure airport. As he approached the airport, the surging worsened and, after touchdown, the engine power started to increase. He tried to shut down the engine, but the power continued to increase. He applied heavy braking to slow the airplane; the left brake then locked, and the airplane departed the runway and the airplane’s wings were substantially damaged. Postaccident examination of the engine revealed damage indicative of an engine that was rotating and operating at the time of impact; no pre-existing condition was found that would have prevented normal engine operation or control. The engine manufacturer issued a Pilot Advisory Letter more than 10 years before the accident addressing the issue of engine oscillations. The letter noted: When performing a takeoff, pilots normally advance the power lever(s) to a takeoff value as specified in the POH/AFM and as indicated on the torque (or equivalent) gauge. If a takeoff is attempted with the Engine Speed Control(s) in any position other than full forward, resulting in the engine not achieving 100-101% RPM, the engine(s) may very well achieve the desired indicated torque; however, the engine(s) will actually develop a reduced level of horsepower. A reduced level of horsepower will result in the degradation of aircraft performance. The letter added that, “One and possibly two adverse effects can result if a takeoff is attempted with the Engine Speed Control(s) in any position other than full forward. They are reduced power output from the engine(s) and the possibility of accompanying engine oscillations.” Since the previous 22 hours of flying did not demonstrate this type of engine behavior, postaccident examination of the engine found no issues that would have prevented normal operation, and the pilot reported both not achieving 100% speed as well as engine oscillations during and after takeoff, the pilot likely did not advance the engine speed control fully forward during takeoff.
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 on ground during landing (landing roll) defining event
- Miscellaneous/other during enroute (climb to cruise)
The NTSB's findings
- Aircraft › Aircraft oper/perf/capability › Performance/control parameters › Powerplant parameters › Incorrect use/operation
- Personnel issues › Action/decision › Action › Incorrect action performance › Pilot
- Aircraft › Aircraft oper/perf/capability › Performance/control parameters › Directional control › Not attained/maintained
Pilot
- Certificate: commercial pilot
- Ratings: single-engine land
- Flight time: 1,001 hours in all
- Medical certificate: Class 2 (without waivers/limitations)
- Seat: sngl
- Injury: no injuries
The aircraft
- Airframe total time: 12,212.1 hours
- Last inspection: 100-hour inspection, May 1, 2024
- Seats: 1
- Landing gear: fixed
- Engine: Honeywell TPE 331-1-151 (piston); 0 hours total
The flight
- Destination: ARG Walnut Ridge AR
- Flight plan: none
- Runway 21, 5,008 ft by 100 ft
Weather at the time
- Light: daylight
- Wind: from 090° at 4 knots
- Visibility: 10 statute miles
- Sky: broken clouds at 3,900 ft
- Temperature: 90°F (32°C), dew point 73°F (23°C)
- Altimeter: 30.08 inHg
- Observation at 6:35 pm from TOC
Weather report (METAR): KTOC 292235Z AUTO 09004KT 10SM BKN039 BKN050 32/23 A3008 RMK AO2 T03250227
Injuries
| Fatal | Serious | Minor | None | |
|---|---|---|---|---|
| Flight crew | 1 |
Photographs from the investigation 2 pictures from the NTSB's docket, as the NTSB released them
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
10 documents, released by the NTSB on September 11, 2025. 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 | Memorandum for Record - 6120.1 Pilot/operator Report Form | PDF, 1 page | View Download |
| 2 | Memorandum for Record A�� Telephone Interview, Pilot | PDF, 1 page | View Download |
| 3 | Maintenance Records | PDF, 5 pages | View Download |
| 4 | Honeywell Pilot Advisory Letter | PDF, 2 pages | View Download |
| 5 | Honeywell Teardown Report | PDF, 177 pages | View Download |
| 6 | Honeywell Metallurgy Report | PDF, 14 pages | View Download |
| 7 | Investigative Photographs | PDF, 3 pages · our copy | View Download |
| 8 | Wreckage Examination Summary | PDF, 5 pages | View Download |
| 9 | Statement of Party Representatives to NTSB Investigation | PDF, 1 page | View Download |
| 10 | Evidence Control Form | PDF, 1 page | View Download |
The same docket at the NTSB · documents without a copy here are fetched from the NTSB when you open them.
Connections how this case links to the rest of the register
- N7849 on the register today · the tail number may have moved to another aircraft since
- Grumman G-164 119 registered today · the model family and its accident history
- Grumman 443 aircraft on the register
- Engine: Honeywell TPE 331-1-151 27 aircraft carry this series today · as the NTSB recorded it
- Toccoa RG Letourneau Field · nearest airport
- Walnut Ridge Regional · bound for
- Accidents and incidents in Georgia 2,138 since 1982 · 361 in the last ten years
- Georgia 8,801 aircraft registered
The whole map of how records connect · these connections as data: /graph/accident/ERA24LA286.json.
The bigger picture in Aviation Analytics: accidents over time since 1982, by model, by phase of flight and conditions, by place and on the map.
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 does not name anyone involved, its policy at this time. A preliminary report can change; the final report usually follows one to two years later, and the page is refreshed when it does.


