Schweizer Aircraft CORP G-164B accident near Tracy, California, July 30, 2021
On July 30, 2021 at about 9:23 pm local time, a 1984 Schweizer Aircraft CORP G-164B, registered N3629F, was substantially damaged in an accident during emergency descent near Tracy, California. It was an aerial application (crop spraying) flight under agricultural flying rules (Part 137). 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
A loss of thrust during a low-level agricultural application flight, which resulted in a descent and impact with terrain. The reason for the loss of thrust could not be determined based on available information.
Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.
What the record shows
- Date
- July 30, 2021 · about 9:23 pm local time
- Place
- Tracy, California · map
- Type
- Accident
- Injuries
- No one was hurt; 1 person was on board or involved.
- Weather
- visual conditions (good weather)
- Aircraft
- Schweizer Aircraft CORP G-164B, built 1984 · all G-164Bs on the register
- Registration
- N3629F · no longer on the register · serial 745B
- Damage
- Substantial damage
- Flight
- Aerial application (crop spraying) flight · agricultural flying rules (Part 137)
The NTSB's narrative final · quoted from the NTSB record
The pilot reported that he was performing a low-level agricultural pesticide application on a hay field when the engine suddenly lost all power. Although the airplane was at a high airspeed at the time, the pilot was unable to climb due to the presence of high-tension powerlines above him in his flightpath. During the subsequent descent, he flew beneath a set of powerlines, turned, and landed in a field after his airspeed had decreased. During the landing, the airplane contacted the ground and trees, which resulted in substantial damage to the fuselage and wings. Postaccident examination of the engine and accessories did not reveal any mechanical anomalies that could have precluded normal operation. Evidence of rotational scoring and metal spray deposits in the engine indicate that it was operating at the time of impact. The fuel solenoid shutoff valve was in the CLOSED position, which would have prevented fuel flow to the engine. However, due to the overwhelming evidence that the engine was rotating at the time of impact, it is likely that the shutoff valve moved to the CLOSED position as a result of the impact. Propeller signatures indicated that the blades impacted the ground while rotating at low power. An examination of the propeller did not reveal any visible discrepancies that would have affected performance prior to impact. The damage to the start lock brackets, start lock plates, and a contact mark on the internal surface of the piston suggest the propeller was on or below the start lock angle at impact. This was likely the result of impact forces, as the pilot stated that he did not reduce throttle input or attempt to feather blades before impact. Previous maintenance indicated that the blade radius was properly set. The pilot did not recall the power lever position at the time of the power loss and the investigation did not reveal any evidence of preimpact mechanical malfunctions or failures. Therefore, the reason for the pilot’s reported loss of power could not be determined.
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 engine power (total) during maneuvering (low-alt flying)
- Unknown or undetermined during emergency descent defining event
The NTSB's findings
- Aircraft › Aircraft power plant › Engine (turbine/turboprop) › (general) › Failure
- Aircraft › Aircraft power plant › Engine (turbine/turboprop) › (general) › Unknown/Not determined
Pilot
- Certificate: airline transport pilot, flight instructor
- Ratings: multi-engine land; single-engine land; instructor: airplane multi-engine; instructor: airplane single-engine; instructor: helicopter; instrument: airplane; rotorcraft: helicopter
- Flight time: 6,250 hours in all; 2,300 in this make and model; 5,843 as pilot in command
- Last flight review: January 8, 2021
- Medical certificate: Class 2 (with waivers/limitations)
- Seat: sngl
- Injury: no injuries
The aircraft
- Airframe total time: 197,778 hours
- Last inspection: 100-hour inspection, July 12, 2021; 58 hours since
- Maximum gross weight: 5,200 lb
- Seats: 1
- Landing gear: fixed
- Engine: Garrett/Honeywell TPE331-2 (turboprop); 10,204 hours total
The flight
- Departed from: NA Tracy CA at 9:10 pm
- Destination: NA Tracy CA
- Flight plan: none
Weather at the time
- Light: daylight
- Wind: from 320° at 11 knots, gusting 19
- Visibility: 10 statute miles
- Sky: clear
- Temperature: 104°F (40°C), dew point 32°F (0°C)
- Altimeter: 29.82 inHg
- Observation at 3:22 pm from TCY
Injuries
| Fatal | Serious | Minor | None | |
|---|---|---|---|---|
| Flight crew | 1 |
Documents from the investigation the NTSB's docket: the evidence folder behind the report
10 documents, released by the NTSB on June 8, 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 | Pilot/operator Aircraft Accident Report, NTSB Form 6120.1 | PDF, 10 pages | View Download |
| 2 | Email Correspondence with Accident Pilot | PDF, 4 pages | View Download |
| 3 | Aircraft Logbooks | PDF, 9 pages | View Download |
| 4 | Propeller Maintenance Records | PDF, 3 pages | View Download |
| 5 | Woodward Propeller Governor Functional Test Report | PDF, 1 page | View Download |
| 6 | Memorandum for Record, Honeywell Engine Teardown Report Excerpt | PDF, 6 pages | View Download |
| 7 | Fuel Control Unit Functional Test Report | PDF, 2 pages | View Download |
| 8 | Manufacturer Propeller Examination Report | PDF, 11 pages | View Download |
| 9 | Statement of Party Representatives to NTSB Investigation | PDF, 2 pages | View Download |
| 10 | Release of Aircraft Wreckage, NTSB Form 6120.15 | PDF, 2 pages | View Download |
The same docket at the NTSB · documents without a copy here are fetched from the NTSB when you open them.
Other NTSB records under N3629F 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.
