Beech 19A accident near Oroville, California, June 2, 2022
On June 2, 2022 at about 7:18 pm local time, a 1969 Beech 19A, registered N7641R, was substantially damaged in an accident during approach (VFR pattern crosswind) near Oroville, California (Oroville Muni airport). It was a personal flight under general aviation rules (Part 91). 2 people were killed. The weather was visual conditions (good weather).
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The NTSB's probable cause their words, unchanged
The pilot’s failure to maintain proper airspeed during a turn and his exceedance of the airplane’s critical angle of attack, which resulted in an accelerated stall. Contributing to the accident was the improper placement of the fuel selector, which resulted in fuel starvation and a partial loss of engine power.
Source: NTSB aviation accident database, copy made October 4, 2026. Docket and reports at the NTSB.
What the record shows
- Date
- June 2, 2022 · about 7:18 pm local time
- Place
- Oroville, California · Oroville Muni · map
- Type
- Accident
- Injuries
- 2 people were killed.
- Weather
- visual conditions (good weather)
- Aircraft
- Beech 19A, built 1969 · all 19As on the register
- Registration
- N7641R · registry record · serial MB-432
- Damage
- Substantial damage
- Flight
- Personal flight · general aviation rules (Part 91)
The NTSB's narrative final · quoted from the NTSB record
The accident pilot was a partial owner of the accident airplane, which had not flown for several months until he attempted to fly the airplane about 2 weeks before the accident. During this previous flight the pilot and his student were forced to abort two takeoff attempts after the airplane failed to climb. The pilot and pilot-rated passenger, who was also a flight instructor, had planned to fly the airplane on the day of the accident to troubleshoot the performance deficiency. During takeoff on the accident flight, the airplane reached an intermediate altitude before it started to settle momentarily. The airplane then continued to climb to a peak altitude of about 100 ft above ground level and then it started a right turn that progressively became steeper. Subsequently, the airplane impacted the ground in a nose-down attitude. An analysis of the engine harmonics during takeoff suggested that the engine may have encountered anomalies when the airplane began its right turn, but this could not be substantiated as postaccident examination of the airframe and engine did not reveal any preimpact mechanical anomalies. The fuel selector was found between the RIGHT tank detent and the OFF position at the accident site. During the flight 2 weeks earlier the accident the pilot had placed the handle in a similar position before takeoff. As there were no preimpact mechanical anomalies with the engine, it is likely that the improper placement of the fuel selector in the OFF position during takeoff resulted in fuel starvation and a partial loss of engine power. Performance computations indicated that the airplane was capable of a successful takeoff as it was below its maximum gross weight. The airplane’s center of gravity (CG) was nose-heavy, which likely would have resulted in difficulty in lifting the nose during takeoff and during reduced power situations. However, this CG condition is only likely to have affected takeoff and likely did not contribute to the accident. Recorded data suggests the airplane entered an accelerated stall in the turn when it exceeded the critical angle of attack without maintaining adequate airspeed. The investigation was unable to determine if the pilot-rated passenger was aware of the airplane’s takeoff issues 2 weeks before the accident. It is also unclear who was piloting the airplane in its final moments; however, the pilot was likely flying at the time considering he was a part owner in the airplane and given his motivation to troubleshoot the performance deficiency. While cardiovascular conditions placed the pilot at an increased risk for a sudden cardiac event, operational evidence does not suggest that this occurred and was likely not a factor in this 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
- Aerodynamic stall/spin during approach (VFR pattern crosswind) defining event
The NTSB's findings
- Aircraft › Aircraft systems › Fuel system › Fuel selector/shutoff valve › Incorrect use/operation
- Personnel issues › Task performance › Use of equip/info › Aircraft control › Pilot
- Aircraft › Aircraft oper/perf/capability › Performance/control parameters › Airspeed › Not attained/maintained
Pilot
- Certificate: flight instructor, commercial pilot, remote
- Ratings: multi-engine land; single-engine land; instructor: airplane multi-engine; instructor: airplane single-engine; instructor: instrument airplane; instrument: airplane; rotorcraft: unmanned (suas)
- Flight time: 1,300 hours in all
- Last flight review: November 11, 2019
- Medical certificate: Class 3 (with waivers/limitations)
- Seat: left
- Injury: fatal
Pilot-Rated Passenger
- Certificate: flight instructor, commercial pilot
- Ratings: multi-engine land; single-engine land; instructor: airplane single-engine; instructor: instrument airplane; instrument: airplane
- Flight time: 3,761 hours in all; 0 in this make and model
- Last flight review: January 26, 2021
- Medical certificate: Class 2 (with waivers/limitations)
- Seat: rgt
- Injury: fatal
The aircraft
- Airframe total time: 4,373.2 hours
- Last inspection: annual inspection, November 16, 2021; 1.2 hours since
- Maximum gross weight: 2,250 lb
- Seats: 4
- Landing gear: fixed
- Engine: Lycoming O-320-B2D (piston); 3,118 hours total
The flight
- Flight plan: none
- Runway 13, 3,540 ft by 98 ft
Weather at the time
- Light: daylight
- Wind: from 180° at 11 knots, gusting 17
- Visibility: 10 statute miles
- Sky: clear
- Temperature: 88°F (31°C), dew point 43°F (6°C)
- Altimeter: 29.80 inHg
- Observation at 12:53 pm from KOVE, 1 miles away
Weather report (METAR): KOVE 021953Z AUTO 18011G17KT 10SM CLR 31/06 A2980 RMK AO2 SLP092 T03060056
Injuries
| Fatal | Serious | Minor | None | |
|---|---|---|---|---|
| Flig | 1 | |||
| Passengers | 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.
About this page
Everything above comes from the NTSB's public accident database: the narrative, probable cause and findings are the NTSB's own words, and the coded tables behind its report (pilot, aircraft, flight, weather, injuries, sequence of events) are written out in plain English. Pilots' ages, home towns and medical details are left out on purpose. The documents and photographs are the NTSB's docket, the folder of records gathered during the investigation, shown as the NTSB released them (the NTSB redacts some personal details first) and listed under the NTSB's own titles. This site's own text never names pilots, passengers or anyone else involved. A preliminary report describes what is known soon after the event and can change; the final report, with the probable cause, usually follows one to two years later and this page is refreshed when it does. Case number WPR22FA196.
